Garmin | G1000 NXi: Piper PA-46 M350 Mirage | Garmin G1000 NXi: Piper PA-46 M350 Mirage G1000 NXi Cockpit Reference Guide for the Piper M350

Garmin G1000 NXi: Piper PA-46 M350 Mirage G1000 NXi Cockpit Reference Guide for the Piper M350
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL AND CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
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This manual reflects the operation of System Software version
2783.00 or later for the G1000 NXi Piper M350. Some differences
in operation may be observed when comparing the information in
this manual to earlier or later software versions.
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for any incidental, special or consequential damages that result from
the use or inability to use the software or related documentation,
even if AOPA or an AOPA authorized representative has been
advised of the possibility of such damages. User agrees not to sue
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hold harmless AOPA from any causes of action, claims or losses
related to any actual or alleged inaccuracies in the information.
Some jurisdictions do not allow the limitation or exclusion of
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damages so the above limitations or exclusions may not apply to
you.
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respect to the AC-U-KWIK information included in this data, express
or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information
is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or
otherwise. Licensee agrees not to sue AC-U-KWIK Organizations
and, to the maximum extent allowed by law, to release and hold
harmless AC-U-KWIK Organizations from any cause of action,
claims or losses related to any actual or alleged inaccuracies in the
information arising out of Garmin’s use of the information in the
datasets. Some jurisdictions do not allow the limitation or exclusion
of implied warranties or liability for incidental or consequential
damages so the above limitations or exclusions may not apply to
licensee.
Printed in the U.S.A.
Warning, Cautions, and Notes
WARNING: Do not use terrain avoidance displays as the sole source of
information for maintaining separation from terrain and obstacles. Garmin
obtains terrain and obstacle data from third party sources and cannot
independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for
verification of displayed aeronautical information. Displayed aeronautical data
may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control
altitude requirements. The primary barometric altimeter must be used for
compliance with all air traffic control altitude regulations, requirements,
instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole
means of navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered only an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack of
equipment, poor signal reception, and/or inaccurate information from aircraft or
ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near,
or around areas of hazardous weather. Information contained within data link
weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather data
for data link transmission, the weather information shown by the data link
weather product may be older than the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory in
nature and should not be relied upon as the sole source of obstacle and terrain
avoidance information. Always refer to current aeronautical charts for
appropriate minimum clearance altitudes.
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Warning, Cautions, and Notes
WARNING: Always obtain qualified instruction prior to operational use of this
equipment.
WARNING: Do not use GPS to navigate to any active waypoint identified as a
‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible with
the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
WARNING: When using the autopilot to fly an approach with vertical guidance,
the autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set
in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision
avoidance maneuvering. The traffic display does not provide collision avoidance
resolution advisories and does not under any circumstances or conditions relieve
the pilot’s responsibility to see and avoid other aircraft.
WARNING: Because of variation in the earth’s magnetic field, do not rely on the
accuracy of attitude and heading indications in the following geographic areas:
North of 72° North latitude at all longitudes; South of 70° South latitude at all
longitudes; North of 65° North latitude between longitude 75° W and 120° W.
(Northern Canada); North of 70° North latitude between longitude 70° W and
128° W. (Northern Canada); North of 70° North latitude between longitude 85°
E and 114° E. (Northern Russia); South of 55° South latitude between longitude
120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not rely on information from a lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations and
interference may cause the system to display inaccurate or incomplete
information. Refer to documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situational
awareness only and may not provide either the accuracy or reliability upon
which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles,
or traffic.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Warning, Cautions, and Notes
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the
Garmin SVT display or may appear as a partial symbol.
WARNING: Do not use the Garmin SVT runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining the
proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when
personnel or objects are within the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for
viewing the actual intensity of precipitation. Changing the gain in weather mode
causes precipitation intensity to be displayed as a color not representative of the
true intensity.
WARNING: Do not use TAWS information for primary terrain or obstacle
avoidance. TAWS is intended only to enhance situational awareness.
WARNING: Do not use SurfaceWatch™ information as the primary method of
flight guidance during airborne or ground operations. SurfaceWatch does not
have NOTAM or ATIS information regarding the current active runway,
condition, or information about the position of hold lines.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only a QNH
altimeter setting for height above mean sea level, or the standard pressure
setting, as applicable.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners
containing ammonia. They will harm the anti-reflective coating.
CAUTION: Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and affect
the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight
Restriction (TFR) information. Always confirm TFR information through official
sources such as Flight Service Stations or Air Traffic Control.
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Warning, Cautions, and Notes
NOTE: All visual depictions contained within this document, including screen
images of the system panel and displays, are subject to change and may not
reflect the most current system and aviation databases. Depictions of equipment
may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System
and is solely responsible for its accuracy and maintenance. The GPS system is
subject to changes which could affect the accuracy and performance of all GPS
equipment. Portions of the system utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information
presented by the system can be misused or misinterpreted and, therefore,
become unsafe.
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject
to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received, including
interference that may cause undesired operation.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft is
on the ground. Moving the aircraft more than 100 yards away from the source
of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim or
blank.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please refer
to our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures,
or electromagnetic fields can cause sensor differences that may result in
nuisance miscompare annunciations during start up, shut down, or while
taxiing. If one or more of the sensed values are unavailable, the annunciation
indicates no comparison is possible.
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Warning, Cautions, and Notes
NOTE: The system responds to a terminal procedure based on data coded
within that procedure in the Navigation Database. Differences in system
operation may be observed among similar types of procedures due to
differences in the Navigation Database coding specific to each procedure.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and
advisory guidance and information related to the use of databases in the
National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained
from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen that
have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type 2
LOA is available for each applicable database and can be viewed at http://
fly.garmin.com by selecting ‘Aviation Database Declarations.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment is
required for compliance with established FAA regulatory guidance, but does
not constitute authorization to fly any and all terminal procedures that may be
presented by the system. It is the pilot’s responsibility to operate in
accordance with established AFM(S) and regulatory guidance or limitations as
applicable to the pilot, the aircraft, and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.com by
selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database
alerts and consider their impact on the intended aircraft operation. The database
alerts can be viewed at www.flygarmin.com by selecting ‘Aviation Database
Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support.
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Warning, Cautions, and Notes
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form of
an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any
other displayed item used for navigation or communication in the air or on the
ground. Go to FlyGarmin.com and select ‘Aviation Data Error Report’.
NOTE: The system supports approval of AC 120-76C Hardware Class 3,
Software Type B Electronic Flight Bag (EFB) electronic aeronautical chart
applications. Possible additional requirements may make a secondary source
(traditional paper or additional electronic display) necessary onboard the aircraft.
If the secondary source is a Portable Electronic Device (PED), its use must be
consistent with guidance in AC 120-76C.
NOTE: Terrain and obstacle alerting is not available north of 89º North latitude
and south of 89º South latitude. This is due to limitations present within the
Terrain database and the system’s ability to process the data representing the
affected areas.
NOTE: When using Stormscope, there are several atmospheric phenomena in
addition to nearby thunderstorms that can cause isolated discharge points in the
strike display mode. However, clusters of two or more discharge points in the
strike display mode do indicate thunderstorm activity if these points reappear
after the screen has been cleared.
NOTE: Operate G1000NXi system power through at least one cycle in a period
of four days of continuous operation to avoid an autonomous system reboot.
NOTE: The navigation databases used in Garmin navigation systems contain
Special Procedures. Prior to flying these procedures, pilots must have specific
FAA authorization, training, and possession of the corresponding current, and
legitimately-sourced chart (approach plate, etc.). Inclusion of the Special
Procedure in the navigation database DOES NOT imply specific FAA
authorization to fly the procedure.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Software License Agreement
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Software License Agreement
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190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Software License Agreement
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Record of Revisions
Part
Number
190–
02362-00
190–02362–00 Rev. A
Rev.
A
Record of Revisions
Date
Page
Range
12/5/17
All
Description
Production Release
with GDU
Software 20.80
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Record of Revisions
BLANK PAGE
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Table of Contents
FLIGHT INSTRUMENTS...........................................................................................1
Flight Instruments...............................................................................................1
Supplemental Flight Data...................................................................................6
PFD Annunciations and Alerting Functions...................................................... 7
SVT Operation..................................................................................................... 7
ENGINE INDICATION SYSTEM............................................................................. 9
Engine Indication System (EIS) Display............................................................. 9
Engine Page.......................................................................................................10
Reversionary Mode...........................................................................................13
AUDIO PANEL AND CNS......................................................................................15
COM Operation................................................................................................. 15
NAV Operation.................................................................................................. 16
Mode S Transponder.........................................................................................18
Additional Audio Panel Functions................................................................... 20
Audio Panel Preflight Procedure......................................................................25
FLIGHT MANAGEMENT....................................................................................... 27
Introduction.......................................................................................................27
Using Map Displays.......................................................................................... 27
Waypoints......................................................................................................... 33
Airspaces............................................................................................................41
Direct-To Navigation......................................................................................... 43
Flight Planning.................................................................................................. 46
Vertical Navigation........................................................................................... 66
Procedures......................................................................................................... 72
Weight Planning............................................................................................... 80
Trip Planning..................................................................................................... 81
RAIM Prediction................................................................................................ 82
HAZARD AVOIDANCE.......................................................................................... 85
Data Link Weather............................................................................................ 85
Stormscope Lightning Detection System...................................................... 100
Airborne Color Weather Radar...................................................................... 103
Terrain Displays............................................................................................... 106
Traffic Information Service (TIS).....................................................................108
TAS/TCAS I Traffic............................................................................................110
ADS-B Traffic....................................................................................................112
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
iii
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM.................................................... 117
Activating The Flight Director........................................................................117
Vertical Modes.................................................................................................118
Lateral Modes..................................................................................................119
Combination Modes (VNV, APR, NAV, GA).................................................... 120
Procedures....................................................................................................... 121
ADDITIONAL FEATURES.................................................................................... 123
SafeTaxi............................................................................................................123
Charts...............................................................................................................123
SiriusXM Radio Entertainment.......................................................................130
Satellite Telephone and SMS Messaging...................................................... 132
Connext Setup.................................................................................................152
SurfaceWatch.................................................................................................. 153
Electronic Stability & Protection (ESP)...........................................................154
Electronic Checklists........................................................................................155
ABNORMAL OPERATION.................................................................................. 159
Reversionary Mode.........................................................................................159
Abnormal COM Operation............................................................................. 161
Flight Instruments...........................................................................................162
Dead Reckoning.............................................................................................. 167
ANNUNCIATIONS & ALERTS............................................................................ 171
System Annunciations.................................................................................... 171
CAS Messages................................................................................................. 172
Garmin Connext Weather Request Status.................................................... 178
TAWS Annunciations/Alerts........................................................................... 179
TIS Annunciations/Alerts................................................................................187
ADS-B Traffic Annunciations/Alerts...............................................................190
Voice Alerts......................................................................................................193
System Messages............................................................................................ 194
Flight Plan Import/Export Messages............................................................. 214
Crew Profile Import/Export Messages...........................................................216
APPENDIX...............................................................................................................219
Updating Databases using an SD Card:.........................................................259
Updating Databases from any MFD page (except the Aux - Databases
page):............................................................................................................... 261
Updating Databases from the Aux - Databases page:.................................263
iv
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Table of Contents
Loading the magnetic field variation database update:..............................265
INDEX.........................................................................................................................I-1
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
v
Table of Contents
BLANK PAGE
vi
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
FLIGHT INSTRUMENTS
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, press the Setup 1 Softkey to display the ‘Aux — System Setup 1’
Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the ‘Format Active’ setting in the ‘Flight
Director’ box.
6)
Turn the small FMS Knob to highlight the desired format.
Flight
Management
Turn the FMS Knobs to select the ‘Aux’ page group on the MFD.
Audio Panel
and CNS
1)
EIS
Changing the Command Bar format:
Hazard
Avoidance
’Single Cue’ to display the aircraft symbol and Command Bars as a single cue.
Or:
AFCS
’X Pointer’ to display the aircraft symbol and Command Bars as a crosspointer.
Enabling/disabling individual Vspeed Reference Bugs:
2)
Turn the large FMS Knob to highlight the On/Off field for the desired bug.
3)
Turn the small FMS Knob clockwise to On or counterclockwise to Off.
4)
To remove the window, press the CLR Key or the Tmr/Ref Softkey.
Abnormal
Operation
Press the Tmr/Ref Softkey.
Additional
Features
1)
Enabling/disabling Vspeed Reference Bugs as a group:
2)
Press the MENU Key.
3)
Turn the FMS Knob to scroll as needed to highlight the desired selection.
4)
Press the ENT Key.
5)
To remove the References Window, press the CLR Key or the Tmr/Ref Softkey.
Appendix
Press the Tmr/Ref Softkey.
Annunciations
& Alerts
1)
Selecting the altitude display units:
Turn the FMS Knobs to select the ‘Aux - System Setup 1’ Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
1
3)
Turn the large FMS Knob to highlight the ‘ALT, VS’ datafield in the ‘Display
Units’ Window.
4)
Turn the small FMS Knob to highlight either ‘Feet(FT,FPM)’ or ‘Meters(MT,MPS)’
and press the ENT Key. This setting affects altitude displays system-wide, in
addition to those shown on the PFD.
Setting the Selected Altitude:
1)
Turn the ALT SEL Knob to set the Selected Altitude. If the Altimeter display
units are set to feet, the Selected Altitude increments are 100 feet. If the
Altimeter is set to Metric, the Selected altitude increments are 50 meters. When
the altitude units overlays are enabled, the increments alternate between a
rounded value of feet or meters while turning the ALT SEL Knob. If set, the
Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for
the Selected Altitude.
2)
If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also
available for the Selected altitude.
Enabling altitude units overlays:
1)
Press the PFD Opt Softkey to display the second-level softkeys..
2)
Press the ALT Units Softkey.
3)
Press the Meters or Feet Softkeyto enable/disable the altitude overlays.
4)
Press the Back Softkey twice to return to the top-level softkeys.
Selecting the altimeter barometric pressure setting:
Turn the BARO Knob to select the desired setting.
Synchronizing the altimeter barometric pressure settings:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Instruments
1)
Turn the large FMS Knob to select the Aux page group on the MFD.
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, press the Setup 1 Softkey to display the ‘Aux - System Setup 1’
Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight ‘BARO’ in the ‘Synchronization’ box.
6)
Turn the small FMS Knob clockwise to ‘On’ or counterclockwise to ‘Off’.
7)
Press the ENT Key.
8)
Turn the small FMS Knob to change the altitude.
9)
Press the ENT Key.
10) To cancel the selection, press the FMS Knob.
2
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Instruments
Press the PFD Opt Softkey to display the second-level softkeys.
2)
Press the ALT Units Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
EIS
1)
Flight
Instruments
Changing altimeter barometric pressure setting units:
Or:
4)
Press the Back Softkey twice to return to the top-level softkeys.
Flight
Management
Setting the Baro Transition Alerts:
2)
Press the FMS Knob to activate the cursor.
3)
To enable/disable the Baro Transition Alert based on altitude, turn the large FMS
Knob to highlight the ‘On’ or ‘Off’ field for the BARO Transition Alert Altitude in
the ‘BARO Transition Alert’ Box.
4)
If desired, turn the small FMS Knob to set the BARO Transition Alert Altitude
‘On’ or ‘Off’.
5)
Turn the large FMS Knob to highlight the ‘Altitude’ field.
6)
Use the FMS Knobs to change the altitude and press the ENT Key to accept or
press the CLR Key to return to the previous altitude selection.
7)
Turn the large FMS Knob to highlight the ‘On’ or ‘Off’ field for the BARO
Transition Alert Level.
8)
If desired, turn the small FMS Knob to set the BARO Transition Alert Flight Level
‘On’ or ‘Off’.
9)
Turn the large FMS Knob to highlight the ‘Flight Level’ field.
AFCS
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page on the MFD.
Hazard
Avoidance
1)
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
10) Use the FMS Knobs to change the Flight Level for the alert and press the ENT
Key to accept or press the CLR Key to return to the previous altitude selection.
11) Push the FMS Knob to deactivate the cursor.
Appendix
Enabling/disabling the HSI Map on the PFD:
1)
Audio Panel
and CNS
Press the HPA Softkey to display the barometric pressure setting in hectopascals
(hPa).
Press the Map/HSI Softkey.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
3
Flight
Instruments
Flight Instruments
2)
Press the Layout Softkey.
3)
Press the HSI Map Softkey to enable the HSI Map.
Or:
Adjusting the selected heading:
Turn the HDG Knob to set the selected heading.
2)
Press the HDG Knob to synchronize the bug to the current heading.
1)
Turn the CRS Knob to set the Selected Course.
2)
Press the CRS Knob to re-center the CDI and return the course pointer to the
bearing of the active waypoint or navigation station (see OBS Mode for
adjusting a GPS course).
Changing the navigation angle true/magnetic setting:
1)
Use the FMS Knob to select the ‘AUX - System Setup 1‘ Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight ‘Nav Angle’ in the ‘Display Units’ box.
4)
Turn the small FMS Knob to highlight the desired setting and press the ENT
Key.
Additional
Features
AFCS
Hazard
Avoidance
1)
Adjusting the Selected Course:
Flight
Management
Audio Panel
and CNS
EIS
Press the Map Off Softkey to disable the HSI Map.
• True - References angles to true north (T)
Changing navigation sources:
1)
Press the CDI Softkey to change from FMS to VOR1 or LOC1. This places the
cyan tuning box over the NAV1 standby frequency in the upper left corner of
the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2.
This places the cyan tuning box over the NAV2 standby frequency.
3)
Press the CDI Softkey a third time to return to FMS.
Synchronizing the CDIs:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
• Magnetic - Angles corrected to the computed magnetic variation (Mag Var)
4
1)
Select the ‘Aux - System Setup 1’ Page using the FMS Knob.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the CDI On/Off option in the
Synchronization box.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Instruments
Turn the small FMS Knob clockwise to ‘On’ or counterclockwise to ‘Off’.
5)
Press the FMS Knob to remove the cursor.
Flight
Instruments
4)
Changing the selected FMS CDI setting:
Use the FMS Knob to select the ‘AUX - System Setup 1’ Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight ‘Format Allowed’ in the ‘GPS CDI’ box.
4)
Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
5)
To cancel the selection, press the FMS Knob or the CLR Key.
EIS
1)
2)
Turn the CRS Knob to select the desired course to/from the waypoint. Press the
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to return to automatic waypoint sequencing.
Hazard
Avoidance
Press the OBS Softkey to select OBS Mode.
Flight
Management
1)
AFCS
Selecting bearing display and changing sources:
Press the PFD Opt Softkey.
2)
Press either Bearing 1 or Bearing 2 Softkey to display the desired bearing
pointer and information window with a NAV source.
3)
Press either Bearing 1 or Bearing 2 Softkey again to change the bearing source
to FMS.
4)
Press either Bearing 1 or Bearing 2 Softkey a third time to change the bearing
source to ADF (note: ADF radio installation is optional).
5)
To remove the bearing pointer and information window, press either Bearing 1
or Bearing 2 Softkey again.
Additional
Features
1)
Abnormal
Operation
2)
Press the DME Softkey to display the DME Information Window above the
BRG1 Information Window.
3)
To remove the DME Information Window, press the DME Softkey again.
Appendix
Press the PFD Opt Softkey.
Annunciations
& Alerts
Displaying the DME Information Window:
1)
Audio Panel
and CNS
Enabling/disabling OBS Mode while navigating a GPS
flight plan:
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
5
SUPPLEMENTAL FLIGHT DATA
Setting the Generic Timer:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Instruments
1)
Press the Tmr/Ref Softkey.
2)
Turn the large FMS Knob to select the timer field (HH:MM:SS).
3)
Use the FMS Knob to enter the desired time.
4)
Press the ENT Key. The Up/Dn field is now highlighted.
5)
Turn the small FMS Knob to display the UP/DOWN Window.
6)
Turn the small FMS Knob to select ‘Up’ or ‘Dn’.
7)
Press the ENT Key. ‘Start?’ is now highlighted.
8)
Press the ENT Key to start the timer. The field changes to ‘Stop?’. If the timer is
counting DOWN, it will start counting UP after reaching zero.
9)
To stop the timer, press the ENT Key with ‘Stop?’ highlighted. The field changes
to ‘Reset?’.
AFCS
10) To reset the timer, press the ENT Key with ‘Reset?’ highlighted. The field
changes back to ‘Start?’ and the digits are reset.
11) To remove the window, press the CLR Key or the Tmr/Ref Softkey.
1)
Select the ‘Aux - System Setup 1’ Page on the MFD using the FMS Knob.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the Temperature datafield in the ‘Display
Units’ box.
4)
Turn the small FMS Knob to highlight either ‘Celsius’ or ‘Fahrenheit’ and press
the ENT Key to confirm the selection.
5)
To cancel the selection, press the FMS Knob or the CLR Key.
Displaying wind data:
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Changing temperature display units:
1)
Press the PFD Opt Softkey.
2)
Press the Wind Softkey to display wind data to the left of the HSI.
3)
Press one of the Option Softkeys to change how wind data is displayed:
Index
• Option 1: Headwind/tailwind and crosswind arrows with numeric speed
components
• Option 2: Wind direction arrow and speed
6
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Instruments
components
Flight
Instruments
• Option 3: Wind direction arrow with headwind/tailwind and crosswind
To remove the window, press the Off Softkey.
EIS
PFD ANNUNCIATIONS AND ALERTING FUNCTIONS
2)
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select ‘BARO’ or ‘TEMP COMP.’ ‘OFF’ is selected by
default. Press the ENT Key or turn the large FMS Knob to highlight the next
field.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet).
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS Knob to
highlight the next field and then enter the temperature (-59˚C to 59˚C)
6)
To remove the window, press the CLR Key or the Tmr/Ref Softkey.
Hazard
Avoidance
Press the Tmr/Ref Softkey.
Flight
Management
1)
Audio Panel
and CNS
Setting the Minimum Descent Altitude/Decision Height and
bug:
AFCS
SVT OPERATION
Additional
Features
Activating and deactivating SVT:
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the Terrain Softkey. The SVT display will cycle on or off with the Terrain
Softkey.
Abnormal
Operation
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the Pathways Softkey. The Pathway feature will cycle on or off with the
Pathways Softkey.
Appendix
1)
Annunciations
& Alerts
Activating and deactivating Pathways:
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
7
Activating and deactivating Horizon Headings:
EIS
Flight
Instruments
Flight Instruments
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the HDG LBL Softkey. The horizon heading display will cycle on or off with
the HDG LBL Softkey.
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the APT Sign Softkey. Display of airport signs will cycle on or off with the
APT Sign Softkey.
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the Wire Softkey. Display of aerial wire obstruction will cycle on or off
with the Wire Softkey.
Enabling/Disabling SVT Field of View on the Navigation
Map:
1)
While viewing the ‘Map - Navigation Map’ Page, press the MENU Key to display
the ‘Page Menu’ Window.
2)
Turn the large FMS Knob to highlight ‘Map Settings’ and press the ENT Key.
3)
Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key.
4)
Turn the large FMS Knob to scroll through the ‘Map’ Group options to ‘Field of
View’.
5)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
6)
Press the FMS Knob to return to the ‘Map - Navigation Map’ page.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
1)
Activating and deactivating Wire Obstacles on SVT:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Activating and deactivating Airport Signs:
8
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Engine Indication System
Flight
Instruments
ENGINE INDICATION SYSTEM
ENGINE INDICATION SYSTEM (EIS) DISPLAY
EIS
1
1
2
Audio Panel
and CNS
9
9
2
10
10
11
3
13
12
4
11
Flight
Management
3
4
5
13
Hazard
Avoidance
6
6
7
7
AFCS
14
14
8
8
Figure 2 EIS Display when Engine
Softkey is Selected
2
Tachometer Indicator
Displays engine tachometer in revolutions per minute
(RPM)
3
Turbine Inlet
Temperature
Indicator
Displays turbine inlet temperature (TIT) in degrees
Celsius (°C) or Fahrenheit (°F)
4
Fuel Flow Indicator
Displays fuel flow in gallons per hour (FFLOW GPH)
5
Cylinder Head
Temperature
Indicator
Displays cylinder head temperature (CHT) in degrees
Celsius (°C) or Fahrenheit (°F) and shows digital
number of hottest cyclinder
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Displays manifold pressure in inches of mercury (MAP
IN HG)
Appendix
Manifold Pressure
Indicator
Annunciations
& Alerts
1
Abnormal
Operation
Figure 1 EIS Display (Normal)
Additional
Features
15
15
9
Engine Indication System
Oil Pressure Indicator
Displays oil pressure in pounds per square inch (psi)
7
Oil Temperature
Indicator
Displays oil temperature in degrees Celsius (°C) or
Fahrenheit (°F)
8
Fuel Quantity
Indicator
Displays the amount of fuel in gallons (GAL) for each
side fuel tank
9
Cabin Pressurization
Group
Displays the altitude feet on a slide indicator with
digits displayed below and the rate of climb/decent
in feet per minute (FPM)
10
Differential Pressure
Indicator
Displays the differential pressure (DIFF) in pounds per
square inch (PSI)
11
Destination Elevation Displays the elevation and the destination airport in
feet
12
Pulse Oximeter
Group)
Displays blood oxygen indicator in percentage and
heart rate indicator in beats per minute (BPM)
13
Electrical Group
Displays left (L) and right (R) alternator current in
amperes (ALT AMPS), bus voltage (VOLTS), and
battery current in amperes (BATT AMPS)
14
Flap Indicator
Displays flap indication in angle degrees 0°, 10°, 20°,
and 36°
15
Landing Gear
Indicator
Displays landing gear indications
ENGINE PAGE
The Engine Page displays all engine, fuel, electrical, and fuel calculation information. To
access this page, press the Engine Softkey or turn the large FMS Knob and select the ‘EIS Engine Page.’
Level 1
Level 2
Engine
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
6
10
Description
Displays EIS - Engine Page and second-level
engine softkeys; press again to exit page
DEC Fuel
Decreases displayed fuel remaining in 1-gal
increments
INC Fuel
Increases displayed fuel remaining in 1-gal
increments
RST Fuel
Resets displayed fuel remaining to maximum fuel
capacity for aircraft and fuel used to zero
CO RST
Resets the CO Detector
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Engine Indication System
Flight
Instruments
1
EIS
Audio Panel
and CNS
5
2
Flight
Management
Hazard
Avoidance
3
4
AFCS
Figure 3 Engine Page Display (MFD)
2
System Group
(PULSE
OXIMETER
Group)
Displays the oxygen indicator in percentage, heart rate
indicator in beats per minute (BPM), the vacuum indicator in
inches of mercury (IN HG), and the CO detector indication in
parts per million (CO PPM). The pulse oximeter is not
displayed in reversionary mode
3
Fuel Calculation
Group
Displays the gallons remaining (GAL REM), gallons used
(GAL USED, endurance range (ENDUR) in hours and
minutes, range in nautical miles (RANGE NM), and nautical
miles per gallon (NMPG)
4
Engine Softkey
Displays the engine softkey selection
5
Engine Strip
Displays engine (EIS) strip
Annunciations
& Alerts
Displays cylinder head temperature in °F along vertical bars.
If the temperature of any cylinder exceeds the normal range,
the bars will turn amber for caution or red for warning
Abnormal
Operation
Cylinder Head
Temperature
Indicator
Additional
Features
1
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
11
Flight
Instruments
Engine Indication System
Adjusting the fuel totalizer quantity:
On the Engine Page, use the DEC Fuel and INC Fuel Softkeys to obtain the
desired fuel remaining (GAL REM).
EIS
Resetting the fuel totalizer:
Audio Panel
and CNS
On the Engine Page, select the RST Fuel Softkey; this resets displayed fuel
remaining (GAL REM) to the maximum fuel capacity for the aircraft and fuel
used to zero.
Set Fuel Remaining
Calculated Fuel Used
Calculated Endu rance
Figure 4 Fuel Calculation Group
Reset the Carbon Monoxide Detector:
On the Engine Page, push CO RST softkey.
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Calculated Range
Abnormal
Operation
Figure 5 Carbon Monoxide Detector (CO DETECTOR)
Landing Gear Indicator
Index
Appendix
Annunciations
& Alerts
Landing gear statuses are shown using the indications in the following table.
12
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Engine Indication System
EIS
Flight
Instruments
Position
Engine Page
Up & Locked
EIS
In Transition
Audio Panel
and CNS
Flight
Management
Down &
Locked
Hazard
Avoidance
Warning
AFCS
The Engine Display, in reversionary mode, is identical to the normal EIS Display on the
MFD.
Abnormal
Operation
In the event of a PFD or MFD display failure, the display(s) operating in Reversionary
Mode are configured to present PFD symbology together with the EIS Display (refer to the
System Overview for information about display reversionary mode).
Additional
Features
REVERSIONARY MODE
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
13
Flight
Instruments
Engine Indication System
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
EIS Display
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Figure 6 Reversionary Mode (EIS Shown)
14
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
Flight
Instruments
AUDIO PANEL AND CNS
COM OPERATION
EIS
Manually tuning a COM frequency:
2)
Press the Frequency Transfer Key to transfer the frequency to the active field.
3)
Adjust the volume level with the COM VOL/SQ Knob.
4)
Press the COM VOL/SQ Knob to turn automatic squelch on and off.
Flight
Management
Turn the COM Knob to tune the desired frequency (large knob for MHz; small
knob for kHz).
Manually tuning a COM frequency from the Control Unit:
Press the COM Key to select the COM frequency box.
2)
Turn the NAV/COM Knob to tune the desired frequency in the COM Tuning Box
(large knob for MHz; small knob for kHz).
3)
Press the Frequency Transfer Key to transfer the frequency to the active field.
AFCS
Auto-tuning a COM frequency for a nearby airport from
the PFD:
Turn the FMS Knob to scroll through the list and highlight the desired COM
frequency.
3)
Press the ENT Key to load the COM frequency into the COM Standby Frequency
Field.
4)
Press the Frequency Transfer Key to transfer the frequency to the COM Active
Frequency Field.
Auto-tuning a COM frequency from the WPT and NRST
Pages:
2)
Turn the FMS Knob to place the cursor on the desired COM frequency.
3)
Press the ENT Key to load the COM frequency into the standby field of the
selected COM radio.
4)
Press the Frequency Transfer Key on the PFD or MFD to transfer the frequency
to the COM Active Frequency Field.
15
Index
From any page that the COM frequency can be auto-tuned, activate the cursor
by pressing the FMS Knob or pressing the appropriate softkey.
Appendix
1)
Annunciations
& Alerts
2)
Abnormal
Operation
Press the Nearest Softkey on the PFD to open the Nearest Airports Window. A
list of 25 nearest airport identifiers and COM frequencies is displayed.
Additional
Features
1)
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Hazard
Avoidance
1)
190–02362–00 Rev. A
Audio Panel
and CNS
1)
Audio Panel and CNS
1)
Press the MENU Key to display the page menu.
2)
Turn the large FMS Knob to scroll through the menu options.
3)
Press the ENT Key to place the cursor on the desired selection.
4)
Scroll through the frequency selections with the FMS Knob or the ENT Key.
5)
Press the ENT Key to load the COM frequency into the standby field of the
selected COM radio.
6)
Press the Frequency Transfer Key to transfer the frequency to the COM Active
Frequency Field.
Changing COM frequency channel spacing:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Or:
1)
Select the Aux – System Setup 1 Page.
2)
Press the FMS Knob to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the Channel Spacing Field in the COM
Configuration Box.
4)
Turn the small FMS Knob to select the desired channel spacing.
5)
Press the ENT Key to complete the channel spacing selection.
Manually tuning a NAV frequency:
1)
Rotate the NAV Knob to tune the desired frequency in the NAV Tuning Box.
2)
Press the Frequency Transfer Key to transfer the frequency to the NAV Active
Frequency Field.
3)
Adjust the volume level with the NAV VOL/ID Knob.
4)
Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off.
Auto-tuning a NAV frequency from the WPT and NRST
Pages:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
NAV OPERATION
16
1)
From any page that the NAV frequency can be auto-tuned, activate the cursor
by pressing the FMS Knob or the appropriate softkey.
2)
Turn the FMS Knob to place the cursor on the desired NAV identifier or NAV
frequency.
3)
On the Nearest VOR and Nearest Airports pages, press the FREQ Softkey to
place the cursor on the NAV frequency.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
Press the ENT Key to load the NAV frequency into the standby field of the
selected NAV radio.
5)
Press the Frequency Transfer Key to transfer the frequency to the NAV Active
Frequency Field.
EIS
Press the ENT
Key to load a
highlighted
Frequency into
the NAV Standby
Frequency Box
Flight
Instruments
4)
Audio Panel
and CNS
Turn the FMS Knob to
scroll through a list of
Frequencies
Flight
Management
Figure 7 NAV Frequency Auto-Tuning from the MFD
Or:
When on the NRST pages, press the MENU Key on the MFD control unit to
display the page menu.
2)
Turn the large FMS Knob to scroll through the menu options.
3)
Press the ENT Key to place the cursor in the desired window.
4)
Scroll through the frequency selections with the FMS Knob or the ENT Key.
5)
Press the ENT Key to load the NAV frequency into the standby field of the
selected NAV radio.
6)
Press the Frequency Transfer Key to transfer the frequency to the NAV Active
Frequency Field.
Hazard
Avoidance
1)
AFCS
Additional
Features
Abnormal
Operation
Nearest VOR Menu
Nearest Frequencies Menu
Annunciations
& Alerts
Nearest Airports Menu
Nearest Airspaces Menu
Appendix
Figure 8 Nearest Pages Menu
Tuning ADF Frequency:
Press the ADF/DME Softkey to display the ADF/DME Tuning Window.
2)
Turn the large FMS Knob to place the selection cursor over the standby ADF
frequency field.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
17
Hazard
Avoidance
Turn the small FMS Knob to begin data entry and change each digit.
4)
Turn the large FMS Knob to move the cursor to the next digit position.
5)
Press the ENT Key to complete data entry for the standby frequency.
1)
Turn the large FMS Knob to place the selection cursor over the standby ADF
frequency field.
2)
Press the ENT Key to complete the frequency transfer.
Adjusting ADF receiver volume:
1)
Turn the large FMS Knob to place the selection cursor over the ADF volume
field.
2)
Turn the small FMS Knob to adjust volume as desired.
Selecting ADF Receiver Mode:
1)
Turn the large FMS Knob to place the selection cursor over the ADF mode field.
2)
Turn the small FMS Knob to select the desired ADF receiver mode.
Selecting DME transceiver pairing:
Additional
Features
AFCS
3)
Tranferring the active and standby ADF frequencies:
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Audio Panel and CNS
1)
Press the ADF/DME or DME Softkey to display the ADF/DME Tuning Window.
2)
Turn the small FMS Knob to select the DME tuning mode.
3)
Press the ENT Key to complete the selection.
Selecting and Activating Transponder 1 or Transponder 2
(Optional)
1)
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2)
Press the XPDR1 or XPDR2 Softkey to select and activate the desired
transponder.
Selecting a transponder mode:
1)
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2)
Press the desired softkey to activate the transponder mode.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
MODE S TRANSPONDER
18
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
Flight
Instruments
Entering a transponder code with softkeys:
2)
Press the CODE Softkey to display the Transponder Code Selection Softkeys, for
digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering the
code, the next softkey in sequence must be pressed within 10 seconds, or the
entry is cancelled and restored to the previous code. Pressing the BKSP Softkey
moves the code selection cursor to the previous digit. Five seconds after the
fourth digit has been entered, the transponder code becomes active.
Audio Panel
and CNS
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
EIS
1)
Entering a Code
Flight
Management
Figure 9 Entering a Code
Hazard
Avoidance
Entering a transponder code with the PFD FMS Knob:
Press the XPDR and the CODE Softkeys as in the previous procedure to enable
code entry.
2)
Turn the small FMS Knob on the PFD to enter the first two code digits.
3)
Turn the large FMS Knob to move the cursor to the next code field.
4)
Enter the last two code digits with the small FMS Knob.
5)
Press the ENT Key to complete code digit entry.
Additional
Features
Press the
ENT Key to
Complete
Code Entry
Annunciations
& Alerts
Turn the Large
FMS Knob
to Move the
Cursor to the
Next Code Field
Abnormal
Operation
Turn the Small
FMS Knob to
Enter Two Code
Digits at a Time
AFCS
1)
Figure 10 Entering a Code with the FMS Knob
Appendix
Entering a transponder code with the Control Unit FMS
Knob
Press the XPDR and the Code Softkeys on the PFD.
2)
Turn the small FMS Knob to enter the first two code digits.
3)
Turn the large FMS Knob to move the cursor to the next code field.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
19
Flight
Instruments
Audio Panel and CNS
4)
Enter the last two code digits with the small FMS Knob.
5)
Press the ENT Key to complete code digit entry.
EIS
ADDITIONAL AUDIO PANEL FUNCTIONS
Speaker
Audio Panel
and CNS
All of the radios can be heard over the cabin speaker. Pressing the SPKR Key selects and
deselects the cabin speaker. Speaker audio is muted when the PTT is pressed.
Passenger Address Mode (PA Mode)
Flight
Management
Press and hold the SPKR Key for 2 seconds to initiate Passenger Address Mode. PA
Mode is annunciated by a rapid blinking of the SPKR annunciator. When in PA Mode
the crew can use the PTT “Push-to-Talk” button to deliver announcements over the
speaker, to the passenger headsets, or both depending on configuration.
Hazard
Avoidance
Split-PA Mode
AFCS
During Split-PA Mode the pilot can continue to use the radio(s) while the copilot
delivers PA announcements. To initiate Split-PA Mode, first enter Split-COM Mode by
pressing more than one MIC Key simultaneously, then press and hold the SPKR Key for
2 seconds.
Intercom
Abnormal
Operation
Additional
Features
The GMA 350 includes a six-position intercom system (ICS), one music input, and one
telephone/entertainment input for the pilot, copilot and passengers. The intercom
provides Pilot, Copilot, and Passenger audio isolation.
Figure 11 Intercom Controls
Annunciations
& Alerts
Press the PILOT, COPLT, and/or PASS Keys to distribute as required. If the
annunciators are lit, those positions will share intercom audio. If an annunciator is NOT
lit that position is isolated from the others.
Appendix
Copilot Configured as Crew or Passenger
Index
NOTE: When the copilot position is configured as a passenger, the COPLT Key is
disabled and the copilot headset is treated as a ‘passenger’ for intercom and
entertainment audio distribution.
The copilot position can be configured as crew (COPLT Key enabled) or as a
passenger (COPLT Key disabled). Pressing and holding the COPLT Key toggles the
20
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
Intercom Modes
EIS
NOTE: In the following modes the copilot position is configured as crew.
Flight
Instruments
copilot position configuration between passenger and crew. The aural message “Copilot
Configured as Passenger” or “Copilot Configured as Crew” is heard.
In ‘All Intercom’ mode the Pilot, Copilot, and Passengers hear each other and hear
the aircraft audio.
Audio Panel
and CNS
ALL INTERCOM MODE
Flight
Management
In ‘Pilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft audio.
The Copilot and Passengers also hear each other.
Hazard
Avoidance
PILOT ISOLATE MODE
AFCS
In ‘Passenger/Crew Isolate’ mode the Pilot and Copilot hear the aircraft audio and
each other. The Passengers hear each other.
Additional
Features
PASSENGER/CREW ISOLATE MODE
Abnormal
Operation
In ‘Copilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft audio.
The Pilot and Passengers also hear each other. The Copilot has the option to use
Split-COM mode.
Annunciations
& Alerts
COPILOT ISOLATE MODE
Appendix
Index
ALL ISOLATE MODE
In ‘All Isolate’ mode the Pilot and Copilot hear the aircraft audio. The Copilot has
the option to use Split-COM mode. The Passengers hear each other.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
21
Flight
Instruments
Audio Panel and CNS
EIS
PILOT & COPILOT ISOLATE MODE
Flight
Management
Audio Panel
and CNS
In ‘Pilot & Copilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft
audio. The Passengers hear each other. The Copilot has the option to use Split-COM
mode.
PILOT & PASSENGER ISOLATE MODE
Hazard
Avoidance
In ‘Pilot & Passenger Isolate’ mode the Pilot and Copilot hear the aircraft audio.
The Passengers hear each other.
AFCS
COPILOT & PASSENGER ISOLATE MODE
Abnormal
Operation
Additional
Features
In ‘Copilot & Passenger Isolate’ mode the Pilot and Copilot can hear the aircraft
audio. The Copilot has the option to use Split-COM mode. The Passengers hear each
other.
Annunciations
& Alerts
Blue-Select Mode (Telephone/Entertainment
Distribution)
Index
Appendix
The music (MUSIC) and telephone/entertainment (
) audio are distributed using
the Blue-Select Mode. The following example indicates that the pilot, copilot, and
passengers will all hear the telephone/entertainment audio.
22
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
Flight
Instruments
EIS
When the cursor is on PILOT, COPLT, or PASS, the Volume Control Knob adjusts
the intercom volume for the listener.
ADJUSTING MKR, AUX,
, AND MUS VOLUME
ADJUSTING MANUAL SQUELCH
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
23
Index
When the cursor is on MAN SQ, the Volume Control Knob adjusts the ICS
Squelch Threshold (the volume level that must be exceeded to be heard over the
intercom).
Appendix
, MUS1, or MUS2 the Volume Control
When the cursor is on MKR, AUX,
Knob adjusts the individual volume of the selected source.
Annunciations
& Alerts
When the cursor is on SPKR, the Volume Control Knob adjusts the speaker
volume of the selected sources (COM, NAV, AUX, MKR). Alert volumes are not
affected by the speaker volume control knob.
Abnormal
Operation
ADJUSTING SPEAKER VOLUME
Additional
Features
ADJUSTING INTERCOM VOLUME
AFCS
Selecting any button other than PILOT, COPLT, PASS, MUS or
will cancel BlueSelect Mode. Pressing the small knob will also cancel Blue-Select Mode. After
approximately ten seconds with no input, the Blue-Select Mode will automatically
cancel.
Hazard
Avoidance
The annunciator over the
Button will be flashing blue. Any combination of the
annunciators over the PILOT, COPLT, and PASS buttons may be blue. Select the
desired button to turn the blue annunciator on or off to distribute the telephone audio
to selected crew/passenger positions. Turn the large knob to select MUS, and select the
crew/passenger positions to receive the music audio.
Flight
Management
The Blue-Select Mode is entered by pressing the small knob when the volume control
cursor (flashing white annunciator) is not active. If the volume control cursor is active,
press the small knob twice. The first press will cancel the volume control cursor, the
second will activate Blue-Select Mode.
Audio Panel
and CNS
Figure 12 Blue-Select Mode (Telephone/Entertainment Distribution)
Flight
Instruments
Audio Panel and CNS
Relative Volume/
Squelch Scale
Audio Panel
and CNS
EIS
Manual Squelch Annunciator; Off for
Automatic Squelch, On for Manual Squelch
Volume or Manual Squelch
Cursor
Flight
Management
Figure 13 Volume/Squelch Control
Clearance Recorder and Player
Hazard
Avoidance
The Audio Panel contains a digital clearance recorder that records up to 2.5 minutes of
the selected COM radio signal. Recorded COM audio is stored in separate memory blocks.
Once 2.5 minutes of recording time have been reached, the recorder begins recording over
the stored memory blocks, starting from the oldest block.
AFCS
The PLAY Key controls the play function. Pressing the PLAY Key once plays the latest
recorded memory block. Pressing the PLAY Key while audio is playing begins playing the
previously recorded memory block. Each subsequent press of the PLAY Key selects the
previously recorded memory block.
Pressing the MKR/MUTE Key during play of a memory block stops play. If a COM
input signal is detected during play of a recorded memory block, play is halted.
Additional
Features
Powering off the unit automatically clears all recorded blocks.
Abnormal
Operation
Split-COM Operation
Annunciations
& Alerts
NOTE: Split COM performance is affected by the distance between the COM
antennas and the separation of the tuned frequencies. If the selected COM1 and
COM2 frequencies are too close together, interference may be heard during
transmission on the other radio.
Appendix
Pressing both MIC Keys simultaneously initiates Split COM Mode (i.e., COM1/COM2).
The respective COM1/MIC1 or COM2/MIC2 annunciators are illuminated indicating Split
COM operation. Split COM operation is cancelled by pressing one of the selected MIC
Keys again.
Index
During Split COM operation, both the pilot and the copilot can transmit
simultaneously over separate radios. In Split COM mode, the pilot is uses COM1 and the
copilot is uses COM2.
Entertainment Inputs
The audio panel provides three stereo telephone/entertainment inputs:
24
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Audio Panel and CNS
EIS
The telephone/entertainment Key (
)controls a telephone or entertainment device
connected to the rear of the audio panel or to the Front Panel Jack. For GSR 56
equipped aircraft, the Iridium phone audio is connected to the rear input of the audio
panel. To use the Iridium phone, ensure there is no other audio source plugged into the
Front Panel Jack.
Flight
Instruments
•
• The MUS1 and MUS2 Key controls the Entertainment Music audio input. External
Hazard
Avoidance
Distribution of the entertainment inputs are configured in Blue-Select Mode.
Flight
Management
The Front Panel Jack can be used as an entertainment input or a telephone input.
Plugging a device into the Front Panel Jack will disable any audio source connected to the
rear telephone/entertainment jack (i.e. GSR 56, if so equipped). The Front Panel Jack is a
3.5-mm stereo jack that is compatible with popular portable entertainment devices such
as cell phones and other tablet devices. The headphone outputs of the entertainment
devices are plugged into the Front Panel Jack.
Audio Panel
and CNS
audio jacks can also be used as an entertainment input. GDL 69 (SiriusXM Radio)
audio, if equipped, is wired to the MUS1 and MUS2 inputs. The Front Panel Jack does
not disable audio connected to the MUS1 and MUS2 inputs.
Telephone and Entertainment Muting
Enabling/Disabling Muting
Additional
Features
Press and hold the MUS1, MUS2, or (
) Key for two seconds to toggle muting
on and off. The aural message “Mute Music on Reception Enabled/Disabled” or “Mute
Tel and Jack on Reception Enabled/Disabled” is heard.
AFCS
Telephone and entertainment muting can be enabled or disabled by the user,
however it is always muted during alerts.
SiriusXM Radio Entertainment
AUDIO PANEL PREFLIGHT PROCEDURE
1)
Verify that the PILOT , COPLT and PASS annunciators are lit.
2)
Adjust radio volume levels (COM, NAV) to a suitable level.
Appendix
Setting the Audio Panel During Preflight:
Annunciations
& Alerts
Connecting a stereo input to the Stereo Input jack removes the SiriusXM Radio
Audio from that input.
Abnormal
Operation
SiriusXM Radio audio from the Data Link Receiver may be heard by the pilot and
passengers simultaneously (optional: requires subscription to SiriusXM Radio Service).
Refer to the Additional Features Section for more details on the Data Link Receiver.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
25
3)
Use the Blue-Select Mode to distribute the telephone/entertainment (
MUS1, and MUS2 appropriately.
4)
Use the VOL/CRSR Knobs to adjust the intercom volumes to the desired level.
),
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Audio Panel and CNS
26
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
FLIGHT MANAGEMENT
INTRODUCTION
EIS
Changing a field in the MFD Navigation Data Bar:
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the desired field number in the ‘MFD Data
Bar Fields’ Box.
4)
Turn the small FMS Knob to display and scroll through the data options list to
select the desired data.
5)
Press the ENT Key. Pressing the Defaults Softkey returns all fields to the default
setting.
Flight
Management
Select the ‘Aux - System Setup 1’ Page.
Audio Panel
and CNS
1)
Hazard
Avoidance
USING MAP DISPLAYS
Changing the Navigation Map orientation:
With the ‘Map - Navigation Map’ Page displayed, press the MENU Key. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key to display the ‘Map Settings’ Window. Select the ‘Map’
group if necessary.
3)
Turn the large FMS Knob, or press the ENT Key once, to select the ‘Orientation’
field.
4)
Turn the small FMS Knob to select the desired orientation.
5)
Press the ENT Key to select the new orientation.
6)
Press the FMS Knob to return to the base page.
AFCS
1)
Abnormal
Operation
Annunciations
& Alerts
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ group.
4)
Press the ENT Key.
5)
Highlight the ‘North Up Above’ Field.
6)
Select ‘On’ or ‘Off’ using the small FMS Knob.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
Appendix
1)
Additional
Features
Enabling/disabling Auto North Up and selecting the
minimum switching range:
27
Flight
Instruments
Flight Management
7)
Press the ENT Key to accept the selected option. The flashing cursor highlights
the range field.
8)
Use the small FMS Knob to select the desired range.
9)
Press the ENT Key to accept the selected option.
EIS
10) Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Configuring automatic zoom:
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ Group.
4)
Press the ENT Key.
5)
Highlight the ‘Auto Zoom’ On/Off Field, and select ‘Off’ or ‘On’ using the small
FMS Knob.
6)
Press the ENT Key to accept the selected option. The flashing cursor highlights
the ‘Auto Zoom’ display selection field.
7)
Select ‘MFD’, ‘PFD’, or ‘All’ using the small FMS Knob.
8)
Press the ENT Key to accept the selected option. The flashing cursor highlights
the ‘Max Look FWD’ Field. Times are from zero to 999 minutes.
9)
Use the FMS Knobs to set the ‘Max Look FWD’ time. Press the ENT Key.
10) Repeat step 9 for ‘Min Look FWD’ (zero to 99 minutes) and ‘Time Out’ (zero to
99 minutes).
Panning the map:
1)
Push the Joystick to display the Map Pointer.
2)
Move the Joystick to move the Map Pointer around the map.
3)
Push the Joystick to remove the Map Pointer and recenter the map on the
aircraft’s current position.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
11) Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
28
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Reviewing information for an airport, NAVAID, or user
waypoint:
With the desired map page displayed on the MFD, push the Joystick to display
the Map Pointer and place the Map Pointer on a waypoint.
2)
Press the ENT Key to display the ‘WPT - Waypoint Information’ Page for the
selected waypoint.
3)
Press the Go Back Softkey, the CLR Key, or the ENT Key to exit the ‘WPT Waypoint Information’ Page and return to the Navigation Map showing the
selected waypoint.
EIS
1)
Audio Panel
and CNS
2)
Press the ENT Key to display an options menu.
3)
‘Review Airspaces’ should already be highlighted, if not select it. Press the ENT
Key to display the ‘Information’ Window for the selected airspace.
4)
Press the FMS Knob, the CLR Key, or the ENT Key to exit the ‘Information’
Window.
Additional
Features
Measuring bearing and distance between any two points:
AFCS
With the desired map page displayed on the MFD, push the Joystick to display
the Map Pointer and place the Map Pointer on an open area within the
boundaries of an airspace. (As the Map Pointer crosses the airspace boundary,
the boundary is highlighted and airspace information is shown.)
Hazard
Avoidance
1)
Flight
Management
Reviewing information for a special-use or controlled
airspace:
Press the MENU Key (with the ‘Map - Navigation Map’ Page displayed).
2)
Highlight the ‘Measure Bearing/Distance’ Field.
3)
Press the ENT Key. A Measure Pointer is displayed on the map at the aircraft’s
present position.
4)
Move the Joystick to place the reference pointer at the desired location. The
bearing and distance are displayed at the top of the map. Elevation at the
current pointer position is also displayed. Pressing the ENT Key changes the
starting point for measuring.
5)
To exit the Measure Bearing/Distance option, push the Joystick; or select ‘Stop
Measuring’ from the ‘Page Menu’ Window and press the ENT Key.
Abnormal
Operation
1)
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
29
Displaying/removing topographic data on all MFD pages
displaying navigation maps:
1)
Press the Map Opt Softkey.
2)
Press the TER Softkey until ‘Topo’ is shown on the softkey to display
topographic data.
3)
Press the TER Softkey until ‘Off’ is shown on the softkey to remove topographic
data from the navigation map. When topographic data is removed from the
page, all navigation data is presented on a black background.
Displaying/removing topographic data on the PFD Map:
1)
Press the Map/HSI Softkey.
2)
Press the TER Softkey until ‘Topo’ is shown on the softkey to display
topographic data.
3)
Press the TER Softkey until ‘Off’ is shown on the softkey to remove topographic
data from the navigation map. When topographic data is removed from the
page, all navigation data is presented on a black background.
Displaying/removing topographic data using the
Navigation Map Page Menu:
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ Group.
4)
Press the ENT Key.
5)
Highlight the ‘Terrain Display’ Field.
6)
Select ‘Topo’ or ‘Off’.
7)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Selecting a topographical data range (Terrain Display):
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
30
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ Group.
4)
Press the ENT Key.
5)
Highlight the ‘Terrain Display’ range Field. Ranges are from 1 nm to 1000 nm.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
7)
Select the desired range using the small FMS Knob.
8)
Press the ENT Key.
9)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
EIS
To change the Terrain Display range setting, turn the small FMS Knob to display
the range list.
Flight
Instruments
6)
Displaying/removing the topographic scale (Topo Scale):
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ Group and select the ENT Key.
4)
Highlight the ‘Topo Scale’ Field.
5)
Select ‘On’ or ‘Off’.
6)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Hazard
Avoidance
2)
Flight
Management
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
Audio Panel
and CNS
1)
Setting up the Land, Aviation or Airspace group items:
Press the MENU Key with the Navigation Map Page displayed. The cursor
flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The Map Settings Menu is displayed.
3)
Turn the small FMS Knob to select the desired group.
4)
Press the ENT Key. The cursor flashes on the first field.
5)
Turn the large FMS Knob to select the desired option.
6)
Turn the small FMS Knob to select the desired setting (e.g. On/Off or maximum
range).
7)
Press the ENT Key to accept the selected option and move the cursor to the
next item.
8)
Repeat steps 5-7 as necessary.
9)
Press the FMS Knob to return to the Navigation Map Page.
AFCS
1)
Additional
Features
Annunciations
& Alerts
Appendix
Press the Detail Softkey with the Navigation Map Page displayed. The current
declutter level is shown. With each softkey press, another level of map
information is removed.
Index
Or:
190–02362–00 Rev. A
Abnormal
Operation
Decluttering the MFD Map:
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
31
Press the MENU Key with the Navigation Map Page displayed.
2)
Select ‘Declutter’. The current declutter level is shown.
3)
Press the ENT Key.
1)
Press the Map/HSI Softkey.
2)
Press the Detail Softkey. The current declutter level is shown. With each
selection, another level of map information is removed.
Displaying/removing airways:
Hazard
Avoidance
1)
Press the Map Opt Softkey.
2)
Press the AWY Softkey. Both High and Low Altitude Airways are displayed
(AWY On).
3)
Press the softkey again to display Low Altitude Airways only (AWY LO).
4)
Press the softkey again to display High Altitude Airways only (AWY HI).
5)
Press the softkey again to remove High Altitude Airways. No airways are
displayed (AWY Off).
Abnormal
Operation
Additional
Features
AFCS
Or:
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key.
4)
Turn the large FMS Knob to highlight the ‘Low ALT Airways’ On/Off Field.
5)
Turn the FMS Knob to select ‘Off’ or ‘On’.
6)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Selecting an airway range (Low ALT Airways or High ALT
Airways):
Index
Appendix
Annunciations
& Alerts
1)
Decluttering the PFD Map:
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
32
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Airways’ Group, and press the ENT Key.
4)
Highlight the ‘Low ALT Airways’ or ‘High ALT Airways’ range Field.
5)
To change the range setting, turn the small FMS Knob to display the range list.
6)
Select the desired range using the small FMS Knob.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the ENT Key.
8)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Flight
Instruments
7)
Setting up additional Map group items:
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Map’ Group.
4)
Press the ENT Key. The cursor flashes on the first field.
5)
Turn the large FMS Knob to select the desired option.
6)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
Flight
Management
2)
Audio Panel
and CNS
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
EIS
1)
If it is a data field, use the FMS Knob to select the range or time value.
Press the ENT Key to accept the selected option and move the cursor to the
next item.
8)
Repeat steps 5-7 as necessary.
9)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Hazard
Avoidance
7)
AFCS
WAYPOINTS
2)
Use the FMS Knobs and enter an identifier, facility name, or location.
3)
Press the ENT Key.
4)
Press the FMS Knob to remove the cursor.
Selecting a runway:
2)
Turn the large FMS Knob to place the cursor in the ‘Runways’ Box, on the
runway designator.
3)
Turn the small FMS Knob to display the desired runway (if more than one) for
the selected airport.
4)
To remove the flashing cursor, press the FMS Knob.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
With the ‘WPT - Airport Information’ Page (Info 1 Softkey) displayed, press the
FMS Knob to activate the cursor.
Appendix
1)
Annunciations
& Alerts
From the ‘WPT - Airport Information’ Page (Info 1 Softkey), press the FMS
Knob.
Abnormal
Operation
1)
Additional
Features
Selecting an airport for review by identifier, facility name,
or location:
33
Flight
Instruments
Flight Management
Viewing a destination airport:
From the ‘WPT - Airport Information’ Page (Info 1 Softkey) press the MENU
Key. Select ‘View Destination Airport’. The Destination Airport is displayed.
Press the Nearest Softkey to display the Nearest Airports Window.
2)
Highlight the airport identifier with the FMS Knob and press the ENT Key to
display the Airport Information Window.
3)
To return to the Nearest Airports Window press the ENT Key (with the cursor on
‘BACK’) or press the CLR Key. The cursor is now on the next airport in the
nearest airports list. (Repeatedly pressing the ENT Key moves through the
airport list, alternating between the Nearest Airports Window and the Airport
Information Window.)
4)
Press the CLR Key or the Nearest Softkey to close the PFD Nearest Airports
Window.
Additional
Features
Abnormal
Operation
1)
Turn the large FMS Knob to select the ‘NRST’ page group.
2)
Turn the small FMS Knob to select the ‘Nearest Airports’ Page (it is the first
page of the group, so it may already be selected). If there are no Nearest
Airports available, ‘None Within 200nm’ is displayed.
3)
Press the APT Softkey; or press the FMS Knob; or press the MENU Key,
highlight ‘Select Airport Window’ and press the ENT Key. The cursor is placed in
the ‘Nearest Airports’ Box. The first airport in the nearest airports list is
highlighted.
4)
Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also
moves to the next airport.)
5)
Press the FMS Knob to remove the flashing cursor.
Viewing runway information for a specific airport:
1)
1) With the ‘NRST - Nearest Airports’ Page displayed, press the RNWY Softkey;
or press the MENU Key, highlight ‘Select Runway Window’; and press the ENT
Key. The cursor is placed in the ‘Runways’ Box.
2)
2) Turn the small FMS Knob to select the desired runway.
3)
3) Press the FMS Knob to remove the flashing cursor.
Index
Appendix
Annunciations
& Alerts
1)
Viewing information for a nearest airport on the MFD:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Viewing information for a nearest airport on the PFD:
34
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Selecting nearest airport surface and minimum runway
length matching criteria:
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the ‘Runway Surface’ Field in the ‘Nearest
Airport’ Box.
4)
Turn the small FMS Knob to select the desired runway option (Any, Hard Only,
Hard/Soft).
5)
Press the ENT Key. The cursor moves to the ‘Minimum Length’ Field in the
‘Nearest Airport’ Box.
6)
Use the FMS Knob to enter the minimum runway length (zero to 25,000 feet)
and press the ENT Key.
7)
Press the FMS Knob to remove the flashing cursor.
Audio Panel
and CNS
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page.
EIS
1)
Flight
Management
With the ‘WPT - Intersection Information’ Page displayed, enter an identifier in
the ‘Intersection’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
AFCS
1)
Hazard
Avoidance
Selecting an intersection:
Or:
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
INT’ Box.
3)
Press the FMS Knob to remove the flashing cursor.
Abnormal
Operation
With the ‘NRST - Nearest Intersections’ Page displayed, press the FMS Knob.
Selecting an NDB:
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Appendix
With the ‘WPT - NDB Information’ Page displayed, enter an identifier, the name
of the NDB, or the city in which it’s located in the ‘NDB’ Box.
Or:
With the Nearest NDB Page displayed, press the FMS Knob.
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
NDB’ Box.
3)
Press the FMS Knob to remove the flashing cursor.
35
Index
1)
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Annunciations
& Alerts
1)
190–02362–00 Rev. A
Additional
Features
1)
Selecting a VOR:
EIS
Flight
Instruments
Flight Management
1)
With the ‘WPT - VOR Information’ Page displayed, enter an identifier, the name
of the VOR, or the city in which it’s located in the ‘VOR’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Flight
Management
Audio Panel
and CNS
Or:
1)
With the ‘NRST - Nearest VOR’ Page displayed, press the FMS Knob or press the
VOR Softkey.
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
VOR’ Box.
3)
Press the FMS Knob to remove the flashing cursor.
AFCS
Hazard
Avoidance
Or:
1)
With the ‘NRST - Nearest VOR’ Page displayed, press the MENU Key.
2)
Highlight ‘Select VOR Window’, and press the ENT Key.
3)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
VOR’ Box.
4)
Press the FMS Knob to remove the flashing cursor.
Abnormal
Operation
Additional
Features
Selecting a VRP:
With the ‘WPT - VRP Information’ Page displayed, enter the identifier or the
name of the VRP in the ‘VRP’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Annunciations
& Alerts
Or:
1)
With the ‘NRST - Nearest VRP’ Page displayed, press the FMS Knob.
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
VRP’ Box.
3)
Press the FMS Knob to remove the flashing cursor.
Selecting a User Waypoint:
Index
Appendix
1)
36
1)
With the ‘WPT - User WPT Information’ Page displayed, enter the name of the
User Waypoint, or scroll to the desired waypoint in the ‘User Waypoint List’ Box
using the large FMS Knob.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Or:
With the ‘NRST - Nearest User WPTS’ Page displayed, press the FMS Knob.
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the ‘Nearest
User’ Box.
3)
Press the FMS Knob to remove the flashing cursor.
EIS
1)
Audio Panel
and CNS
Creating user waypoints from the User WPT Information
Page:
Press the New Softkey, or press the MENU Key and select ‘Create New User
Waypoint’.
2)
Enter a user waypoint name (up to six characters).
3)
Press the ENT Key. The current aircraft position is the default location of the
new waypoint.
4)
If desired, define the type and location of the waypoint in one of the following
ways:
Flight
Management
1)
Hazard
Avoidance
Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the
two reference waypoint identifiers and radials into the ‘Reference Waypoints’
Box using the FMS Knobs.
AFCS
Or:
Or:
Press the ENT Key to accept the new waypoint.
6)
If desired, change the storage method of the waypoint to temporary by moving
the cursor to ‘Temporary’ and selecting the ENT Key to check the box.
7)
Press the FMS Knob to remove the flashing cursor.
Annunciations
& Alerts
5)
Abnormal
Operation
Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the
latitude and longitude into the ‘Information’ Box using the FMS Knobs.
Additional
Features
Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the
reference waypoint identifier, the radial, and the distance into the ‘Reference
Waypoints’ Box using the FMS Knobs.
Or:
Appendix
Press the FMS Knob to activate the cursor.
2)
Enter a user waypoint name (up to six characters).
3)
Press the ENT Key. The message ‘Are you sure you want to create the new user
waypoint AAAAAA?’ is displayed.
4)
With ‘YES’ highlighted, press the ENT Key.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
37
Index
1)
Flight Management
Flight
Instruments
5)
If desired, define the type and location of the waypoint in one of the following
ways:
EIS
Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the
two reference waypoint identifiers and radials into the ‘Reference Waypoints’
Box using the FMS Knobs.
Or:
Audio Panel
and CNS
Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the
reference waypoint identifier, the radial, and the distance into the ‘Reference
Waypoints’ Box using the FMS Knobs.
Or:
Hazard
Avoidance
Flight
Management
Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the
latitude and longitude into the ‘Information’ Box using the FMS Knobs.
6)
Press the ENT Key to accept the new waypoint.
7)
If desired, change the storage method of the waypoint to temporary by moving
the cursor to ‘Temporary’ and selecting the ENT Key to check the box.
8)
Press the FMS Knob to remove the flashing cursor.
1)
Push the Joystick to activate the panning function and pan to the map location
of the desired user waypoint.
2)
Press the ENT Key. The ‘WPT - User WPT Information’ Page is displayed with the
captured position.
Additional
Features
AFCS
Creating user waypoints from map pages:
Appendix
Annunciations
& Alerts
Abnormal
Operation
NOTE: If the pointer has highlighted a map database feature, one of three
things happens upon pressing the ENT Key: 1) information about the selected
feature is displayed instead of initiating a new waypoint, 2) a menu pops up
allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a
new waypoint is initiated with the default name being the selected map item.
3)
Enter a user waypoint name (up to six characters).
4)
Press the ENT Key to accept the selected name. The first reference waypoint
box is highlighted.
5)
If desired, define the type and location of the waypoint in one of the following
ways:
Index
Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the
two reference waypoint identifiers and radials into the ‘Reference Waypoints’
Box using the FMS Knobs.
Or:
38
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the
reference waypoint identifier, the radial, and the distance into the ‘Reference
Waypoints’ Box using the FMS Knobs.
Or:
7)
If desired, change the storage method of the waypoint to temporary or normal
by moving the cursor to ‘Temporary’ and selecting the ENT Key to check or
uncheck the box.
8)
Press the FMS Knob to remove the flashing cursor.
9)
Press the Go Back Softkey to return to the map page.
Flight
Management
Press the ENT Key to accept the new waypoint.
Audio Panel
and CNS
6)
EIS
Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the
latitude and longitude into the ‘Information’ Box using the FMS Knobs.
Editing a user waypoint comment or location:
2)
Select a user waypoint in the ‘User Waypoint List’ Box, if required, and press the
ENT Key.
3)
Move the cursor to the desired field.
4)
Turn the small FMS Knob to make any changes.
5)
Press the ENT Key to accept the changes.
6)
Press the FMS Knob to remove the flashing cursor.
AFCS
With the ‘WPT - User WPT Information’ Page displayed, press the FMS Knob to
activate the cursor.
Hazard
Avoidance
1)
Additional
Features
Renaming user waypoints:
With the ‘WPTS - User WPT Information’ Page displayed, highlight a user
waypoint in the ‘User Waypoint List’ Box. Press the Rename Softkey, or press the
MENU Key and select ‘Rename User Waypoint’.
Abnormal
Operation
2)
Enter a new name.
3)
Press the ENT Key. The message ‘Do you want to rename the user waypoint
AAAAAA to BBBBBB?’ is displayed.
Annunciations
& Alerts
4)
With ‘YES’ highlighted, press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Appendix
1)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
39
Changing the location of an existing waypoint to the
aircraft present position:
Abnormal
Operation
Additional
Features
AFCS
With the ‘WPT - User WPT Information’ Page displayed, enter a waypoint name
or select the waypoint in the ‘User Waypoint List’ Box, then press the ENT Key.
2)
Press the MENU Key.
3)
Select ‘Use Present Position’.
4)
Press the ENT Key twice. The new waypoint’s location is saved.
5)
Press the FMS Knob to remove the flashing cursor.
1)
With the ‘WPT - User WPT Information’ Page displayed, enter a waypoint name
or select the waypoint in the ‘User Waypoint List’ Box, then press the ENT Key.
2)
Press the MENU Key.
3)
Select ‘Auto Comment’.
4)
Press the ENT Key. The generated comment is based on the reference point
used to define the waypoint.
Changing the user waypoint storage duration default
setting:
1)
With the ‘WPT - User WPT Information’ Page displayed, press the MENU Key.
2)
Move the cursor to select ‘Waypoint Setup’, and press the ENT Key.
3)
Select ‘Normal’ or ‘Temporary’ as desired, and press the ENT Key.
4)
Press the FMS Knob to remove the flashing cursor and return to the ‘WPT - User
WPT Information’ Page.
Deleting a single user waypoint:
Index
Appendix
Annunciations
& Alerts
1)
Resetting the comment field to the system generated
comment:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
1)
With the ‘WPT - User WPT Information’ Page displayed, highlight a User
Waypoint in the ‘User Waypoint List’ Box, or enter a waypoint in the ‘User
Waypoint’ Box.
2)
Press the Delete Softkey or press the CLR Key. ‘YES’ is highlighted in the
confirmation window.
3)
Press the ENT Key.
4)
Press the FMS Knob to remove the flashing cursor.
Or:
40
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
2)
Press the MENU Key.
3)
Select ‘Delete User Waypoint’.
4)
Press the ENT Key twice to confirm the selection.
5)
Press the FMS Knob to remove the flashing cursor.
EIS
With the ‘WPT - User WPT Information’ Page displayed, highlight a User
Waypoint in the ‘User Waypoint List’ Box, or enter a waypoint in the ‘User
Waypoint’ Box.
Flight
Instruments
1)
Audio Panel
and CNS
Deleting all user waypoints:
2)
Press the MENU Key.
3)
Select ‘Delete All User Waypoints.’
4)
Press the ENT Key twice to confirm the selection.
5)
Press the FMS Knob to remove the flashing cursor.
AFCS
With the ‘WPT - User WPT Information’ Page displayed, highlight a User
Waypoint in the ‘User Waypoint List’ Box.
Hazard
Avoidance
1)
Flight
Management
NOTE: The option to ‘Delete All User Waypoints’ is not available while the
aircraft is in flight.
Additional
Features
AIRSPACES
Displaying and removing airspace altitude labels:
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Airspace’ Group, if necessary, and press
the ENT Key.
4)
Turn the large FMS Knob to select the ‘Airspace ALT LBL’ Field.
5)
Turn the small FMS Knob to select ‘On’ to display labels and ‘Off’ to remove
labels.
6)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
Abnormal
Operation
1)
Annunciations
& Alerts
Appendix
Changing the altitude buffer distance setting:
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page (Setup 1 Softkey).
2)
Press the FMS Knob momentarily to activate the flashing cursor.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
41
Index
1)
3)
Turn the large FMS Knob to highlight the ‘Altitude Buffer’ Field in the ‘Airspace
Alerts’ Box.
4)
Use the FMS Knob to enter an altitude buffer value and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page (Setup 1 Softkey).
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the desired field in the ‘Airspace Alerts’
Box.
4)
Turn the small FMS Knob clockwise to turn the airspace alert On or
counterclockwise to turn the alert Off.
5)
Press the FMS Knob to remove the flashing cursor.
Selecting and viewing an airspace alert with its associated
information:
Additional
Features
AFCS
Hazard
Avoidance
1)
Audio Panel
and CNS
Turning an airspace alert on or off:
Flight
Management
EIS
Flight
Instruments
Flight Management
1)
Use the FMS Knob on the MFD to select the ‘NRST - Nearest Airspaces’ Page.
2)
Press the Alerts Softkey; or press the FMS Knob; or press the MENU Key,
highlight ‘Select Alerts Window’, and press the ENT Key. The cursor is placed in
the ‘Airspace Alerts’ Box.
3)
Select the desired airspace.
4)
Press the FMS Knob to remove the flashing cursor.
Abnormal
Operation
Use the FMS Knob to select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key, and press the ENT Key. The cursor is placed in the ‘Group’
Box.
3)
Turn the small FMS Knob to highlight the ‘Airspace’ and press the ENT Key.
4)
Turn the large FMS Knob to highlight the ‘Smart Airspace’ Field.
5)
Turn the small FMS Knob clockwise to turn smart airspace On or
counterclockwise to turn smart airspace Off.
6)
Press the FMS Knob to remove the flashing cursor.
Index
Appendix
1)
Annunciations
& Alerts
Turning smart airspace on or off:
42
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
DIRECT-TO NAVIGATION
Entering a waypoint identifier, facility name, or city as a
direct-to destination:
EIS
Turn the small FMS Knob clockwise to begin entering a waypoint identifier
(turning it counter-clockwise brings up the waypoint selection submenu - press
the CLR Key to remove it), or turn the large FMS Knob to select the facility
name, or city field and turn the small FMS Knob to begin entering a facility
name or city. If duplicate entries exist for the entered facility or city name,
additional entries can be viewed by turning the small FMS Knob during the
selection process.
3)
Press the ENT Key. ‘Activate?’ is highlighted.
4)
Press the ENT Key to activate the direct-to.
Hazard
Avoidance
2)
Turn the small FMS Knob counter-clockwise to display a list of flight plan
waypoints (the FPL list is populated only when navigating a flight plan).
3)
Select the desired waypoint.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
Abnormal
Operation
2)
Additional
Features
While navigating an active flight plan, press the Direct-to Key. The ‘Direct To’
Window is displayed with the active flight plan waypoint as the default
selection.
AFCS
Selecting an active flight plan waypoint as a direct-to
destination:
1)
2)
Select the desired waypoint.
3)
Press the Direct-to Key.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
Appendix
Select the ‘FPL - Active Flight Plan’ Page on the MFD, or the ‘Flight Plan’
Window on the PFD.
Annunciations
& Alerts
Or:
1)
Flight
Management
Press the Direct-to Key. The ‘Direct To’ Window is displayed (with the active
flight plan waypoint as the default selection or a blank waypoint field if no
flight plan is active).
Audio Panel
and CNS
1)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
43
Selecting a Nearest, Recent or User waypoint as a direct-to
destination:
1)
Press the Direct-to Key. The ‘Direct To’ Window is displayed (with the active
flight plan destination as the default selection or a blank destination if no flight
plan is active).
2)
Turn the small FMS Knob counter-clockwise to display a list of flight plan
waypoints (the FPL list is populated only when navigating a flight plan).
3)
Turn the small FMS Knob clockwise to display the Nearest, Recent or User
waypoints.
4)
Turn the large FMS Knob clockwise to select the desired waypoint.
5)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
6)
Press the ENT Key again to activate the direct-to.
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
Select the page or window containing the desired waypoint type and select the
desired waypoint.
2)
Press the Direct-to Key to display the ‘Direct To’ Window with the selected
waypoint as the direct-to destination.
3)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
4)
Press ENT again to activate the direct-to.
1)
Press the Nearest Softkey on the PFD; or turn the FMS Knob to display the
‘NRST - Nearest Airports’ Page on the MFD and press the FMS Knob.
2)
Select the desired airport (the nearest one is already selected).
3)
Press the Direct-to Key.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
Selecting a manual direct-to course:
Index
Appendix
Annunciations
& Alerts
1)
Selecting a nearby airport as a direct-to destination:
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Selecting any waypoint as a direct-to destination:
44
1)
Press the Direct-to Key. The ‘Direct To’ Window is displayed with the
destination field highlighted.
2)
Highlight the ‘Course’ Field.
3)
Enter the desired course.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the Direct-to Key. The ‘Direct To’ Window is displayed with the cursor
flashing in the ‘Ident, Facility, City’ Box.
2)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
3)
Press the ENT Key again to activate the direct-to.
EIS
1)
Flight
Instruments
Reselecting the direct course from the current position:
2)
Move the Joystick to place the pointer at the desired destination location.
3)
If the pointer is placed on an existing airport, NAVAID, VRP, or user waypoint,
the waypoint name is highlighted.
4)
Press the Direct-to Key to display the ‘Direct To’ Window with the selected
point entered as the direct-to destination.
5)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
6)
Press the ENT Key again to activate the direct-to.
Hazard
Avoidance
From a navigation map page, push the Joystick to display the pointer.
Flight
Management
1)
Audio Panel
and CNS
Selecting a waypoint as a direct-to destination using the
pointer:
Press the Direct-to Key to display the ‘Direct To’ Window.
2)
Press the MENU Key.
3)
With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is
still active, the system resumes navigating the flight plan along the closest leg.
Additional
Features
1)
AFCS
Cancelling a Direct-to:
Abnormal
Operation
Entering a VNV altitude and along-track offset for the
waypoint:
Turn the large FMS Knob to place the cursor over the ‘VNV’ Box altitude field.
3)
Enter the desired altitude.
4)
Press the ENT Key to accept the altitude constraint; if the selected waypoint is
an airport, an additional choice is displayed. Turn the small FMS Knob to choose
‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude.
5)
The cursor is now flashing in the ‘VNV’ Box offset distance field.
6)
Enter the desired along-track distance before the waypoint.
7)
Press the ENT Key. ‘Activate?’ is highlighted.
8)
Press the ENT Key to activate.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
2)
Appendix
Press the Direct-to Key to display the ‘Direct To’ Window.
Annunciations
& Alerts
1)
45
Removing a VNV altitude constraint:
EIS
Flight
Instruments
Flight Management
1)
Press the Direct-to Key to display the ‘Direct To’ Window.
2)
Press the MENU Key.
3)
With ‘Clear Vertical Constraints’ highlighted, press the ENT Key.
Creating an active flight plan:
1)
Press the FPL Key. Press the small FMS Knob to activate the cursor (only on
MFD).
2)
Select the origin airport and runway.
a)
Highlight the field below the Origin header to enter the origin airport
identifier using the FMS Knob.
b)
Use the FMS Knob or the waypoint submenu to enter the identifier, facility,
or city name of the departure waypoint.
c)
Press the ENT Key. The ‘Set Runway’ Window is displayed with the
‘Runway’ Field highlighted.
d)
Turn the small FMS Knob to select the runway, and press the ENT Key.
e)
Press the ENT Key again to add the origin airport/runway to the flight plan.
3)
Repeat step number 2 for the destination airport and runway.
4)
Select the enroute waypoints.
a)
Highlight the location to insert the waypoint using the FMS Knob (If the
enroute header is selected, the new waypoint is placed following the
header. If an enroute waypoint or the dashes are selected, the new
waypoint will be placed ahead of the selected item).
b)
Use the FMS Knob or the waypoint submenu to enter the identifier, facility,
or city name of the waypoint. The active flight plan is modified as each
waypoint is entered.
5)
Repeat step number 4 to enter each additional enroute waypoint.
6)
When all waypoints have been entered, press the FMS Knob to remove the
cursor (if required).
Creating a stored flight plan:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
FLIGHT PLANNING
46
1)
From the MFD, press the FPL Key.
2)
Turn the small FMS Knob clockwise to display the ‘FPL - Flight Plan Catalog’
Page.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the New Softkey; or press the MENU Key, highlight ‘Create New Flight
Plan’, and press the ENT Key to display a blank flight plan for the first empty
storage location.
4)
Select the origin airport and runway.
Flight
Instruments
3)
Highlight the field below the Origin header to enter the origin airport
identifier using the FMS Knob.
b)
Use the FMS Knob or the waypoint submenu to enter the identifier, facility,
or city name of the departure
c)
Press the ENT Key. The ‘Set Runway’ Window is displayed with the
‘Runway’ Field highlighted.
d)
Turn the small FMS Knob to select the runway, and press the ENT Key.
e)
Press the ENT Key again to add the origin airport/runway to the flight plan.
Select the enroute waypoints.
Hazard
Avoidance
6)
b)
Use the FMS Knob or the waypoint submenu to enter the identifier, facility,
or city name of the waypoint.
c)
Press the ENT Key. The stored flight plan is modified as each waypoint is
entered.
8)
When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Abnormal
Operation
Repeat step number 6 to enter each additional enroute waypoint.
Additional
Features
Highlight the location to insert the waypoint using the FMS Knob (If the
enroute header is selected, the new waypoint is placed following the
header. If an enroute waypoint or the dashes are selected, the new
waypoint will be placed ahead of the selected item.)
Importing a Flight Plan from an SD Card:
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
3)
Turn the small FMS Knob to select the ‘FPL - Flight Plan Catalog’ Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the Import Softkey; or press the MENU Key, select “Import Flight Plan”,
and press the ENT Key.
If an empty slot is selected, a list of the available flight plans on the SD card will
be displayed.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
47
Index
2)
Appendix
Insert the SD card containing the flight plan in the top card slot on the MFD.
Annunciations
& Alerts
1)
AFCS
a)
7)
Flight
Management
Repeat step number 4 for the destination airport and runway.
Audio Panel
and CNS
5)
EIS
a)
Flight Management
Flight
Instruments
Or:
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key to initiate the import.
9)
Press the ENT Key again to confirm the import.
Flight
Management
Audio Panel
and CNS
EIS
If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK or
CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the
selected flight plan and see the list of available flight plans on the SD card. If
overwriting the existing flight plan is not desired, select ‘CANCEL’ using the
FMS Knob, press the ENT Key, select another flight plan slot, and press the
Import Softkey again.
Hazard
Avoidance
NOTE: If the imported flight plan contains a waypoint with a name that
duplicates the name of a waypoint already stored on the system, the system
compares the coordinates of the imported waypoint with those of the existing
waypoint. If the coordinates are different, the imported waypoint is
automatically renamed by adding characters to the end of the name.
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Exporting a Flight Plan to an SD Card:
1)
Insert the SD card into the top card slot on the MFD.
2)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
3)
Turn the small FMS Knob to select the ‘FPL - Flight Plan Catalog’ Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the Export Softkey; or press the MENU Key, select ‘Export Flight Plan’.
7)
If desired, change the name for the exported file by turning the large FMS Knob
to the left to highlight the name, then use the small and large FMS knobs to
enter the new name, and press the ENT Key.
8)
Press the ENT Key to initiate the export.
9)
Press the ENT Key to confirm the export.
Index
Appendix
NOTE: The exported flight plan will not contain any procedures or airways.
48
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
When a flight plan transfer has been initiated from a mobile device, a Pending
Flight Plan pop-up alert appears in the lower right corner of the MFD, and a
Connext annunciation appears to the right of the MFD page name.
2)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the MFD.
EIS
1)
Flight
Instruments
Previewing a pending flight plan transfer from a wireless
connection:
Press the Preview Softkey to display the ‘FPL - Preview Flight Plan’ Page on the
MFD.
Audio Panel
and CNS
Or:
Or:
b)
Turn the FMS Knob to highlight ‘Preview Flight Plan’.
c)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the
MFD.
Hazard
Avoidance
Press the MENU Key,
Flight
Management
a)
Ignoring a pending flight plan transfer from a wireless
connection:
2)
Press the CLR Key to remove the pop-up alert and ignore the pending flight
plan. The pending flight plan will still be available on the ‘FPL - Flight Plan
Catalog’ Page.
Additional
Features
When a flight plan transfer has been initiated from a mobile device, a Pending
Flight Plan pop-up alert appears in the lower right corner of the MFD, and a
Connext annunciation appears to the right of the MFD page name.
AFCS
1)
Or:
Annunciations
& Alerts
Storing a pending flight plan:
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the FMS Knob to highlight the pending flight plan.
Appendix
1)
Abnormal
Operation
Press the Ignore Softkey to remove the pop-up alert and ignore the pending
flight plan. The pending flight plan will still be available on the ‘FPL - Flight Plan
Catalog’ Page.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
49
Flight
Instruments
Flight Management
5)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the MFD.
6)
Press the Store Softkey to store the flight plan. The pending flight plan is stored
and the pending annunciation is removed.
Audio Panel
and CNS
EIS
Or:
Press the FMS Knob to activate the cursor.
b)
Turn the FMS Knob to highlight ‘Store?’.
c)
Press the ENT Key to store the flight plan. The pending flight plan is stored
and the pending annunciation is removed.
Flight
Management
Or:
a)
Press the MENU Key.
b)
Turn the FMS Knob to highlight ‘Store Flight Plan’.
c)
Press the ENT Key to store the flight plan. The pending flight plan is stored
and the pending annunciation is removed.
Activating a pending flight plan:
Additional
Features
AFCS
Hazard
Avoidance
a)
1)
Press the FPL Key on the MFD and turn the small FMS Knob to display the ‘FPL Flight Plan Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight
the pending flight plan.
3)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page.
4)
Press the Activate Softkey. The ‘Activate Flight Plan?’ Window is displayed.
Abnormal
Operation
Or:
a)
Press the FMS Knob to activate the cursor.
b)
Turn the FMS Knob to highlight ‘Activate?’.
c)
Press the ENT Key. The ‘Activate Flight Plan?’ Window is displayed.
Appendix
Annunciations
& Alerts
Or:
Index
5)
50
a)
Press the MENU Key.
b)
Turn the FMS Knob to highlight ‘Activate Flight Plan’.
c)
Press the ENT Key. The ‘Activate Flight Plan?’ Window is displayed.
With ‘OK’ highlighted, press the ENT Key to activate the pending flight plan.
The pending flight plan becomes the active flight plan and is removed from the
Flight Plan Catalog Page. To cancel the request, press the CLR Key, or highlight
‘CANCEL’ and press the ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the FMS Knob to highlight the desired pending flight plan.
5)
Press the Delete Softkey. The ‘Delete Flight Plan XX?’ Window is displayed.
EIS
1)
Flight
Instruments
Deleting a pending flight plan:
Audio Panel
and CNS
Or:
Press the CLR Key. The ‘Delete Flight Plan XX?’ Window is displayed.
Press the MENU Key.
b)
Turn the FMS Knob to highlight ‘Delete Flight Plan’.
c)
Press the ENT Key. The ‘Delete Flight Plan XX?’ Window is displayed.
With ‘OK’ highlighted, press the ENT Key to delete the pending flight plan. The
pending flight plan is removed from the Flight Plan Catalog Page. To cancel the
request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
AFCS
Deleting all pending flight plans:
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the MENU Key.
4)
Turn the FMS Knob to highlight ‘Delete All Pending’.
5)
Press the ENT Key. A ‘Delete all pending flight plans?’ confirmation Window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete all pending flight plans. To
cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT
Key.
Additional
Features
1)
2)
Highlight the desired flight plan.
3)
Press the Edit Softkey; or press the ENT Key, turn the large FMS Knob
clockwise to select “EDIT” and press the ENT Key. The Stored Flight Plan Page is
displayed.
51
Index
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Appendix
On the ‘FPL - Flight Plan Catalog’ Page, press the FMS Knob to activate the
cursor.
Annunciations
& Alerts
1)
Abnormal
Operation
Adding a waypoint to a stored flight plan:
190–02362–00 Rev. A
Hazard
Avoidance
6)
a)
Flight
Management
Or:
4)
Select the point in the flight plan to add the new waypoint. The new waypoint
is placed directly in front of the highlighted waypoint.
5)
Turn the small FMS Knob to display the ‘Waypoint Information’ Window.
(Turning it clockwise displays a blank ‘Waypoint Information’ Window, turning it
counter-clockwise displays the ‘Waypoint Information Window’ with a waypoint
selection submenu allowing selection of active flight plan, nearest, recent, user,
or airway waypoints).
6)
Enter the identifier, facility, or city name of the waypoint or select a waypoint
from the submenu of waypoints and press the ENT Key. The new waypoint now
exists in the flight plan.
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
Adding a waypoint to the active flight plan:
1)
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Select the point in the flight plan to add the new waypoint. The new waypoint
is placed prior to the highlighted waypoint.
4)
Turn the small FMS Knob to display the ‘Waypoint Information’ Window.
(Turning it clockwise displays a blank ‘Waypoint Information’ Window, turning it
counter-clockwise displays the ‘Waypoint Information’ Window with a waypoint
selection submenu allowing selection of active flight plan, nearest, recent, user,
or airway waypoints).
5)
Enter the identifier, facility, or city name of the waypoint or select a waypoint
from the submenu of waypoints and press the ENT Key. The active flight plan is
modified as each waypoint is entered.
Creating and adding user waypoints to the active flight
plan:
1)
Press the FPL Key
2)
Press the FMS Knob on the MFD to activate the cursor.
3)
Select the point in the flight plan to add the new waypoint.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
NOTE: If the identifier entered in the Waypoint Information Window has
duplicates, a Duplicate Waypoint Window is displayed. Use the FMS Knob to
select the correct waypoint.
52
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Push the Joystick on the MFD to activate the panning function on the ‘FPL Active Flight Plan’ Page and pan to the map location of the desired user
waypoint.
5)
Press the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and
press the ENT Key. The user waypoint is created with a name of USRxxx (using
the next available in sequence) and is added to the active flight plan.
Flight
Instruments
4)
EIS
Designating a fly-over waypoint:
For the active flight plan, press the FPL Key and press the FMS Knob to activate
the cursor (not required on the PFD).
Audio Panel
and CNS
1)
Or:
3)
Press the MENU Key, highlight ‘Set Fly-Over Waypoint’, and press the ENT Key.
The ‘Set [waypoint] to be a fly-over waypoint?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘Cancel’ and press the ENT Key.
5)
To change the waypoint back to a fly-by waypoint, highlight the desired
waypoint. Press the MENU Key, highlight ‘Set Fly-By Waypoint’, and press the
ENT Key. The ‘Set [waypoint] to be a fly-by waypoint?’ Window is displayed.
With ‘OK’ highlighted, press the ENT Key.
AFCS
Highlight the desired waypoint.
Hazard
Avoidance
2)
Flight
Management
For a stored flight plan, highlight the desired flight plan on the ‘FPL - Flight Plan
Catalog Page’ and press the Edit Softkey.
Additional
Features
Adding an airway to a flight plan:
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry point
should be entered at this time.
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey,
or press the MENU Key and select ‘Load Airway’. The Select Airway Page/
Window is displayed. The LD AIRWY Softkey or the ‘Load Airway’ menu item is
available only when a valid airway entry waypoint has been chosen (the
waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the ENT
Key.
Appendix
2)
Annunciations
& Alerts
Press the FPL Key.
Abnormal
Operation
1)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
53
Flight
Management
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘Load?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the new
airway inserted.
1)
Select a stored flight plan from the ‘FPL - Flight Plan Catalog’ Page.
2)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and
press the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
3)
Press the LD DP Softkey; or press the MENU Key, select ‘Load Departure’, and
press the ENT Key. The ‘PROC - Departure Loading’ Page is displayed.
4)
Select a departure. Press the ENT Key.
5)
Select a runway served by the selected departure, if required. Press the ENT Key.
6)
Select a transition for the selected departure. Press the ENT Key.
7)
Press the ENT Key to load the selected departure procedure.
Loading an arrival procedure into a stored flight plan:
1)
Select a stored flight plan from the ‘FPL - Flight Plan Catalog’ Page.
2)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and
press the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
3)
Press the LD STAR Softkey; or press the MENU Key, select “Load Arrival”, and
press the ENT Key. The ‘PROC - Arrival Loading’ Page is displayed.
4)
Select an arrival. Press the ENT Key.
5)
Select a transition for the selected arrival. Press the ENT Key.
6)
Select a runway served by the selected arrival, if required. Press the ENT Key.
7)
Press the ENT Key to load the selected arrival procedure.
Loading an approach procedure into a stored flight plan:
Index
Appendix
Annunciations
& Alerts
6)
Loading a departure procedure into a stored flight plan:
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
54
1)
Select a stored flight plan from the ‘FPL - Flight Plan Catalog’ Page.
2)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and
press the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
3)
Press the LD APR Softkey; or press the MENU Key, select ‘Load Approach’, and
press the ENT Key. The ‘PROC - Approach Loading’ Page is displayed.
4)
Select the airport and approach:
a)
Use the FMS Knob to select an airport and press the ENT Key.
b)
Select an approach from the list and press the ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
If necessary, push the FMS Knob to exit the approach list, and use the large
FMS Knob to move the cursor to the ‘Approach Channel’ Field.
b)
Use the FMS Knob to enter the approach channel number, and press the
ENT Key to accept the approach channel number. The airport and
approach are selected.
Select a transition for the selected approach. Press the ENT Key.
6)
Press the ENT Key to load the selected approach procedure.
Audio Panel
and CNS
5)
EIS
a)
2)
Highlight ‘Store Flight Plan’.
3)
Press the ENT Key.
4)
With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the next
available position in the flight plan list on the ‘FPL - Flight Plan Catalog’ Page.
Hazard
Avoidance
Press the MENU Key.
Flight
Management
Storing an active flight plan from the Active Flight Plan
Page or the Active Flight Plan Window:
1)
Flight
Instruments
Or:
Viewing information about a stored flight plan:
AFCS
2)
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the desired flight plan.
4)
The ‘Flight Plan Info’ Box displays departure, destination, total distance, and
enroute safe altitude information for the selected flight plan.
5)
Press the Edit Softkey to open the ‘FPL - Stored Flight Plan’ Page and view the
waypoints in the flight plan.
6)
Press the FMS Knob to exit the ‘FPL - Stored Flight Plan’ Page.
Abnormal
Operation
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Additional
Features
1)
Annunciations
& Alerts
Activating a stored flight plan on the MFD:
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight Plan
Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight
the desired flight plan.
Appendix
1)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
55
Press the Activate Softkey; or press the ENT Key twice; or press the MENU Key,
highlight ‘Activate Flight Plan’, and press the ENT Key. The ‘activate stored flight
plan?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
Flight
Management
1)
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight Plan
Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight
the desired flight plan.
3)
Press the Invert Softkey; or press the MENU Key, highlight ‘Invert & Activate
FPL?’, and press the ENT Key. The ‘Invert and activate stored flight plan?’
Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
Copying a stored flight plan on the MFD:
1)
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight Plan
Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight
the desired flight plan.
3)
Press the Copy Softkey; or press the MENU Key, highlight ‘Copy Flight Plan’,
and press the ENT Key. The ‘Copy to flight plan XX?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel the
request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
Deleting an individual waypoint from a stored flight plan:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
3)
Inverting and activating a stored flight plan on the MFD:
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
56
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the flight plan to be edited.
4)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press
the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
5)
Turn the large FMS Knob to highlight the waypoint to be deleted.
6)
Press the CLR Key. The ‘Remove XXXXX?’ Window is displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
8)
Press the FMS Knob to remove the flashing cursor.
Flight
Instruments
7)
Deleting an entire airway from a stored flight plan:
EIS
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the flight plan to be edited.
4)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press
the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
5)
Turn the large FMS Knob to highlight the header of the airway to be deleted.
6)
Press the CLR Key. The ‘Remove [airway name]from flight plan?’ Window is
displayed.
7)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
8)
Press the FMS Knob to remove the flashing cursor.
AFCS
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
Deleting an entire procedure from a stored flight plan:
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the flight plan to be edited.
4)
Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and
press the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
5)
Turn the large FMS Knob to highlight the header of the procedure to be
deleted.
6)
Press the CLR Key. The ‘Remove [procedure name] from flight plan?’ Window is
displayed.
7)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
8)
Press the FMS Knob to remove the flashing cursor.
Additional
Features
1)
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
Or:
190–02362–00 Rev. A
Hazard
Avoidance
2)
Flight
Management
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Audio Panel
and CNS
1)
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
57
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the flight plan to be edited.
4)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press
the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
5)
Press the MENU Key to display the Page Menu and turn the FMS Knob to
highlight ‘Remove [procedure]’.
6)
Press the ENT Key. The ‘Remove [procedure name] from flight plan?’ Window is
displayed.
7)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
8)
Press the FMS Knob to remove the flashing cursor.
Changing a stored flight plan comment:
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Turn the small FMS Knob clockwise one click to display the ‘FPL - Flight Plan
Catalog’ Page.
3)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the flight plan to be edited.
4)
Press the Edit Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press
the ENT Key. The ‘FPL - Stored Flight Plan’ Page is displayed.
5)
Turn the large FMS Knob to highlight the comment field.
6)
Use the FMS Knobs to edit the comment.
7)
Press the ENT Key to accept the changes.
8)
Press the FMS Knob to remove the flashing cursor.
Deleting a stored flight plan:
1)
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight Plan
Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight
the desired flight plan.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
58
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the Delete Softkey; press the CLR Key; or press the MENU Key, highlight
‘Delete Flight Plan’, and press the ENT Key. The ‘Delete flight plan XX?’ Window
is displayed.
4)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel the
request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
Flight
Instruments
3)
EIS
Deleting all stored flight plans:
2)
Press the MENU Key.
3)
Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all flight plans?’
confirmation window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key to delete all flight plans. To cancel the
request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
AFCS
Activating a flight plan leg:
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the destination waypoint for the desired leg.
3)
Press the ACT Leg Softkey (MFD only); or press the MENU Key, highlight
‘Activate Leg’, and press the ENT Key. A confirmation window is displayed with
‘Activate’ highlighted.
4)
Press the ENT Key to activate the flight plan leg. To cancel, press the CLR Key,
or highlight ‘Cancel’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Annunciations
& Alerts
2)
Inverting the active flight plan:
Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key. An
‘Invert active flight plan?’ confirmation window is displayed.
3)
Select ‘OK’.
4)
Press the ENT Key to invert and activate the active flight plan. To cancel, press
the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
2)
Appendix
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Abnormal
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Additional
Features
1)
1)
Hazard
Avoidance
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight Plan
Catalog’ Page.
Flight
Management
1)
Audio Panel
and CNS
NOTE: The option to delete all stored flight plans is not available while the
aircraft is in flight.
59
Deleting the active flight plan:
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The
‘Delete all waypoints in flight plan?’ Window is displayed.
3)
With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To
cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT
Key.
Deleting an individual waypoint from the active flight
plan:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key. The ‘Remove XXXXX?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Deleting an entire airway from the active flight plan:
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the header of the airway to be deleted.
3)
Press the CLR Key. The ‘Remove [airway name] from flight plan?’ Window is
displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
NOTE: If removal of a flight plan item (waypoint, procedure, etc.) results in
deletion of the end waypoint of the active leg, an off-route direct-to to the
deleted waypoint is created and activated.
60
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Deleting an entire procedure from the active flight plan:
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the header of the procedure to be deleted.
3)
Press the CLR Key. The ‘Remove [procedure name] from flight plan?’ Window is
displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
EIS
1)
Flight
Management
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key to display the Page Menu and turn the FMS Knob to
highlight ‘Remove [procedure]’.
3)
Press the ENT Key. The ‘Remove [procedure name] from flight plan?’ Window is
displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
Hazard
Avoidance
1)
3)
Use the FMS Knobs to edit the comment.
4)
Press the ENT Key to accept the changes.
5)
Press the FMS Knob to remove the flashing cursor.
Annunciations
& Alerts
Press the FMS Knob to activate the cursor and turn the large FMS Knob to
highlight the comment field.
Abnormal
Operation
2)
Additional
Features
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Entering an along track offset distance:
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the waypoint for the along track offset.
3)
Press the ATK OFS Softkey (MFD only); or press the MENU Key, highlight
‘Create ATK Offset Waypoint’, and press the ENT Key.
4)
Enter a positive or negative offset distance in the range of +/- 1 to 999 nm
(limited by leg distances).
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Appendix
1)
AFCS
Changing the active flight plan comment:
1)
Audio Panel
and CNS
Or:
61
Flight
Instruments
Flight Management
5)
Press the ENT Key to create the offset waypoint.
6)
Press the FMS Knob to remove the flashing cursor.
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The
‘Parallel Track’ Window is displayed with the ‘Direction’ Field highlighted.
3)
Turn the small FMS Knob to select ‘LEFT’ or ‘RIGHT’ and press the ENT Key. The
‘Distance’ Field is highlighted.
4)
Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT
Key. ‘Activate Parallel Track’ is highlighted.
5)
Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key
to cancel the parallel track activation.
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The
‘Parallel Track’ Window is displayed with ‘Cancel Parallel Track?’ highlighted.
3)
Press the ENT Key.
Changing the flight plan view:
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the View Softkey to display the Wide, Narrow, Leg-Leg, and CUM
Softkeys.
3)
Press the CUM Softkey to view cumulative waypoint distance, or press the LegLeg Softkey to view leg-to-leg waypoint distance.
4)
Press the Wide Softkey to display the wide view, or select the Narrow Softkey
to display the narrow view.
5)
Press the Back Softkey to return to the top level active flight plan softkeys.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
1)
Cancelling parallel track:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Activating parallel track:
62
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Viewing charts and active flight plan page in split screen
mode:
2)
Press the Charts Softkey. Split screen mode is now enabled showing the Charts
Page alongside the Active Flight Plan Page, and Charts Page is bordered by a
cyan box indicating it is the active display pane.
3)
To quickly view the chart corresponding to the active flight plan leg, press the
AUTO Softkey.
Audio Panel
and CNS
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the Charts Softkey. Split screen mode is now enabled showing the Charts
Page alongside the active flight plan, and the Charts Page is bordered by a cyan
box indicating it is the active display pane.
3)
Move the Joystick to select the Active Flight Plan page as the active display
pane.
4)
Press the MENU Key. ‘Show Flight Plan Map’ is highlighted. Press the ENT Key.
5)
To remove the Flight Plan Map, press the MENU Key and select ‘Hide Flight Plan
Map’. Press the ENT Key.
2)
Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and
press the ENT Key. The airways are collapsed/expanded.
Abnormal
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Annunciations
& Alerts
Determining the closest point along the active flight plan
to a selected waypoint:
2)
Press the MENU Key, highlight ‘Closest Point Of FPL’’, and press the ENT Key. A
window appears with the reference waypoint field highlighted.
3)
Enter the identifier of the reference waypoint. The system displays the bearing
(BRG) and distance (DIS) to the closest point along the flight plan to the selected
reference waypoint and creates a user waypoint at this location. Press the ENT
Key. The name for the new user waypoint is derived from the identifier of the
reference waypoint.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
63
Index
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Appendix
1)
190–02362–00 Rev. A
Additional
Features
Collapsing/expanding the airways in the active flight plan:
AFCS
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Hazard
Avoidance
1)
Flight
Management
Displaying the flight plan map on the active flight plan
page in split mode:
1)
EIS
1)
Creating a user-defined hold at an active flight plan
waypoint:
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key. The
‘Hold at’ Window appears with the ‘Course’ Field highlighted.
4)
Use the FMS Knobs to edit the course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
6)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the
ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and
press the ENT Key.
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
Creating a user-defined hold at the aircraft present
position:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
10) Press the ENT Key while ‘Load?’ is highlighted to insert the hold into the flight
plan.
64
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the ENT
Key. The ‘Hold at’ Window appears with the ‘Course’ Field highlighted.
3)
If desired, use the FMS Knobs to edit the course, and press the ENT Key.
4)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
5)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press
the ENT Key.
6)
Use the FMS Knobs to edit the length, and press the ENT Key.
7)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the
ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and
press the ENT Key.
9)
Press the ENT Key while ‘Activate?’ is highlighted to create an Offroute Directto hold waypoint at the aircraft present position and activate the hold.
EIS
Creating a user-defined hold at a direct-to waypoint:
Flight
Instruments
8)
Press a Direct-to Key and set up the direct-to waypoint as desired, but select
‘Hold?’ instead of ‘Activate?’ when finished.
2)
Use the FMS Knobs to edit the course, and press the ENT Key.
3)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
4)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press
the ENT Key.
5)
Use the FMS Knobs to edit the length, and press the ENT Key.
6)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the
ENT Key.
7)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and
press the ENT Key.
8)
Press the ENT Key while ‘Activate?’ is highlighted to activate the direct-to with
the user-defined hold defined at the direct-to waypoint. (If the direct-to
waypoint is part of the active flight plan, the hold is inserted into the active
flight plan. If the direct-to waypoint is not part of the active flight plan, an offroute direct-to hold is created.)
Audio Panel
and CNS
1)
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Editing a user-defined hold:
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Edit Hold’, and press the ENT Key. The ‘Hold at’
Window appears with the Course Field highlighted.
4)
Use the FMS Knobs to edit the course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
6)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
Appendix
Index
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Annunciations
& Alerts
190–02362–00 Rev. A
Abnormal
Operation
1)
65
Flight
Instruments
Flight Management
EIS
Audio Panel
and CNS
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and
press the ENT Key.
Press the SUSP Softkey. The system will provide guidance to follow the holding
pattern to the inbound course and resume automatic waypoint sequencing.
Removing a user-defined hold inserted into the active
flight plan:
AFCS
Hazard
Avoidance
Flight
Management
9)
Exiting a user-defined hold inserted into the active flight
plan:
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and turn
the large FMS Knob to highlight the ‘HOLD’ waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from the
active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal
of the holding pattern.
Removing a user-defined hold at an off-route direct-to:
Abnormal
Operation
Additional
Features
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the
ENT Key.
10) Press the ENT Key while ‘Update?’ is highlighted to update the hold.
1)
Press a Direct To Key to display the ‘Direct To’ Window (PFD or MFD).
2)
Press the MENU Key to display the Page Menu with the cursor on the ‘Cancel
Direct-To NAV’ selection.
3)
Press the ENT Key. The holding pattern is removed.
VERTICAL NAVIGATION
Enabling and Disabling VNV guidance:
1)
Press the FPL Key on the MFD to display the ‘FPL- Active Flight Plan’ Page.
2)
Press the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’,
and press the ENT Key. Vertical navigation is enabled, and vertical guidance
begins with the waypoint shown in the ‘Active VNV Profile’ Box (defaults first
Index
Appendix
Annunciations
& Alerts
8)
66
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
3)
To Disable VNV guidance, press the Cncl VNV Softkey; or press the MENU Key,
highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled.
EIS
Activating a vertical navigation direct-to:
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight
the desired waypoint.
Press the ENT Key. Vertical guidance begins to the altitude constraint for the
selected waypoint.
5)
Press the FMS Knob to remove the flashing cursor.
AFCS
4)
Hazard
Avoidance
Press the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV
Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to: NNNNNFT
at XXXXXX?’ confirmation window is displayed.
Flight
Management
NOTE: The selected waypoint must have a designated altitude constraint (cyan
number) to be used. If not, the first waypoint in the flight plan with a
designated altitude constraint is selected.
Audio Panel
and CNS
1)
3)
Flight
Instruments
waypoint in the active flight plan with an altitude enabled for vertical
navigation).
Modifying the VS TGT and FPA:
2)
Press the VNV Prof Softkey; or press the MENU Key, highlight ‘Select VNV
Profile Window’, and press the ENT Key. The cursor is now located in the
‘Active VNV Profile’ Box.
3)
Turn the FMS Knobs as needed to edit the values.
4)
Press the FMS Knob to remove the flashing cursor.
Abnormal
Operation
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Additional
Features
1)
The system can use altitude constraints associated with lateral waypoints to give
guidance for vertical navigation. These altitudes are, depending on the specific instance,
manually entered or retrieved from the published altitudes in the navigation database.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
67
Index
190–02362–00 Rev. A
Appendix
Altitudes associated with arrival and approach procedures are “auto-designated”. This
means the system automatically provides descending vertical speed and deviation
guidance to an altitude(s) chosen by the system for any waypoint prior to the FAF. These
altitudes are displayed as cyan text. Additionally, altitudes can be manually designated
prior to the FAF. The FAF can be manually designated if the selected approach provides no
vertical guidance (i.e. glidepath). Manually designated altitudes are displayed as cyan text.
For all designated altitudes, the system will automatically calculate altitude constraints
prior to the designated altitude, which are displayed as white text.
Annunciations
& Alerts
Altitude Constraints
Flight Management
Flight
Instruments
Altitudes that have been designated for use in vertical guidance can be “un-designated”
using the CLR Key. The altitude is now displayed only as a reference (white text). It is not
used to give vertical guidance. Other displayed altitudes may change due to recalculations or be rendered invalid as a result of manually changing an altitude to a nondesignated altitude.
Flight
Management
Audio Panel
and CNS
EIS
Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the
nearest hundred. An altitude constraint in feet above ground level (AGL) format is
supported for airports. When a database altitude restriction is displayed, the system
allows entry of a different altitude when creating a waypoint, effectively overriding the
database restriction (only before the FAF). When a database altitude restriction of type
“AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the
restriction to define the vertical profile.
Altitude Constraint
Examples
Hazard
Avoidance
Cross AT or ABOVE
5,000 ft
Displayed Text
Examples
System Calculated Altitude
(White Text)
Edited Altitude Constraint
(Cyan Text with Pencil Icon)
Designated Altitude Constraint
(Cyan Text)
AFCS
Cross AT 2,300 ft
Additional
Features
Cross AT or BELOW
3,000 ft
White Text with
Altitude Restriction Bar
Temperature
Compensated
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Figure 14 Waypoint Altitude Constraints
68
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
White Text
Cyan Text
5OOOFT
Altitude is designated for use in
determining vertical guidance. A pencil
icon indicates manual designation or
manually edited data entry.
EIS
Altitude calculated by the system
estimating the altitude of the aircraft
as it passes over the navigation point.
No white line above or below to
indicate a potential constraint.
The system cannot use this altitude in
determining vertical guidance because of
an invalid constraint condition.
Hazard
Avoidance
Table 1 Altitude Constraint Color Coding
Additional
Features
Manually designating a waypoint altitude to be used for
vertical guidance:
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3)
Turn the small FMS Knob to enter editing mode.
4)
Press the ENT Key. The altitude is now shown in cyan, indicating it is usable for
vertical guidance.
Abnormal
Operation
1)
2)
Press the FMS Knob, and highlight the desired waypoint altitude. Turn the small
FMS Knob to enter editing mode.
3)
Press the ENT Key. The altitude is now shown in cyan, indicating it is usable for
vertical guidance.
An altitude constraint is invalid if:
69
Index
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Appendix
1)
Annunciations
& Alerts
Manually designating a procedure waypoint altitude to be
used for vertical guidance:
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
AFCS
NOTE: All designated altitudes (cyan text) will be displayed in the Active Flight
Plan Page and Flight Plan Window without restriction bars regardless of what is
shown on the published procedure.
190–02362–00 Rev. A
Flight
Management
Altitude retrieved from the navigation
database. White line above or below
indicates the type of constraint, as
shown in the preceding figure. These
altitudes are provided as a reference,
and are not designated to be used in
determining vertical guidance.
Audio Panel
and CNS
5OOOFT
Flight Management
Flight
Instruments
• Meeting the constraint requires the aircraft to climb
• Meeting the constraint requires the maximum flight path angle or maximum vertical
speed to be exceeded
EIS
• The altitude constraint results in a TOD behind the aircraft present position
• The constraint is within a leg type for which altitude constraints are not supported
• The altitude constraint is added to the FAF of an approach that provides vertical
Audio Panel
and CNS
guidance (i.e., ILS or GPS SBAS approach)
• The altitude constraint is added to a waypoint past the FAF
Entering/modifying an altitude constraint:
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a
flight level, turn the small FMS Knob counter-clockwise past zero or clockwise
past 9 on the first character, and the system automatically changes to show
units of Flight Level. Turn the large FMS Knob clockwise to highlight the first
zero and enter the three digit flight level.
4)
Press the ENT Key to accept the altitude constraint; if the selected waypoint is
an airport, an additional choice is displayed. Turn the small FMS Knob to choose
‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude.
Deleting an altitude constraint provided by the navigation
database:
1)
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove VNV altitude?’ confirmation window is displayed.
4)
Select ‘OK’ and press the ENT Key.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Altitude constraints can be modified or deleted after having been added to the flight
plan. In the event an altitude constraint is deleted and the navigation database contains an
altitude restriction for the lateral waypoint, the system displays the altitude restriction
from the database provided no predicted altitude can be provided. The system also
provides a way to reinstate a published altitude constraint that has been edited.
70
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
Deleting an altitude constraint that has been manually
entered:
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’
confirmation window is displayed.
4)
Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is
deleted (it is replaced by a system calculated altitude, if available).
EIS
1)
Flight
Management
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’
confirmation window is displayed.
4)
Select ‘REVERT’ and press the ENT Key. The altitude is changed to the
navigation database value.
5)
Press the FMS Knob to remove the flashing cursor.
AFCS
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
3)
Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’
confirmation window is displayed.
4)
Select ‘EDIT’ and press the ENT Key.
5)
Edit the value using the FMS Knobs, and press the ENT Key.
6)
Press the FMS Knob to remove the flashing cursor.
Annunciations
& Alerts
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
Abnormal
Operation
2)
Additional
Features
Modifying a system calculated altitude constraint:
Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Appendix
Enabling the Vertical Situation Display:
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Inset Softkey.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
Hazard
Avoidance
1)
1)
Audio Panel
and CNS
Reverting a manually entered altitude constraint back to
the navigation database value:
71
Flight
Instruments
Flight Management
4)
Press the VSD Softkey to enable the Vertical Situation Display.
5)
Press the VSD Mode Softkey to choose between Auto, FPL, or TRK.
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Show VSD’ and press the ENT Key.
4)
Press the Map Opt Softkey.
5)
Press the Inset Softkey.
6)
Press the VSD Mode Softkey to choose between Auto, FPL, or TRK.
Disabling the Vertical Situation Display:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Or:
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Inset Softkey
4)
Press the Off Softkey.
Additional
Features
AFCS
Or:
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Hide VSD’ and press the ENT Key.
Viewing available procedures at an airport:
1)
From the ‘WPT - Airport Information’ Page:
Press the DP Softkey. The ‘WPT - Departure Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Annunciations
& Alerts
Abnormal
Operation
PROCEDURES
Or:
Appendix
Press the STAR Softkey. The ‘WPT - Arrival Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Or:
Index
Press the APR Softkey. The ‘WPT - Approach Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
2)
72
To select another airport, press the FMS Knob to activate the cursor, enter an
identifier/facility name/city, and press the ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
5)
Turn the small FMS Knob to view the available runway or transition. Press the
ENT Key to select the runway or transition. The cursor moves to the next box (if
available). The procedure is previewed on the map.
6)
Turn the small FMS Knob to view the available runway or transition. Press the
ENT Key to select the runway or transition. The cursor moves to the ‘Sequence’
Box or the ‘Minimums’ Box. The procedure is previewed on the map.
7)
Press the Info 1 Softkey or the Info 2 Softkey to return to the ‘WPT - Airport
Information’ Page.
Flight
Management
Turn the small FMS Knob to view the available procedures. Press the ENT Key to
select the procedure. The cursor moves to the next box (runway or transition).
The procedure is previewed on the map.
Hazard
Avoidance
Loading a procedure into the active flight plan from the
[Procedure] Information Page:
1)
Audio Panel
and CNS
4)
EIS
Turn the large FMS Knob to highlight the procedure. The procedure is
previewed on the map.
Flight
Instruments
3)
From the ‘WPT - Airport Information’ Page:
Press the DP Softkey. The ‘WPT - Departure Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
AFCS
Or:
Additional
Features
Press the STAR Softkey. The ‘WPT - Arrival Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Or:
Press the APR Softkey. The ‘WPT - Approach Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
3)
Select a different procedure, if desired.
Turn the large FMS Knob to highlight the procedure. The procedure is
previewed on the map.
b)
Turn the small FMS Knob to view the available procedures. Press the ENT
Key to select the procedure. The cursor moves to the next box (runway or
transition). The procedure is previewed on the map.
Appendix
a)
Annunciations
& Alerts
To select another airport, press the FMS Knob to activate the cursor, enter an
identifier/facility name/city, and press the ENT Key.
Abnormal
Operation
2)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
73
c)
Turn the small FMS Knob to view the available runway or transition. Press
the ENT Key to select the runway or transition. The cursor moves to the
next box (if available). The procedure is previewed on the map.
d)
Turn the small FMS Knob to view the available transitions. Press the ENT
Key to select the transition. The cursor moves to the ‘Sequence’ Box or the
‘Minimums’ Box. The procedure is previewed on the map.
Press the MENU Key to display the [Procedure] Information Page Menu.
5)
Turn the FMS Knob to highlight ‘Load [procedure]’.
6)
Press the ENT Key to load the procedure into the active flight plan.
AFCS
1)
Press the PROC Key. The ‘Procedures’ Window is displayed.
2)
Highlight ‘Select Departure’.
3)
Press the ENT Key. The Departure Loading Page/Window is displayed.
4)
Use the FMS Knob to select an airport, if necessary, and press the ENT Key.
5)
Select a departure from the list and press the ENT Key.
6)
Select a runway (if required) and press the ENT Key.
7)
Select a transition (if required) and press the ENT Key. ‘Load?’ is highlighted.
8)
Press the ENT Key to load the departure procedure.
Removing a departure procedure from the active flight
plan:
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
4)
Loading a departure into the active flight plan using the
PROC Key:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, and highlight ‘Remove Departure’.
3)
Press the ENT Key. A confirmation window is displayed listing the departure
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request,
highlight ‘CANCEL’ and press the ENT Key.
Index
Or:
74
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob, and turn to highlight the departure header in the active
flight plan.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request,
highlight ‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
EIS
Press the CLR Key. A confirmation window is displayed listing the departure
procedure.
Flight
Instruments
3)
2)
Highlight ‘Select Arrival’.
3)
Press the ENT Key. The Arrival Loading Page/Window is displayed.
4)
Use the FMS Knob to select an airport, if necessary, and press the ENT Key.
5)
Select an arrival from the list and press the ENT Key.
6)
Select a transition (if required) and press the ENT Key.
7)
Select a runway (if required) and press the ENT Key. ‘Load?’ is highlighted.
8)
Press the ENT Key to load the arrival procedure.
Hazard
Avoidance
Press the PROC Key. The ‘Procedures’ Window is displayed.
Flight
Management
1)
Audio Panel
and CNS
Loading an arrival into the active flight plan using the
PROC Key:
2)
Press the MENU Key, and highlight ‘Remove Arrival’.
3)
Press the ENT Key. A confirmation window is displayed listing the arrival
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request,
highlight ‘CANCEL’ and press the ENT Key.
Abnormal
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Additional
Features
1)
AFCS
Removing an arrival from the active flight plan:
Or:
2)
Press the FMS Knob, and turn to highlight the arrival header in the active flight
plan.
3)
Press the CLR Key. A confirmation window is displayed listing the arrival
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request,
highlight ‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
190–02362–00 Rev. A
Appendix
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Annunciations
& Alerts
1)
75
Loading an approach into the active flight plan using the
PROC Key:
1)
Press the PROC Key. The ‘Procedures’ Window is displayed.
2)
Highlight ‘Select Approach’, and press the ENT Key. The Approach Loading
Page/Window is displayed.
3)
Select the airport and approach:
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
a)
Use the FMS Knob to select an airport, if necessary, and press the ENT Key.
b)
Select an approach from the list and press the ENT Key.
a)
If necessary, push the FMS Knob to exit the approach list, and use the large
FMS Knob to move the cursor to the Approach Channel Field.
b)
Use the FMS Knob to enter the approach channel number, and press the
ENT Key to accept the approach channel number. The airport and
approach are selected.
4)
Select a transition (if required) and press the ENT Key.
5)
Minimums
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Or:
a)
To set ‘Minimums’, turn the small FMS Knob to select ‘BARO’ or ‘TEMP
COMP’, and press the ENT Key. Turn the small FMS Knob to select the
altitude, and press the ENT Key.
b)
If ‘TEMP COMP’ was selected, the cursor moves to the ‘TEMP At’ [airport]
Field. Turn the small FMS Knob to select the temperature, and press the
ENT Key
Abnormal
Operation
Or:
To skip setting minimums, press the ENT Key.
Annunciations
& Alerts
6)
Press the ENT Key with ‘Load?’ highlighted to load the approach procedure; or
turn the large FMS Knob to highlight ‘Activate’ and press the ENT Key to load
and activate the approach procedure.
Index
Appendix
NOTE: When GPS is not approved for the selected final approach course, the
message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the
approach, but the HSI must to be switched to a NAV receiver to fly the final
course of the approach.
76
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Flight
Instruments
NOTE: If there is no arrival procedure in the active flight plan, loading an
approach after a destination airport has already been entered will result in a
duplicate destination airport waypoint being added to the end of the enroute
segment.
EIS
Loading an approach into the active flight plan from the
Nearest Airport Page:
3)
Press the APR Softkey; or press the MENU Key, highlight ‘Select Approach
Window’, and press the ENT Key.
4)
Turn the FMS Knob to highlight the desired approach.
5)
Press the LD APR Softkey; or press the MENU Key, highlight ‘Load Approach’,
and press the ENT Key. The ‘PROC - Approach Loading’ Page is displayed with
the ‘Transition’ Field highlighted.
6)
Turn the FMS Knob to highlight the desired transition, and press the ENT Key.
7)
Minimums
AFCS
Press the FMS Knob, then turn the large FMS Knob to highlight the desired
nearest airport. The airport is previewed on the map.
Hazard
Avoidance
2)
Flight
Management
Select the ‘NRST - Nearest Airports’ Page.
Audio Panel
and CNS
1)
b)
If ‘TEMP COMP’ was selected, the cursor moves to the ‘TEMP At’ [airport]
Field. Turn the small FMS Knob to select the temperature, and press the
ENT Key.
Abnormal
Operation
To set ‘Minimums’, turn the small FMS Knob to select ‘BARO’ or ‘TEMP
COMP’, and press the ENT Key. Turn the small FMS Knob to select the
altitude, and press the ENT Key.
Additional
Features
a)
Or:
To skip setting minimums, press the ENT Key. ‘Load?’ is highlighted.
Appendix
Press the ENT Key with ‘Load?’ highlighted to load the approach procedure; or
turn the large FMS Knob to highlight ‘Activate’ and press the ENT Key to load
and activate the approach procedure. The system continues navigating the
current flight plan until the approach is activated. When GPS is not approved for
the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is
displayed. GPS provides guidance to the approach, but the HSI must to be
switched to a NAV receiver to fly the final course of the approach.
Annunciations
& Alerts
8)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
77
Removing an approach from the active flight plan:
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, and highlight ‘Remove Approach’.
3)
Press the ENT Key. A confirmation window is displayed listing the approach
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight
‘CANCEL’ and press the ENT Key.
AFCS
Hazard
Avoidance
Flight
Management
Or:
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob, and turn to highlight the approach header in the active
flight plan.
3)
Press the CLR Key. A confirmation window is displayed listing the approach
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight
‘CANCEL’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
1)
Press the PROC Key. The ‘Procedures’ Window is displayed with ‘Activate
Approach’ highlighted.
2)
Press the ENT Key to activate the approach.
Activating a previously loaded approach with vectors to
final:
1)
Press the PROC Key to display the ‘Procedures‘ Window.
2)
Highlight ‘Activate Vector-to-Final’ and press the ENT Key.
Loading and activating an approach using the MENU Key:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Activating a previously loaded approach:
78
1)
From the ‘PROC - Approach Loading’ Page, press the MENU Key on the MFD.
The page menu is displayed with ‘Load & Activate Approach’ highlighted.
2)
Press the ENT Key. When GPS is not approved for the selected final approach
course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides
guidance to the approach, but the HSI must to be switched to a NAV receiver to
fly the final course of the approach.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Press the PROC Key.
2)
Turn the FMS Knob to highlight ‘Activate Missed Approach’.
3)
Press the ENT Key. The aircraft automatically sequences to the MAHP.
EIS
1)
Flight
Instruments
Activating a missed approach in the active flight plan:
Or:
Fly past the MAP, and press the SUSP Softkey on the PFD.
Audio Panel
and CNS
Or:
Press the Go-Around Button.
From the ‘FPL - Active Flight Plan’ Page, press the MENU Key on the MFD. The
‘Page Menu’ Window is displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The ‘Temperature Compensation’ Window is displayed.
4)
Use the small FMS Knob to select the ‘TEMP At’ [airport] Field. The
compensated altitude is computed as the temperature is selected.
Hazard
Avoidance
1)
Press the ENT Key. The compensated altitudes for the approach are shown in
the flight plan.
Abnormal
Operation
6)
Annunciations
& Alerts
Cancelling temperature compensated altitude:
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The Temperature Compensation Window is displayed.
4)
Press the ENT Key. ‘Cancel Compensation?’ is highlighted.
5)
Press the ENT Key. The temperature compensated altitude at the FAF is
cancelled.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
From the Active Flight Plan Page, press the MENU Key. The ‘Page Menu’
Window is displayed.
Appendix
1)
Additional
Features
Press the ENT Key. ‘Activate Compensation?’ is highlighted.
AFCS
NOTE: The temperature at the destination can be entered in the Temperature
Compensation Window on the MFD, or in the References Window on the PFD.
There is only one compensation temperature for the system, therefore, changing
the temperature will affect both the loaded approach altitudes and the
minimums. Refer to the Flight Instruments section for information about
applying temperature compensation to the MDA/DH.
5)
Flight
Management
Manually activating temperature compensated altitude:
79
Flight
Instruments
Flight Management
EIS
NOTE: Activating/cancelling temperature compensation for the loaded approach
altitudes does not select/deselect temperature compensated minimums (MDA/
DH), nor does selecting/deselecting temperature compensated minimums
activate/cancel temperature compensated approach altitudes.
Entering basic empty weight:
Abnormal
Operation
Additional
Features
From the ‘Aux - Weight Planning’ Page, press the Config Softkey; or press the
MENU Key, highlight ‘Set Basic Empty Weight’, and press the ENT Key to select
the ‘Basic Empty Weight’ Field.
2)
Turn the small FMS Knob to enter the basic empty weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
1)
From the ‘Aux - Weight Planning’ Page, press the FMS Knob to activate the
cursor and highlight the ‘Pilot & Stores’ Field.
2)
Turn the small FMS Knob to enter the pilot and stores weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Entering the number of passengers:
1)
From the ‘Aux - Weight Planning’ Page, press the FMS Knob to activate the
cursor and highlight the ‘Passengers #’ Field.
2)
Turn the small FMS Knob to enter the number of passengers.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Entering the average passenger weight:
Index
Appendix
Annunciations
& Alerts
1)
Entering pilot and stores weight:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
WEIGHT PLANNING
80
1)
From the ‘Aux - Weight Planning’ Page, press the FMS Knob to activate the
cursor and highlight the passenger weight (‘at’) field.
2)
Turn the small FMS Knob to enter the average passenger weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
From the ‘Aux - Weight Planning’ Page, press the FMS Knob to activate the
cursor and highlight the ‘Cargo’ Field.
2)
Turn the small FMS Knob to enter the cargo weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
EIS
1)
Flight
Instruments
Entering the cargo weight:
Press the FMS Knob to activate the cursor and highlight the ‘Fuel Reserves’
Field.
2)
Turn the small FMS Knob to enter the fuel reserves amount.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Flight
Management
1)
Audio Panel
and CNS
Entering fuel reserves weight:
AFCS
Press the FOB Sync Softkey on the ‘Aux - Weight and Balance’ Page; or press
the MENU and highlight ‘Synchronize Fuel on Board’, and press the ENT Key.
The actual measured fuel on board is displayed in the ‘Fuel On Board’ Field.
Hazard
Avoidance
Synchronizing the fuel on board with the actual measured
fuel on board:
Additional
Features
TRIP PLANNING
Selecting automatic or manual page mode:
From the ‘Aux - Trip Planning’ Page, press the FPL Softkey or the WPTs Softkey;
or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints Mode’, and
press the ENT Key.
Annunciations
& Alerts
Selecting flight plan or waypoint mode:
Abnormal
Operation
From the ‘Aux - Trip Planning’ Page, press the Auto Softkey or the Manual
Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and
press the ENT Key.
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
81
Selecting a flight plan and leg for trip statistics:
1)
From the ‘Aux - Trip Planning’ Page, press the FMS Knob to activate the cursor
in the ‘FPL’ Field.
2)
Turn the small FMS Knob to select the desired flight plan number.
3)
Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each
leg can be viewed by turning the small FMS Knob to select the desired leg. The
Trip Planning Map also displays the selected data.
Selecting waypoints for waypoint mode:
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Flight Management
1)
From the ‘Aux - Trip Planning’ Page, press the WPTs Softkey; or press the
MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The cursor is
positioned in the waypoint field directly below the FPL Field.
2)
Turn the FMS Knobs to select the desired waypoint (or select from the Page
Menu ‘Set WPT to Present Position’ if that is what is desired), and press the ENT
Key. The cursor moves to the second waypoint field.
3)
Turn the FMS Knobs to select the desired waypoint, and press the ENT Key. The
statistics for the selected leg are displayed.
1)
From the ‘Aux - Trip Planning’ Page, press the Manual Softkey or select
‘Manual Mode’ from the Page Menu, and press the ENT Key. The cursor may
now be positioned in any field in the top right two boxes.
2)
Turn the FMS Knobs to move the cursor onto the ‘Departure Time’ Field and
enter the desired value. Press the ENT Key. The statistics are calculated using the
new value and the cursor moves to the next entry field. Repeat until all desired
values have been entered.
RAIM PREDICTION
Predicting RAIM availability at a selected waypoint:
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Entering manual data for trip statistics calculations:
1)
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the RAIM Softkey.
3)
Press the FMS Knob. The ‘Waypoint’ Field is highlighted.
4)
Turn the small FMS Knob to display the ‘Waypoint Information’ Window.
5)
Enter the desired waypoint:
Index
Use the FMS Knob to enter the desired waypoint by identifier, facility, or city
name and press the ENT Key.
Or:
82
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Flight Management
Turn the small FMS Knob clockwise to display the Flight Plan, Nearest,
Recent, or User waypoints, if required.
c)
Turn the large FMS Knob clockwise to select the desired waypoint. The
system automatically fills in the identifier, facility, and city fields with the
information for the selected waypoint.
d)
Press the ENT Key to accept the waypoint entry.
Audio Panel
and CNS
b)
EIS
Turn the small FMS Knob counter-clockwise to display a list of flight plan
waypoints (the FPL list is populated only when navigating a flight plan).
Flight
Instruments
a)
Use the FMS Knob to enter an arrival time and press the ENT Key.
7)
Use the FMS Knob to enter an arrival date and press the ENT Key.
8)
With the cursor highlighting ‘Compute RAIM?’, press the ENT Key. Once RAIM
availability is computed, one of the following is displayed:
• ‘Compute RAIM?’—RAIM has not been computed for the current waypoint, time,
Flight
Management
6)
and date combination
• ‘RAIM Available’—RAIM is predicted to be available for the specified waypoint,
Hazard
Avoidance
• ‘Computing Availability’—RAIM calculation in progress
time, and date
waypoint, time, and date
AFCS
• ‘RAIM Not Available’—RAIM is predicted to be unavailable for the specified
Predicting RAIM availability at present position:
Additional
Features
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the RAIM Softkey.
3)
Press the FMS Knob. The ‘Waypoint’ Field is highlighted.
4)
Press the MENU Key.
5)
With ‘Set WPT to Present Position’ highlighted, press the ENT Key.
6)
Press the ENT Key to accept the waypoint entry.
7)
Use the FMS Knob to enter an arrival time and press the ENT Key.
8)
Use the FMS Knob to enter an arrival date and press the ENT Key.
9)
With the cursor highlighting ‘Compute RAIM?’, press the ENT Key. Once RAIM
availability is computed, one of the following is displayed:
Abnormal
Operation
1)
Annunciations
& Alerts
Appendix
• ‘Compute RAIM?’—RAIM has not been computed for the current waypoint, time,
and date combination
Index
• ‘Computing Availability’—RAIM calculation in progress
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
83
Flight Management
Flight
Instruments
• ‘RAIM Available’—RAIM is predicted to be available for the specified waypoint,
time, and date
• ‘RAIM Not Available’ is predicted to be unavailable for the specified waypoint,
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the SBAS Softkey.
3)
Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’,
‘MSAS’ or ‘WAAS’.
4)
Press the ENT Key to uncheck the box.
5)
Press the FMS Knob to remove the cursor.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
1)
Audio Panel
and CNS
Disabling SBAS:
Flight
Management
EIS
time, and date
84
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
DATA LINK WEATHER
2)
Press the Layout Softkey.
3)
Press the WX LGND to show/remove the weather product age information for
PFD maps.
4)
Press the Back Softkey twice to return to the top-level softkeys.
Symbol
Broadcast
Rate
(Minutes)
NEXRAD
30
5 (U.S.)
10 (Canada)
Cloud Top (CLD TOP)
60
15 (69/69A)
Additional
Features
Expiration
Time
(Minutes)
AFCS
SiriusXM Weather Product
30
5
Cell Movement
30
1.25
SIGMETs/AIRMETs
60
12
METARs
90
12
City Forecast
90
12
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
SiriusXM Lightning (LTNG)
Appendix
7.5
Annunciations
& Alerts
30
Abnormal
Operation
30 (69/69A
SXM)
Echo Top (ECHO TOP)
Hazard
Avoidance
The following tables show the weather product symbols, the expiration times and the
broadcast rates for SiriusXM Weather and FIS-B Weather, respectively. The broadcast rate
represents the interval at which the SiriusXM Weather service transmits new signals that
may or may not contain updated weather product information. It does not represent the
rate at which the weather information is updated or when the Data Link Receiver receives
new data. The service provider and its weather data suppliers define and control the data
update intervals, which are subject to change.
Flight
Management
Press the Map/HSI Softkey.
Audio Panel
and CNS
1)
EIS
Enabling/disabling the weather product age for PFD Maps:
85
Hazard Avoidance
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
SiriusXM Weather Product
Symbol
Expiration
Time
(Minutes)
Broadcast
Rate
(Minutes)
Surface Analysis
60
12
Freezing Levels
120
12
Winds Aloft
90
12
County Warnings
60
5
Cyclone Warnings
60
12
Icing Potential (CIP and SLD)
90
22
Pilot Weather Report (PIREP)
90
12
Air Report(AIREP)
90
12
Turbulence
180
12
Radar Coverage Not Available
No product
image
30
5
Temporary Flight Restriction
(TFR)
No product
image
60
12
Terminal Aerodrome Forecast
(TAF)
No product
image
60
12
Annunciations
& Alerts
Table 2 SiriusXM Weather Product Symbols and Data Timing
Index
Appendix
FIS-B Weather Product
86
Symbol
Expiration
Time
(Minutes)
Broadcast Rate
(Minutes)
NEXRAD Composite (US)
30
15
NEXRAD Composite
(Regional)
30
2.5
METARs
90
5
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Symbol
Broadcast Rate
(Minutes)
Pilot Weather Report (PIREP)
90
10
Winds Aloft
90
10
SIGMETs/AIRMETs
60
5
30
2.5
Terminal Aerodrome Forecast
(TAF)
no product
image
60
10
Temporary Flight Restriction
(TFR
no product
image
Flight
Management
no product
image
Audio Panel
and CNS
No Radar Coverage
EIS
Expiration
Time
(Minutes)
10
Hazard
Avoidance
Table 3 FIS-B Weather Product Symbols and Data Timing
Refresh Rate
(Minutes)
Abnormal
Operation
Expiration
Time
(Minutes)
U.S.: 3*
30
Canada: 3*†
Annunciations
& Alerts
Radar
Precipitation
Europe: 15
Australia: 15^
30
Datalink
Lightning
30
Continuous
SIGMETs/
AIRMETs
60
Continuous
METARs
90
Continuous
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
60
Appendix
Infrared Satellite
Additional
Features
Symbol
AFCS
The following table shows the Garmin Connext Weather product symbols, the
expiration times and the refresh rates. The refresh rate represents the interval at which
Garmin Connext weather service makes available the most current known weather data. It
does not necessarily represent the rate at which the service receives new data from various
weather sources. The pilot chooses how often to contact the Garmin Connext weather
service in order to retrieve weather data through the Connext Data Request.
Garmin
Connext
Weather
Product
Flight
Instruments
FIS-B Weather Product
87
Hazard Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Garmin
Connext
Weather
Product
Winds Aloft
90
Continuous
Pilot Weather
Report (PIREPs)
90
Continuous
Temporary Flight
Restrictions
(TFRs)
no product
image
60
Continuous
Terminal
Aerodrome
Reports TAFs)
no product
image
60
Continuous
Hazard
Avoidance
AFCS
Table 4 Garmin Connext Weather Product Symbols and Data Timing
Viewing the Weather Data Link Page and changing the
data link weather source, if applicable:
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link (XM or CNXT) Page.
The currently selected data link weather source appears in the page title.
3)
If the page title does not contain the desired weather source, press the MENU
Key.
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Refresh Rate
(Minutes)
* The composite precipitation image is updated every 3 minutes, but
individual radar sites may take between 3 and 10 minutes to provide new
data.
† Canadian radar precipitation data provided by Environment Canada.
^ Australian radar precipitation data provided by the Australian Bureau of
Meteorology.
a)
Turn the FMS Knob to highlight ‘Display XM Weather’, or ‘Display Connext
Weather’ (choices may vary depending on the installed equipment).
b)
Press the ENT Key.
Viewing legends for displayed weather products on the
Weather Data Link Page:
Index
Appendix
Expiration
Time
(Minutes)
Symbol
88
1)
Select the Weather Data Link Page.
2)
Press the Legend Softkey to display the legends for the displayed weather
products.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
a)
Press the MENU Key.
b)
Select ‘Weather Legend’ and press the ENT Key.
Flight
Instruments
Or:
4)
To remove the Weather Legends Window, press the Legend Softkey, the ENT
or the CLR Key, or press the FMS Knob.
Audio Panel
and CNS
Turn the FMS Knob to scroll through the legends if more are available than fit in
the window.
Setting up and customizing the Weather Data Link Page:
Select the Weather Data Link Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Weather Setup’, then press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’, and
press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/OFF,
range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Weather Data Link (XM) Page
with the changed settings.
Flight
Management
1)
AFCS
Additional
Features
Abnormal
Operation
Select the Weather Data Link Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Weather Setup’.
4)
Turn the small FMS Knob to display the Group options.
5)
If SiriusXM is the selected data link weather source, turn the small FMS Knob to
highlight the ‘Map’ Group and press the ENT Key.
Annunciations
& Alerts
1)
Appendix
Or:
Index
If FIS-B or Garmin Connext is the selected data link weather source, turn the
large FMS Knob to highlight the ‘Orientation ‘ field at the bottom of the
Product Group 1 list.
Turn the small FMS Knob to highlight the desired map orientation: North up,
Track up, HDG up, or SYNC, then press the ENT Key.
190–02362–00 Rev. A
Hazard
Avoidance
Selecting a map orientation for the Weather Data Link
Page:
6)
EIS
3)
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
89
Restoring default Weather Data Link Page settings:
Select the Weather Data Link Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Weather Setup’, then press the ENT Key.
4)
Press the MENUKey.
5)
Highlight the desired default(s) to restore (all or for selection) and press ENT
Key.
6)
When finished, press the FMS Knob or press the CLR Key.
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the softkey to enable/disable the desired weather product.
Showing/removing the weather legend on the Navigation
Map Page:
Additional
Features
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Legend Softkey to show the weather legends window.
4)
When finished, press the Legend Softkey again, or press the FMS Knob or the
CLR Key to remove the window.
Setting up and customizing weather data for the
navigation maps:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
1)
Displaying Data Link Weather Products on the Navigation
Map Page:
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
90
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (On/Off,
range settings).
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with the
changed settings.
Flight
Instruments
7)
Displaying Data Link Weather products on the PFD:
2)
Press the desired weather product softkey(s) to enable/disable the display of
data link products on the PFD map.
Audio Panel
and CNS
On the PFD, press the Map/HSI Softkey.
EIS
1)
Enabling/disabling the weather product icon and age
display (PFD maps):
Flight
Management
On the PFD, press the Map/HSI Softkey.
2)
Press the Layout Softkey.
3)
Press the WX LGND Softkey to enable/disable the weather product age, source,
and icon box display on PFD Maps.
Manually Requesting Garmin Connext Weather
information:
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
urn the large FMS Knob to highlight the desired coverage option(s) and press
the ENT Key to show or hide a green check mark to select one of more of the
following coverage selections:
Additional
Features
Select the ‘Map - Weather Data Link (CNXT)’ Page.
AFCS
1)
Hazard
Avoidance
1)
• Destination – Requests data based on the active flight plan destination (Direct-To
• FPL – Requests data along an active flight plan, if one currently exists. Turn the
• Waypoint – Requests data based on a waypoint (which may be off-route). Turn the
Appendix
small FMS Knob to select the desired flight plan look-ahead distance option (or
choose ‘Remaining FPL’ to request weather data for the remainder of the flight
plan), then press the ENT Key.
Annunciations
& Alerts
destinations excluded). See the Flight Management section for more information
about entering and activating flight plans.
Abnormal
Operation
• Present Position – Requests data based on current location.
large and small FMS Knobs to enter a waypoint, then press the ENT Key.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
91
5)
Turn the large FMS Knob highlight to the ‘Diameter / Route Width’ distance
field and turn the small FMS Knob to select the desired diameter and route
width of the request, then press the ENT Key.
6)
Turn the large FMS Knob until the ‘Send Request’ field is highlighted. Press the
ENT Key to initiate the request immediately or press the FMS Knob to return to
the Weather Data Link (CNXT) Page without requesting weather data.
EIS
Flight
Instruments
Hazard Avoidance
1)
Select the ‘Map - Weather Data Link (CNXT)’ Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Turn the large FMS Knob to select the ‘Cancel Request’ field and press the ENT
Key. The request status box indicates ‘Request Cancelled’.
5)
Press the FMS Knob to return to the Weather Data Link (CNXT) Page.
Enabling/disabling automatic Connext Data Requests:
1)
Select the ‘Map - Weather Data Link (CNXT)’ Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Choose the desired weather coverage options.
5)
Turn the large FMS Knob to select the ‘Update Rate’ field. Then turn the small
FMS Knob to highlight the desired automatic update frequency (Off, 5 Min, 10
Min, 15 Min, 20 Min, 30 Min, 45 Min, or 60 Min), then press the ENT Key
6)
The ‘Send Request’ field is highlighted and a countdown timer is displayed in
the ‘Request Status’ Window based on the currently selected update rate. Press
the ENT Key to immediately send an immediate Connext Data Request.
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Cancelling a Connext Data Request in Progress:
Press the FMS Knob to return to the Weather Data Link (CNXT) Page.
Enabling/disabling NEXRAD weather information on the
Weather Data Link (XM) Page:
1)
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Press the NEXRAD Softkey.
Index
Appendix
Annunciations
& Alerts
Or:
92
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
1)
Press the Map Opt Softkey.
2)
Press the NEXRAD Softkey.
Flight
Instruments
Enabling/disabling NEXRAD weather information on MFD
navigation maps:
EIS
Enabling/disabling NEXRAD weather information on PFD
maps:
Press the Map/HSI Softkey.
2)
Press the NEXRAD Softkey.
Audio Panel
and CNS
1)
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Press the MENU Key.
3)
Turn the large FMS Knob to highlight ‘Weather Setup’ and press the ENT Key.
4)
Turn the large FMS Knob to highlight the NEXRAD Region datafield.
5)
Turn the small FMS Knob to highlight ‘US’ or ‘CNDA’ (Canada) and press the
ENT Key.
Hazard
Avoidance
1)
Flight
Management
Changing the NEXRAD coverage region:
AFCS
Displaying the NEXRAD weather product on the Weather
Data Link (FIS-B) Page:
2)
Press the NXRD Softkey. Each selection cycles though a coverage option as the
softkey name changes (Each selection cycles though a coverage option
displayed in cyan on the softkey (‘Off’, ‘US’, or ‘REG’, or ‘All’)..
Or:
Press the MENU Key.
2)
Turn the FMS Knob to highlight ‘Weather Setup’ and press the ENT Key.
3)
To enable/disable the display of NEXRAD informations, turn the small FMS Knob
to highlight the NEXRAD On/Off field.
Turn the small FMS Knob to highlight ‘On’ to enable the display of
NEXRAD or ‘Off’ to disable.
b)
Press the ENT Key.
Appendix
4)
a)
Annunciations
& Alerts
1)
Abnormal
Operation
Select the ‘Map - Weather Data Link (FIS-B)’ Page.
Additional
Features
1)
Turn the large FMS Knob to highlight the ‘Region’ field..
Turn the small FMS Knob to select one of the following options: ‘CONUS’
for the continental United States, ‘Regional’ for regional NEXRAD, or
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
93
Index
a)
Hazard Avoidance
Flight
Instruments
‘Combined’ to show regional NEXRAD where data is available, and
continental NEXRAD outside of the regional coverage area.
b)
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
1)
Select the Map Opt Softkey.
2)
Select the NEXRAD Softkey.
3)
To change the type of NEXRAD displayed, press the MENU Key.
4)
With ‘Map Settings’ highlighted, press the ENT Key.
5)
Turn the small FMS Knob to select the ‘Weather’ Group, then press the ENT
Key.
6)
Turn the large FMS Knob to highlight the NEXRAD Data Region field.
7)
Turn the small FMS Knob to highlight ‘CONUS’ (continental United States),
‘RGNL’ (regional), or ‘Combined’, then press the ENT Key. This selection also
affects display of NEXRAD on the PFD Maps.
8)
When finished, press the FMS Knob or press the CLR Key.
Displaying the FIS-B NEXRAD weather product on PFD
maps:
1)
Press the Map/HSI Softkey.
2)
Press the NEXRAD Softkey to enable/disable the display of NEXRAD
information.
Displaying Precipitation weather information:
Annunciations
& Alerts
Abnormal
Operation
When finished, push the FMS Knob.
Displaying the FIS-B NEXRAD weather product on the
Navigation Map Page:
Audio Panel
and CNS
EIS
5)
Press the ENT Key.
1)
Select the Map Opt Softkey (for PFD maps, press the Map/HSI or Map Opt
Softkey). This step is not necessary on the Weather Data Link (CNXT) Page.
2)
Select the PRECIP Softkey.
Appendix
Displaying Echo Tops information:
1)
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Press the Echo Top Softkey.
Index
Displaying Cloud Tops information:
94
1)
Select the ‘Map - Weather Data Link (XM)’ Page with the FMS Knob.
2)
Select the CLD Top Softkey.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Turn the FMS Knob to select the ‘Map - Weather Data Link (XM or CNXT)’
Page.
2)
Press the XM LTNG or DL LTNG Softkey.
EIS
1)
Flight
Instruments
Displaying Data Link Lightning information on Weather
Data Link Page:
Turn the FMS Knob to select the Navigation Map Page.
2)
Select the Map Opt Softkey.
3)
Select the XM LTNG or DL LTNG Softkey.
Flight
Management
1)
Audio Panel
and CNS
Displaying Data Link Lightning information on the
Navigation Map Page:
Displaying Cell Movement information on the Weather
Data Link (XM) Page:
Select the ‘Map - Weather Data Link (XM)’ Page using the FMS Knob.
2)
Select the Cell MOV Softkey.
Hazard
Avoidance
1)
AFCS
Setting up the system to display Cell Movement with
NEXRAD on navigation maps:
Use the FMS Knob to select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’ and press the ENT Key.
5)
Turn the large FMS Knob to ‘On’ or ‘Off’ for the Cell Movement menu option.
When set to ‘On’, Cell Movement is enabled/disabled with the NEXRAD
weather product on navigation maps. When set to ‘Off’, Cell Movement is not
displayed on navigation maps.
6)
When finished, push the FMS Knob or CLR Key to remove the menu.
Additional
Features
1)
2)
Press the IR SAT Softkey.
Appendix
Select the ‘Map — Weather Data Link (CNXT)’ Page.
Annunciations
& Alerts
1)
Abnormal
Operation
Displaying Infrared Satellite Information:
Displaying SIGMETs and AIRMETs:
Select the ‘Map- Weather Data Link (XM or CNXT or FIS-B)’ Page.
2)
Press the SIG/AIR Softkey.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
95
Flight
Instruments
Hazard Avoidance
3)
To view the text of the SIGMET or AIRMET, press the Joystick and move the
Map Pointer over the icon.
4)
Press the ENT key. The following figure shows sample SIGMET text.
Flight
Management
Audio Panel
and CNS
EIS
Displaying METAR and TAF text on the MFD:
1)
On the ‘Map - Weather Data Link (XM or FIS-B or CNXT)’ Page, press the
METAR Softkey.
2)
Press the Joystick and pan to the desired airport.
3)
Press the ENT Key. The Weather Information Page is shown with METAR and
TAF text.
4)
Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text.
METAR text must be completely scrolled through before scrolling through the
TAF text.
5)
Press the FMS Knob or the CLR Key to return to the Weather Data Link Page.
Hazard
Avoidance
Or:
Select the Weather Information Page.
a)
Turn the large FMS Knob to select the Waypoint Page Group.
b)
Select the WX Softkey to select the Weather Information Page.
2)
Press the FMS Knob to display the cursor.
3)
Use the FMS Knob to enter the desired airport and press the ENT Key.
4)
Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text.
Note that the METAR text must be completely scrolled through before scrolling
through the TAF text.
Displaying original METAR text on the Active Flight Plan
Page:
1)
Select the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight a waypoint with an available METAR
(indicated with a METAR flag next to it). The METAR text will appear in the
‘Selected Waypoint Weather’ Window below.
4)
When finished, press the FMS Knob to remove the cursor or press the FPL Key
to exit the Active Flight Plan Page.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
1)
96
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
2)
Press the METAR Softkey.
3)
Press the Joystick and pan to the desired METAR flag. Original METAR text
appears on the map.
4)
When finished, press the Joystick to remove the Map Pointer.
Displaying Surface Analysis and City Forecast information:
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Select the More WX Softkey.
3)
Select the SFC Softkey.
4)
Press the softkey for the desired forecast time: Current, 12 HR, 24 HR, 36 HR,
or 48 HR. The SFC Softkey label changes to show the forecast time selected.
Flight
Management
1)
Audio Panel
and CNS
On the PFD, press the Map/HSI Softkey.
EIS
1)
Flight
Instruments
Displaying original METAR text information on the PFD
Inset Map:
Hazard
Avoidance
Or:
Press the Off Softkey to disable the display of the weather product.
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Press the More WX Softkey.
3)
Press the FRZ LVL Softkey.
Additional
Features
1)
AFCS
Displaying Freezing Level information:
Displaying the Winds Aloft weather product:
2)
Select the More WX Softkey.
3)
Select the Wind Softkey.
4)
Select a softkey for the desired altitude level: SFC (surface) up to 42,000 feet.
Select the Next or Prev Softkey to cycle through the altitude softkeys. The
Wind Softkey label changes to reflect the altitude selected.
Annunciations
& Alerts
Select the ‘Map - Weather Data Link (XM)’ Page.
Abnormal
Operation
1)
Appendix
Index
Figure 15 Winds Aloft Data with Legend
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
97
Enabling/disabling the Vertical Situation Display
(containing winds aloft data):
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Inset Softkey.
4)
Press the VSD Softkey to enable/disable the Vertical Situation Display.
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
Flight
Management
Or:
a)
Select the Navigation Map Page.
b)
Press the MENU Key.
c)
Turn the FMS Knob to highlight ‘Show VSD’ or ‘Hide VSD’ and press the
ENT Key.
Index
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select ‘VSD’ and press the ENT Key.
5)
Turn the large FMS Knob to highlight the Winds on/off field.
6)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
7)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with the
changed settings.
Displaying County Warning information:
1)
Select the ‘Map - Weather Data Link (XM)’ Page.
2)
Press the More WXSoftkey.
3)
Press the County Softkey.
Displaying cyclone (hurricane) track information:
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Enabling/disabling winds aloft data display for the VSD:
1)
Select the ‘Map — Weather Data Link (XM) Page.
2)
Press the More WX Softkey.
3)
Press the Cyclone Softkey.
Displaying icing information:
98
1)
Select the ‘Weather Data Link (XM) Page.
2)
Press the More WX Softkey.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Press the ICNG Softkey.
4)
Press a softkey for the desired altitude level: 1,000 feet up to 30,000 feet. Press
the Next or PREV Sofktey to cycle through the altitude softkeys. The ICNG
SOftkey label changes to indicate the icing altitude selected.
EIS
Displaying turbulence information:
Select the ‘Map — Weather Data Link (XM) Page.
2)
Press the More WX Softkey.
3)
Press the TURB Softkey.
4)
Press a softkey for the desired altitude: 21,000 up to 45,000 feet. Press the
Next or PREV Softkey to cycle though the available softkeys. The TURB Softkey
label changes to indicate the turbulence altitude selection.
Audio Panel
and CNS
1)
Select the ‘Map - Weather Data Link (XM or FIS-B or CNXT)’ Page.
2)
Press the More WX Softkey.
3)
Press the PIREPS or AIREPS Softkey. (Note the AIREPS Softkey is only available
with the SiriusXM Weather service.)
4)
Press the Joystick and pan to the desired weather report. A gray circle will
appear around the weather report when it is selected.
5)
Press the ENT Key. The Weather Information Page is shown with PIREP or AIREP
text. The data is first displayed in a decoded fashion, followed by the original
text. Note the original text may contain additional information not present in
the decoded version.
6)
Turn the FMS Knob or the ENT Key to scroll through the PIREP or AIREP text.
7)
Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM)
Page.
Hazard
Avoidance
1)
AFCS
Additional
Features
Abnormal
Operation
Select the ‘Map - Weather Data Link (XM or FIS-B or CNXT)’ Page or Navigation
Map Page.
2)
Press the Joystick and pan the map pointer over a TFR to highlight it. The
system displays TFR summary information above the map.
3)
Press the ENT Key. The system displays a pop-up menu.
4)
If necessary, turn the FMS Knob to select ‘Review Airspaces’ and press the ENT
Key. The system displays the TFR Information window.
5)
Press the FMS Knob or the CLR Key to remove the TFR Information window.
Appendix
1)
Annunciations
& Alerts
Displaying TFR Data:
99
Index
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Flight
Management
Displaying PIREP and AIREP text:
190–02362–00 Rev. A
Flight
Instruments
3)
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
Setting up and customizing TFR data for maps on which
TFR data can be displayed:
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Aviation’ Group and press the ENT Key.
5)
Turn the large FMS Knob to scroll to the TFR product range settings.
6)
Turn the small FMS Knob to scroll through options (Off, range settings).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with the
changed settings.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Viewing FIS-B status:
1)
Turn the large FMS Knob to select the Aux Page Group.
2)
Turn the small FMS Knob to select the ‘Aux - ADS-B Status’ Page.
Enabling/disabling the FIS-B weather feature:
1)
Select the ‘Map - Weather Data Link (FIS-B)’ Page.
2)
Press the MENU Key.
3)
Turn the small FMS Knob to highlight ‘Enable FIS-B Weather’ or ‘Disable FIS-B
Weather’, and press the ENT Key. The system will not receive FIS-B weather
information when FIS-B Weather is disabled.
STORMSCOPE LIGHTNING DETECTION SYSTEM
Adjusting the Stormscope Map Range:
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Stormscope Page.
3)
Turn the Joystick clockwise to increase the map range or counter-clockwise to
decrease the map range.
Selecting ‘cell’ or ‘strike’ mode on the Stormscope Page:
1)
Select the Stormscope Page.
2)
Select the Mode Softkey. The Cell and Strike Softkeys are displayed.
100
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Press the Cell Softkey to display cell data or press the Strike softkey to display
strike data. ‘Cell’ or ‘Strike’ is annunciated in the mode box in the top-right
corner of the Stormscope Page.
4)
Press the Back Softkey to return to the top level softkeys for the Stormscope
Page.
Flight
Instruments
3)
EIS
Or:
2)
Press the MENU Key to display the Stormscope Page Menu. Either ‘Cell Mode’
or ‘Strike Mode’ is highlighted in cyan to indicate the mode to be selected.
3)
Press the ENT Key to select the highlighted mode and remove the menu. To
remove the menu without changing the modes, press the MENU Key or the
CLR Key, or push the FMS Knob.
Flight
Management
Select the Stormscope Page.
Manually clearing Stormscope cell or strike information:
Select the Stormscope Page.
2)
Press the Clear Softkey.
Hazard
Avoidance
1)
Audio Panel
and CNS
1)
Or:
Press the MENU Key.
b)
Turn the FMS Knob to highlight ‘Clear Lightning Data’, then press the ENT
Key.
AFCS
a)
Additional
Features
Or:
Select the Navigation Map Page.
b)
Press the MENU Key.
c)
Turn the FMS Knob to highlight ‘Clear Stormscope Lightning’, then press
the ENT Key.
Press the Map Opt Softkey.
2)
Press the STRMSCP Softkey.
Appendix
1)
Annunciations
& Alerts
Displaying Stormscope information on MFD navigation
maps:
Displaying Stormscope information on PFD maps:
On the PFD, press the Map/HSI Softkey.
2)
Press the Lightning Softkey.
3)
Press the STRMSCP Softkey.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
Abnormal
Operation
a)
101
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
Setting up Stormscope options on the Navigation Map:
1)
On the Navigation Map Page, press the MENU Key.
2)
With ‘Map Settings’ selected, press the ENT Key.
3)
Turn the small FMS Knob to display the group selection window. Turn the small
FMS Knob to select ‘Weather’ and press the ENT Key.
4)
Turn the large FMS Knob to highlight and move the cursor among the product
selections.
5)
When an item is highlighted, turn the small FMS Knob to select the option.
6)
Press the ENT Key.
7)
Press the FMS Knob to return to the Navigation Map Page.
Setting up Stormscope options on the Navigation Map
Page:
1)
On the Navigation Map Page, press theMENU Key.
2)
Turn the FMS Knob to highlight ‘Map Settings’ and press the ENT Key.
3)
Turn the small FMS Knob to display the group selection window. Turn the small
FMS Knob to select the ‘Weather’ group and press the ENT Key.
4)
Turn the large FMS Knob to highlight the Stormscope On/Off field. Turn the
small FMS Knob to enable/disable the Stormscope overlay.
5)
Turn the large FMS Knob to highlight the Stormscope maximum display range
field. Turn the small FMS Knob to choose the maximum map range to display
Stormscope lightning symbols, then press the ENT Key. If the pilot selects a map
range greater than this distance, the system removes lightning symbols from the
map.
6)
Turn the large FMS Knob to highlight the Stormscope Mode field. Turn the
small FMS Knob to select ‘Cell’ Mode to display clusters of electrical activity, or
‘Strike’ Mode to show the approximate location of individual lightning strikes.
With the desired mode highlighted, press the ENT Key.
7)
When finished, press the FMS Knob or the CLR Key to remove the menu.
Index
Appendix
Selecting a Stormscope range on the Navigation Map Page:
1)
Press the MENU Key.
2)
With ‘Map Settings’ highlighted, press the ENT Key.
3)
Turn the FMS Knob to select the ‘Weather’ group, and press the ENT Key.
4)
Turn the large FMS Knob to highlight the Stormscope maximum map display
range distance.
102
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Press the ENT Key.
6)
Press the FMS Knob to return to the Navigation Map Page.
Flight
Instruments
5)
Press the MENU Key.
2)
Turn the FMS Knob to highlight ‘Clear Stormscope Lightning’.
3)
Press the ENT Key.
Audio Panel
and CNS
1)
EIS
Manually clearing Stormscope data on the Navigation Map
Page:
AIRBORNE COLOR WEATHER RADAR
Flight
Management
Displaying weather on the Weather Radar Page:
Select the ‘Map — Weather Radar’ Page.
2)
Press the Mode Softkey.
3)
If on the ground, press the Standby Softkey. A one-minute warm-up period
begins with a countdown displayed on the screen. After the warm-up is
complete, the weather radar enters Standby Mode.
4)
Press the Weather Softkey. If the on the ground, a confirmation window
appears. Turn the FMS Knob to highlight ‘Yes’ to confirm activation or ‘No’ to
cancel activation
5)
Turn the Joystick to select the desired map range.
6)
The horizontal scan is initially displayed. If desired, press the Vertical Softkey to
change to vertical scan mode.
Hazard
Avoidance
1)
Abnormal
Operation
Appendix
Or:
Press the Menu Key and turn the large FMS Knob to select ‘Show Bearing
Line’. Then press the ENT Key.
3)
Press the VerticalSoftkey. A vertical scan of the selected area is displayed.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Turn the small FMS Knob or move the Joystick left or right to position the
Bearing Line on the desired storm cell or area to be vertically scanned.
Annunciations
& Alerts
While in Horizontal Scan view, press the BRG Softkey. This places the cursor in
the ‘Bearing’ field and displays the Bearing Line.
2)
Additional
Features
NOTE: Vertical scanning of a storm cell should be done with the aircraft’s wings
level to avoid the need to constantly adjust the position of the Bearing Line.
1)
AFCS
Vertically scanning a storm cell:
103
4)
With the cursor still in the ‘Bearing’ field, turn the small FMS Knob to adjust the
bearing as needed.
5)
To remove the cursor from the ‘Bearing’ field, press the FMS Knob.
6)
Turn the Joystick as needed to adjust the range.
7)
To select a new area to be vertically scanned, press the Horizon Softkey to
return to the Horizontal scan mode and repeat the previous steps.
Adjusting antenna tilt angle on the Horizontal Scan
display:
1)
Press the FMS Knob to activate the cursor in the ‘Tilt’ field.
2)
Turn the small FMS Knob or press the Joystick up or down to select the desired
antenna tilt angle.
3)
Press the ENT Key to accept the setting.
4)
Press the FMS Knob to remove the cursor.
Vertically scanning a storm cell:
1)
While in Horizontal Scan mode, press the BRG Softkey to display the bearing
line. The cursor highlights the setting in the ‘Bearing’ field.
2)
Move the Joystick left or right or turn the small FMS Knob to position the
bearing line over the storm cell or area to be vertically scanned.
3)
Press the Vertical Softkey, and the system displays a vertical scan.
4)
If desired, move the Joystick left or right or turn the small FMS Knob to make
additional adjustments to the ‘Bearing’ field.
5)
Turn the Joystick as needed to adjust the range.
6)
Press the FMS Knob to remove the cursor from the ‘Bearing’ field.
7)
To select a new area to be vertically scanned, press the Horizon Softkey to
return to the Horizontal Scan mode, then repeat the previous steps.
Adjusting weather radar gain:
WARNING: Always position the weather radar gain setting to Calibrated for
viewing the actual intensity of precipitation. Changing the gain in weather mode
causes precipitation intensity to be displayed as a color not representative of the
true intensity.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
104
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
2)
Turn the small FMS Knob to adjust the gain for the desired level. The gain
setting is visible in the ‘Gain’ field as a moveable horizontal bar in a flashing
box. A pointer with a solid bar represents the calibrated gain setting in the field.
3)
With the gain set at the desired level, press the FMS Knob to remove the cursor.
4)
To return to the calibrated gain setting, press the Gain Softkey again.
‘Calibrated’ appears in the ‘Gain’ field.
Audio Panel
and CNS
Enabling/disabling Sector Scanning:
Move the Joystick left or right or turn the small FMS Knob to position the
Bearing Line to the position which will define the center of the sector scan.
3)
Turn the large FMS Knob to highlight the ‘Sector Scan’ field.
4)
Turn the small FMS Knob to select the sector scan width in 20 degree
increments, or select ‘Full’ to select the full scan width.
5)
If desired, move the Joystick left or right to move the center position of the
sector scan.
6)
To remove the Bearing Line and cursor, press the BRG Softkey again. The
bearing reference is reset to zero degrees.
AFCS
2)
Hazard
Avoidance
While in horizontal scan mode, press the BRG Softkey to display the Bearing
Line, which also places the cursor in the ‘Bearing’ field.
Flight
Management
1)
2)
Press the STAB Softkey to enable/disable antenna stabilization. The current
stabilization status is shown in the upper right on the Weather Radar Page.
Abnormal
Operation
Press the Features Softkey.
Additional
Features
Enabling/disabling Antenna Stabilization:
1)
Enabling/disabling the WATCH feature:
Press the Features Softkey.
2)
Press the WATCH Softkey to enable/disable the WATCH feature.
Operating the Weather Radar in Ground Map Mode on the
Weather Radar Page:
Appendix
Press the Mode Softkey.
2)
Press the Ground Softkey to place the weather radar in Ground Map mode.
3)
Press the Back softkey to return to the top-level Weather Radar Page Softkeys.
4)
To adjust the antenna tilt angle, press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the ‘Tilt’ field.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
190–02362–00 Rev. A
Annunciations
& Alerts
1)
EIS
Press the Gain Softkey to activate the cursor in the ‘Gain’ field.
Flight
Instruments
1)
105
6)
Adjust the antenna tilt angle by turning the small FMS Knob to display ground
returns at the desired distance.
7)
Press the FMS Knob to remove the cursor.
Enabling/disabling the airborne weather radar overlay on
the Navigation Map Page:
1)
Select the Navigation Map Page.
2)
Press the Map Opt Softkey.
3)
Press the WX RadarSoftkey.
4)
Press the Back Softkey to return to the top-level MFD softkeys.
Or:
1)
On the Navigation Map Page, press the MENU Key.
2)
With ‘Map Settings’ highlighted, press the ENT Key.
3)
Turn the small FMS Knob to select the ‘Weather’ group, then press the ENT
Key.
4)
Turn the large FMS Knob to scroll through product selections, and highlight the
Weather Radar overlay selection ‘On’ or ‘Off’. Turn the small FMS Knob to
highlight the desired selection.
5)
To remove the menu, press the FMS Knob or the CLR Key.
TERRAIN DISPLAYS
Displaying relative terrain information (MFD maps other
than the terrain page)
1)
Press the Map Opt Softkey (for the PFD Inset Map, press the Map/HSI Softkey).
2)
Press the TER Softkey as needed to cycle through the terrain options, with the
current selection displayed in cyan on the softkey (‘Off’, ‘Topo’ or ‘REL’). ‘REL’
indicates relative terrain is selected.
Displaying the terrain page:
1)
Turn the FMS Knob to select the Map page group.
2)
Turn the small FMS Knob to select the Terrain Proximity/Terrain-SVT/TAWS-B
Page.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
106
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
1)
Press the MENU Key.
2)
Turn the FMS Knob to highlight ‘Show Aviation Data’ or ‘Hide Aviation Data’
(choice dependent on the current state), then press the ENT Key.
EIS
Enabling/disabling the Vertical Situation Display (VSD):
2)
Press the Map Opt Softkey.
3)
Press the Inset Softkey.
4)
Press the VSD Softkey to enable/disable the VSD.
Flight
Management
Select the Navigation Map Page.
Audio Panel
and CNS
1)
Flight
Instruments
Showing/hiding aviation information on the terrain page:
Or:
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Show VSD’ or ‘Hide VSD’ (choice dependent
on current state) and press the ENT Key.
Hazard
Avoidance
1)
Selecting a VSD Mode:
AFCS
Select the Navigation MapPage.
2)
Press the Inset Softkey.
3)
Press the VSD Softkey, which displays the VSD mode in cyan. Each press of the
softkey selects a mode: FPL (Flight Plan), TRK (track), or Auto.
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to highlight the ‘VSD’ group, then press the ENT Key.
5)
Turn the large FMS Knob to highlight the Track Mode Boundary ‘On’ or ‘Off’
field. Turn the small FMS Knob if needed to change this setting.
6)
Turn the large FMS Knob to highlight the maximum map range to display the
Track Mode Boundary. Turn the small FMS Knob to select a maximum range,
then press the ENT Key.
7)
Press the FMS Knob or the CLR Key to return to the Navigation Map Page with
the changed settings.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
107
Index
2)
Appendix
Select the Navigation Map Page.
Annunciations
& Alerts
1)
Abnormal
Operation
Customizing the Track Mode Boundary display on the ‘Map
- Navigation Map’ Page:
Additional
Features
1)
Inhibiting/enabling FLTA Alerting (Terrain SVT and TAWS-B
only):
1)
Select the terrain page.
2)
Press the Inhibit Softkey. FLTA alerting is inhibited when softkey annunciator is
green.
EIS
Flight
Instruments
Hazard Avoidance
1)
Press the MENU Key.
2)
Turn the FMS Knob to highlight the desired inhibit or enable option, then press
the ENT Key.
TRAFFIC INFORMATION SERVICE (TIS)
Enabling/disabling traffic overlays (MFD navigation maps):
1)
Press the Map Opt Softkey.
2)
Press the Traffic Softkey. Traffic is now displayed on the navigation map.
Enabling/disabling traffic information on the PFD Inset
Map or HSI Map:
1)
On the PFD, press the Map/HSI Softkey.
2)
Press the TrafficSoftkey to enable/disable the display traffic information on the
Inset Map or HSI Map.
Customizing traffic display on the Navigation Map Page:
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
• Traffic – Turns the display of traffic data on or off
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Or:
• Traffic Mode – Selects the traffic mode for display; select from:
• All Traffic - Displays all traffic
Index
• TA Only - Displays Traffic Alerts only
108
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
• Traffic Labels – Selects the maximum range at which traffic labels are shown (with
Flight
Instruments
• Traffic Symbols – Selects the maximum range at which traffic symbols are shown
the option to turn off)
Turn the small FMS Knob to scroll through options for each product (On/Off,
range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the ‘Map - Navigation Map’ Page
with the changed settings.
EIS
6)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Confirm TIS is in Operating Mode:
Flight
Management
1)
Audio Panel
and CNS
Displaying traffic on the Traffic Map Page:
Hazard
Avoidance
Press the TIS OPER Softkey to begin displaying traffic.
Or:
Press the MENU Key.
b)
Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT
Key.
AFCS
a)
Muting the “TIS Not Available” voice alert:
Select the ‘Map - Traffic Map’ Page.
2)
Press the TNA Mute Softkey. The status is displayed in the upper left corner of
the Traffic Map Page.
Abnormal
Operation
Or:
Press the MENU Key.
b)
Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off)
and press the ENT Key.
Annunciations
& Alerts
a)
Additional
Features
1)
Switching between TIS modes:
Select the ‘Map - Traffic Map’ Page.
2)
Press the Standby or Operate Softkey to switch between modes. The mode is
displayed in the upper right corner of the Traffic Map Page.
Appendix
1)
Or:
Press the MENU Key.
b)
Select ‘Operate Mode’ or ‘Standby Mode’ (choice dependent on current
state) and press the ENT Key.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
a)
109
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
TAS/TCAS I TRAFFIC
Testing the Traffic System:
1)
Select the Traffic Map Page.
2)
Turn the Joystick to adjust the map range to 2 NM for the inner range ring, and
6 NM for the outer range ring. This ensures the full traffic test pattern is
depicted on the map.
3)
If the traffic system is Operating Mode, press the Standby or TAS Standby
Softkey.
4)
Press the Test Softkey.
Or:
1)
On the Traffic Map Page, press the MENU Key and turn the FMS Knob
highlight ‘Test Mode’.
2)
Press the ENT Key.
Selecting a TAS/TCAS I Operating Mode:
1)
Select the Traffic Map Page.
2)
To select Standby Mode, press the Standby or TAS STBY Softkey.
Additional
Features
Or:
1)
Press the MENU Key.
2)
Turn the FMS Knob to highlight the desired mode and press the ENT Key.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Displaying traffic on the Traffic Map Page:
1)
Turn the large FMS Knob to select the Map page group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the Operate or TAS OPER Softkey to select Operating Mode.
4)
Press the Standby or TAS STBY Softkey to select Standby Mode.
Customizing the traffic display on the Navigation Map
Page:
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the Traffic Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through the selections.
110
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Flight
Instruments
• Traffic – Turns the display of traffic data on or off
• Traffic Mode – Selects the traffic mode for display; select from:
• All Traffic - Displays all traffic
EIS
• TA/PA - Displays Traffic Advisories and Proximity Advisories
• TA Only - Displays Traffic Advisories only
• All Traffic - Displays all traffic
Audio Panel
and CNS
• TA/PA - Displays Traffic Advisories and Proximity Advisories
• TA Only - Displays Traffic Advisories only
• Traffic Labels – Selects the maximum range at which traffic labels are shown with
the option to turn off
Turn the small FMS Knob to scroll through options (On/Off, range settings,
etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page.
Hazard
Avoidance
6)
AFCS
Selecting a display range on the Traffic Map Page:
Select the Traffic Map Page.
2)
Turn the Joystick clockwise to increase the map range or counter-clockwise to
decrease the map range.
2)
Press the Traffic Softkey to enable/disable the traffic overlay.
3)
Press the Back Softkey to return to the top-level softkeys.
Annunciations
& Alerts
Press the Map Opt Softkey.
Abnormal
Operation
Enabling/disabling traffic information (MFD navigation
maps):
Customizing the traffic display on the Navigation Map
Page:
Appendix
Select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the Traffic Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through the selections.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
190–02362–00 Rev. A
Additional
Features
1)
1)
Flight
Management
• Traffic Symbols – Selects the maximum range at which traffic symbols are shown
111
Hazard Avoidance
Flight
Instruments
• Traffic – Turns the display of traffic data on or off
• Traffic Mode – Selects the traffic mode for display; select from:
• All Traffic - Displays all traffic
EIS
• TA/PA - Displays Traffic Advisories and Proximity Advisories
• TA Only - Displays Traffic Advisories only
Audio Panel
and CNS
• All Traffic - Displays all traffic
• TA/PA - Displays Traffic Advisories and Proximity Advisories
• TA Only - Displays Traffic Advisories only
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
• Traffic Symbols – Selects the maximum range at which traffic symbols are shown
• Traffic Labels – Selects the maximum range at which traffic labels are shown with
the option to turn off
6)
Turn the small FMS Knob to scroll through options (On/Off, range settings,
etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page.
Enabling/disabling traffic information on PFD navigation
maps:
1)
With the Inset Map or HSI Map displayed, press the Map/HSI Softkey.
2)
Press the Traffic Softkey to enable/disable the traffic overlay.
3)
Press the Back Softkey to return to the top-level PFD softkeys.
ADS-B TRAFFIC
Annunciations
& Alerts
Enabling/disabling the display of ADS-B traffic.
1)
Select the ‘Map - Traffic Map’ Page.
2)
Press the ADS-B Softkey.
a)
Press the MENU Key and turn the small FMS Knob to highlight ‘ADS-B On’
or ‘ADS-B Off’.
b)
Press the ENT Key.
Index
Appendix
Or:
112
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
Flight
Instruments
Testing the display of ADS-B traffic:
Select the ‘Map - Traffic Map’ Page.
2)
If necessary, turn the Joystick to select a map range of 2 and 6 nm to ensure full
test pattern display.
3)
Ensure the the ADS-B Softkey is disabled.
4)
If the optional TAS/TCAS I is installed, ensure the TAS STBY Softkey is enabled.
5)
Press the Test Softkey.
EIS
1)
Audio Panel
and CNS
Or:
Press the MENU Key.
Turn the small FMS Knob to highlight ‘Test Mode’.
b)
Press the ENT Key.
Flight
Management
a)
1)
On the ‘Map - Traffic Map’ Page, press the ALT Mode Softkey.
2)
Select one of the following softkeys:
Hazard
Avoidance
Changing the altitude range:
aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight.
AFCS
• Above: Displays Other Non-Threat and proximity traffic from 9000 feet above the
• Normal: Displays Other Non-Threat and proximity traffic from 2700 feet above
• Below:Displays Other Non-Threat and proximity traffic from 2700 feet above the
• UNREST (unrestricted): All traffic is displayed from 9900 feet above and 9900 feet
below the aircraft.
To return to the ‘Map - Traffic Map’ Page, select the Back Softkey.
Annunciations
& Alerts
3)
Abnormal
Operation
aircraft to 9000 feet below the aircraft. Typically used during descent phase of
flight.
Additional
Features
the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of
flight.
Or:
Press the MENU Key.
2)
Turn the small FMS Knob to highlight one of the following options (see softkey
description in step 2 above):
Appendix
1)
• Above
• Normal
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
113
Hazard Avoidance
Flight
Instruments
• Below
• Unrestricted
Audio Panel
and CNS
EIS
3)
Press the ENT Key.
Enabling/disabling the Motion Vector display:
1)
Select the ‘Map - Traffic Map’ Page.
2)
Press the Motion Softkey.
3)
Press one of the following softkeys:
• Relative: Displays the motion vector relative to own aircraft
• Off: Disables the display of the motion vector.
4)
Select the ‘Map - Traffic Map’ Page.
5)
Press the MENU Key.
6)
Turn the small FMS Knob to highlight ‘Relative Motion’, ‘Absolute Motion’ or
‘Motion Vector Off’.
7)
Press the ENT Key.
Adjusting the duration for the Motion Vector projected
time:
1)
Select the ‘Map - Traffic Map’ Page.
2)
Press the Motion Softkey.
3)
Press the Duration Softkey.
4)
Press a softkey for the desired duration (30 SEC, 1 MIN, 2 MIN, 5 MIN).
5)
When finished, press the Back Softkey to return to the ‘Map - Traffic Map’
Page.
Showing additional traffic information:
1)
Select the ‘Map - Traffic Map’ Page.
2)
Press the FMS Knob. The first selected traffic symbol is highlighted in cyan.
Additional information appears in a window in the upper-right corner of the
‘Map - Traffic Map’ Page.
3)
To select a different aircraft symbol, turn the FMS Knob until the selected
aircraft traffic symbol is highlighted.
4)
When finished, press the FMS Knob again to disable the traffic selection.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
• Absolute: Displays the motion vector pointing in the absolute direction.
114
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Hazard Avoidance
1)
Turn the Joystick.
2)
The following range options are available:
Flight
Instruments
Changing the display range on the Traffic Map Page:
EIS
• 500 feet
• 500 feet and 1000 feet
Audio Panel
and CNS
• 1000 feet and 2000 feet
• 2000 feet and 1 nm
• 1 and 2 nm
Flight
Management
• 2 and 6 nm
• 6 and 12 nm
• 12 and 24 nm
Hazard
Avoidance
• 24 and 40 nm
Viewing ADS-B Traffic Status:
Turn the large FMS Knob to select the Aux Page Group.
2)
Turn the small FMS Knob to select the ‘Aux - ADS-B Status’ Page.
AFCS
1)
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
115
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Hazard Avoidance
BLANK PAGE
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Automatic Flight Control System
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
ACTIVATING THE FLIGHT DIRECTOR
EIS
Activating The Flight Director
Modes Selected
FD Key
ROL
Pitch Hold (default)
PIT
AP Key
Roll Hold (default)
ROL
Roll Hold (default)
PIT
CWS Button
Roll Hold (default)
ROL
Roll Hold (default)
PIT
GA Button
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on Ground)
Go Around (in air)
TO
GA
ALT Key
Roll Hold (default)
ROL
Altitude Hold
ALT
VS Key
Roll Hold (default)
ROL
Vertical Speed
VS
VNV Key
Roll Hold (default)
ROL
Vertical Path
Tracking*
VPTH
NAV Key
Navigation**
FMS
VOR
LOC
Pitch Hold (default)
PIT
BC Key
Backcourse***
BC
Pitch Hold (default)
PIT
APR Key
Approach**
FMS
VOR
LOC
Pitch Hold (default)
PIT
HDG Key
Heading Select
HDG
Pitch Hold (default)
PIT
Vertical
Hazard
Avoidance
Lateral
Roll Hold (default)
Flight
Management
Control
Pressed
Audio Panel
and CNS
An initial press of a key listed in Table 7-1 (when the flight director is not active)
activates the pilot-side flight director in the listed modes. The flight director may
be turned off and the Command Bars removed from the displays by pressing
the FD Key again. The FD Key is disabled when the autopilot is engaged.
AFCS
Abnormal
Operation
Annunciations
& Alerts
Appendix
**The selected navigation receiver must have a valid VOR or LOC signal or active
FMS course before NAV or APR Key press activates flight director.
Additional
Features
*Valid VNV flight plan must be entered before VNV Key press activates flight
director.
***The selected navigation receiver must have a valid LOC signal before BC Key
press activates flight director.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
117
VERTICAL MODES
Vertical Modes
The following table lists the vertical modes with their corresponding controls and
annunciations. The mode reference is displayed next to the active mode annunciation for
Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/DN Wheel
can be used to change the vertical mode reference while operating under Pitch Hold,
Vertical Speed, or Flight Level Change Mode. Increments of change and acceptable ranges
of values for each of these references using the NOSE UP/DN Wheel are also listed in the
table.
Vertical Mode
Description
Contr
ol
Annunciatio
n
Pitch Hold
Holds the current
aircraft pitch
attitude; may be
used to climb/
descend to the
Selected Altitude
(defau
lt)
PIT
Selected
Altitude
Capture
Captures the
Selected Altitude
*
ALTS
Altitude Hold
Holds the current
Altitude
Reference
ALT
Key
ALT
nnnnn
ft
Vertical Speed
Maintains the
current aircraft
vertical speed;
may be used to
climb/descend to
the Selected
Altitude
VS
Key
VS
nnnn
fpm
-4000 to
+3000
fpm
100 fpm
Flight Level
Change, IAS
Hold
Maintains the
current aircraft
airspeed (in IAS)
while the aircraft
is climbing/
descending to the
Selected Altitude
FLC
Key
FLC
nnn kt
78 to
183 kt
1 kt
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Automatic Flight Control System
118
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Referen
ce
Range
-15° to
+25°
Referen
ce
Change
Increme
nt
0.5°
190–02362–00 Rev. A
Automatic Flight Control System
Flight
Instruments
LATERAL MODES
Lateral Modes
Annunciati
on
Maxim
um Roll
Comma
nd
Limit
Roll Hold
Holds the current
aircraft roll attitude
or rolls the wings
level, depending on
the commanded
bank angle
(default)
ROL
25°
Low Bank
Limits the maximum
commanded roll
angle
BANK
Key
*
15°
Heading Select
Captures and tracks
the Selected
Heading
HDG Key
HDG
25°
Navigation, GPS Arm/
Capture/Track
Captures and tracks
the selected
navigation source
(GPS, VOR, LOC
NAV Key
FMS
25°
Navigation, VOR
Enroute Arm/Capture/
Track
Captures and tracks
the selected
navigation source
(GPS, VOR, LOC
NAV Key
VOR
25°
Navigation, LOC Arm/
Capture/Track (No
Glideslope)
Captures and tracks
the selected
navigation source
(GPS, VOR, LOC
NAV Key
LOC
25°
Hazard
Avoidance
Control
Flight
Management
Description
Audio Panel
and CNS
Lateral Mode
EIS
The following table relates each Garmin AFCS lateral mode to its respective control and
annunciation. Refer to the combination modes section for information regarding Go
Around and Takeoff modes.
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is
indicated in green along the Roll Scale of the Attitude Indicator.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
119
Index
The CWS Button does not change lateral references for Heading Select, Navigation,
Backcourse, or Approach Mode. The autopilot guides the aircraft back to the Selected
Heading/Course upon release of the CWS Button.
COMBINATION MODES (VNV, APR, NAV, GA)
Combination Modes (VNV, APR, NAV, BC, GA)
The following table lists the modes that operating by using both Vertical and Lateral
Modes with their corresponding controls and annunciations.
Audio Panel
and CNS
EIS
Flight
Instruments
Automatic Flight Control System
Description
Control
Annunciat
ion
Vertical Path
Tracking
Captures and
tracks descent legs
of an active
vertical profile
VNV
Key
VPTH
VNV Target
Altitude
Capture
Captures the
Vertical Navigation
(VNV) Target
Altitude
*
ALTV
Glidepath
Captures and
tracks the SBAS
glidepath on
approach
Glideslope
Captures and
tracks the ILS
glideslope on
approach
Backcourse
Arm/Capture/
Track
Captures and
tracks a localizer
signal for
backcourse
approaches
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Mode
Approach, FMS
Arm/Capture/
Track
Referen
ce
Range
GP
APR
Key
GS
BC Key
BC
25°
Capture
10 Track
FMS
25°
VAPP
25°
Capture
10 Track
°
APR
Key
Index
Appendix
Captures and
tracks the selected
Approach, VOR navigation source
(FMS, VOR, LOC)
Arm/Capture/
Track
Maxim
um Roll
Comma
nd
Limit
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Automatic Flight Control System
Description
Control
EIS
Approach, ILS
Arm/Capture/
Track
(Glideslope
Mode
automatically
armed)
Annunciat
ion
Referen
ce
Range
Flight
Instruments
Mode
Maxim
um Roll
Comma
nd
Limit
Audio Panel
and CNS
LOC
GA
Button
TO
10°
Go Around
Disengages the
autopilot and
commands a
constant pitch
angle and wings
level in the air
GA
Button
GA
10°
Flight
Management
Takeoff
Disengages the
autopilot and
commands a
constant pitch
angle and wings
level on the
ground in
preparation for
takeoff
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
* ALTV is armed automatically under VPTH when VNV Target Altitude is to be
captured instead of Selected Altitude.
PROCEDURES
Annunciations
& Alerts
Suspected Autopilot Malfunction
If an autopilot failure or trim failure is suspected to have occurred, perform the
following steps:
Firmly grasp the control wheel.
2)
Press and hold the AP DISC Switch. The autopilot will disconnect and power is
removed from the trim motor. Power is also removed from all primary servo
190–02362–00 Rev. A
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121
Index
1)
Appendix
NOTE: Consult the aircraft documentation for the location of circuit breakers as
well as specifics that may supplement or amplify this procedure.
motors and engaged solenoids. Note the visual and aural alerting indicating
autopilot disconnect.
3)
Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4)
Pull the appropriate circuit breaker(s) to electrically isolate the servo and
solenoid components.
5)
Release the AP DISC Switch.
Overpowering Autopilot Servos
In the context of this discussion, “overpowering” refers to any pressure or force
applied to the pitch controls when the autopilot is engaged. A small amount of
pressure or force on the pitch controls can cause the autopilot automatic trim to
run to an out-of-trim condition. Therefore, any application of pressure or force
to the controls should be avoided when the autopilot is engaged.
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Automatic Flight Control System
Hazard
Avoidance
Overpowering the autopilot during flight will cause the autopilot’s automatic
trim to run, resulting in an out-of-trim condition or cause the trim to hit the
stop if the action is prolonged. In this case, larger than anticipated control
forces are required after the autopilot is disengaged.
1)
Check for proper autopilot operation and ensure the autopilot can be
overpowered.
2)
Note the forces required to overpower the autopilot servo clutches.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
The following steps should be added to the preflight check:
122
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SAFETAXI
EIS
Configuring SafeTaxi Range
While viewing the ‘Map-Navigation Map’ Page, press the MENU Key to display
the ‘Page Menu.’
2)
Turn the large FMS Knob to highlight the ‘Map Settings’ Menu Option and
press the ENT Key.
3)
Turn the FMS Knob to select the ‘Aviation’ Group and press the ENT Key.
4)
Turn the large FMS Knob to scroll through the ‘Aviation’ Group options to
SafeTaxi.
5)
Turn the small FMS Knob to display the range of distances.
6)
Turn either FMS Knob to select the desired distance for maximum SafeTaxi
display range.
7)
Press the ENT Key to complete the selection.
8)
Press the FMS Knob to return to the ‘Map-Navigation Map’ Page.
Audio Panel
and CNS
1)
Flight
Management
Hazard
Avoidance
AFCS
CHARTS
While viewing the ‘Map-Navigation Map’ Page, ‘NRST-Nearest Airport’ Page, or
‘FPL-Active Flight Plan’ Page, press the Charts Softkey.
Press the MENU Key to display the ‘Page Menu.’
2)
Turn the large FMS Knob to scroll through the ‘Options’ Menu to Charts.
3)
Press the ENT Key to display the chart.
Annunciations
& Alerts
1)
Abnormal
Operation
Or:
Additional
Features
Selecting Terminal Procedures Charts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
123
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Navigation Map Page Options Menu
Waypoint Airport Information Page Options Menu
Flight
Management
Figure 16 Option Menus
Hazard
Avoidance
When no terminal procedure chart is available, the banner No Available Charts
appears on the screen. The No Available Charts banner does not refer to the
FliteCharts subscription, but rather the availability of a particular airport chart
selection or procedure for a selected airport.
AFCS
Figure 17 Chart Not Available Banner
Additional
Features
If there is a problem in rendering the data (such as a data error or a failure of an
individual chart), the banner Unable To Display Chart is then displayed.
Abnormal
Operation
When a chart is not available by pressing the Charts Softkey or selecting a Page
Menu Option, charts may be obtained for other airports from the WPT Pages or
Flight Plan Pages.
Annunciations
& Alerts
Figure 18 Unable To Display Chart Banner
If a chart is available for the destination airport, or the airport selected in the
active flight plan, the chart appears on the screen. When no flight plan is active,
or when not flying to a direct-to destination, pressing the Charts Softkey
displays the chart for the nearest airport, if available.
Index
Appendix
The chart shown is one associated with the ‘WPT–Airport Information’ page.
Usually this is the airport runway diagram. Where no runway diagram exists, but
Take Off Minimums or Alternate Minimums are available, that page appears. If
Airport Information pages are unavailable, the Approach Chart for the airport is
shown.
124
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Additional Features
While viewing the ‘Map-Navigation Map’ Page, ‘FPL-Active Flight Plan’ Page, or
‘NRST-Nearest Airports’ Page, press the Charts Softkey. The airport diagram or
approach chart is displayed on the ‘WPT-Airport Information’ Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to select either the Airport Identifier Box or the
‘Approach’ Box. (Press the APR Softkey if the ‘Approach’ Box is not currently
shown).
4)
Turn the small and large FMS Knob to enter the desired airport identifier.
5)
Press the ENT Key to complete the airport selection.
6)
Turn the large FMS Knob to select the ‘Approach’ Box.
7)
Turn the small FMS Knob to show the approach chart selection choices.
8)
Turn either FMS Knob to scroll through the available charts.
9)
Press the ENT Key to complete the chart selection.
EIS
1)
Flight
Instruments
Selecting a chart
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Figure 19 Approach Information Page, Chart Selection
Selecting Additional Information
While viewing the Airport Taxi Diagram, press the Full SCN Softkey to display
the information windows (Airport, Info).
2)
Press the FMS Knob to activate the cursor.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
1)
125
3)
Turn the large FMS Knob to highlight the Airport, Info, Runways, or Frequencies
Box.
4)
Turn the small FMS Knob to select the Info Box choices. If multiple choices are
available, scroll to the desired choice with the large FMS Knob and press the
ENT Key to complete the selection.
5)
Press the FMS Knob again to deactivate the cursor.
Pressing the Back Softkey, or waiting for 45 seconds reverts to the chart
selection softkeys. The full screen view can also be selected by using the page
menu option.
Selecting full screen On or Off:
1)
While viewing a terminal chart press the MENU Key to display the ‘Page Menu’
Options.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press
the ENT Key.
3)
Turn the large FMS Knob to move between the ‘Full Screen’ and ‘Color Scheme’
Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ ‘Full Screen’
Options.
Chart Setup Option
Full Screen On/Off Selection
Figure 20 Page Menus
Selecting Day/Night View:
1)
ChartView can be displayed on a white or black background for day or night
viewing. The Day View offers a better presentation in a bright environment. The
Night View gives a better presentation for viewing in a dark environment. When
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
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Additional Features
While viewing a terminal chart press the MENU Key to display the ‘Page Menu’
Options.
3)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press
the ENT Key.
EIS
2)
Flight
Instruments
the Chart Setup Box is selected the MFD softkeys are blank. Selecting Day,
Night, or Automatic View:
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Figure 21 Page Menu Chart Setup
5)
Turn the small FMS Knob to choose between ‘Day, Auto, and Night’ Options.
6)
If Auto Mode is selected, turn the large FMS Knob to select the percentage
field. Use the small FMS Knob to change the percentage value. The percentage
value is the day/night crossover point based on the percentage of backlighting
intensity. For example, if the value is set to 15%, the day/night display changes
when the display backlight reaches 15% of full brightness.
7)
Press the FMS Knob when finished to remove the ‘Chart Setup’ Menu.
Appendix
The display must be changed in order for the new setting to become active. This
may be accomplished by selecting another page or changing the display range.
Annunciations
& Alerts
Turn the large FMS Knob to move to the ‘Color Scheme’ Option.
Abnormal
Operation
4)
Index
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127
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Additional
Features
AFCS
Hazard
Avoidance
Figure 22 Chart Information Page, Day View
FliteCharts
FliteCharts resemble the paper version of AeroNav Services terminal procedures charts.
The charts are displayed with high-resolution and in color for applicable charts.
The geo-referenced aircraft position is indicated by an aircraft symbol displayed on the
chart when the current position is within the boundaries of the chart. Not all charts are
geo-referenced. These charts will display an Aircraft Not Shown Icon in the lower right
corner of the MFD.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Figure 23 Chart Information Page, Night View
Figure 24 Aircraft Not Shown Icon
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Additional Features
Flight
Instruments
EIS
An aircraft symbol may be displayed within an off-scale area depicted on some charts.
Off-scale areas are indicated by the grey shading. Note, these areas are not shaded on the
published chart. These off-scale areas appear on the chart to convey supplemental
information. However, the depicted geographical position of this information, as it relates
to the chart planview, is not the actual geographic position. Therefore, when the aircraft
symbol appears within one of these areas, the aircraft position indicated is relative to the
chart planview, not to the off-scale area.
The FliteCharts database subscription is available from Garmin. Available data includes:
Audio Panel
and CNS
- Arrivals (STAR)
- Departure Procedures (DP)
- Approaches
Flight
Management
- Airport Diagrams
Airport Directory
Additional
Features
Both Airport Directories are available for downloading at flygarmin.com. However, copy
only one of the databases to the Supplemental Data Card. The system cannot recognize
both databases simultaneously.
AFCS
The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK Airport
Directory databases offer detailed information regarding services, hours of operation,
lodging options, and more. This information is viewed on the Airport Information Page by
pressing the Info Softkey until Info 2 is displayed.
Hazard
Avoidance
NOTE: Do not maneuver the aircraft based solely upon the geo-referenced
aircraft symbol.
Selecting the Airport Directory Page:
2)
Turn the small FMS Knob to select the Airport Information Page. Initially,
information for the airport closest to the aircraft’s present position is displayed.
3)
If necessary, press the Info softkey until Info 2 is displayed.
Annunciations
& Alerts
Turn the large FMS Knob to select the ‘WPT’ page group.
Abnormal
Operation
1)
Appendix
Index
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129
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Figure 25 AOPA Information on the Airport Information Page
Selecting the Chart to Display:
1)
Press the MENU Key with the IFR Low / IFR High Chart displayed. The cursor
flashes on the ‘Settings’ option.
2)
Press the ENT Key. The cursor flashes on the ‘Color Scheme’ setting.
3)
Turn the small FMS Knob to select ‘Day’, ‘Auto’, or ‘Night’. The IFR Chart
display changes to reflect the setting.
4)
If ‘Auto’ was selected, turn the large FMS Knob to select the backlight
threshold field (sets value for automatic day/night switching).
Index
Appendix
Annunciations
& Alerts
Modifying the Chart Settings:
1)
Press the MENU Key with the ‘Map - IFR/VFR Charts’ Page displayed.
2)
Turn the FMS Knob to highlight the ‘Display VFR’ Field, the ‘Display IFR Low’
Field, or the ‘Display IFR High’ Field.
3)
Press the ENT Key. The selected chart is displayed.
SIRIUSXM RADIO ENTERTAINMENT
Using SiriusXM Radio
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
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Additional Features
Flight
Instruments
Selecting the XM Radio Page:
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed ‘Aux - XM Information’ Page.
3)
Press the Radio Softkey to show the ‘XM Radio’ Page where audio
entertainment is controlled.
EIS
1)
Active Channel and Channel List
Selecting a channel from the channel list:
While on the ‘Aux-XM Radio’ Page, press the Channel Softkey.
2)
Press the CH+ Softkey to go up through the list in the ‘Channels’ Box, or move
down the list with the CH– Softkey.
Hazard
Avoidance
1)
Flight
Management
The Channels List Box of the XM Radio Page shows a list of the available channels for
the selected category. Channels can be stepped through one at a time or may be selected
directly by channel number.
Audio Panel
and CNS
The Active Channel Box on the XM Radio Page displays the currently selected channel
that the SiriusXM Radio is using.
Or:
Press the FMS Knob to highlight the channel list and turn the large FMS Knob
to scroll through the channels.
2)
Press the ENT Key to activate the selected channel.
Additional
Features
Selecting a channel directly:
2)
Press the Direct CH Softkey. The channel number in the ‘Active Channel’ Box is
highlighted.
3)
Press the numbered softkeys located on the bottom of the display to directly
select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Annunciations
& Alerts
While on the ‘Aux-XM Radio’ Page, press the Channel Softkey.
Selecting a category:
2)
Press the CAT + and CAT - Softkeys to cycle through the categories.
Appendix
Press the Category Softkey on the ‘Aux-XM Radio’ Page.
Abnormal
Operation
1)
1)
AFCS
1)
Or:
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Turn the small FMS Knob to display the Categories list. Highlight the desired
category with the small FMS Knob and press the ENT Key. Selecting All
Categories places all channels in the list.
131
Setting a preset channel number:
1)
On the ‘Aux-XM Radio’ Page, while listening to an ‘Active Channel’ that is
wanted for a preset, press the Presets Softkey to access the first five preset
channels (Preset 1 - Preset 5).
2)
Press the More Softkey to access the next five channels (Preset 6 – Preset 10),
and again to access the last five channels (Preset 11 – Preset 15). Pressing the
More Softkey repeatedly cycles through the preset channels.
3)
Press any one of the (Preset 1 - Preset 15) softkeys to assign a number to the
active channel.
4)
Press the Set Softkey on the desired channel number to save the channel as a
preset.
Pressing the Back Softkey, or 45 seconds of softkey inactivity, returns the system
to the top level softkeys.
Adjusting the volume:
1)
With the ‘Aux-XM Radio’ Page displayed, press the Volume Softkey.
2)
Press the VOL – Softkey to reduce volume or press the VOL + Softkey to
increase volume. (Once the VOL Softkey is pressed, the volume can also be
adjusted using the small FMS Knob.)
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
1)
Select the ‘Aux-XM Radio’ Page or ‘Aux-XM Information’ Page.
2)
Press the Mute Softkey to mute the audio. Press the Mute Softkey again to
unmute the audio.
SATELLITE TELEPHONE AND SMS MESSAGING
Disabling/enabling telephone and low speed data services:
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the ‘Aux-Telephone’ Page.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Muting SiriusXM audio:
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
3)
Press the MENU Key. The Page Menu window is now displayed.
4)
Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list.
Additional
Features
Figure 26 Report Status Page
Abnormal
Operation
Annunciations
& Alerts
Appendix
Figure 27 Select Disable Iridium Transmission
Press the ENT Key. The Iridium transceiver is now disabled.
6)
To enable the Iridium transceiver, repeat steps 1 through 3, then select ‘Enable
Iridium Transceiver’.
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133
Index
5)
Viewing the Telephone Page
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the ‘Aux - Telephone’ or ‘Aux - Text
Messaging’ Page.
3)
If necessary, select the TEL Softkey to display the ‘Aux-Telephone’ Page.
The phone status display gives a graphical representation of the current
disposition of voice and/or data transmissions.
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Internal
Phone
External
Phone
Description
Flight
Management
Phone is idle
Hazard
Avoidance
Phone is ringing
Phone has a dial tone (off hook) or connected to another
phone
AFCS
Phone dialed is busy
Additional
Features
Phone is dialing another phone
Phone has failed
Abnormal
Operation
Phone Status not known
Annunciations
& Alerts
Phone is disabled
Appendix
Phone is reserved for data transmission
Calling other phone or incoming call from other phone
Index
Other phone is on hold
Phones are connected
Telephone Symbols
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Additional Features
With the ‘Aux - Telephone’ Page displayed, press the FMS Knob to display the
cursor.
2)
If necessary, turn either FMS Knob to place the cursor on ‘New Entry’.
3)
Press the ENT Key. The cursor moves the ‘Name’ field of the ‘Contact Details’
window.
4)
Enter the desired name of the new contact. Entry can be accomplished through
the alphanumeric keys on the MFD Controller, or the FMS Knobs on the
controller or the MFD.
5)
Press the ENT Key. The cursor moves to the ‘Phone Number’ field.
6)
Enter the desired telephone number. Entry can be accomplished through the
alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller
or the MFD.
7)
Press the ENT Key. The cursor moves to the ‘Email’ field.
8)
Enter the desired email address. Entry can be accomplished through the
alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller
or the MFD.
9)
Press the ENT Key. The Save button is highlighted.
EIS
1)
Turn either FMS Knob to place the cursor on the desired contact name.
4)
With ‘OK’ highlighted, press the ENT Key to delete the selected contact.
Abnormal
Operation
3)
Additional
Features
Select the Delete Softkey. A confirmation window is displayed.
AFCS
2)
Hazard
Avoidance
With the ‘Aux-Telephone’ Page displayed, press the FMS Knob to display the
cursor.
Flight
Management
Deleting a contact:
Audio Panel
and CNS
10) Press the ENT Key. The new contact entry is added to the list of saved contacts.
1)
Flight
Instruments
Entering a new contact
Annunciations
& Alerts
Appendix
Index
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135
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Figure 28 Editing a Contact
Editing a contact:
1)
With the ‘Aux - Telephone’ Page displayed, press the FMS Knob to display the
cursor.
2)
Turn either FMS Knob to place the cursor on the desired contact name.
3)
Select the Edit Softkey. The cursor is placed in the ‘Name’ field. Enter the
desired changes. Entry can be accomplished through the alphanumeric keys on
the MFD Controller, or the FMS Knobs on the controller or the MFD.
4)
Press the ENT Key when each field is complete. The Save Button is now
highlighted.
5)
Press the ENT Key to save the changes.
Answering an incoming call in the cockpit:
1)
Press the TEL Key on the appropriate audio panel.
2)
Select the Answer Softkey on the MFD.
OR
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Additional Features
While viewing the ‘Aux-Telephone’ Page, press the MENU Key to display
the Page Menu.
b)
Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’.
c)
Press the ENT Key.
Flight
Instruments
a)
2)
Turn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’.
3)
Press the ENT Key. The voice and pop-up alert will not be displayed now when
an incoming call is received.
Making an external call from the cockpit using the Iridium
satellite network:
Press the TEL Key on the appropriate audio panel.
2)
Select the Dial Softkey on the MFD.
3)
Turn the small FMS Knob to select ‘Iridium’.
4)
Press the ENT Key. The cursor has now moved to the phone number entry field.
AFCS
1)
Hazard
Avoidance
With the ‘Aux-Telephone’ Page displayed, press the MENU Key on the MFD to
display the Page Menu.
Flight
Management
1)
Audio Panel
and CNS
Muting incoming call alerts:
EIS
Selecting the Ignore Softkey will extinguish the pop-up window and leave
the call unanswered. Selecting the TEL Softkey will display the ‘AuxTelephone’ Page allowing additional call information to be viewed before
answering.
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
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137
Figure 29 Enter Phone Number
5)
Enter the desired telephone number (country code first) by selecting the number
softkeys on the MFD or by pressing the numeric keys on the MFD Control Unit.
6)
Press the ENT Key. ‘OK’ is highlighted.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
7)
Additional
Features
Figure 30 Make the Call
Press the ENT Key. The system will begin calling the number.
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
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139
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Additional
Features
Figure 31 System is Making the Connection
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
When the phone is answered, the connection is established. To exit the call,
select the Hangup Softkey.
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Figure 32 Phone is Answered, Connection is Complete
Making an external call from the cockpit by using the
Contact List:
Press the TEL Key on the appropriate audio panel.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the small FMS Knob to select the desired contact name in the list of
contacts.
4)
Select the Call Softkey. The external call is initiated and the number associated
with the contact name is dialed.
Abnormal
Operation
1)
Annunciations
& Alerts
Appendix
Placing a call on hold:
Select the Hold Softkey on the MFD.
Or
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
141
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’.
3)
Press the ENT Key.
The cockpit phone is now isolated from the call. This figure illustrates a call
between the cockpit and an external phone in which the cockpit phone has
been put on hold. Select the Hold Softkey again to resume the call.
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Viewing the Text Messaging Page:
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the ‘Aux-Telephone’ or ‘Aux-Text Messaging’
Page.
3)
If necessary, select the SMS Softkey to display the ‘Aux-Text Messaging’ Page.
Index
Appendix
Annunciations
& Alerts
Figure 33 Cockpit Phone on Hold
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
Figure 34 Text Messaging Page
Description
AFCS
Message Symbol
Received text message that has not been opened
Received text message that has been opened
Additional
Features
Saved text message, draft not sent
Abnormal
Operation
System is sending text message
Text message has been sent
Annunciations
& Alerts
System failed to send text message
Predefined text message
Appendix
Text Message Symbols
Index
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143
Enabling/disabling incoming text message pop-up alerts:
1)
With the ‘Aux-Text Messaging’ Page displayed, press the MENU Key on the
MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Disable New Message Popups’ or
‘Enable New Message Popups’.
3)
Press the ENT Key. The pop-up alert will not be displayed when an incoming
text message is received.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Figure 35 Disabling New Text Message Pop-Ups
AFCS
Replying to a text message:
While viewing the text message, press the Reply Softkey.
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Reply To Message’.
3)
Press the ENT Key.
Sending a New Text Message:
1)
While viewing the ‘Aux-Text Messaging’ Page, press the New Softkey.
Or:
a)
Press the MENU Key to display the Page Menu.
b)
Turn either FMS Knob to place the cursor on ‘Draft New Message’.
c)
Press the ENT Key.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Or:
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Figure 36 Composing a New Text Message
Enter the desired message using any combination of entry methods as described
in step 2.
5)
Press the ENT Key.
6)
Confirm you wish to send the message by pressing the ENT Key with ‘Yes’
highlighted. Select ‘No’ to return to the message entry field and either select
the Cancel Softkey to delete the message or select the Save Softkey to save the
message as a draft.
190–02362–00 Rev. A
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145
Index
4)
Appendix
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
Annunciations
& Alerts
3)
Abnormal
Operation
The SMS Text Message Draft Window is now displayed with the cursor in the
‘To’ field. Enter the desired telephone number or email address. Entry can be
accomplished through the alphanumeric keys on the MFD Controller, or
combination of the FMS Knob on the controller and softkeys on the MFD. The
FMS Knob is used to enter letters and numbers, or numbers can be entered
from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to
create upper and lower case alpha characters. Special characters can be
accessed by pressing the Symbols Softkey.
Additional
Features
2)
Sending a New Text Message/Email to a Saved Contact:
1)
With the ‘Aux - Telephone’ Page displayed, press the FMS Knob to display the
cursor.
2)
Turn either FMS Knob to place the cursor on the desired contact name.
3)
Select either the Text Email Softkey to send to the email address saved for the
contact or Text Phone Softkey to send to the phone number saved for the
contact. The cursor is placed in the ‘To’ field. Confirm the contact you wish to
send a message to by pressing the ENT Key.
4)
Enter the desired message, then press the ENT Key.
5)
Confirm you wish to send the message by pressing the ENT Key with ‘Yes’
highlighted. Select ‘No’ to return to the message entry field and either select
the Cancel Softkey to delete the message or select the Save Softkey to save the
message as a draft.
Creating a predefined text message:
1)
While viewing the ‘Aux-Text Messaging’ Page, press the MENU Key to display
the Page Menu.
Figure 37 Creating/Editing Predefined Messages
2)
Turn either FMS Knob to select ‘Edit Predefined Messages’.
3)
Press the ENT Key. The Predefined Messages view is now displayed.
4)
Press the New Softkey.
Or:
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
146
a)
Press the MENU Key to display the Page Menu.
b)
Turn either FMS Knob to place the cursor on ‘Draft New Predefined
Message’.
c)
Press the ENT Key. The Predefined SMS Text Message Window is now
displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Figure 38 Composing a Predefined Message
7)
Enter the desired message using any combination of entry methods as described
in step 5.
8)
Press the ENT Key.
9)
Press the Save Softkey. The new predefined message is now shown in the
displayed list. Pressing the Cancel Softkey will delete the message without
saving.
Appendix
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
Annunciations
& Alerts
6)
Abnormal
Operation
The cursor is displayed in the ‘Title’ field. Enter the desired message title. Entry
can be accomplished through the alphanumeric keys on the MFD Controller, or
combination of the FMS Knob on the controller and softkeys on the MFD. The
FMS Knob is used to enter letters and numbers, or numbers can be entered
from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to
create upper and lower case alpha characters. Special characters can be
accessed by pressing the Symbols Softkey.
Additional
Features
5)
10) Press the MENU Key to display the Page Menu.
Index
11) Turn either FMS Knob to place the cursor on ‘Cancel Drafting Message’.
12) Press the ENT Key.
190–02362–00 Rev. A
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147
Sending a predefined text message:
1)
While viewing the ‘Aux-Text Messaging’ Page, press the New Softkey.
2)
The Predefined SMS Text Message Window is now displayed with the cursor in
the ‘To’ field. Enter the desired telephone number or email address. Entry can be
accomplished through the alphanumeric keys on the MFD Controller, or
combination of the FMS Knob on the controller and softkeys on the MFD. The
FMS Knob is used to enter letters and numbers, or numbers can be entered
from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to
create upper and lower case alpha characters. Special characters can be
accessed by pressing the Symbols Softkey.
3)
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
4)
Press the Predefined Softkey. The Predefined Message Menu Window is
displayed.
5)
Turn either FMS Knob to select the desired predefined message.
6)
Press the ENT Key. The predefined message text is inserted into the message
field. If desired, the message can be edited by using the FMS Knobs.
7)
Press the ENT Key.
8)
Press the Send Softkey to transmit the message.
Show Inbox messages:
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Inbox Softkey.
Or:
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at the
bottom left of the list window.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
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Additional Features
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
Figure 39 Text Message Inbox
Show Outbox messages:
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at the
bottom left of the list window.
Abnormal
Operation
1)
Additional
Features
Or:
Show Draft messages:
Or:
2)
Turn either FMS Knob to place the cursor on ‘Show Draft Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at the
bottom left of the list window.
Appendix
Press the MENU Key to display the Page Menu.
Annunciations
& Alerts
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Drafts Softkey.
1)
AFCS
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Outbox Softkey.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
149
Flight
Instruments
Additional Features
Viewing messages sorted by message date/time:
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Time Softkey.
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center of the
list window.
Viewing messages sorted by message type:
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Type Softkey.
Or:
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Type’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center of the
list window.
Viewing messages sorted by address:
While viewing the ‘Aux-Text Messaging’ Page, press the Arrange Softkey, then
press the Address Softkey.
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Or:
Or:
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Address’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center of the
list window..
Viewing the content of a text message:
1)
While viewing the ‘Aux-Text Messaging’ Page, select the desired message box.
2)
Press the FMS Knob to activate the cursor.
3)
Turn either FMS Knob to select the desired message.
4)
Press the View Softkey.
Index
Or:
Press the ENT Key.
Or:
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
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Additional Features
Press the MENU Key to display the Page Menu.
b)
Turn either FMS Knob to place the cursor on ‘View Selected Message’.
c)
Press the ENT Key.
Flight
Instruments
a)
Message content is displayed.
EIS
5)
To close the text message, press the Close Softkey.
Or:
Press the MENU Key to display the Page Menu.
b)
Turn either FMS Knob to place the cursor on ‘Close Message’.
c)
Press the ENT Key.
Audio Panel
and CNS
a)
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the FMS Knob
to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the MRK Read Softkey.
Hazard
Avoidance
1)
Flight
Management
Marking selected message as read:
Or:
AFCS
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Mark Selected Message As Read’.
3)
Press the ENT Key.
Additional
Features
1)
The message symbol now indicates the message has been opened.
Marking all messages as read:
Abnormal
Operation
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the MENU
Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Mark All New Messages As Read’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With cursor highlighting ‘YES’, press the ENT Key. The message symbols now
indicate all the message have been opened.
Annunciations
& Alerts
1)
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the FMS Knob
to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the Delete Softkey.
Index
1)
Or:
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Appendix
Deleting a message:
151
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Delete Selected Message’.
3)
Press the ENT Key.
CONNEXT SETUP
The Connext Setup Page allows for setting up the installed optional Flight Stream device
for a Bluetooth connection between the system and a mobile device running the Garmin
Pilot™ application.
The mobile device must be ‘paired’ with the system in order to use the various functions.
Pairing is accomplished by first placing the system in pairing mode by displaying the
Connext Setup Page. The system is ‘discoverable’ whenever this page is displayed. The
pairing operation is completed from the mobile device and the Garmin Pilot application. See
the device Bluetooth pairing instructions and the connection instructions in the Garmin Pilot
application.
Viewing the Connext Setup Page:
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the Connext Setup page.
Changing the Bluetooth Name:
1)
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘Bluetooth Name’ field.
3)
Enter the desired name by using the large FMS Knob to select the character
field, and the small FMS Knob select the desired alphanumeric character for
that field.
4)
Press the ENT Key. The cursor is removed and the new name is displayed.
Enabling/Disabling Flight Plan Importing from Garmin
Pilot:
1)
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘Flight Plan Import’ field.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
4)
Press the FMS Knob to remove the cursor.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
152
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Additional Features
2)
Turn the large FMS Knob to place the cursor in the ‘WiFi Database Import’ field.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
4)
Press the FMS Knob to remove the cursor.
Audio Panel
and CNS
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
Enabling/Disabling Automatic Reconnection of a Specific
Paired Device:
Flight
Management
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to highlight the desired paired device.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’. Selecting ‘Enabled’
allows the system to automatically connect to a previously paired device when
detected.
4)
Press the FMS Knob to remove the cursor.
AFCS
Remove a Specific Paired Device from the List of Paired
Devices:
Turn the large FMS Knob to highlight the desired paired device.
3)
Press the Remove Softkey. A confirmation screen is displayed.
4)
If necessary, turn the large FMS Knob to select ‘Yes’.
5)
Press the ENT Key to remove the device from the list of paired devices.
Abnormal
Operation
2)
Additional
Features
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
Annunciations
& Alerts
SURFACEWATCH
Inhibit/Uninhibit SurfaceWatch:
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the SurfaceWatch field.
4)
Turn the small FMS Knob to toggle the SurfaceWatch alerts on or off.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Select the ‘Aux - System Setup 1’ Page.
Appendix
1)
Hazard
Avoidance
1)
1)
EIS
1)
Flight
Instruments
Enabling/Disabling WiFi Database Importing from Garmin
Pilot:
153
Entering Origin/Destination Airport:
1)
Select the ‘FPL - SurfaceWatch Setup’ Page.
2)
Press the FMSKnob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob if necessary to highlight the Origin or Destination
Airport field.
4)
Use the FMS Knobs to input the desired Origin or Destination Airport.
Selecting Origin/Destination Runway:
1)
Select the ‘FPL - SurfaceWatch Setup’ Page.
2)
Press the FMSKnob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob if necessary to highlight the Runway or Landing
Runway field.
4)
Turn the small FMS Knob to select the desired available Runway or Landing
Runway. As the small FMS Knob is turned, the preview of the selected runway
or landing runway is also displayed.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
1)
Select the ‘FPL - SurfaceWatch Setup’ Page.
2)
Press the FMSKnob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob if necessary to highlight the ‘REQD Takeoff DIS’ or
‘REQD Landing DIS’ field.
4)
Use the FMS Knobs to enter the required takeoff or landing distance. Upon
pressing the FMS Knob and committing the required takeoff or landing
distance, the Runway Length field will turn amber if an insufficient runway
length exists.
Abnormal
Operation
Additional
Features
AFCS
Selecting Required Takeoff/Landing Distance:
Index
Appendix
Annunciations
& Alerts
ELECTRONIC STABILITY & PROTECTION (ESP)
Electronic Stability and Protection (ESP™) is an optional feature that is intended to
discourage the exceedance of attitude and established airspeed parameters. This feature will
only function when the aircraft is above 200 feet AGL and the autopilot is not engaged.
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo, Mmo,
and/or angle of attack) beyond the normal flight parameters. Enhanced stability for each
condition is provided by applying a force to the appropriate control surface to return the
aircraft to the normal flight envelope. This is perceived by the pilot as resistance to control
movement in the undesired direction when the aircraft approaches a steep attitude, high
airspeed, or when a stall is imminent.
As the aircraft deviates further from the normal attitude, angle of attack, or airspeed
continues to increase, the force increases (up to an established maximum) to encourage
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Additional Features
Audio Panel
and CNS
Flight
Management
The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering
(CWS) or Autopilot Disconnect (AP/YD DISC TRIM INTRPT) switch. Upon releasing the
CWS or AP/YD DISC TRIM INTRPT switch, ESP force will again be applied, provided
aircraft attitude, angle of attack and/or airspeed are within their respective engagement
limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit.
EIS
When ESP has been engaged for more than ten seconds (cumulative; not necessarily
consecutive seconds) of a 20-second interval, the autopilot is automatically engaged with the
flight director in Level Mode, bringing the aircraft into level flight. An aural “Engaging
Autopilot” alert is played and the flight director mode annunciation will indicate ‘LVL’ for
vertical and lateral modes.
Flight
Instruments
control movement in the direction necessary to return to the normal attitude and/or airspeed
range. Except in the case of high airspeed, when maximum force is reached, force remains
constant up to the maximum engagement limit. Above the maximum engagement limit,
forces are no longer applied. There is no maximum engagement related to a high airspeed
condition.
ESP can be enabled or disabled on the ‘Aux-System Setup 2’ Page on the MFD.
Hazard
Avoidance
ESP is automatically enabled on system power up.
Enabling/Disabling ESP:
Turn the large FMS Knob to select the Aux Page Group.
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, select the SETUP 2 Softkey to display the Aux-System Setup 2
Page. If the Aux-System Setup 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the Stability & Protection field.
6)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
7)
Press the FMS Knob to remove the cursor.
AFCS
1)
Abnormal
Operation
2)
Turn the large FMS Knob to select the ‘Group’ field.
3)
Turn the small FMS Knob to select the desired procedure and press the ENT
Key.
4)
Turn the large FMS Knob to select the ‘Checklist’ field.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
From any page on the MFD (except the EIS Pages), press the Checklist Softkey
or turn the large FMS Knob to select the Checklist Page.
Appendix
1)
Annunciations
& Alerts
Accessing and Navigating Checklist
190–02362–00 Rev. A
Additional
Features
ELECTRONIC CHECKLISTS
155
5)
Turn the FMS Knob to select the desired checklist and press the ENT Key. The
selected checklist item is indicated with white text surrounded by a white box.
6)
Press the ENT Key or Check Softkey to check the selected checklist item. The
line item turns green and a checkmark is placed in the associated box. The next
line item is automatically selected for checking.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Press the CLR Key or Uncheck Softkey to remove a check mark from an item.
7)
When all checklist items have been checked, ‘*Checklist Finished*’ is displayed
in green text at the bottom left of the checklist window. If all items in the
checklist have not be checked, ‘*Checklist Not Finished*’ will be displayed in
yellow text.
8)
Press the ENT Key. ‘Go To Next Checklist?’ will be highlighted by the cursor.
9)
Press the ENT Key to advance to the next checklist.
10) Press the Exit Softkey to exit the Checklist Page and return to the page last
viewed.
1)
From any page on the MFD (except the EIS Pages), press the Checklist Softkey
or turn the large FMS Knob to select the Checklist Page.
2)
Press the EMER Softkey.
3)
Turn the FMS Knob to select the desired emergency checklist and press the ENT
Key.
4)
Press the ENT Key or Check Softkey to check the selected emergency checklist
item. The line item turns green and a checkmark is placed in the box next to it.
The next line item is automatically highlighted for checking.
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Press the CLR Key or Uncheck Softkey to remove a check mark from an item.
5)
When all checklist items have been checked, ‘*Checklist Finished*’ is displayed
in green text at the bottom left of the checklist window. If all items in the
checklist have not be checked, ‘*Checklist Not Finished*’ will be displayed in
yellow text.
6)
Press the ENT Key. ‘Go To Next Checklist?’ will be highlighted by the cursor.
7)
Press the ENT Key to advance to the next checklist.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Accessing Emergency Checklist
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Additional Features
Press the Return Softkey to return to the previous checklist.
9)
Press the Exit Softkey to exit the Checklist Page and return to the page last
viewed.
Flight
Instruments
8)
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
157
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Additional Features
BLANK PAGE
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Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Audio Panel
and CNS
System Power-up
EIS
This section discusses powering up the system, normal and reversionary display
operation, annunciations, system status, air data and attitude heading reference system
(AHRS) modes of operation, and GPS receiver operation.
NOTE: See the Pilot’s Operating Handbook (POH) for specific procedures
concerning avionics power application and emergency power supply operation.
Additional
Features
When the MFD powers up, the MFD Power-up Page displays the following
information:
AFCS
When powering up the system, test annunciations are displayed and key annunciator
lights also become momentarily illuminated on the audio panel and the display bezels. On
the PFD, the AHRS begins to initialize and an alignment message is displayed. All system
annunciations should disappear typically within one minute of power-up.
Hazard
Avoidance
The system is integrated with the aircraft electrical system and receives power directly
from electrical busses. The PFD, MFD, and supporting sub-systems include both poweron and continuous built-in test features that exercise the processor, RAM, ROM, and
external inputs and outputs to provide safe operation.
Flight
Management
NOTE: See the Appendices for additional information regarding system-specific
annunciations and alerts.
• System version
Abnormal
Operation
• Checklist File
• Land database name and version
Annunciations
& Alerts
• Safe Taxi database name and effective dates
• Terrain database name and version
• Obstacle database name and effective dates
Appendix
• Navigation database name and effective dates
• Airport Directory name and effective dates
• FliteCharts/ChartView database information
Index
• IFR/VFR charts database information
• Crew Profile
• Copyright
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
159
Flight
Instruments
Abnormal Operation
Current database information includes the valid operating dates, cycle number and
database type. When this information has been reviewed for currency (to ensure that no
databases have expired), the pilot is prompted to continue.
NOTE: In normal operating mode, backlighting can only be adjusted from the
PFD. In reversionary mode, it can be adjusted from the remaining display. (See
the Display Backlighting chapter for more information)
In normal operating mode, the PFD presents graphical flight instrumentation (attitude,
heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument
cluster. The MFD normally displays a full-color moving map with navigation information,
while the left portion of the MFD is dedicated to the Engine Indication Syste. Both
displays offer control for COM and NAV frequency selection.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Normal Operation
AFCS
PFD1
PFD2
Figure 40 Normal Operation
NOTE: The system alerts the pilot when backup paths are utilized by the LRUs.
Refer to the Appendices for further information regarding system-specific alerts.
Reversionary mode is a mode of operation in which all important flight information is
presented identically on at least one of the remaining displays. Transition to reversionary
mode should be straightforward for the pilot, for flight parameters are presented in the same
format as in normal mode.
Appendix
Abnormal
Operation
Reversionary Mode
Annunciations
& Alerts
Additional
Features
MFD
In the event of an MFD failure, the system automatically switches to reversionary
(backup) mode. In reversionary mode, all important flight information is presented on the
remaining display(s) in the same format as in normal operating mode.
Index
• PFD1 Failure — MFD and PFD2 remain in normal mode.
• MFD failure – Both PFDs automatically switch to reversionary mode.
• PFD2 failure – MFD and PFD1 remain in normal mode.
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Abnormal Operation
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Figure 41 Reversionary Mode
Hazard
Avoidance
Reversionary mode can be activated manually by pressing a dedicated reversionary switch
installed in the cockpit. Pressing this switch again deactivates reversionary mode.
Each display can be configured to operate in reversionary mode, as follows:
• PFD1 – By pressing the left reversionary switch.
AFCS
• MFD – By pressing the left or right reversionary switch.
• PFD2 – By pressing the right reversionary switch.
Annunciations
& Alerts
Appendix
ABNORMAL COM OPERATION
COM Tuning Failure
161
Index
In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is
automatically tuned in the radio in which the tuning failure occurred. Depending on the
failure mode, a red X may appear on the frequency display.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Abnormal
Operation
Figure 42 Inoperative Input (NAV1 Shown)
190–02362–00 Rev. A
Additional
Features
Should the connection between a PFD and the GIA functions become inoperative, the GIA
can no longer communicate with the PFD (refer to Figure 1-1). As a result, the NAV and
COM functions provided to the failed PFD or MFD by the GIA are flagged as invalid (red
“X”) on the remaining PFD. The system reverts to backup paths for the AHRS, ADC, Engine/
Airframe Unit, and Transponder, as required. The change to backup paths is completely
automated for all LRUs and no pilot action is required.
FLIGHT INSTRUMENTS
Abnormal GPS Conditions
The annunciations listed in Table 2-4 can appear on the HSI when abnormal GPS
conditions occur. Refer to the Flight Management Section for more information on Dead
Reckoning Mode.
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Abnormal Operation
Annunciation
Location
GPS LOI
Right of HSI
Loss of Integrity Monitoring–GPS
integrity is insufficient for the
current phase of flight
Right of HSI
Integrity OK–GPS integrity has been
restored to within normal limits
(annunciation displayed for 5
seconds)
Lower left of aircraft
symbol if HSI Map is
disabled, or on
aircraft icon if HSI
Map enabled
Dead Reckoning–System is using
projected position rather than GPS
position to compute navigation
data and sequence active flight plan
waypoints
AFCS
Hazard
Avoidance
GPS
INTEG OK
Description
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Table 5 Abnormal GPS Conditions Annunciated on HSI
Figure 43 Example HSI Annunciations
In Dead Reckoning Mode, the CDI is removed (when FMS is the selected navigation
source), and the following items on the PFD are then shown in amber:
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Abnormal Operation
Flight
Instruments
• Current Track Bug
• Wind Data
• Distances in the Bearing Information windows
EIS
• FMS bearing pointers
These items should be verified when operating in Dead Reckoning Mode and they
become increasingly inaccurate over time.
Flight
Management
The Comparator monitors critical values generated by redundant sensors. If differences
in the sensors exceed a specified amount, a miscompare annunciation is displayed in
black text on an amber background. If one or both of the sensed values are unavailable, a
no compare annunciation is displayed with black text on a white background. Refer to the
Appendix A for more information on alerts and annunciations.
Audio Panel
and CNS
Comparator Annunciations
Miscompa re Annunci ations
Hazard
Avoidance
AFCS
No Compa re
Annunci ations
Additional
Features
Annunciation
HDG
190–02362–00 Rev. A
If either airspeed sensor detects > 35 knots, and the
difference in sensors is > 10 knots
If either airspeed sensor detects > 80 knots, and the
difference in sensors is > 7 knots.
Difference in heading sensors is > 6 degrees.
Difference in pitch sensors is > 5 degrees.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
PIT
Difference in altitude sensors is > 200 ft.
Appendix
IAS
Condition
Annunciations
& Alerts
ALT
Abnormal
Operation
Figure 44 Sensor Comparator Annunciations
163
Abnormal Operation
Flight
Instruments
Annunciation
Condition
Difference in roll sensors is > 6 degrees.
ROL
No data from one or both altitude sensors.
EIS
ALT
No data from one or both airspeed sensors.
Audio Panel
and CNS
IAS
Flight
Management
Hazard
Avoidance
No data from one or both pitch sensors.
PIT
No data from one or both roll sensors.
ROL
Reversionary Sensor Annunciations
Reversionary sensor selection is annunciated on the upper left center of the PFD. These
annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the PFD
Opt Softkey accesses the Sensors Softkey. Pressing the Sensors Softkey accesses the ADC
and AHRS softkeys These softkeys allow switching of the sensors being viewed on each
PFD. With certain types of sensor failures, the system may make some sensor selections
automatically. The FMS sensor cannot be switched manually.
Abnormal
Operation
Additional
Features
AFCS
No data from one or both heading sensors.
HDG
Figure 45 Reversionary Sensor Annunciations
Annunciations
& Alerts
Reversionary Sensor
Window Text
Appendix
BOTH ON ADC1
BOTH ON ADC2
Index
BOTH ON AHRS1
BOTH ON AHRS2
164
Condition
Both PFDs are displaying data from ADC1.
Both PFDs are displaying data from ADC2
Both PFDs are displaying data from AHRS1.
Both PFDs are displaying data from AHRS2
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Abnormal Operation
BOTH
ON GPS1
Both PFDs are displaying data from GPS1.
EIS
BOTH
ON GPS2
Condition
Flight
Instruments
Reversionary Sensor
Window Text
Both PFDs are displaying data from GPS2.
PFD1 is displaying data from ADC2. Shown while PFD2
is displaying data from ADC1.
USING AHRS1
PFD2 is displaying data from AHRS1. Shown while PFD1
is displaying data from AHRS2.
USING AHRS2
PFD1 is displaying data from AHRS2. Shown while PFD2
is displaying data from AHRS1.
USING
GPS1
PFD1 is displaying data from the #2 GPS.
AFCS
USING
GPS2
PFD2 is displaying data from the #1 GPS.
Hazard
Avoidance
USING ADC2
Flight
Management
PFD2 is displaying data from ADC1. Shown while PFD1
is displaying data from ADC2.
Audio Panel
and CNS
USING ADC1
SVT becomes disabled without the following data resources:
Abnormal
Operation
SVT is intended to be used with traditional attitude, heading, obstacle, terrain, and
traffic inputs. SVT is disabled when valid attitude or heading data is not available for the
display. In case of invalid SVT data, the PFD display reverts to the standard blue-overbrown attitude display.
Additional
Features
SVT Troubleshooting
• Attitude data
Annunciations
& Alerts
• Heading data
• GPS position data
• 4.9 Arc-second Terrain data
Appendix
• Obstacle data
• TAWS function is not available, in test mode, or failed
• The position of the aircraft exceeds the range of the terrain database.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
165
SVT in Reversionary Mode
SVT can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is
enabled when switching to Reversionary Mode, SVT will take up to 30 seconds to be
displayed. The standard, non-SVT PFD display will be shown in the interim.
Unusual Attitudes
When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the
horizon warn of extreme pitch. The chevrons are displayed on the Attitude Indicator,
starting at 50˚ above and 30˚ below the horizon line.
Nose High
Nose Low
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Abnormal Operation
If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD
is removed. The Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal
Situation indicators remain on the display and the Bearing Information, Alerts, and
Annunciation windows can be displayed during such situations. The following
information is removed from each PFD and their softkeys are disabled when the aircraft
experiences unusual attitudes:
Traffic Annunciations
System Time
Minimum Descent
Altitude/Decision Height
readout
AFCS Annunciations
PFD Setup Menu
Vertical Deviation,
Glideslope, and Glidepath
Indicators
Inset Map
Windows displayed in the
lower right corner of the
PFD:
Altimeter Barometric
Setting
Outside Air Temperature
(OAT)
— References Window
Selected Altitude
ISA temperature deviation
— Nearest Airports
VNV Target Altitude
Wind data
— Flight Plan
Ground Speed
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Figure 46 Pitch Attitude Warnings with SVT Disabled
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Abnormal Operation
— Messages
Selected Course readout
— Procedures
True Airspeed
Flight
Instruments
Selected Heading readout
Transponder Status Box
EIS
SVT Unusual Attitudes
Flight
Management
Blue Band
Audio Panel
and CNS
During extreme pitch attitudes, the display shows either a brown or blue colored bar at
the top or bottom of the screen to represent earth or sky. The blue colored bar is also
displayed when terrain gradient is great enough to completely fill the display. This is
intended to prevent losing sight of the horizon during extreme pitch attitudes.
Hazard
Avoidance
Terrain
Comple tely
Fills Display
AFCS
Additional
Features
Figure 47 Blue Sky Bar with Synthetic Terrain Enabled
This section discusses the Dead Reckoning mode of operation and the subsequent
indications.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
167
Index
It is important to note that estimated navigation data supplied by the system in DR Mode
may become increasingly unreliable and must not be used as a sole means of navigation. If
Appendix
While in Enroute or Oceanic phase of flight, if the system detects an invalid GPS solution
or is unable to calculate a GPS position, the system automatically reverts to Dead Reckoning
(DR) Mode. In DR Mode, the system uses its last-known position combined with
continuously updated airspeed and heading data (when available) to calculate and display
the aircraft’s current estimated position.
Annunciations
& Alerts
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN)
phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS
POSITION” annunciation on the map and the system stops using GPS.
Abnormal
Operation
DEAD RECKONING
while in DR Mode airspeed and/or heading data is also lost or not available, the DR function
may not be capable of accurately tracking estimated position and, consequently, the system
may display a path that is different than the actual movement of the aircraft. Estimated
position information displayed by the system through DR while there is no heading and/or
airspeed data available should not be used for navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the lack of
satellite measurements needed to determine a position. Changes in wind speed and/or wind
direction compound the relative inaccuracy of DR Mode. Because of this degraded accuracy,
other navigation equipment must be relied upon for position awareness until GPS-derived
position data is restored.
DR Mode is indicated on the system by the appearance of the letters ‘DR’ superimposed in
amber over the ‘own aircraft’ symbol. In addition, ‘DR’ is prominently displayed in amber on
the HSI slightly below and to the left of the aircraft symbol on the CDI. The CDI deviation
bar remains, but is removed from the display after 20 minutes in DR Mode. The autopilot
will remain coupled in DR mode as long as the deviation info is available (20 min.)
Furthermore, a ‘GPS NAV LOST’ alert message appears on the PFD. Normal navigation using
GPS/SBAS source data resumes automatically once a valid GPS solution is restored.
As a result of operating in DR Mode, all GPS-derived data is computed based upon an
estimated position and is displayed as amber text on the display to denote degraded
navigation source information as shown in the following figure. If the VSD Inset is selected
on the MFD, ‘VSD Not Available’ will be displayed.
Also, while the system is in DR Mode, some terrain functions are not available.
Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is
questionable. Finally, airspace alerts continue to function, but with degraded accuracy.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Abnormal Operation
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Abnormal Operation
Flight
Instruments
Distance &
Bearing
EIS
Current
Track
Indicator
Audio Panel
and CNS
Course Deviation
Indicator
GPS Navigation
Lost Message
Flight
Management
Dead Reckoning
Annunciation
Hazard
Avoidance
Nav Data Bar
AFCS
All data except
Active Leg, TAS,
and DTK are in
amber
Additional
Features
Dead Reckoning
Annunciation
Abnormal
Operation
Annunciations
& Alerts
Figure 48 Dead Reckoning Mode - GPS Derived Data Shown in Amber
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
169
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Abnormal Operation
BLANK PAGE
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Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
SYSTEM ANNUNCIATIONS
EIS
System Annunciations
NOTE: Upon power-up, certain windows remain invalid as system equipment
begins to initialize. All windows should be operational within one minute of
power-up. If any window continues to remain flagged, the system should be
serviced by a Garmin-authorized repair facility.
Audio Panel
and CNS
When an LRU or an LRU function fails, a large red or amber “X” is typically displayed
on windows associated with the failed data. Refer to the Pilot’s Operating Handbook
(POH) for additional information regarding pilot responses to these annunciations.
Flight
Management
NOTE: Refer to the POH for additional information regarding pilot responses to
these annunciations.
Hazard
Avoidance
System Annunciation
Comment
AFCS
Air Data, Attitude and Heading Reference System is
aligning.
Additional
Features
Abnormal
Operation
Display system is not receiving attitude information
from the AHRS (GRS unit).
Appendix
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
GPS information is either not present or is invalid for
navigation use. Note that AHRS utilizes GPS inputs
during normal operation. AHRS operation may be
degraded if GPS signals are not present (see POH).
190–02362–00 Rev. A
Annunciations
& Alerts
AHRS calibration incomplete or configuration module
failure.
171
Annunciations & Alerts
Flight
Instruments
System Annunciation
Comment
Audio Panel
and CNS
EIS
Display system is not receiving airspeed input from the
air data computer.
Flight
Management
Display system is not receiving valid heading input
from the AHRS or magnetometer.
Hazard
Avoidance
Display system is not receiving vertical speed input
from the air data computer.
Display system is not receiving altitude input from the
AHRS or magnetometer.
AFCS
Display system is not receiving valid OAT information
from the air data computer.
Additional
Features
Display system is not receiving valid ISA information
from the air data computer.
Display system is not receiving valid transponder
information.
A red ‘X’ through any other display field (such as
engine instrumentation fields) indicates that the field is
not receiving valid data.
Table 6 System Annunciations
CAS MESSAGES
CAS Message Prioritization
NOTE: Refer to the Pilot’s Operating Handbook (POH) for corrective pilot
actions.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Other Various Amber/Red
X Indications
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Annunciations & Alerts
appears on the CAS display, it is shown in black on white inverse video in conjunction
with the Advisory Softkey (see Figure 59) and may be accompanied by a single chime.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
173
Index
190–02362–00 Rev. A
Appendix
Some CAS messages can be display in more than one alert level group. For example, a
message might display as both a warning and a caution, but cannot appear more than
once at any given time (unless the CAS is being tested). If the received signals justify
multiple priorities for a certain message, the message is displayed for the higher priority
condition. When graduating to a higher priority, the message flashes and requires new
acknowledgment. When degrading to a lower priority condition, the message moves to
the top of the appropriate grouping, but does not require new acknowledgment.
Annunciations
& Alerts
• Advisory: This level of alert provides general information. When a new white advisory
Abnormal
Operation
aircraft that may require intervention. When a new caution message appears in the CAS
Window, it is shown in black on amber inverse video in conjunction with the Caution
Softkey (see Figure 59) and may be accompanied by a double chime. Pressing the
Caution Softkey Indicator acknowledges all amber messages and extinguishes the
softkey. Once acknowledged, caution messages are displayed until the issue is
corrected.
Additional
Features
• Caution: This level of alert indicates the existence of abnormal conditions on the
AFCS
message appears in the CAS Window, it flashes (inversely red on white) in conjunction
with the Warning Softkey (see Figure 59) and may be accompanied by a repeating triple
chime. Pressing the Warning Softkey acknowledges all flashing warning messages and
extinguishes the softkey. Once acknowledged, warning messages are shown in red text
and are displayed until the issue is corrected. Warning voice alerts repeat continuously
until acknowledged by pressing the Warning Softkey.
Hazard
Avoidance
• Warning: This level of alert requires immediate attention. When a new warning CAS
Flight
Management
NOTE: Aural alerts associated with abnormal conditions and advisories are
managed through the audio panels. Refer to the Audio Panel and CNS Section
for more information.
Audio Panel
and CNS
The Crew Alerting System (CAS) Window is located on the right side of the PFD.
Warning messages cannot be scrolled through and remain at the top of the CAS display.
The scroll bar appears if more caution and advisory messages exist than can be displayed
at once or if messages have been scrolled off the display. The CAS softkeys also become
available.
EIS
The Alerting System uses three alert levels. Messages are grouped by criticality
(warning, caution, advisory) and sorted by order of appearance (most recent messages on
top). The color of the message is based on its urgency and on required action.
Flight
Instruments
NOTE: Any CAS messages that are generated when the system is first powered
on are considered already acknowledged. They do not flash or trigger the
Warning or Caution softkeys.
Flight
Instruments
Annunciations & Alerts
Flight
Management
Audio Panel
and CNS
EIS
CAS
Window
Hazard
Avoidance
Softkey
Annunci ation
AFCS
Figure 49 CAS Message Prioritization
Figure 50 Softkey Annunciation (Message Softkey Labels)
Additional
Features
CAS Annunciations
Abnormal
Operation
The following annunciations are configured specifically for the Piper Archer. Red
annunciation window text signifies warnings, amber signifies cautions, and white
signifies advisories. See the POH for recommended pilot actions.
Display Inhibits
Annunciations
& Alerts
Inhibits prevent certain CAS messages from being displayed during the following
conditions:
If two alert levels of the same message are active simultaneously (e.g., L FUEL QTY
warning and L FUEL QTY caution) only the higher alert level is displayed.
Index
Appendix
If a GEA or GIA fails, all CAS messages depending on sensors associated with that
LRU are automatically inhibited. Inhibits cannot be activated by invalid sensor data.
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Annunciations & Alerts
Annunciation Text
Flight
Instruments
Warning Messages
Description
Alternator 1 has failed
ALTR 2 FAIL
Alternator 2 has failed
AUTO DESCENT has been active for 60 seconds,
EDM activated. Repeating double chime. ‘AUTO
DESCENT - Aircraft descending to 14,000FT’ in
Messages Window.
AUTO DESCENT
No interaction detected for four minutes after
aircraft reaches 14,000 feet. Repeating double
chime. ‘AUTO DESCENT - Aircraft descending to
12,500FT’ in Messages Window.
CABIN ALT 10K
Cabin altitude above 10,000 feet
Hazard
Avoidance
AUTO DESCENT
Flight
Management
HYPOXIA ALERT has been active for 60 seconds,
aircraft will begin descent in 60 seconds. Double
chime. ‘AUTO DESCENT - Automatic descent to
14,000FT in 60 seconds’ in Messages Window.
Audio Panel
and CNS
AUTO DESCENT
EIS
ALTR 1 FAIL
CO LVL HIGH
Carbon monoxide level is high
DOOR AJAR
Forward baggage door or cabin door is not closed
Fuel pressure is low
L FUEL QTY LOW
Left fuel quantity is in warning range
R FUEL QTY LOW
Right fuel quantity is in warning range
A component of the gear system has failed
PITOT HEAT FAIL
Pitot heat left and/or right failed
SPDBRAKES EXTD
Speedbrakes extended during takeoff
Underspeed protection is active
Appendix
USP ACTIVE
Annunciations
& Alerts
GEAR SYS
WDSHLD
OVRTMP
Abnormal
Operation
FUEL PRESS LOW
Additional
Features
Landing gear not down and locked, or landing gear
selected UP when on ground
AFCS
CHECK GEAR
Windshield heater over-temperature or controller
malfunction
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
175
Annunciations & Alerts
Flight
Instruments
Caution Messages
Audio Panel
and CNS
EIS
Annunciation Text
BOOST PUMP
FAIL
Boost pump failed
CHECK GEAR
Landing gear not down and locked
CO LVL HIGH
Carbon monoxide level is high
CPCS FAIL
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
CPCS FAULT
Cabin Pressure Controller has failed or lost ARINC
communication on the ground
Cabin Pressure Controller has lost ARINC
communication
FLAP FAIL
A flap system failure has occurred
FUEL IMBALANCE
Fuel imbalance is over 10.7 gallons
GEAR SYS
A component of the gear system has failed
HYDR PUMP ON
Hydraulic pump is on and should not be on
HYPOXIA ALERT
ARE YOU ALERT? has been active for 60 seconds
OXYGEN GEN ON
Oxygen generation system has been turned on
L PITOT HT FAIL
Left pitot heat has failed
R PITOT HT FAIL
Right pitot heat has failed
PITOT HEAT OFF
Pitot heat selected off
PROP HEAT FAIL
Propeller heat failure
SPDBRAKES EXTD
Speedbrakes extended during landing, or in flight
with engine off or being started
STALL HEAT FAIL
Stall heat selected on and OAT is equal to or less
than 5° C, but has not been activated
STALL WARN FAIL
Failure detected in stall warning system
START ENGAGED
Starter engaged when engine is running
SURF DEICE FAIL
Surface de-ice fail
VAC PRESS LOW
Vacuum system pressure abnormal
Index
Appendix
Description
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Annunciations & Alerts
Annunciation Text
ARE YOU ALERT?
Description
A period of inactivity exceeding limits has been
detected
AV2 FAN FAIL
Avionics 2 forward cooling fan has failed
AV3 FAN FAIL
Avionics 3 forward cooling fan has failed
Audio Panel
and CNS
Avionics 1 forward cooling fan has failed
EIS
AV1 FAN FAIL
DOOR AJAR
Flight
Instruments
Advisory Messages
Forward baggage door or cabin door is not closed
Emergency fuel on
FUEL IMBALANCE
Fuel imbalance is over 10.7 gallons
L FUEL QTY LOW
Left fuel quantity is in advisory range
R FUEL QTY LOW
Right fuel quantity is in advisory range
MAINT MODE ON
The maintenance mode is active
AFCS
EMERG FUEL ON
Hazard
Avoidance
Emergency fuel off
Flight
Management
EMERG FUEL OFF
The cooling fan for the MFD has failed
PFD1 FAN FAIL
The cooling fan for PFD1 has failed
PFD2 FAN FAIL
PFD2 FAN FAIL The cooling fan for PFD2 has failed
SPDBRAKES EXTD
Speedbrakes extended while on ground, or in flight
with engine running
STALL HEAT INHIB
Stall heat selected on and OAT is greater than 5° C,
but has not been activated
Normal surface de-ice cycle is active
VACUUM 1 FAIL
Vacuum pump 1 failure
VACUUM 2 FAIL
Vacuum pump 2 failure
Appendix
SURF DEICE ON
Annunciations
& Alerts
Stall heat is on
Abnormal
Operation
STALL HEAT ON
Additional
Features
MFD FAN FAIL
Index
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177
GARMIN CONNEXT WEATHER REQUEST STATUS
Abnormal Operations for Garmin Connext Weather
If the system cannot complete a Connext Data Request, one or more messages will
appear in the Request Status Window.
Weather Request
Status Message
Annunciations
& Alerts
Appendix
Index
178
Description
Auto requests inhibited
Send manual request to
reset.
The system has disabled automatic weather data
requests due to excessive errors. Automatic weather
data requests have stopped. Send a manual weather
data request to resume automatic updates.
Auto update retry: ##
Seconds
The system will attempt another automatic weather
data request after an error occurred during the previous
request. Timer counts down until the next automatic
request occurs.
Connext Comm Error
[1]
A general error has occurred. If the error persists, the
system should be serviced.
Connext Comm Error
[2]
A communications error has occurred. The system
should be serviced if this error persists.
Connext Comm Error
[3]
A general error has occurred. If the error persists, the
system should be serviced.
Connext Comm Error
[4]
This occurs if multiple automatic weather data requests
have recently failed, or the an LRU is off-line.
Connext Comm Error
[5]
This can occur if an LRU is off-line or not configured, or
the Iridium or Garmin Connext services are not
accessible. Check Iridium signal strength. If this error
persists, the system should be serviced.
Connext Comm Error
[6]
A communications error has occurred. It this error
persists, the system should be serviced.
Connext Comm Error
[7]
A weather data transfer has timed out. Check Iridium
signal strength and re-send the data request.
Connext Comm Error
[8]
A server error has occurred or invalid data received.
Connext Comm Error
[9]
An error occurred while reading or writing data. If the
error persists, the system should be serviced.
Connext Login Invalid
There is a problem with the Garmin Connext
registration. Contact Garmin through the phone
number listed at its website, www.flygarmin.com..
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Description
The weather data request coverage area does not
contain at least one of the following: a waypoint, a
flight plan, or a flight plan destination. Verify at least
one of the coverage options is enabled (checked) and
contains required criteria, then re-send the data request.
No Connext
Subscription
The system is not be currently subscribed to Garmin
Connext services or the access code is incorrect. Verify
the access code. Contact Garmin via the phone number
listed on its website at www.flygarmin.com..
Reduce Request Area
The size of the received weather data has exceeded
system memory limits. Reduce the size of the coverage
area and issue another Connext Data Request to ensure
all available weather data has been received.
Request Canceled
The user has cancelled a Connext Data Request.
Request Failed - Try
Again
The weather data request timed-out. Re-send data
request.
AFCS
Invalid Coverage Area
Hazard
Avoidance
The Garmin Connext Weather data server will be out of
service for at least 30 minutes.
Flight
Management
Connext Server Inop
Audio Panel
and CNS
The Garmin Connext Weather data server is temporarily
out of service, but is expected to return to service in less
than 30 minutes.
EIS
Connext Server Temp
Inop
Flight
Instruments
Weather Request
Status Message
Additional
Features
Table 7 Abnormal Garmin Connext Data Request Status Messages
Abnormal
Operation
Annunciations
& Alerts
When the system is operating in Reversionary Mode, only those weather products
which can be displayed on the PFD maps will be available for display. f manual Connext
Data Requests were enabled prior to entering Reversionary Mode, no new weather data
will be retrieved while operating in Reversionary Mode. If automatic Connext Data
Requests were enabled prior to Reversionary Mode operation, the system will continue the
automatic data requests in Reversionary Mode (provided automatic requests have not
been inhibited due to a system error).
TAWS ANNUNCIATIONS/ALERTS
Appendix
Relative Terrain Symbology
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
179
Index
The terrain system uses colors and symbols to represent terrain and point obstacles (with
heights greater than 200 feet above ground level, AGL) present in the databases relative to
aircraft altitude. The system dynamically adjusts these colors as the aircraft altitude changes,
and after takeoff and landing.
While the aircraft is on the ground, the system displays relative terrain 400 feet or more
above the aircraft altitude using red, and terrain at less than 400 feet above aircraft altitude
using black, as shown on the On-Ground Legend. When the aircraft is in the air, the system
displays relative terrain information using red, yellow, green, and black, as shown on the InAir Legend. As the aircraft transitions from on-ground to in-air, or from in-air to on-ground,
the display of relative terrain momentarily fades into the corresponding colors. For TerrainSVT or TAWS-B systems, if an alert occurs, the relative terrain colors transition to the In-Air
Legend if the On-Ground Legend was shown in order to provide the pilot with the most
information possible.
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
On-Ground Legend
Hazard
Avoidance
Flight
Management
In-Air Legend
The following figure shows the relative terrain coloring for the Terrain Proximity system.
100 ft Threshold
Additional
Features
AFCS
Figure 51 Relative Terrain Legend
Red
Terrain above or within 100 feet
below the aircraft altitude
Yellow
Terrain is between 100 feet and
1000 feet below aircraft altitude
Lighted Obstacle
2000 ft
Abnormal
Operation
Green Terrain is between 1000 feet and
2000 feet below aircraft altitude
Figure 52 Terrain Altitude/Color Correlation for Terrain Proximity
The following figure shows relative terrain coloring for the Terrain-SVT and TAWS-B
systems.
Index
Appendix
Annunciations
& Alerts
Black Terrain is at least 2000 feet
below aircraft altitude
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Annunciations & Alerts
100 ft Threshold
Terrain above or within 100 feet
below the aircraft altitude
Yellow
Terrain is between 100 feet and
1000 feet below aircraft altitude
Lighted Obstacle
2000 ft
EIS
Red
Flight
Instruments
Projected Flight Path
Green Terrain is between 1000 feet and
2000 feet below aircraft altitude
Audio Panel
and CNS
Black Terrain is at least 2000 feet
below aircraft altitude
The following tables show the relative obstacle coloring used by the terrain systems.
Unlighted Obstacle
> 1000’
AGL
< 1000’
AGL
Obstacle Location
AFCS
< 1000’
AGL
Lighted Obstacle
Hazard
Avoidance
NOTE: The Vertical Situation Display (VSD) Inset Window shows terrain at least
2000 feet below the aircraft altitude as gray.
Flight
Management
Figure 53 Terrain Altitude/Color Correlation for Terrain-SVT or TAWS-B
Systems
> 1000’
AGL
Annunciations
& Alerts
White point obstacle is
more than 250 ft below
the aircraft altitude
Abnormal
Operation
Yellow point obstacle is
between the aircraft
altitude to within 250 feet
below the aircraft altitude
Additional
Features
Red point obstacle is at or
above the aircraft altitude
Table 8 Relative Point Obstacle Symbols and Colors
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
181
Flight
Instruments
Annunciations & Alerts
Wire Obstacle
Red wire obstacle is at or above the aircraft
altitude
EIS
Yellow wire obstacle is between the aircraft
altitude to within 250 feet below the aircraft
altitude
Table 9 Relative Wire Obstacles and Colors
Unlighted Wind
Turbine Obstacle
Lighted Wind
Turbine Obstacle
Wind Turbine Obstacle Location
Red wind turbine obstacle is at or above
the aircraft altitude
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
White wire obstacle is more than 250 ft below
the aircraft altitude
AFCS
Yellow wind turbine obstacle is between
the aircraft altitude to within 250 feet
below the aircraft altitude
White wind turbine obstacle is more than
250 ft below the aircraft altitude
Table 10 Relative Wind Turbine Obstacles and Colors
The Terrain-SVT and TAWS-B systems show potential impacts areas for terrain and
obstacles using yellow and red as shown in the following table.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
Wire Obstacle Location
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Annunciations & Alerts
Warning
Example Annunciation
EIS
or
Alert Type
Flight
Instruments
Potential Impact Area
Examples
TAWS-B Warning:
Terrain-SVT Warning:
Audio Panel
and CNS
Flight
Management
or
Caution
Trip Planning Page
‘Map - Navigation Map Page’
Flight Plan Page
Additional
Features
PFD Maps
AFCS
The ‘Map - Terrain Proximity’ or ‘Map - Terrain-SVT’ or ‘Map - TAWS-B’ Page is the
principal map page for viewing terrain information. Terrain and obstacle information can be
displayed on the following maps and pages:
Hazard
Avoidance
Table 11 Terrain-SVT and TAWS-B Potential Impact Area with Annunciations
Terrain Proximity/Terrain-SVT/TAWS-B Page
Appendix
When an alert is issued, annunciations appear on the PFD and MFD. The terrain alert
annunciation appears to the left of the Selected Altitude box on the PFD, and bottom on the
MFD. If the terrain page is not displayed at the time, a pop-up alert appears on the MFD. To
acknowledge the pop-up alert:
Annunciations
& Alerts
Alerts are issued when flight conditions meet parameters that are set within Terrain-SVT
or TAWS-B software algorithms. Terrain-SVT and TAWS-B alerts typically employ a caution
or a warning alert severity level, or both. When an alert is issued, visual annunciations are
displayed and voice alerts are simultaneously issued.
Abnormal
Operation
Terrain-SVT and TAWS-B Alerting Displays
• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the ‘Map - Terrain-SVT’ or ‘Map - TAWS-B’ Page)
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
183
Flight
Instruments
Annunciations & Alerts
Pop-up
Alert
Flight
Management
Audio Panel
and CNS
EIS
Alert Annunciation
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Figure 54 TAWS-B Alert Annunciations
Alert Annunciation
Figure 55 TAWS-B Page with Annunciation (After MFD Pop-up Alert
Acknowledgment)
Index
Appendix
Annunciations
& Alerts
Alert Type
PFD/Terrain—
SVT Page Alert
Annunciation
MFD Pop-Up
Alert (except
Terrain-SVT
Page)
Voice Alert
Reduced Required
Terrain Clearance
Warning (RTC)
“Warning; Terrain,
Terrain”
Reduced Required
Line Clearance
(RLC) Warning
“Warning; Wire, Wire”
Imminent Terrain
Impact Warning
(ITI)
“Warning; Terrain,
Terrain”
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Annunciations & Alerts
PFD/Terrain—
SVT Page Alert
Annunciation
MFD Pop-Up
Alert (except
Terrain-SVT
Page)
Voice Alert
Flight
Instruments
Alert Type
“Warning; Obstacle,
Obstacle”
Imminent Obstacle
Impact Warning
(IOI)
“Warning; Obstacle,
Obstacle”
Reduced Required
Terrain Clearance
Caution (RTC)
“Caution; Terrain,
Terrain”
Imminent Line
Impact Caution
(ILI)
“Caution, Wire, Wire”
Imminent Terrain
Impact Caution
(ITI)
“Caution; Terrain,
Terrain”
Reduced Required
Line Clearance
Caution (RLC)
“Caution, Wire, Wire”
AFCS
Reduced Required
Obstacle
Clearance Caution
(ROC)
“Caution; Obstacle,
Obstacle”
Additional
Features
Imminent Obstacle
Impact Caution
(IOI)
“Caution; Obstacle,
Obstacle”
EIS
Reduced Required
Obstacle
Clearance
Warning (ROC)
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
Abnormal
Operation
Annunciations
& Alerts
Table 12 Terrain-SVT Alerts Summary
Appendix
Index
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185
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Alert Type
PFD/TAWS—B
Page Alert
Annunciation
MFD Pop-Up Alert
(except TAWS-B
Page)
Voice Alert
Excessive
Descent Rate
Warning (EDR)
“Pull Up”
Reduced
Required Terrain
Clearance
Warning (RTC)
“Terrain, Terrain; Pull
Up, Pull Up”
Imminent Line
Impact Warning
(ILI)
“Wire Ahead; Pull
Up, Pull Up”
Reduced
Required Line
Clearance
Warning (RLC)
“Wire, Wire; Pull Up,
Pull Up”
Imminent Terrain
Impact Warning
(ITI)
“Terrain, Terrain; Pull
Up, Pull Up”
Reduced
Required
Obstacle
Clearance
Warning (ROC)
“Obstacle, Obstacle;
Pull Up, Pull Up”
Imminent
Obstacle Impact
Warning (IOI)
“Obstacle, Obstacle;
Pull Up, Pull Up”
Reduced
Required Terrain
Clearance
Caution (RTC)
“Caution, Terrain;
Caution, Terrain”
Imminent Terrain
Impact Caution
(ITI)
“Caution, Terrain;
Caution, Terrain”
Required
Reduced Line
Clearance (RLC)
Impact Caution
“Caution, Wire;
Caution, Wire”
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Annunciations & Alerts
PFD/TAWS—B
Page Alert
Annunciation
MFD Pop-Up Alert
(except TAWS-B
Page)
Voice Alert
Flight
Instruments
Alert Type
“Wire Ahead; Wire
Ahead”
Reduced
Required
Obstacle
Clearance
Caution (ROC)
“Caution, Obstacle;
Caution, Obstacle”
Imminent
Obstacle Impact
Caution (IOI)
“Caution, Obstacle;
Caution, Obstacle”
Premature
Descent Alert
Caution (PDA)
“Too Low, Terrain”
Hazard
Avoidance
None
Flight
Management
None
Audio Panel
and CNS
“Five-Hundred”
AFCS
Altitude Voice
Callout (VCO)
“500”
EIS
Imminent Line
Clearance
Impact Caution
(ILI)
“Sink Rate”
Negative Climb
Rate Caution
(NCR)
“Don’t Sink”
Additional
Features
Excessive
Descent Rate
Caution (EDR)
Abnormal
Operation
Table 13 TAWS-B Alerts Summary
Annunciations
& Alerts
TIS ANNUNCIATIONS/ALERTS
System Status
Appendix
The system performs an automatic test of TIS during power-up. If TIS passes the test, TIS
enters Standby Mode (on the ground) or Operating Mode (in the air). If TIS fails the power
up test, an annunciation is shown in the center of the Traffic Map Page.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
187
Traffic Map Page Center
Banner Annunciation
Description
NO DATA
Data is not being received from the transponder*
DATA FAILED
Data is being received from the transponder, but
a failure is detected in the data stream*
FAILED
The transponder has failed*
FAILED
TIS is unavailable or out of range
* Contact a service center or Garmin dealer for corrective action
Table 14 TIS Failure Annunciations
The traffic mode is annunciated in the upper right corner of the Traffic Map Page. When
the aircraft is on the ground, TIS automatically enters Standby Mode. If traffic is selected for
display on another map while Standby Mode is selected, the traffic display enabled icon is
crossed out (also the case whenever TIS has failed). Once the aircraft is airborne, TIS
switches to Operating Mode and traffic information is displayed. The mode can be changed
manually using softkeys or the page menu.
Traffic Map Mode
Annunciation
Traffic Map Center
Banner Annunciation
DATA FAILED
TRFC FAIL
Data is being
received from
the
transponder,
but a failure is
detected in the
data stream*
NO DATA
TRFC FAIL
Data is not
being received
from the
transponder*
OPERATING
NONE
TIS is operating
and is receiving
traffic data
from a data
link.
Traffic Overlay
Status Icon
(Navigation
Maps
Description
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
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Annunciations & Alerts
Traffic Overlay
Status Icon
(Navigation
Maps
Description
STANDBY
STANDBY
TIS is in
Standby Mode.
UNIT FAILED
TRFC FAIL
The
transponder
has failed*
Hazard
Avoidance
TIS is
operating, but
the traffic
service is
currently
unavailable or
is out of
reception
range.
Flight
Management
UNAVAILABLE
Audio Panel
and CNS
OPERATING
EIS
Traffic Map Center
Banner Annunciation
Flight
Instruments
Traffic Map Mode
Annunciation
* Contact a service center or Garmin dealer for corrective action
AFCS
Table 15 TIS Modes and Status Annunciations
The annunciations to indicate the status of traffic information appear in a banner at the
lower left corner of maps on which traffic can be displayed, as shown in the following table.
TA OFF SCALE
Additional
Features
Traffic Status Banner
Annunciation
Description
Abnormal
Operation
A Traffic Advisory is outside the selected display range*
Annunciation is removed when traffic comes within the
selected display range
Appears if traffic data is not refreshed within 6 seconds If
after another 6 seconds data is not received, traffic is
removed from the display The quality of displayed traffic
information is reduced as the age increases
TRFC COAST
The displayed data is not current (6 to 12 seconds since
last message) The quality of displayed traffic information is
reduced when this message is displayed
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
189
Index
AGE MM:SS
Appendix
System cannot determine bearing of Traffic Advisory**
Annunciation indicates distance in nm, altitude separation
in hundreds of feet, and altitude trend arrow (climbing/
descending)
Annunciations
& Alerts
TA X.X ± XX
Traffic Status Banner
Annunciation
Description
TRFC RMVD
Traffic is removed because it is too old for coasting (12 to
60 seconds since last message) Traffic may exist within the
selected display range, but it is not displayed
TRFC FAIL
Traffic data has failed
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
NO TRFC DATA
Traffic has not been detected
TRFC UNAVAIL
The traffic service is unavailable or out of range
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
Table 16 TIS Traffic Status Annunciations
ADS-B TRAFFIC ANNUNCIATIONS/ALERTS
ADS-B System Status
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
The traffic mode is annunciated in the upper right corner of the ‘Map - Traffic Map’ Page.
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
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Annunciations & Alerts
Traffic Mode
Annunciation
(Traffic Map
Page)
Traffic Map Page
Center Banner
Annunciation
NONE
ADS-B Operating
in Surface Mode
ADS-B:
SURF
NONE
ABS-B Traffic Off
ADS-B:
OFF
ADS-B TRFC
OFF
ADS-B Traffic Not
Available
ADS-B:
N/A
NO
TRK/HDG
ADS-B Failed*
ADS-B:
FAIL
ADS-B TRFC
FAIL
AFCS
ADS-B:
AIRB
Hazard
Avoidance
ADS-B Operating
in Airborne Mode
Flight
Management
TEST MODE
Audio Panel
and CNS
ADS-B:
TEST
EIS
ADS-B System Test
Initiated
Traffic Display
Status Icon (Other
Maps)
* See ‘Traffic Failure Annunciations’ Table for additional failure annunciations
If the traffic unit fails, an annunciation as to the cause of the failure is shown in the center
of the ‘Map - Traffic Map’ Page. During a failure condition, the Operating Mode cannot be
selected.
Additional
Features
Table 17 ADS-B Modes
Abnormal
Operation
Traffic Map Page Center Annunciation
Flight
Instruments
ADS-B Mode
Description
Data is not being received from the
traffic unit
DATA FAILED
Data is being received from the traffic
unit, but the unit is self-reporting a
failure
FAILED
Incorrect data format received from the
traffic unit
Annunciations
& Alerts
NO DATA
Appendix
Table 18 Traffic Failure Annunciations
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
191
Index
The annunciations to indicate the status of traffic information appear in a banner at the
lower left corner of maps on which traffic can be displayed.
Traffic Status Banner
Annunciation
Description
TA OFF SCALE
A Traffic Advisory is outside the selected display range*.
Annunciation is removed when traffic comes within the
selected display range.
TA X.X±XX
System cannot determine bearing of Traffic Advisory**.
Annunciation indicates distance in nm, altitude
separation in hundreds of feet, and altitude trend arrow
(climbing/descending).
TRFC FAIL
Traffic unit has failed (unit is self-reporting a failure or
sending incorrectly formatted data)
NO TRFC DATA
Data is not being received from the traffic unit
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Table 19 Traffic Status Annunciations
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Additional information about the status of ADS-B traffic products is available on the ‘Aux ADS-B Status’ Page.
Index
Appendix
Figure 56 ‘Aux — ADS-B Status’ Page
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Annunciations & Alerts
Flight
Instruments
VOICE ALERTS
Voice Alerts
Priority
“Stall”
Warning
Warning
The aircraft has descended
below the preset barometric
minimum descent altitude.
Warning
The ‘CHECK GEAR’ CAS
message has been triggered.
Caution
TAS Traffic Advisory (TA) is
issued with the optional GTS
825 TAS system. See the
Hazard Avoidance section for
additional details on GTS 825
voice alerts.
Additional
Features
Caution
The ‘CHECK GEAR’ CAS
message has been triggered.
Abnormal
Operation
Caution
The ESP system is engaging the
autopilot. See the AFCS section
for more details.
“Engaging autopilot”
“TAS System Test
Passed”
190–02362–00 Rev. A
Advisory
Played when the optional GTS
825 traffic system fails a pilotinitiated self test.
Advisory
Aircraft is one minute from Top
of Descent. Issued only when
vertical navigation is enabled.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
193
Index
“Vertical track”
Played when the optional GTS
825 traffic system passes a
pilot-initiated self test.
Appendix
“TAS System Test
Failed”
Advisory
Annunciations
& Alerts
Caution
“Traffic, (distance,
bearing, altitude)”
“Check gear”
TIS Traffic Advisory (TA) is
issued with the TIS system
AFCS
“Traffic”
Hazard
Avoidance
Aircraft has descended below
the preset barometric minimum
descent altitude
Flight
Management
“Check gear”
Imminent stall is sensed by stall
vane
Warning
”Airspeed”
“Minimums,
minimums”
Description
Audio Panel
and CNS
Voice Alert
EIS
The following aural alerts are announced by the system using a voice. If an optional
terrain system is installed, voice alerts are also generated (refer to the appropriate terrain
alerts section).
Annunciations & Alerts
Flight
Instruments
Voice Alert
“TIS Not Available”
Advisory
Countdown timer on the PFD
has reached zero
Advisory
A call has been received via the
Iridium system.
SYSTEM MESSAGES
System Messages
NOTE: This section provides information regarding message advisories that may
be displayed by the system. Knowledge of the aircraft, systems, flight
conditions, and other existing operational priorities must be considered when
responding to a message. Always use sound pilot judgment. The Pilot’s
Operating Handbook (POH) takes precedence over any conflicting guidance
found in this section.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
“Incoming Call”
AFCS
This section describes various system message advisories. Certain messages are issued
due to an LRU or an LRU function failure. Such messages are normally accompanied by
a corresponding red amber ‘X’ annunciation as shown previously in the System
Annunciation section.
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
Description
Aircraft is outside TIS coverage
area
EIS
“Timer Expired”
Priority
Advisory
Message Advisory
Comments
ABORT APR – Loss of
GPS navigation. Abort
approach.
Abort approach due to loss of GPS navigation.
ADC1 ALT EC – ADC1
altitude error correction is
unavailable.
GDC is reporting that the altitude error correction is
unavailable.
ADC1 AS EC – ADC1
airsp eed error correction
is unavailable.
GDC is reporting that the airspeed error correction is
unavailable.
ADC1 SERVICE – ADC1
needs service. Return unit
for repair.
The AHRS should be serviced..
ADC2 ALT EC – ADC1
altitude error correction is
unavailable.
GDC is reporting that the altitude error correction is
unavailable.
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Annunciations & Alerts
Comments
ADC2 SERVICE – ADC1
needs service. Return unit
for repair.
The AHRS should be serviced..
EIS
GDC is reporting that the airspeed error correction is
unavailable.
Flight
Instruments
Message Advisory
ADC2 AS EC – ADC1
airsp eed error correction
is unavailable.
AHRS1 GPS – AHRS1 not
receiving any GPS
information.
The #1 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
AHRS1 GPS – AHRS1 not
receiving backup GPS
information.
The #1 AHRS is not receiving backup GPS
information. The system should be serviced.
AHRS1 GPS – AHRS1
operating exclusively in
no-GPS mode.
The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
AHRS1 SRVC – AHRS1
Magnetic-field model
needs update.
The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
AHRS1 TAS – AHRS1 not
receiving valid airspeed.
The #1 AHRS is not receiving true airspeed from the
air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
AHRS12 CAL – AHRS2
calibration version error.
Srvc req’d
The #2 AHRS calibration version error. The system
should be serviced.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The #1 AHRS is using the backup GPS path. Primary
GPS path has failed. The system should be serviced
when possible.
Appendix
AHRS1 GPS – AHRS1
using backup GPS source.
Annunciations
& Alerts
AHRS configuration settings do not match those of
backup configuration memory. The system should
be serviced.
Abnormal
Operation
AHRS1 CONFIG – AHRS1
config error. Config
service req’d
Additional
Features
The #1 AHRS calibration version error. The system
should be serviced.
AFCS
AHRS1 CAL – AHRS1
calibration version error.
Srvc req’d
Hazard
Avoidance
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
Flight
Management
AHRS MAG DB – AHRS
magnetic model database
version mismatch.
Audio Panel
and CNS
The cooling fan for the aft remote avionics has
AFT AV FAN FAIL – The
cooling fan for aft avionics failed.
has failed.
195
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
AHRS2 CONFIG – AHRS2
config error. Config
service req’d
#2 AHRS configuration settings do not match those
of backup configuration memory. The system should
be serviced.
AHRS2 GPS – AHRS2
using backup GPS source.
The #2 AHRS is using the backup GPS path. Primary
GPS path has failed. The system should be serviced
when possible.
AHRS2 GPS – AHRS2 not
receiving any GPS
information.
The #2 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
AHRS2 GPS – AHRS2 not
receiving backup GPS
information.
The #2 AHRS is not receiving backup GPS
information. The system should be serviced.
AHRS2 GPS – AHRS2
operating exclusively in
no-GPS mode.
The #2 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
AHRS2 SRVC – AHRS2
Magnetic-field model
needs update.
The #2 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
AHRS2 TAS – AHRS2 not
receiving valid airspeed.
The #2 AHRS is not receiving true airspeed from the
air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
APR ADVISORY – SBAS
VNAV not available.
SBAS VNAV not available. Check GPS sensor.
APR DWNGRADE –
Approach downgraded.
Vertical guidance generated by SBAS is unavailable,
use LNAV only minimums.
APR INACTV – Approach
is not active.
The system notifies the pilot that the loaded
approach is not active. Activate approach when
required.
ARSPC AHEAD –
Airspace ahead less than
10 minutes.
Special use airspace is ahead of aircraft. The aircraft
will penetrate the airspace within 10 minutes.
ARSPC NEAR – Airspace
near and ahead.
Special use airspace is near and ahead of the aircraft
position.
ARSPC NEAR – Airspace
near – less than 2 nm.
Special use airspace is within 2 nm of the aircraft
position.
AUDIO MANIFEST –
AUDIO MANIFEST
Incorrect audio software installed. The system
should be serviced
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190–02362–00 Rev. A
Annunciations & Alerts
Comments
AUTO DESCENT has been active for 60 seconds,
EDM activated.
AUTO DESCENT –
Aircraft descending to
12,500FT.
No interaction detected for four minutes after
aircraft reaches 14,000 feet.
Audio Panel
and CNS
AUTO DESCENT –
Aircraft descending to
14,000FT.
EIS
HYPOXIA ALERT has been active for 60 seconds,
aircraft will begin descent in 60 seconds.
Flight
Instruments
Message Advisory
AUTO DESCENT –
Automatic descent to
14,000FT in 60 seconds.
Flight
Management
Selected course for LOC1 differs from published
CHECK CRS – Database
course for LOC1 / [LOC ID] localizer course by more than 10 degrees.
is [CRS]°.
CNFG MODULE – PFD1
configuration module is
inoperative.
Hazard
Avoidance
Selected course for LOC2 differs from published
CHECK CRS – Database
course for LOC2 / [LOC ID] localizer course by more than 10 degrees.
is [CRS]°.
The PFD1 configuration module backup memory has
failed. The system should be serviced.
AFCS
A failure in the carbon monoxide detector has been
CO DET FAIL – The
carbon monoxide detector detected. The system should be serviced.
is inoperative.
The COM1 configuration settings do not match
backup configuration memory. The system should
be serviced
Abnormal
Operation
COM1 CONFIG – COM1
config error. Config
service req’d.
Additional
Features
A failure has been detected in carbon monoxide
CO DET SRVC – The
carbon monoxide detector detector has been detected. The detector may still
be available. The system should be serviced when
needs service.
possible.
The COM1 external push-to-talk switch is stuck in
the enable (or “pressed”) position. Press the PTT
switch again to cycle its operation. If the problem
persists, the system should be serviced.
Appendix
COM1 PTT – COM1
push-to-talk key is stuck.
Annunciations
& Alerts
COM1 software mismatch. The system should be
COM1 MANIFEST –
serviced.
COM1 software
mismatch, communication
halted.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
COM1 RMT XFR – COM1 The COM1 transfer switch is stuck in the enabled (or
“pressed”) position. Press the transfer switch again
remote transfer key is
to cycle its operation. If the problem persists, the
stuck.
system should be serviced.
197
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
COM1 SERVICE – COM1
needs service. Return unit
for repair.
The system has detected a failure in COM1. COM1
may still be usable. The system should be serviced
when possible.
COM1 TEMP – COM1
over temp. Reducing
transmitter power.
The system has detected an over temperature
condition in COM 1. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
COM2 CONFIG – COM2
config error. Config
service req’d.
The COM2 configuration settings do not match
backup configuration memory. The system should
be serviced
COM2 software mismatch. The system should be
COM2 MANIFEST –
serviced.
COM2 software
mismatch, communication
halted.
COM2 PTT – COM2
push-to-talk key is stuck.
The COM2 external push-to-talk switch is stuck in
the enable (or “pressed”) position. Press the PTT
switch again to cycle its operation. If the problem
persists, the system should be serviced.
COM2 RMT XFR – COM2 The COM2 transfer switch is stuck in the enabled (or
“pressed”) position. Press the transfer switch again
remote transfer key is
to cycle its operation. If the problem persists, the
stuck.
system should be serviced.
COM2 SERVICE – COM2
needs service. Return unit
for repair.
The system has detected a failure in COM2. COM2
may still be usable. The system should be serviced
when possible.
COM2 TEMP – COM2
over temp. Reducing
transmitter power.
The system has detected an over temperature
condition in COM2. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
CNFG MODULE – PFD1
configuration module is
inoperative.
The PFD1 configuration module backup memory has
failed. The system should be serviced.
DATA LOST – Pilot stored
data was lost. Recheck
settings.
The pilot profile data was lost. System reverts to
default pilot profile and settings. The pilot may
reconfigure the MFD & PFD with preferred settings,
if desired.
DB CHANGE – Database
changed. Verify user
modified procedures.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures in
stored flight plans are correct and up to date.
198
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Annunciations & Alerts
Comments
ESP is not configured properly. The system should be
serviced.
ESP FAIL – ESP IAS mode
is inoperative.
IAS mode of ESP is inoperative. The system should
be serviced.
ESP DEGRADE – ESP is
inoperative.
The ESP function has failed and is inoperative. The
system should be serviced.
ESP OFF – ESP selected
off.
Electronic Stability and Protection has been disabled
on the SYSTEM SETUP 2 page.
EXCEEDANCE – Engine
exceedance data is being
logged.
An engine exceedance log has been captured
FAILED PATH – A data
path has failed.
A data path connected to the GDU, GSD 41, or the
GIA 63/W has failed.
FPL TRUNC – Flight plan
has been truncated.
This occurs when a newly installed navigation
database eliminates an obsolete approach or arrival
used by a stored flight plan. The obsolete procedure
is removed from the flight plan. Update flight plan
with current arrival or approach.
Annunciations
& Alerts
ESP CONFIG – ESP config
error. Config service req’d
Abnormal
Operation
The PFDs and MFD have different terrain database
versions or types installed. Install correct terrain
database version or type in all displays.
Additional
Features
DB MISMATCH – Terrain
database mismatch.
AFCS
The PFDs and MFD have different obstacle database
installed. Install correct obstacle database in all
displays.
Hazard
Avoidance
DB MISMATCH –
Obstacle database
mismatch.
Flight
Management
The PFDs and MFD have different navigation
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
Audio Panel
and CNS
DB MISMATCH –
Navigation database
mismatch. Xtalk is off.
EIS
This occurs when a stored flight plan contains an
airway that is no longer consistent with the
navigation database. This alert is issued only after an
navigation database update. Verify use of airways in
stored flight plans and reload airways as needed.
Flight
Instruments
Message Advisory
DB CHANGE – Database
changed. Verify stored
airways.
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
199
Message Advisory
Upon power-up, the system detects that a stored
flight plan waypoint is locked. This occurs when an
navigation database update eliminates an obsolete
waypoint. The flight plan cannot find the specified
waypoint and flags this message. This can also occur
with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database, or update the
waypoint name/identifier to reflect the new
information.
FPL WPT MOVE – Flight
plan waypoint moved.
The system has detected that a waypoint coordinate
has changed due to a new navigation database
update. Verify that stored flight plans contain
correct waypoint locations.
FS510 CARD ERROR –
FS510 not detected in
MFD Bottom Slot.
The SD card was removed from the bottom card slot
of the MFD. The SD card needs to be reinserted.
G/S1 FAIL – G/S1 is
inoperative.
A failure has been detected in glideslope receiver 1.
The system should be serviced.
G/S1 SERVICE – G/S1
needs service. Return unit
for repair.
A failure has been detected in glideslope receiver 1.
The receiver may still be available. The system
should be serviced when possible.
G/S2 FAIL – G/S2 is
inoperative.
A failure has been detected in glideslope receiver 2.
The system should be serviced.
G/S2 SERVICE – G/S2
needs service. Return unit
for repair.
A failure has been detected in glideslope receiver 1.
The receiver may still be available. The system
should be serviced when possible.
GAE 43 FAILURE – Using
controller cabin
information.
A failure has been detected in the altitude encoder.
The cabin altitude controller information is being
used.
GCU1 CONFIG – GCU1
Config error. Config
service req’d.
GCU 476 configuration settings do not match those
of backup configuration memory. The G1000 system
should be serviced.
GCU1 FAIL – GCU1 is
inoperative.
A failure has been detected in the GCU 476. The
GCU 476 is unavailable.
GCU1 KEYSTK – GDC1
software mismatch,
communication halted.
A key is stuck on the GCU 476 bezel. Attempt to
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
Comments
FPL WPT LOCK – Flight
plan waypoint is locked.
EIS
Flight
Instruments
Annunciations & Alerts
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Annunciations & Alerts
Comments
Flight
Instruments
Message Advisory
The GCU 476 has incorrect software installed. The
GCU1 MANIFEST –
GCU1 software mismatch, G1000 system should be serviced.
communication halted.
EIS
The GDC 74 has incorrect software installed. The
GDC1 MANIFEST –
GDC1 software mismatch, system should be serviced.
communication halted.
Audio Panel
and CNS
The GDC 74 has incorrect software installed. The
GDC2 MANIFEST –
GDC2 software mismatch, system should be serviced.
communication halted.
Flight
Management
GDL69 CONFIG – GDL 69 GDL 69AH configuration settings do not match
those of backup configuration memory. The system
config error. Config
should be serviced.
service req’d.
Hazard
Avoidance
GDL69 FAIL – GDL 69 has A failure has been detected in the GDL 69AH. The
receiver is unavailable. The system should be
failed.
serviced
The #1 GEA 71 has incorrect software installed. The
system should be serviced.
GEA2 CONFIG – GEA2
config error. Config
service req’d.
The GEA2 configuration settings do not match
those of backup configuration memory. The system
should be serviced.
GEA2 MANIFEST – GEA2
software mismatch,
communication halted.
The #2 GEA 71 has incorrect software installed. The
system should be serviced.
GEO LIMITS – AHRS1 too
far North/South, no
magnetic compass.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
invalid.
GEO LIMITS – AHRS2 too
far North/South, no
magnetic compass.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
invalid.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
GEA1 MANIFEST – GEA1
software mismatch,
communication halted.
Appendix
The GEA1 configuration settings do not match
those of backup configuration memory. The system
should be serviced.
Annunciations
& Alerts
GEA1 CONFIG – GEA1
config error. Config
service req’d.
Abnormal
Operation
Increases in map range are automatically limited at >
68 degrees 35 minutes north or south.
Additional
Features
GDU ZOOM LIMITED –
Map zoom has been
automatically limited.
AFCS
The GDL 69AH has incorrect software installed. The
GDL69 MANIFEST –
system should be serviced.
GDL69 software
mismatch, communication
halted.
201
Message Advisory
Comments
GFC MANIFEST – GFC
software mismatch,
communication halted.
Incorrect servo software is installed, or gain settings
are incorrect.
GIA1 COOLING – GIA1
temperature too low.
The GIA1 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
GIA1 COOLING – GIA1
over temperature.
The GIA1 temperature is too high. If problem
persists, the system should be serviced.
GIA1 CONFIG – GIA1
config error. Config
service req’d.
The GIA1 configuration settings do not match
backup configuration memory. The system should
be serviced.
GIA1 CONFIG – GIA1
audio config error. Config
service req’d.
The GIA1 have an error in the audio configuration.
The system should be serviced.
GIA1 MANIFEST – GIA1
software mismatch,
communication halted.
The GIA1 has incorrect software installed. The
system should be serviced.
GIA1 SERVICE – GIA1
needs service. Return the
unit for repair.
The GIA1 self-test has detected a problem in the
unit. The system should be serviced.
GIA2 COOLING – GIA2
temperature too low.
The GIA2 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
GIA2 COOLING – GIA2
over temperature.
The GIA2 temperature is too high. If problem
persists, the system should be serviced.
GIA2 CONFIG – GIA2
config error. Config
service req’d.
The GIA2 configuration settings do not match
backup configuration memory. The system should
be serviced.
GIA2 CONFIG – GIA2
audio config error. Config
service req’d.
The GIA2 have an error in the audio configuration.
The system should be serviced.
GIA2 MANIFEST – GIA2
software mismatch,
communication halted.
The GIA 2 has incorrect software installed. The
system should be serviced.
GIA2 SERVICE – GIA2
needs service. Return the
unit for repair.
The GIA2 self-test has detected a problem in the
unit. The system should be serviced.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
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Annunciations & Alerts
Comments
Flight
Instruments
Message Advisory
GMA1 AUX MANIFEST – The digital audio controller has incorrect software
installed. The system should be serviced.
GMA 1 AUX software
mismatch, communication
halted.
GMA1 FAIL – GMA1 is
inoperative.
The audio panel self-test has detected a failure. The
audio panel is unavailable. The system should be
serviced.
Audio Panel
and CNS
The audio panel configuration settings do not match
backup configuration memory. The system should
be serviced.
EIS
GMA1 CONFIG – GMA1
config error. Config
service req’d.
A failure has been detected in the GMC 710. The
GMC 710 is unavailable.
GMC KEYSTK – GMC is
inoperative.
A key is stuck on the GMC 710 bezel. Attempt to
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
GMC MANIFEST – GMC
software mismatch.
Communication halted.
The GMC 710 has incorrect software installed. The
G1000 system should be serviced.
Annunciations
& Alerts
GMC FAIL – GMC is
inoperative.
Abnormal
Operation
Error in the configuration of the GMC 710.
Additional
Features
GMC CONFIG – GMC
Config error. Config
service req’d.
AFCS
The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
Hazard
Avoidance
GMA1 SERVICE – GMA1
needs service. Return unit
for repair.
Flight
Management
The audio panel has incorrect software installed. The
GMA1 MANIFEST –
system should be serviced.
GMA1 software
mismatch, communication
halted.
Appendix
The GMU 44 has incorrect software installed. The
GMU1 MANIFEST –
system should be serviced.
GMU1 software
mismatch, communication
halted.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The GMU 44 has incorrect software installed. The
GMU2 MANIFEST –
system should be serviced.
GMU2 software
mismatch, communication
halted.
203
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
GPS NAV LOST – Loss of
GPS navigation.
Insufficient satellites.
Loss of GPS navigation due to insufficient satellites.
GPS NAV LOST – Loss of
GPS navigation. Position
error.
Loss of GPS navigation due to position error.
GPS NAV LOST – Loss of
GPS navigation. GPS fail.
Loss of GPS navigation due to GPS failure.
GPS1 SERVICE – GPS1
needs service. Return unit
for repair.
A failure has been detected in the GPS1 receiver.
The receiver may still be available. The system
should be serviced.
GPS2 SERVICE – GPS2
needs service. Return unit
for repair.
A failure has been detected in the GPS2 receiver.
The receiver may still be available. The system
should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in the #1 GSR 56H. The
system should be serviced.
GRS1 MANIFEST – GRS1
software mismatch,
communication halted.
The #1 AHRS has incorrect software installed. The
system should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in GSR2. The system
should be serviced.
GSR2 FAIL – GSR2 has
failed.
A failure has been detected in the #2 GSR 56H. The
system should be serviced.
GRS2 MANIFEST – GRS2
software mismatch,
communication halted.
The #2 AHRS has incorrect software installed. The
system should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in GSR2. The system
should be serviced.
GTS CONFIG – GTS
config error. Config
service req’d.
The GTS and GDU have incompatible
configurations. This alert is also set when the GTS
has an invalid mode S address configured or the
mode S address does not match both XPDR mode S
addresses.
GTS MANIFEST – GTS
software mismatch,
communication halted.
The GTS 800 has incorrect software installed. The
G1000H system should be serviced.
GTX1 MANIFEST – GTX1
software mismatch,
communication halted.
The transponder has incorrect software installed.
The system should be serviced.
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190–02362–00 Rev. A
Annunciations & Alerts
Comments
HDG FAULT – AHRS1
magnetometer fault has
occurred.
A fault has occurred in the #1 GMU 44. Heading is
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HDG FAULT – AHRS2
magnetometer fault has
occurred.
A fault has occurred in the #2 GMU 44. Heading is
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HW MISMATCH – GIA
hardware mismatch. GIA1
communication halted.
A GIA mismatch has been detected, where only one
is SBAS capable.
HW MISMATCH – GIA
hardware mismatch. GIA2
communication halted.
A GIA mismatch has been detected, where only one
is SBAS capable.
HDG PRESET MODE –
Magnetic anomoly
detected. HPM is
available.
The magnetometer has detected a magnetic
anomoly that could affect heading indications.
Heading Preset Mode may be used.
INCOMING CALL – Inside
airspace.
Incoming Iridium voice call.
INSIDE ARSPC –
Incoming call.
The aircraft is inside the airspace.
INVALID ADM – Invalid
ADM: ATN
communication halted.
Data link avionics were not configured correctly and
therefore will not be able to communicate with the
ground network.
Appendix
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
Annunciations
& Alerts
GWX SERVICE – GWX
needs service.
Abnormal
Operation
The GWX 68 has incorrect software installed. The
G1000 system should be serviced.
Additional
Features
GWX MANIFEST – GWX
software mismatch,
communication halted.
AFCS
The GDU is not receiving status packet from the
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.
Hazard
Avoidance
GWX FAIL – GWX is
inoperative.
Flight
Management
GWX 68 configuration settings do not match those
of the GDU configuration. The G1000 system
should be serviced.
Audio Panel
and CNS
GWX CONFIG – GWX
config error. Config
service req’d.
EIS
The transponder has incorrect software installed.
The system should be serviced.
Flight
Instruments
Message Advisory
GTX2 MANIFEST – GTX2
software mismatch,
communication halted.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
205
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
LOCKED FPL – Cannot
navigate locked flight
plan.
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan. Update
flight plan with current waypoint.
LRG MAG VAR – Verify
all course angles.
The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
near the magnetic poles. Displayed magnetic course
angles may differ from the actual magnetic heading
by more than 2°.
LOI – GPS integrity lost.
Crosscheck with other
NAVS.
GPS integrity is insufficient for the current phase of
flight.
LOW BANK ACTIVE –
Disengage for approach.
Low Bank mode is active. Disengage to continue
approach.
LOW BANK ACTIVE –
Disengage for RNP less
than 1.0.
Low Bank mode is active. Disengage to continue
RNP 1.0.
MANIFEST – MFD1
software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MANIFEST – PFD1
software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MFD SOFTWARE – MFD The specified GDU has different software versions
mismatch, communication installed. The system should be serviced.
halted.
MFD TERRAIN DSP –
MFD Terrain awareness
display unavailable.
One of the terrain or obstacle databases required for
TAWS in the specified GDU is missing or invalid.
MFD1 CARD 1 ERR –
Card 1 is invalid.
The SD card in the top card slot of the specified PFD
or MFD contains invalid data.
MFD1 BACKLIGHT
CALIBRATION – MFD1
calibration. Return for
repair.
The specified GDU’s backlight calibration cannot be
found or is invalid. The system should be serviced.
MFD1 CARD 2 ERR –
Card 2 is invalid.
The SD card in the bottom card slot of the specified
MFD contains invalid data.
MFD1 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified MFD. The SD card needs to be
reinserted.
206
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Comments
The MFD detected a failure in the basemap
database.
MFD1 DB ERR – MFD1
Chartview database error
exists.
The MFD detected a failure in the ChartView
database (optional feature). Ensure the data card is
properly programmed if present. If problem persists,
the system should be serviced.
MFD1 DB ERR – MFD1
FliteCharts database error
exists.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure the data card is
properly programmed if present. If problem persists,
the system should be serviced.
MFD1 DB ERR – MFD1
navigation database error
exists.
The MFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1
obstacle database error
exists.
The MFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Annunciations
& Alerts
MFD1 DB ERR – MFD1
basemap database error
exists.
Abnormal
Operation
The detected a failure in the basemap database.
Additional
Features
MFD1 DB ERR – MFD1
basemap database error
exists.
AFCS
The MFD detected a failure in the Airport Directory
database. Ensure the data card is properly
programmed if present. If problem persists, the
system should be serviced.
Hazard
Avoidance
MFD1 DB ERR – MFD1
Airport Directory database
error exists.
Flight
Management
The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.
Audio Panel
and CNS
MFD1 CONFIG – MFD1
config error. Config
service req’d.
EIS
The SD card was removed from the bottom card slot
of the specified MFD. The SD card needs to be
reinserted.
Flight
Instruments
Message Advisory
MFD1 CARD 2 REM –
Card 2 was removed.
Reinsert card.
MFD1 DB ERR – MFD1
Safe Taxi database error
exists.
The MFD detected a failure in the Safe Taxi
database. Ensure the data card is properly
programmed if present. If problem persists, the
system should be serviced.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
190–02362–00 Rev. A
Appendix
The obstacle database is present on another LRU,
MFD1 DB ERR – MFD1
obstacle database missing. but is missing on the specified LRU.
207
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
MFD1 DB ERR – MFD1
terrain database error
exists.
The MFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1
terrain database missing.
The terrain database is present on another LRU, but
is missing on the specified LRU.
MFD1 VOLTAGE – MFD1
has low voltage. Reducing
power usage
The MFD voltage is low. The system should be
serviced.
MFD1 COOLING – MFD1
has poor cooling.
Reducing power usage.
The MFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
MFD1 KEYSTK – MFD
[key name] Key is stuck.
A key is stuck on the MFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
MFD1 MANIFEST –
MFD1 software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MFD1 SERVICE – MFD1
needs service. Return unit
for repair.
The MFD self-test has detected a problem. The
system should be serviced.
NAV1 RMT XFR – NAV1
remote transfer key is
stuck.
The remote NAV1 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the system should be serviced.
NAV1 SERVICE – NAV1
needs service. Return unit
for repair.
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
NAV2 RMT XFR – NAV2
remote transfer key is
stuck.
The remote NAV2 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the system should be serviced.
NAV2 SERVICE – NAV2
needs service. Return unit
for repair.
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
NO WGS84 WPT – Non
WGS 84 waypoint for
navigation -[xxxx]
The position of the selected waypoint [xxxx] is not
calculated based on the WGS84 map reference
datum and may be positioned in error as displayed.
Do not use GPS to navigate to the selected nonWGS84 waypoint.
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Annunciations & Alerts
Comments
The PFD detected a failure in the basemap database.
PFD1 DB ERR – PFD1
navigation database error
exists.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
PFD1 DB ERR – PFD1
obstacle database error
exists.
The PFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Hazard
Avoidance
PFD1 DB ERR – PFD1
basemap database error
exists.
Flight
Management
The PFD configuration settings do not match backup
configuration memory. The system should be
serviced.
Audio Panel
and CNS
PFD1 CONFIG – PFD1
config error. Config
service req’d.
EIS
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
Flight
Instruments
Message Advisory
PFD1 COOLING – PFD1
has poor cooling.
Reducing power usage.
AFCS
The obstacle database is present on another LRU,
PFD1 DB ERR – PFD1
obstacle database missing. but is missing on the specified LRU.
PFD1 KEYSTK – PFD1
[key name] Key is stuck.
A key is stuck on the PFD bezel. Attempt to free the
stuck key by pressing it several times. The system
should be serviced if the problem persists.
PFD1 MANIFEST – PFD1
software mismatch,
communication halted.
The PFD has incorrect software installed. The system
should be serviced.
PFD1 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified PFD. The SD card needs to be
reinserted.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The terrain database is present on another LRU, but
is missing on the specified LRU
Appendix
PFD1 DB ERR – PFD1
terrain database missing.
Annunciations
& Alerts
The PFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Abnormal
Operation
PFD1 DB ERR – PFD1
terrain database error
exists.
Additional
Features
PFD1 DB ERR – PFD1 Safe The PFD detected a failure in the Safe Taxi database.
Taxi database error exists. Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
209
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
Comments
PFD1 CARD 2 REM– Card The SD card was removed from the bottom card slot
of the specified PFD. The SD card needs to be
2 was removed. Reinsert
reinserted.
card.
PFD1 CARD 1 REM ERR –
Card 1 is invalid.
The SD card in the top card slot of the specified PFD
contains invalid data.
PFD1 CARD 2 ERR – Card The SD card in the bottom card slot of the specified
PFD contains invalid data.
2 is invalid.
PFD1 SERVICE – PFD1
needs service. Return unit
for repair.
The PFD self-test has detected a problem. The
system should be serviced.
PFD1 VOLTAGE – PFD1
has low voltage. Reducing
power usage
The PFD1 voltage is low. The system should be
serviced.
PILOT RADIOS MUTED –
Pilot radios are muted.
The pilot radios are set on mute
PFD2 COOLING – PFD2
has poor cooling.
Reducing power usage.
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
PFD2 CONFIG – PFD2
config error. Config
service req’d.
The PFD configuration settings do not match backup
configuration memory. The system should be
serviced.
PFD2 DB ERR – PFD2
basemap database error
exists.
The PFD detected a failure in the basemap database.
PFD2 DB ERR – PFD2
navigation database error
exists.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
PFD2 DB ERR – PFD2
obstacle database error
exists.
The PFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
The obstacle database is present on another LRU,
PFD2 DB ERR – PFD2
obstacle database missing. but is missing on the specified LRU.
PFD2 DB ERR – PFD2 Safe The PFD detected a failure in the Safe Taxi database.
Taxi database error exists. Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
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Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Comments
A key is stuck on the PFD bezel. Attempt to free the
stuck key by pressing it several times. The system
should be serviced if the problem persists.
PFD2 MANIFEST – PFD2
software mismatch,
communication halted.
The PFD has incorrect software installed. The system
should be serviced.
PFD2 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified PFD. The SD card needs to be
reinserted.
Hazard
Avoidance
PFD2 KEYSTK – PFD2
[key name] Key is stuck.
Flight
Management
The terrain database is present on another LRU, but
is missing on the specified LRU
Audio Panel
and CNS
PFD21 DB ERR – PFD2
terrain database missing.
EIS
The PFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Flight
Instruments
Message Advisory
PFD2 DB ERR – PFD2
terrain database error
exists.
PFD2 CARD 2 REM– Card The SD card was removed from the bottom card slot
of the specified PFD. The SD card needs to be
2 was removed. Reinsert
reinserted.
card.
The SD card in the top card slot of the specified PFD
contains invalid data.
AFCS
PFD2 CARD 1 REM ERR –
Card 1 is invalid.
PTK FAIL – Parallel track
unavailable: bad
geometry.
Bad parallel track geometry.
PTK FAIL – Parallel track
unavailable: invalid leg
type.
Invalid leg type for parallel offset.
PTK FAIL – Parallel track
unavailable: past IAF.
IAF waypoint for parallel offset has been passed.
REGISTER GFDS – Data
services are inoperative,
register w/Connext.
The system is not registered with Connext, or its
current registration data has failed authentication.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The PFD1 voltage is low. The system should be
serviced.
Appendix
PFD2 VOLTAGE – PFD2
has low voltage. Reducing
power usage
Annunciations
& Alerts
The PFD self-test has detected a problem. The
system should be serviced.
Abnormal
Operation
PFD2 SERVICE – PFD2
needs service. Return unit
for repair.
Additional
Features
PFD2 CARD 2 ERR – Card The SD card in the bottom card slot of the specified
PFD contains invalid data.
2 is invalid.
211
Comments
SLCT FREQ – Select
appropriate frequency for
approach.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.
SLCT NAV – Select NAV
on CDI for approach.
The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct NAV
receiver.
STEEP TURN – Steep turn
ahead.
A steep turn is 15 seconds ahead. Prepare to turn.
STRMSCP FAIL –
Stormscope has failed.
Stormscope has failed. The system should be
serviced.
SVT DISABLED – Out of
available terrain region.
Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
database.
SVT DISABLED – Terrain
DB resolution too low.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second or
better) is not currently installed.
SW MISMATCH – GDU
software version
mismatch. Xtalk is off.
The MFD and PFDs have different software versions
installed. The system should be serviced.
SYSTEM CONFIG –
SYSTEM config error.
Config service req’d.
The system configuration has changed unexpectedly.
The system should be serviced.
TCAS FAIL –TCAS system
is inoperative.
The TCAS system has failed. The system should be
serviced.
TERRAIN AUD CFG –Trn
Awareness audio config
error. Service req’d
TAWS is disabled because the audio configuration is
invalid. The system should be serviced.
TERRAIN DISABLED –
Terrain Awareness DB
resolution too low.
TAWS is disabled because a terrain database of
sufficient resolution (4.9 arc-second or better) is not
currently installed.
TIMER EXPIRD – Timer
has expired.
The system notifies the pilot that the timer has
expired.
TRAFFIC FAIL – Traffic
device has failed.
The system is no longer receiving data from the
traffic system. The traffic device should be serviced.
TCAS FAIL - TCAS system
is inoperative.
The TCAS or TAS system is not operational.
Index
Appendix
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Message criteria entered by the user.
Abnormal
Operation
Message Advisory
SCHEDULER [#] –
Annunciations
& Alerts
Flight
Instruments
Annunciations & Alerts
212
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Comments
UNABLE V WPT – Can’t
reach current vertical
waypoint.
The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system automatically
transitions to the next vertical waypoint.
EIS
Terrain Awareness audio is unavailable. The system
should be serviced.
Flight
Instruments
Message Advisory
TRN AUD FAIL – Trn
Awareness audio source
unavailable
Audio Panel
and CNS
The current track angle error exceeds the limit,
VNV– UNAVAILABLE.
Excessive track angle error. causing the vertical deviation to go invalid.
WPT ARRIVAL – Arriving
at waypoint -[xxxx]
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
WX ALERT – Possible
severe weather ahead.
The GWX 68 indicates severe weather within ±10
degrees of the aircraft heading at a range of 80 to
320 nm.
XPDR1 ADS-B 1090 –
Datalinik: ADS-B 1090
receiver has failed.
A failure has been detected in the 1090 receiver.
XPDR1 ADS-B FAIL –
Transponder: XPDR1 is
unable to transmit ADS-B
messages.
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when possible.
XPDR1 ADS-B NO POS –
Transponder: ADS-B is not
transmitting position.
The transponder is not able to receive position
information.
Annunciations
& Alerts
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
Abnormal
Operation
VNV– UNAVAILABLE.
Unsupported leg type in
flight plan.
Additional
Features
A parallel course has been selected, causing the
vertical deviation to go invalid.
AFCS
VNV– UNAVAILABLE.
Parallel course selected.
Hazard
Avoidance
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
Flight
Management
VNV– UNAVAILABLE.
Excessive crosstrack error.
190–02362–00 Rev. A
A failure has been detected in the UAT receiver.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
XPDR1 ADS-B UAT –
Datalink: ADS-B in UAT
receiver has failed.
Appendix
The Transponder is incapable of processing traffic
XPDR1 ADS-B TRFC –
Transponder: ADS-B traffic information.
has failed
213
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Message Advisory
XPDR1 CONFIG – XPDR1
config error. Config
service req’d.
Comments
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
XPDR1 CSA FAIL - Traffic: ADS-B Conflict Situational Awareness (CSA) is
unavailable.
ADS-B In traffic alerting
has failed.
XPDR1 FAIL – XPDR1 is
inoperative.
There is no communication with the #1 or #2
transponder.
XPDR1 FAULT – Datalink:
ADSB-B in has failed.
The transponder is unable to receive ADS-B
information.
XPDR1 FIS-B WX –
Datalink: FIS-B Weather
has failed.
The transponder is unable to receive FIS-B weather
information.
XPDR1 OVER TEMP Transponder: Transponder
over temp.
The system has detected an over temperature
condition in XPDR1. The transmitter operates at
reduced power. If the problem persists, the system
should be serviced.
XPDR1 PRES ALT –
Transponder: ADS-B no
pressure altitude.
Unable to provide pressure altitude information.
XPDR1 SRVC – XPDR1
needs service. Return unit
for repair.
The #1 transponder should be serviced when
possible.
XPDR1 UNDER TEMP Transponder: Transponder
under temp.
The system has detected an under temperature
condition in XPDR1. The transmitter operates at
reduced power. If the problem persists, the system
should be serviced.
XTALK ERROR – A flight
display crosstalk error has
occurred.
The MFD and PFDs are not communicating with
each other. The system should be serviced.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
Flight Plan Import/Export
Flight plans can be imported from an SD Card or exported to an SD Card from the
Stored Flight Plan Page.
Under certain conditions, the following messages may appear when a flight plan is
imported or exported from or to an SD card. Some messages may appear in conjunction
with others.
214
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Flight
Instruments
‘File contained user waypoints
only. User waypoints imported
successfully. No stored flight plan
data was modified.’
The file stored on the SD card did not contain a
flight plan, only user waypoints. These
waypoints have been saved to the system user
waypoints. No flight plans stored in the system
have been modified.
‘No flight plan files found to
import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported
from the SD card.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully
imported from the SD card, however others
had errors and were not imported. A partial
stored flight plan now exists in the system.
‘File contained user waypoints
only.’
The file stored on the SD card did not contain a
flight plan, only user waypoints. One or more
of these waypoints did not import successfully.
‘Too many points. Flight plan
truncated.’
The flight plan on the SD card contains more
waypoints than the system can support. The
flight plan was imported with as many
waypoints as possible.
‘Some waypoints not loaded.
Waypoints locked.’
The flight plan on the SD card contains one or
more waypoints that the system cannot find in
the navigation database. The flight plan has
been imported, but must be edited within the
system before it can be activated for use.
‘User waypoint database full. Not
all loaded.’
The flight plan file on the SD card contains user
waypoints. The quantity of stored user
waypoints has exceeded system capacity,
therefore not all the user waypoints on the SD
card have been imported. Any flight plan user
waypoints that were not imported are locked in
the flight plan. The flight plan must be edited
within the system before it can be activated for
use.
Hazard
Avoidance
A flight plan file stored on the SD card was
successfully imported as a stored flight plan.
Flight
Management
‘Flight plan successfully
imported.’
Audio Panel
and CNS
Description
EIS
Flight Plan Import/Export
Results
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
215
Flight Plan Import/Export
Results
Description
‘One or more user waypoints
renamed.’
One or more imported user waypoints were
renamed when imported due to naming
conflicts with waypoints already existing in the
system.
‘Flight plan successfully
exported.’
The stored flight plan was successfully exported
to the SD card.
‘Flight plan export failed.’
The stored flight plan was not successfully
exported to the SD card. The SD card may not
have sufficient available memory or the card
may have been removed prematurely.
Table 20 Flight Plan Import/Export Messages
CREW PROFILE IMPORT/EXPORT MESSAGES
Crew Profiles
System settings may be saved under a crew profile. When the system is powered on,
the last selected crew profile is shown on the MFD Power-up Splash Screen. The system
can store up to 25 profiles; the currently active profile, the amount of memory used,
and the amount of memory available are shown at the top of the System Setup Page in
the box labeled “Crew Profile”. From here, crew profiles may be created, selected,
renamed, or deleted. Crew profiles may also be exported from the system to an SD card,
or imported from an SD card into the system.
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
Crew Profile Import/Export Messages
Annunciations
& Alerts
Abnormal
Operation
In some circumstances, some messages may appear in conjunction with others:
Message
Description
‘No crew profile files found.’
Displayed if the SD card does not have
one or more valid pilot profile filenames.
‘Overwrite existing profile?’
Displayed if the profile name matches
the name of existing profile.
Index
Appendix
‘Profile name invalid. Enter a different Displayed if the profile name is invalid.
profile name.’
216
‘All available crew profiles in use.
Delete a profile before importing
another.’
Displayed if the maximum number for
pilot profiles has been reached.
‘Crew profile import failed.’
Displayed if the importing operation fails
for any other reason.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Annunciations & Alerts
Description
‘Crew profile import succeeded.’
Displayed if the importing operation
succeeds.
‘Overwrite existing file?’
Displayed if the filename matches the
name of an existing file on the SD card.
‘Crew profile export failed.’
Displayed if the export operation fails.
‘Crew profile export succeeded.’
Displayed if the export operation
succeeds.
Flight
Instruments
Message
EIS
Audio Panel
and CNS
Table 21 Crew Profile Import/Export Messages
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
217
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Annunciations & Alerts
BLANK PAGE
218
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Flight
Instruments
APPENDIX
Softkey Function
Flight
Management
Hazard
Avoidance
Softkey Names
(displayed)
Bezel-Mounted
Softkeys (press)
Audio Panel
and CNS
Softkey On Softkey Subdued
EIS
Selection softkeys are located along the bottom of the displays. The softkeys shown
depend on the softkey level previously selected. The bezel keys below the softkey labels
can be used to select the appropriate softkey. There are three types of softkeys. One selects
a simple on/off state, indicated by an annunciator on the softkey label displayed as green
(on) or gray (off). The next type of softkey selects among several options, indicated by the
softkey label changing (with the exception of the Map Range keys) to reflect the name of
the chosen option. The last type of softkey, when pressed displays another set of softkeys
available for the selected function. Also, these softkeys revert to the previous level after 45
seconds of inactivity. When a softkey function is disabled, the softkey label is subdued
(dimmed).
Figure 57 Softkeys (First-Level PFD Configuration)
AFCS
PFD Softkeys
Abnormal
Operation
Annunciations
& Alerts
The following table describes PFD Softkey functions. Softkeys which display another
set of softkeys are indicated in the table by showing the given set as an increased level.
For example, the Map/HSI Softkey is shown in the Level 1 column. When pressed, the
Map/HSI softkey will display another set of softkeys and these softkeys are explained in
the Level 2 column. If a softkey on Level 2 provides yet another set of softkey functions,
those new available softkeys are then explained in the Level 3 column, etc.
Additional
Features
The PFD softkeys provide control over the PFD display and some flight management
functions, including GPS, NAV, terrain, traffic, and weather (optional). Each softkey
sublevel has a Back Softkey which can be pressed to return to the previous level. If new
messages remain after acknowledgement, the Messages Softkey will show “Message” in
black text with a white background. The Messages Softkey is visible in all softkey levels.
For the top level softkeys and the transponder (XPDR) levels, the Ident Softkey remains
visible.
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
219
Flight
Instruments
Appendix
Level 1
Level 2
Level 3
CAS
EIS
Audio Panel
and CNS
Flight
Management
CAS Up
Scroll up CAS messages
(Accessible only when the
CAS Softkey is displayed).
CAS Dn
Scroll down CAS
messages (Accessible only
when the CAS Softkey is
displayed).
Hazard
Avoidance
Displays the PFD Map
display settings softkeys.
Layout
Displays the PFD Map
selection softkeys.
Removes the PFD map
from display (Inset or
Traffic).
Inset Map
Displays the Inset Map.
Abnormal
Operation
Additional
Features
AFCS
Map Off
HSI Map
Displays the HSI Map.
Inset Trfc
Replaces the Inset Map
with a dedicated traffic
display.
HSI Trfc
Replaces the HSI Map
with a dedicated traffic
display.
Wx LGND
Annunciations
& Alerts
Description
Displays the scroll keys.
Only displayed when the
number of CAS messages
exceeds the capacity of
the display window.
Map/HSI
Displays/removes the
name of the selected
data link weather
provider (SiriusXM) and
the weather product icon
and age box (for enabled
weather products).
Index
Appendix
Level 4
220
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Level 2
Detail
Level 3
Level 4
Description
Selects desired amount of
map detail:
Flight
Instruments
Level 1
• All (No Declutter): All
EIS
map features visible.
• Detail
• Detail 2: Declutters land
and SUA data.
data.
Traffic
• Topo:
• REL:
• Off: Removes terrain
METAR
Displays METAR
information on PFD Map
(subscription optional).
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
221
Index
Displays Connext weather
and coverage on PFD
Map.
Displays XM NEXRAD
weather and coverage on
PFD Map (subscription
optional).
Appendix
PRECIP
or
NEXRAD
Annunciations
& Alerts
Displays/removes the
name of the selected
data link weather
provider (SiriusXM) and
the weather product icon
and age box (for enabled
weather products).
Abnormal
Operation
190–02362–00 Rev. A
WX LGND
Additional
Features
Displays relative
terrain information on
the PFD Map.
AFCS
Displays
topographical data (e.g.,
coastlines, terrain, rivers,
lakes) and elevation
scale on PFD Map.
Hazard
Avoidance
TER
Displays traffic
information on PFD Map.
Flight
Management
• Detail 3: Declutters land
Audio Panel
and CNS
1:
Removes
everything except for the
active flight plan.
Appendix
Flight
Instruments
Level 1
Level 2
Level 3
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Description
LTNG Off
Disables lightning
function on PFD Map.
The softkey annunciator
is green when the
lightning function is off.
Datalink
Selects the data link
weather source for the
PFD Map.
STRMSCP
Adds or removes the
display of Stormscope
information on the PFD
Map. The softkey
annunciator is green
when the function is on.
When the function is off,
the annunciator is gray.
TFC Map
Replaces the PFD Map
with a dedicated traffic
display. The default
display is the Inset Map.
PFD Opt
Displays second-level
softkeys for additional
PFD options.
SVT
Appendix
Level 4
Adds/removes the display
of SiriusXM lightning
information on PFD Map
(optional).
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Lightning
Displays additional SVT
overlay softkeys.
(optional)
Pathways
Displays Pathway Boxes
on the Synthetic Vision
Display.
Terrain
Enables synthetic terrain
depiction.
Displays compass heading
along the Zero-Pitch line.
Index
HDG LBL
222
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Level 2
Level 3
Level 4
APT Sign
Displays the wind option
softkeys.
Off
Wind direction arrow and
speed.
Option 2
Headwind/Tailwind and
crosswind components
and wind direction arrow.
Option 3
Wind direction arrow
with direction and speed.
Cycles the Bearing 1
Information Window
through NAV1, NAV2,
GPS/waypoint identifier
and GPS-derived distance
information, ADF/
frequency, and Off.
Sensors
Displays the sensor
selection softkeys.
ADC
ADC 1
Selects the #1 ADC.
ADC 2
Selects the #2 ADC.
Appendix
Index
AHRS
Displays ADC selection
softkeys.
Displays the AHRS
selection softkeys.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Annunciations
& Alerts
Bearing 1
Abnormal
Operation
Displays DME Information
(optional).
Additional
Features
DME
AFCS
Option 1
Hazard
Avoidance
Wind information not
displayed.
Flight
Management
Wind
Audio Panel
and CNS
Displays power lines on
the Synthetic Vision
Display.
EIS
Wire
190–02362–00 Rev. A
Description
Displays position markers
for airports within
approximately 15 nm of
the current aircraft
position. Airport
identifiers are displayed
when the airport is within
approximately 9 nm.
Flight
Instruments
Level 1
223
Appendix
Flight
Instruments
Level 1
Level 2
Level 3
Level 4
Description
AHRS 1 Selects the #1 AHRS.
AHRS 2 Selects the #2 AHRS.
Cycles the Bearing 2
Information Window
through NAV1, NAV2,
GPS/waypoint identifier
and GPS-derived distance
information, ADF/
frequency, and Off.
ALT Units
Displays softkeys to select
altitude unit parameters.
Flight
Management
Audio Panel
and CNS
EIS
Bearing 2
AFCS
Hazard
Avoidance
Meters
Additional
Features
STD Baro
IN
Press to display the BARO
setting as inches of
mercury.
HPA
Press to display the BARO
setting as hectopascals.
Sets barometric pressure
to 29.92 in Hg (1013 hPa
if metric units are
selected) and returns to
top-level softkeys.
OBS
Selects OBS mode on the
CDI when navigating by
GPS (only available with
active leg). When OBS is
on, the softkey
annunciator is green.
CDI
Cycles through GPS,
NAV1, and NAV2
navigation modes on the
CDI.
ADF/DME
Displays the ADF/DME
Tuning Window, allowing
selection and tuning of
the ADF and DME
(optional).
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
224
When enabled, displays
overlays altimeter with
meters.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Level 2
Level 3
XPDR
Description
Displays the transponder
selection softkeys.
Only available when two
transponders are
installed. Selects the #1
transponder as active.
EIS
XPDR 2
Only available when two
transponders are
installed. Selects the #2
transponder as active.
Audio Panel
and CNS
Standby
Selects transponder
Standby Mode
(transponder does not
reply to any
interrogations).
On
Activates transponder
(transponder replies to
identification
interrogations).
Alt
Altitude Reporting Mode
(transponder replies to
identification and altitude
interrogations).
VFR
Automatically enters the
VFR code (1200 in the
U.S.A. only).
Flight
Management
XPDR 1
Hazard
Avoidance
Abnormal
Operation
Use numbers to enter
code.
BKSP
Removes numbers
entered, one at a time.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Activates the Special
Position Identification
(SPI) pulse for 18
seconds, identifying the
transponder return on
the ATC screen.
Appendix
Ident
Annunciations
& Alerts
0–7
Additional
Features
Displays transponder
code selection softkeys
0-7.
AFCS
Code
190–02362–00 Rev. A
Level 4
Flight
Instruments
Level 1
225
Appendix
Flight
Instruments
Level 1
Level 2
EIS
Ident
Level 4
Description
Activates the Special
Position Identification
(SPI) pulse for 18
seconds, identifying the
transponder return on
the ATC screen.
Activates the Special
Position Identification
(SPI) pulse for 18
seconds, identifying the
transponder return on
the ATC screen.
Tmr/Ref
Displays References
Window.
Nearest
Displays Nearest Airports
Window.
Messages
or
Message
System generated
messages cause the
Messages Softkey label to
change from Messages to
a flashing ‘Message’
label. Pressing the
Message Softkey opens
the Messages Window,
acknowledges the
message, and the softkey
reverts to the ‘Messages’
label.
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Ident
Level 3
Table 22 PFD Softkeys
Annunciations
& Alerts
MFD Softkeys
Appendix
The MFD softkeys provide control over flight management functions, including GPS,
NAV, terrain, traffic, and weather (optional). There are many softkey functions available
on the MFD depending on the page group and screen selected.
Index
The following table provides an example of the MFD Softkey functions accessed from
the Navigation Map screen. Further information concerning softkeys providing more
navigation and flight planning functions may be found in the Flight Management
Section. Terrain, traffic, and weather softkey descriptions may be found in the Hazard
Avoidance section. Further description of optional equipment and corresponding
softkey functions may be found in the Additional Features Section.
226
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Appendix
Lvl 2
Lvl 3
Engine
Description
Displays EIS - Engine Page; press
again to exit page (see the EIS
Section for more information).
EIS
Decreases calculated fuel
remaining by 1 gallon for each
softkey press.
INC Fuel
Increases calculated fuel
remaining by 1 gallon for each
softkey press.
RST Fuel
Resets calculated fuel remaining
to default and resets fuel used to
zero.
Audio Panel
and CNS
DEC Fuel
Displays traffic information on
Navigation Map Page.
Inset
Displays inset window second
level softkeys.
AFCS
Traffic
Hazard
Avoidance
Displays second level Map
Options softkeys
Flight
Management
Map Opt
Flight
Instruments
Lvl 1
Removes VSD inset from
Navigation Map Page.
VSD
Displays VSD profile information
of terrain/obstacles along the
current track, vertical track
vector, and selected altitude.
• FPL:
Displays VSD profile
information for active flight
plan.
Displays VSD profile
information along current track.
Appendix
• TRK:
Annunciations
& Alerts
Automatically displays
either VSD profile information
for active flight plan information
or along current track with no
active flight plan.
Abnormal
Operation
• Auto:
Additional
Features
Off
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
227
Appendix
Flight
Instruments
Lvl 1
Lvl 2
TER
Lvl 3
Description
Displays terrain on the map;
cycles through the following:
No terrain information
shown on MFD Map.
EIS
• Off:
Displays topographical
data (e.g., coastlines, terrain,
rivers, lakes) and elevation scale
on MFD Map.
Audio Panel
and CNS
• Topo:
• REL: Displays relative terrain
Flight
Management
information on the MFD Map.
AWY
Displays airways on the map;
cycles through the following:
• Off: No airways are displayed.
Hazard
Avoidance
• On: All airways are displayed.
• LO: Only low altitude airways
are displayed.
AFCS
• HI: Only high altitude airways
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
are displayed.
STRMSCP
Displays Stormscope information
on Navigation Map Page
(optional).
NEXRAD
Displays XM NEXRAD weather
and coverage on Navigation
Map Page (optional).
XM LTNG
Displays XM lightning
information on Navigation Map
Page (optional).
METAR
Displays METAR information on
PFD Map (subscription optional).
Legend
Displays legends for the
displayed XM Weather products
(optional).
Displays weather information.
Index
Wx Radar
228
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
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Appendix
Lvl 2
Lvl 3
Description
Flight
Instruments
Lvl 1
Detail
Selects desired amount of map
detail; cycles through the
following levels:
visible.
EIS
• Detail All: All map features
• Detail-3: Declutters land data.
SUA data.
• Detail-1:
Charts
When available, displays optional
airport and terminal procedure
charts (optional).
Show Map displays the
applicable WPT Page information
upon the map for the chart
currently selected.
Chart displays the chart for the
WPT Page that is currently
selected and returns to the
Charts Level 2 Softkeys.
Info
Abnormal
Operation
DP
Pressing the Info 1 or Info 2
Softkey returns to the airport
diagram when the view is on a
different chart.
Additional
Features
Show Map
or
Chart
AFCS
Displays chart display settings
softkeys (if available).
Hazard
Avoidance
CHRT Opt
Flight
Management
Removes everything
except for the active flight plan.
Audio Panel
and CNS
• Detail-2: Declutters land and
Displays standard terminal arrival
procedure chart.
APR
Displays approach procedure
chart.
WX
Displays weather information.
Appendix
STAR
Annunciations
& Alerts
Displays departure procedure
chart.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
229
Appendix
Flight
Instruments
Lvl 1
Lvl 2
NOTAM
Checklist
Lvl 3
Description
Displays NOTAM information for
selected airport, when available.
EIS
When available, displays optional
checklists.
CAS Message Prioritization
NOTE: Refer to the Pilot’s Operating Handbook (POH) for corrective pilot
actions.
NOTE: Any CAS messages that are generated when the system is first powered
on are considered already acknowledged. They do not flash or trigger the
Warning or Caution softkeys.
The Alerting System uses three alert levels. Messages are grouped by criticality
(warning, caution, advisory) and sorted by order of appearance (most recent messages on
top). The color of the message is based on its urgency and on required action.
The Crew Alerting System (CAS) Window is located on the right side of the PFD.
Warning messages cannot be scrolled through and remain at the top of the CAS display.
The scroll bar appears if more caution and advisory messages exist than can be displayed
at once or if messages have been scrolled off the display. The CAS softkeys also become
available.
NOTE: Aural alerts associated with abnormal conditions and advisories are
managed through the audio panels. Refer to the Audio Panel and CNS Section
for more information.
• Warning: This level of alert requires immediate attention. When a new warning CAS
message appears in the CAS Window, it flashes (inversely red on white) in conjunction
with the Warning Softkey (see Figure 59) and may be accompanied by a repeating triple
chime. Pressing the Warning Softkey acknowledges all flashing warning messages and
extinguishes the softkey. Once acknowledged, warning messages are shown in red text
and are displayed until the issue is corrected. Warning voice alerts repeat continuously
until acknowledged by pressing the Warning Softkey.
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Table 23 MFD Navigation Map Page Softkeys
• Caution: This level of alert indicates the existence of abnormal conditions on the
Index
aircraft that may require intervention. When a new caution message appears in the CAS
Window, it is shown in black on amber inverse video in conjunction with the Caution
Softkey (see Figure 59) and may be accompanied by a double chime. Pressing the
Caution Softkey Indicator acknowledges all amber messages and extinguishes the
230
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
• Advisory: This level of alert provides general information. When a new white advisory
Flight
Instruments
softkey. Once acknowledged, caution messages are displayed until the issue is
corrected.
appears on the CAS display, it is shown in black on white inverse video in conjunction
with the Advisory Softkey (see Figure 59) and may be accompanied by a single chime.
EIS
Flight
Management
Hazard
Avoidance
CAS
Window
Audio Panel
and CNS
Some CAS messages can be display in more than one alert level group. For example, a
message might display as both a warning and a caution, but cannot appear more than
once at any given time (unless the CAS is being tested). If the received signals justify
multiple priorities for a certain message, the message is displayed for the higher priority
condition. When graduating to a higher priority, the message flashes and requires new
acknowledgment. When degrading to a lower priority condition, the message moves to
the top of the appropriate grouping, but does not require new acknowledgment.
AFCS
Additional
Features
Abnormal
Operation
Softkey
Annunci ation
Figure 58 CAS Message Prioritization
Annunciations
& Alerts
Figure 59 Softkey Annunciation (Message Softkey Labels)
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
231
Index
The following annunciations are configured specifically for the Piper Archer. Red
annunciation window text signifies warnings, amber signifies cautions, and white
signifies advisories. See the POH for recommended pilot actions.
Appendix
CAS Annunciations
Appendix
Flight
Instruments
Display Inhibits
Inhibits prevent certain CAS messages from being displayed during the following
conditions:
EIS
If two alert levels of the same message are active simultaneously (e.g., L FUEL QTY
warning and L FUEL QTY caution) only the higher alert level is displayed.
If a GEA or GIA fails, all CAS messages depending on sensors associated with that
LRU are automatically inhibited. Inhibits cannot be activated by invalid sensor data.
Audio Panel
and CNS
Warning Messages
Alternator 1 has failed
ALTR 2 FAIL
Alternator 2 has failed
AUTO DESCENT
HYPOXIA ALERT has been active for 60 seconds,
aircraft will begin descent in 60 seconds. Double
chime. ‘AUTO DESCENT - Automatic descent to
14,000FT in 60 seconds’ in Messages Window.
AUTO DESCENT
AUTO DESCENT has been active for 60 seconds,
EDM activated. Repeating double chime. ‘AUTO
DESCENT - Aircraft descending to 14,000FT’ in
Messages Window.
AUTO DESCENT
No interaction detected for four minutes after
aircraft reaches 14,000 feet. Repeating double
chime. ‘AUTO DESCENT - Aircraft descending to
12,500FT’ in Messages Window.
CABIN ALT 10K
Cabin altitude above 10,000 feet
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
CHECK GEAR
Landing gear not down and locked, or landing gear
selected UP when on ground
CO LVL HIGH
Carbon monoxide level is high
DOOR AJAR
Forward baggage door or cabin door is not closed
FUEL PRESS LOW
Fuel pressure is low
L FUEL QTY LOW
Left fuel quantity is in warning range
R FUEL QTY LOW
Right fuel quantity is in warning range
Index
GEAR SYS
232
Description
ALTR 1 FAIL
Hazard
Avoidance
Flight
Management
Annunciation Text
A component of the gear system has failed
PITOT HEAT FAIL
Pitot heat left and/or right failed
SPDBRAKES EXTD
Speedbrakes extended during takeoff
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
USP ACTIVE
Description
Flight
Instruments
Annunciation Text
Underspeed protection is active
Windshield heater over-temperature or controller
malfunction
EIS
WDSHLD
OVRTMP
Caution Messages
Description
Boost pump failed
CHECK GEAR
Landing gear not down and locked
CO LVL HIGH
Carbon monoxide level is high
Flight
Management
BOOST PUMP
FAIL
CPCS FAULT
Hazard
Avoidance
Cabin Pressure Controller has failed or lost ARINC
communication on the ground
CPCS FAIL
Cabin Pressure Controller has lost ARINC
communication
A flap system failure has occurred
FUEL IMBALANCE
Fuel imbalance is over 10.7 gallons
HYDR PUMP ON
Hydraulic pump is on and should not be on
HYPOXIA ALERT
ARE YOU ALERT? has been active for 60 seconds
OXYGEN GEN ON
Oxygen generation system has been turned on
Left pitot heat has failed
R PITOT HT FAIL
Right pitot heat has failed
PITOT HEAT OFF
Pitot heat selected off
PROP HEAT FAIL
Propeller heat failure
STALL HEAT FAIL
Stall heat selected on and OAT is equal to or less
than 5° C, but has not been activated
STALL WARN FAIL
Failure detected in stall warning system
START ENGAGED
Starter engaged when engine is running
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Speedbrakes extended during landing, or in flight
with engine off or being started
Appendix
SPDBRAKES EXTD
Annunciations
& Alerts
L PITOT HT FAIL
Abnormal
Operation
A component of the gear system has failed
Additional
Features
GEAR SYS
AFCS
FLAP FAIL
190–02362–00 Rev. A
Audio Panel
and CNS
Annunciation Text
233
Appendix
Flight
Instruments
Annunciation Text
Description
SURF DEICE FAIL
Surface de-ice fail
VAC PRESS LOW
Vacuum system pressure abnormal
EIS
Advisory Messages
Audio Panel
and CNS
Annunciation Text
Flight
Management
ARE YOU ALERT?
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
A period of inactivity exceeding limits has been
detected
AV1 FAN FAIL
Avionics 1 forward cooling fan has failed
AV2 FAN FAIL
Avionics 2 forward cooling fan has failed
AV3 FAN FAIL
Avionics 3 forward cooling fan has failed
DOOR AJAR
234
Description
Forward baggage door or cabin door is not closed
EMERG FUEL OFF
Emergency fuel off
EMERG FUEL ON
Emergency fuel on
FUEL IMBALANCE
Fuel imbalance is over 10.7 gallons
L FUEL QTY LOW
Left fuel quantity is in advisory range
R FUEL QTY LOW
Right fuel quantity is in advisory range
MAINT MODE ON
The maintenance mode is active
MFD FAN FAIL
The cooling fan for the MFD has failed
PFD1 FAN FAIL
The cooling fan for PFD1 has failed
PFD2 FAN FAIL
PFD2 FAN FAIL The cooling fan for PFD2 has failed
SPDBRAKES EXTD
Speedbrakes extended while on ground, or in flight
with engine running
STALL HEAT INHIB
Stall heat selected on and OAT is greater than 5° C,
but has not been activated
STALL HEAT ON
Stall heat is on
SURF DEICE ON
Normal surface de-ice cycle is active
VACUUM 1 FAIL
Vacuum pump 1 failure
VACUUM 2 FAIL
Vacuum pump 2 failure
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
The following aural alerts are announced by the system using a voice. If an optional
terrain system is installed, voice alerts are also generated (refer to the appropriate terrain
alerts section).
Priority
“Stall”
Warning
Warning
The aircraft has descended
below the preset barometric
minimum descent altitude.
Warning
The ‘CHECK GEAR’ CAS
message has been triggered.
Caution
The ‘CHECK GEAR’ CAS
message has been triggered.
Caution
The ESP system is engaging the
autopilot. See the AFCS section
for more details.
“Engaging autopilot”
Played when the optional GTS
825 traffic system fails a pilotinitiated self test.
Advisory
Aircraft is one minute from Top
of Descent. Issued only when
vertical navigation is enabled.
Advisory
Aircraft is outside TIS coverage
area
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
235
Index
Advisory
“Vertical track”
“TIS Not Available”
Played when the optional GTS
825 traffic system passes a
pilot-initiated self test.
Appendix
“TAS System Test
Failed”
Advisory
Annunciations
& Alerts
“TAS System Test
Passed”
Abnormal
Operation
Caution
Additional
Features
TAS Traffic Advisory (TA) is
issued with the optional GTS
825 TAS system. See the
Hazard Avoidance section for
additional details on GTS 825
voice alerts.
AFCS
Caution
“Traffic, (distance,
bearing, altitude)”
“Check gear”
TIS Traffic Advisory (TA) is
issued with the TIS system
Hazard
Avoidance
“Traffic”
Flight
Management
Aircraft has descended below
the preset barometric minimum
descent altitude
Audio Panel
and CNS
“Check gear”
Description
Imminent stall is sensed by stall
vane
Warning
”Airspeed”
“Minimums,
minimums”
EIS
Voice Alert
Flight
Instruments
Voice Alerts
Appendix
Flight
Instruments
Voice Alert
“Timer Expired”
EIS
“Incoming Call”
Priority
Description
Advisory
Countdown timer on the PFD
has reached zero
Advisory
A call has been received via the
Iridium system.
Audio Panel
and CNS
System Messages
Flight
Management
NOTE: This section provides information regarding message advisories that may
be displayed by the system. Knowledge of the aircraft, systems, flight
conditions, and other existing operational priorities must be considered when
responding to a message. Always use sound pilot judgment. The Pilot’s
Operating Handbook (POH) takes precedence over any conflicting guidance
found in this section.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
This section describes various system message advisories. Certain messages are issued
due to an LRU or an LRU function failure. Such messages are normally accompanied by
a corresponding red amber ‘X’ annunciation as shown previously in the System
Annunciation section.
Message Advisory
Comments
ABORT APR – Loss of
GPS navigation. Abort
approach.
Abort approach due to loss of GPS navigation.
ADC1 ALT EC – ADC1
altitude error correction is
unavailable.
GDC is reporting that the altitude error correction is
unavailable.
ADC1 AS EC – ADC1
airsp eed error correction
is unavailable.
GDC is reporting that the airspeed error correction is
unavailable.
ADC1 SERVICE – ADC1
needs service. Return unit
for repair.
The AHRS should be serviced..
ADC2 ALT EC – ADC1
altitude error correction is
unavailable.
GDC is reporting that the altitude error correction is
unavailable.
ADC2 AS EC – ADC1
airsp eed error correction
is unavailable.
GDC is reporting that the airspeed error correction is
unavailable.
ADC2 SERVICE – ADC1
needs service. Return unit
for repair.
The AHRS should be serviced..
236
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190–02362–00 Rev. A
Appendix
Comments
Flight
Instruments
Message Advisory
The cooling fan for the aft remote avionics has
AFT AV FAN FAIL – The
cooling fan for aft avionics failed.
has failed.
AHRS1 GPS – AHRS1 not
receiving backup GPS
information.
The #1 AHRS is not receiving backup GPS
information. The system should be serviced.
AHRS1 GPS – AHRS1
operating exclusively in
no-GPS mode.
The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
AHRS1 SRVC – AHRS1
Magnetic-field model
needs update.
The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
AHRS1 TAS – AHRS1 not
receiving valid airspeed.
The #1 AHRS is not receiving true airspeed from the
air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
AHRS12 CAL – AHRS2
calibration version error.
Srvc req’d
The #2 AHRS calibration version error. The system
should be serviced.
AHRS2 CONFIG – AHRS2
config error. Config
service req’d
#2 AHRS configuration settings do not match those
of backup configuration memory. The system should
be serviced.
AHRS2 GPS – AHRS2
using backup GPS source.
The #2 AHRS is using the backup GPS path. Primary
GPS path has failed. The system should be serviced
when possible.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The #1 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
Appendix
AHRS1 GPS – AHRS1 not
receiving any GPS
information.
Annunciations
& Alerts
The #1 AHRS is using the backup GPS path. Primary
GPS path has failed. The system should be serviced
when possible.
Abnormal
Operation
AHRS1 GPS – AHRS1
using backup GPS source.
Additional
Features
AHRS configuration settings do not match those of
backup configuration memory. The system should
be serviced.
AFCS
AHRS1 CONFIG – AHRS1
config error. Config
service req’d
Hazard
Avoidance
The #1 AHRS calibration version error. The system
should be serviced.
Flight
Management
AHRS1 CAL – AHRS1
calibration version error.
Srvc req’d
Audio Panel
and CNS
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
EIS
AHRS MAG DB – AHRS
magnetic model database
version mismatch.
237
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Message Advisory
Comments
AHRS2 GPS – AHRS2 not
receiving any GPS
information.
The #2 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
AHRS2 GPS – AHRS2 not
receiving backup GPS
information.
The #2 AHRS is not receiving backup GPS
information. The system should be serviced.
AHRS2 GPS – AHRS2
operating exclusively in
no-GPS mode.
The #2 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
AHRS2 SRVC – AHRS2
Magnetic-field model
needs update.
The #2 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
AHRS2 TAS – AHRS2 not
receiving valid airspeed.
The #2 AHRS is not receiving true airspeed from the
air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
APR ADVISORY – SBAS
VNAV not available.
SBAS VNAV not available. Check GPS sensor.
APR DWNGRADE –
Approach downgraded.
Vertical guidance generated by SBAS is unavailable,
use LNAV only minimums.
APR INACTV – Approach
is not active.
The system notifies the pilot that the loaded
approach is not active. Activate approach when
required.
ARSPC AHEAD –
Airspace ahead less than
10 minutes.
Special use airspace is ahead of aircraft. The aircraft
will penetrate the airspace within 10 minutes.
ARSPC NEAR – Airspace
near and ahead.
Special use airspace is near and ahead of the aircraft
position.
ARSPC NEAR – Airspace
near – less than 2 nm.
Special use airspace is within 2 nm of the aircraft
position.
AUDIO MANIFEST –
AUDIO MANIFEST
Incorrect audio software installed. The system
should be serviced
AUTO DESCENT –
Automatic descent to
14,000FT in 60 seconds.
HYPOXIA ALERT has been active for 60 seconds,
aircraft will begin descent in 60 seconds.
AUTO DESCENT –
Aircraft descending to
14,000FT.
AUTO DESCENT has been active for 60 seconds,
EDM activated.
238
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Comments
Flight
Instruments
Message Advisory
AUTO DESCENT –
Aircraft descending to
12,500FT.
No interaction detected for four minutes after
aircraft reaches 14,000 feet.
EIS
Selected course for LOC1 differs from published
CHECK CRS – Database
course for LOC1 / [LOC ID] localizer course by more than 10 degrees.
is [CRS]°.
The PFD1 configuration module backup memory has
failed. The system should be serviced.
Flight
Management
CNFG MODULE – PFD1
configuration module is
inoperative.
Audio Panel
and CNS
Selected course for LOC2 differs from published
CHECK CRS – Database
course for LOC2 / [LOC ID] localizer course by more than 10 degrees.
is [CRS]°.
Hazard
Avoidance
A failure in the carbon monoxide detector has been
CO DET FAIL – The
carbon monoxide detector detected. The system should be serviced.
is inoperative.
COM1 CONFIG – COM1
config error. Config
service req’d.
AFCS
A failure has been detected in carbon monoxide
CO DET SRVC – The
carbon monoxide detector detector has been detected. The detector may still
be available. The system should be serviced when
needs service.
possible.
The COM1 configuration settings do not match
backup configuration memory. The system should
be serviced
Additional
Features
COM1 PTT – COM1
push-to-talk key is stuck.
Abnormal
Operation
COM1 software mismatch. The system should be
COM1 MANIFEST –
serviced.
COM1 software
mismatch, communication
halted.
Annunciations
& Alerts
The COM1 external push-to-talk switch is stuck in
the enable (or “pressed”) position. Press the PTT
switch again to cycle its operation. If the problem
persists, the system should be serviced.
COM1 SERVICE – COM1
needs service. Return unit
for repair.
Appendix
COM1 RMT XFR – COM1 The COM1 transfer switch is stuck in the enabled (or
“pressed”) position. Press the transfer switch again
remote transfer key is
to cycle its operation. If the problem persists, the
stuck.
system should be serviced.
The system has detected a failure in COM1. COM1
may still be usable. The system should be serviced
when possible.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
239
Message Advisory
Comments
COM1 TEMP – COM1
over temp. Reducing
transmitter power.
The system has detected an over temperature
condition in COM 1. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
COM2 CONFIG – COM2
config error. Config
service req’d.
The COM2 configuration settings do not match
backup configuration memory. The system should
be serviced
COM2 software mismatch. The system should be
COM2 MANIFEST –
serviced.
COM2 software
mismatch, communication
halted.
COM2 PTT – COM2
push-to-talk key is stuck.
The COM2 external push-to-talk switch is stuck in
the enable (or “pressed”) position. Press the PTT
switch again to cycle its operation. If the problem
persists, the system should be serviced.
The system has detected a failure in COM2. COM2
may still be usable. The system should be serviced
when possible.
COM2 TEMP – COM2
over temp. Reducing
transmitter power.
The system has detected an over temperature
condition in COM2. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
CNFG MODULE – PFD1
configuration module is
inoperative.
The PFD1 configuration module backup memory has
failed. The system should be serviced.
DATA LOST – Pilot stored
data was lost. Recheck
settings.
The pilot profile data was lost. System reverts to
default pilot profile and settings. The pilot may
reconfigure the MFD & PFD with preferred settings,
if desired.
DB CHANGE – Database
changed. Verify user
modified procedures.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures in
stored flight plans are correct and up to date.
Index
Appendix
Annunciations
& Alerts
COM2 SERVICE – COM2
needs service. Return unit
for repair.
Additional
Features
COM2 RMT XFR – COM2 The COM2 transfer switch is stuck in the enabled (or
“pressed”) position. Press the transfer switch again
remote transfer key is
to cycle its operation. If the problem persists, the
stuck.
system should be serviced.
Abnormal
Operation
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
240
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190–02362–00 Rev. A
Appendix
Comments
ESP is not configured properly. The system should be
serviced.
ESP FAIL – ESP IAS mode
is inoperative.
IAS mode of ESP is inoperative. The system should
be serviced.
ESP DEGRADE – ESP is
inoperative.
The ESP function has failed and is inoperative. The
system should be serviced.
ESP OFF – ESP selected
off.
Electronic Stability and Protection has been disabled
on the SYSTEM SETUP 2 page.
EXCEEDANCE – Engine
exceedance data is being
logged.
An engine exceedance log has been captured
FAILED PATH – A data
path has failed.
A data path connected to the GDU, GSD 41, or the
GIA 63/W has failed.
FPL TRUNC – Flight plan
has been truncated.
This occurs when a newly installed navigation
database eliminates an obsolete approach or arrival
used by a stored flight plan. The obsolete procedure
is removed from the flight plan. Update flight plan
with current arrival or approach.
Annunciations
& Alerts
ESP CONFIG – ESP config
error. Config service req’d
Abnormal
Operation
The PFDs and MFD have different terrain database
versions or types installed. Install correct terrain
database version or type in all displays.
Additional
Features
DB MISMATCH – Terrain
database mismatch.
AFCS
The PFDs and MFD have different obstacle database
installed. Install correct obstacle database in all
displays.
Hazard
Avoidance
DB MISMATCH –
Obstacle database
mismatch.
Flight
Management
The PFDs and MFD have different navigation
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
Audio Panel
and CNS
DB MISMATCH –
Navigation database
mismatch. Xtalk is off.
EIS
This occurs when a stored flight plan contains an
airway that is no longer consistent with the
navigation database. This alert is issued only after an
navigation database update. Verify use of airways in
stored flight plans and reload airways as needed.
Flight
Instruments
Message Advisory
DB CHANGE – Database
changed. Verify stored
airways.
Appendix
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
241
Message Advisory
Upon power-up, the system detects that a stored
flight plan waypoint is locked. This occurs when an
navigation database update eliminates an obsolete
waypoint. The flight plan cannot find the specified
waypoint and flags this message. This can also occur
with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database, or update the
waypoint name/identifier to reflect the new
information.
FPL WPT MOVE – Flight
plan waypoint moved.
The system has detected that a waypoint coordinate
has changed due to a new navigation database
update. Verify that stored flight plans contain
correct waypoint locations.
FS510 CARD ERROR –
FS510 not detected in
MFD Bottom Slot.
The SD card was removed from the bottom card slot
of the MFD. The SD card needs to be reinserted.
G/S1 FAIL – G/S1 is
inoperative.
A failure has been detected in glideslope receiver 1.
The system should be serviced.
G/S1 SERVICE – G/S1
needs service. Return unit
for repair.
A failure has been detected in glideslope receiver 1.
The receiver may still be available. The system
should be serviced when possible.
G/S2 FAIL – G/S2 is
inoperative.
A failure has been detected in glideslope receiver 2.
The system should be serviced.
G/S2 SERVICE – G/S2
needs service. Return unit
for repair.
A failure has been detected in glideslope receiver 1.
The receiver may still be available. The system
should be serviced when possible.
GAE 43 FAILURE – Using
controller cabin
information.
A failure has been detected in the altitude encoder.
The cabin altitude controller information is being
used.
GCU1 CONFIG – GCU1
Config error. Config
service req’d.
GCU 476 configuration settings do not match those
of backup configuration memory. The G1000 system
should be serviced.
GCU1 FAIL – GCU1 is
inoperative.
A failure has been detected in the GCU 476. The
GCU 476 is unavailable.
GCU1 KEYSTK – GDC1
software mismatch,
communication halted.
A key is stuck on the GCU 476 bezel. Attempt to
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
Comments
FPL WPT LOCK – Flight
plan waypoint is locked.
EIS
Flight
Instruments
Appendix
242
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190–02362–00 Rev. A
Appendix
Comments
Flight
Instruments
Message Advisory
The GCU 476 has incorrect software installed. The
GCU1 MANIFEST –
GCU1 software mismatch, G1000 system should be serviced.
communication halted.
EIS
The GDC 74 has incorrect software installed. The
GDC1 MANIFEST –
GDC1 software mismatch, system should be serviced.
communication halted.
Audio Panel
and CNS
The GDC 74 has incorrect software installed. The
GDC2 MANIFEST –
GDC2 software mismatch, system should be serviced.
communication halted.
Flight
Management
GDL69 CONFIG – GDL 69 GDL 69AH configuration settings do not match
those of backup configuration memory. The system
config error. Config
should be serviced.
service req’d.
Hazard
Avoidance
GDL69 FAIL – GDL 69 has A failure has been detected in the GDL 69AH. The
receiver is unavailable. The system should be
failed.
serviced
The #1 GEA 71 has incorrect software installed. The
system should be serviced.
GEA2 CONFIG – GEA2
config error. Config
service req’d.
The GEA2 configuration settings do not match
those of backup configuration memory. The system
should be serviced.
GEA2 MANIFEST – GEA2
software mismatch,
communication halted.
The #2 GEA 71 has incorrect software installed. The
system should be serviced.
GEO LIMITS – AHRS1 too
far North/South, no
magnetic compass.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
invalid.
GEO LIMITS – AHRS2 too
far North/South, no
magnetic compass.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
invalid.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
GEA1 MANIFEST – GEA1
software mismatch,
communication halted.
Appendix
The GEA1 configuration settings do not match
those of backup configuration memory. The system
should be serviced.
Annunciations
& Alerts
GEA1 CONFIG – GEA1
config error. Config
service req’d.
Abnormal
Operation
Increases in map range are automatically limited at >
68 degrees 35 minutes north or south.
Additional
Features
GDU ZOOM LIMITED –
Map zoom has been
automatically limited.
AFCS
The GDL 69AH has incorrect software installed. The
GDL69 MANIFEST –
system should be serviced.
GDL69 software
mismatch, communication
halted.
243
Message Advisory
Comments
GFC MANIFEST – GFC
software mismatch,
communication halted.
Incorrect servo software is installed, or gain settings
are incorrect.
GIA1 COOLING – GIA1
temperature too low.
The GIA1 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
GIA1 COOLING – GIA1
over temperature.
The GIA1 temperature is too high. If problem
persists, the system should be serviced.
GIA1 CONFIG – GIA1
config error. Config
service req’d.
The GIA1 configuration settings do not match
backup configuration memory. The system should
be serviced.
GIA1 CONFIG – GIA1
audio config error. Config
service req’d.
The GIA1 have an error in the audio configuration.
The system should be serviced.
GIA1 MANIFEST – GIA1
software mismatch,
communication halted.
The GIA1 has incorrect software installed. The
system should be serviced.
GIA1 SERVICE – GIA1
needs service. Return the
unit for repair.
The GIA1 self-test has detected a problem in the
unit. The system should be serviced.
GIA2 COOLING – GIA2
temperature too low.
The GIA2 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
GIA2 COOLING – GIA2
over temperature.
The GIA2 temperature is too high. If problem
persists, the system should be serviced.
GIA2 CONFIG – GIA2
config error. Config
service req’d.
The GIA2 configuration settings do not match
backup configuration memory. The system should
be serviced.
GIA2 CONFIG – GIA2
audio config error. Config
service req’d.
The GIA2 have an error in the audio configuration.
The system should be serviced.
GIA2 MANIFEST – GIA2
software mismatch,
communication halted.
The GIA 2 has incorrect software installed. The
system should be serviced.
GIA2 SERVICE – GIA2
needs service. Return the
unit for repair.
The GIA2 self-test has detected a problem in the
unit. The system should be serviced.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
244
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Appendix
Comments
Flight
Instruments
Message Advisory
GMA1 AUX MANIFEST – The digital audio controller has incorrect software
installed. The system should be serviced.
GMA 1 AUX software
mismatch, communication
halted.
GMA1 FAIL – GMA1 is
inoperative.
The audio panel self-test has detected a failure. The
audio panel is unavailable. The system should be
serviced.
Audio Panel
and CNS
The audio panel configuration settings do not match
backup configuration memory. The system should
be serviced.
EIS
GMA1 CONFIG – GMA1
config error. Config
service req’d.
A failure has been detected in the GMC 710. The
GMC 710 is unavailable.
GMC KEYSTK – GMC is
inoperative.
A key is stuck on the GMC 710 bezel. Attempt to
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
GMC MANIFEST – GMC
software mismatch.
Communication halted.
The GMC 710 has incorrect software installed. The
G1000 system should be serviced.
Annunciations
& Alerts
GMC FAIL – GMC is
inoperative.
Abnormal
Operation
Error in the configuration of the GMC 710.
Additional
Features
GMC CONFIG – GMC
Config error. Config
service req’d.
AFCS
The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
Hazard
Avoidance
GMA1 SERVICE – GMA1
needs service. Return unit
for repair.
Flight
Management
The audio panel has incorrect software installed. The
GMA1 MANIFEST –
system should be serviced.
GMA1 software
mismatch, communication
halted.
Appendix
The GMU 44 has incorrect software installed. The
GMU1 MANIFEST –
system should be serviced.
GMU1 software
mismatch, communication
halted.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The GMU 44 has incorrect software installed. The
GMU2 MANIFEST –
system should be serviced.
GMU2 software
mismatch, communication
halted.
245
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Message Advisory
Comments
GPS NAV LOST – Loss of
GPS navigation.
Insufficient satellites.
Loss of GPS navigation due to insufficient satellites.
GPS NAV LOST – Loss of
GPS navigation. Position
error.
Loss of GPS navigation due to position error.
GPS NAV LOST – Loss of
GPS navigation. GPS fail.
Loss of GPS navigation due to GPS failure.
GPS1 SERVICE – GPS1
needs service. Return unit
for repair.
A failure has been detected in the GPS1 receiver.
The receiver may still be available. The system
should be serviced.
GPS2 SERVICE – GPS2
needs service. Return unit
for repair.
A failure has been detected in the GPS2 receiver.
The receiver may still be available. The system
should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in the #1 GSR 56H. The
system should be serviced.
GRS1 MANIFEST – GRS1
software mismatch,
communication halted.
The #1 AHRS has incorrect software installed. The
system should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in GSR2. The system
should be serviced.
GSR2 FAIL – GSR2 has
failed.
A failure has been detected in the #2 GSR 56H. The
system should be serviced.
GRS2 MANIFEST – GRS2
software mismatch,
communication halted.
The #2 AHRS has incorrect software installed. The
system should be serviced.
GSR1 FAIL – GSR1 has
failed.
A failure has been detected in GSR2. The system
should be serviced.
GTS CONFIG – GTS
config error. Config
service req’d.
The GTS and GDU have incompatible
configurations. This alert is also set when the GTS
has an invalid mode S address configured or the
mode S address does not match both XPDR mode S
addresses.
GTS MANIFEST – GTS
software mismatch,
communication halted.
The GTS 800 has incorrect software installed. The
G1000H system should be serviced.
GTX1 MANIFEST – GTX1
software mismatch,
communication halted.
The transponder has incorrect software installed.
The system should be serviced.
246
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Appendix
Comments
HDG FAULT – AHRS1
magnetometer fault has
occurred.
A fault has occurred in the #1 GMU 44. Heading is
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HDG FAULT – AHRS2
magnetometer fault has
occurred.
A fault has occurred in the #2 GMU 44. Heading is
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HW MISMATCH – GIA
hardware mismatch. GIA1
communication halted.
A GIA mismatch has been detected, where only one
is SBAS capable.
HW MISMATCH – GIA
hardware mismatch. GIA2
communication halted.
A GIA mismatch has been detected, where only one
is SBAS capable.
HDG PRESET MODE –
Magnetic anomoly
detected. HPM is
available.
The magnetometer has detected a magnetic
anomoly that could affect heading indications.
Heading Preset Mode may be used.
INCOMING CALL – Inside
airspace.
Incoming Iridium voice call.
INSIDE ARSPC –
Incoming call.
The aircraft is inside the airspace.
INVALID ADM – Invalid
ADM: ATN
communication halted.
Data link avionics were not configured correctly and
therefore will not be able to communicate with the
ground network.
Appendix
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
Annunciations
& Alerts
GWX SERVICE – GWX
needs service.
Abnormal
Operation
The GWX 68 has incorrect software installed. The
G1000 system should be serviced.
Additional
Features
GWX MANIFEST – GWX
software mismatch,
communication halted.
AFCS
The GDU is not receiving status packet from the
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.
Hazard
Avoidance
GWX FAIL – GWX is
inoperative.
Flight
Management
GWX 68 configuration settings do not match those
of the GDU configuration. The G1000 system
should be serviced.
Audio Panel
and CNS
GWX CONFIG – GWX
config error. Config
service req’d.
EIS
The transponder has incorrect software installed.
The system should be serviced.
Flight
Instruments
Message Advisory
GTX2 MANIFEST – GTX2
software mismatch,
communication halted.
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
247
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Message Advisory
Comments
LOCKED FPL – Cannot
navigate locked flight
plan.
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan. Update
flight plan with current waypoint.
LRG MAG VAR – Verify
all course angles.
The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
near the magnetic poles. Displayed magnetic course
angles may differ from the actual magnetic heading
by more than 2°.
LOI – GPS integrity lost.
Crosscheck with other
NAVS.
GPS integrity is insufficient for the current phase of
flight.
LOW BANK ACTIVE –
Disengage for approach.
Low Bank mode is active. Disengage to continue
approach.
LOW BANK ACTIVE –
Disengage for RNP less
than 1.0.
Low Bank mode is active. Disengage to continue
RNP 1.0.
MANIFEST – MFD1
software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MANIFEST – PFD1
software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MFD SOFTWARE – MFD The specified GDU has different software versions
mismatch, communication installed. The system should be serviced.
halted.
MFD TERRAIN DSP –
MFD Terrain awareness
display unavailable.
One of the terrain or obstacle databases required for
TAWS in the specified GDU is missing or invalid.
MFD1 CARD 1 ERR –
Card 1 is invalid.
The SD card in the top card slot of the specified PFD
or MFD contains invalid data.
MFD1 BACKLIGHT
CALIBRATION – MFD1
calibration. Return for
repair.
The specified GDU’s backlight calibration cannot be
found or is invalid. The system should be serviced.
MFD1 CARD 2 ERR –
Card 2 is invalid.
The SD card in the bottom card slot of the specified
MFD contains invalid data.
MFD1 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified MFD. The SD card needs to be
reinserted.
248
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Comments
The MFD detected a failure in the basemap
database.
MFD1 DB ERR – MFD1
Chartview database error
exists.
The MFD detected a failure in the ChartView
database (optional feature). Ensure the data card is
properly programmed if present. If problem persists,
the system should be serviced.
MFD1 DB ERR – MFD1
FliteCharts database error
exists.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure the data card is
properly programmed if present. If problem persists,
the system should be serviced.
MFD1 DB ERR – MFD1
navigation database error
exists.
The MFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1
obstacle database error
exists.
The MFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Annunciations
& Alerts
MFD1 DB ERR – MFD1
basemap database error
exists.
Abnormal
Operation
The detected a failure in the basemap database.
Additional
Features
MFD1 DB ERR – MFD1
basemap database error
exists.
AFCS
The MFD detected a failure in the Airport Directory
database. Ensure the data card is properly
programmed if present. If problem persists, the
system should be serviced.
Hazard
Avoidance
MFD1 DB ERR – MFD1
Airport Directory database
error exists.
Flight
Management
The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.
Audio Panel
and CNS
MFD1 CONFIG – MFD1
config error. Config
service req’d.
EIS
The SD card was removed from the bottom card slot
of the specified MFD. The SD card needs to be
reinserted.
Flight
Instruments
Message Advisory
MFD1 CARD 2 REM –
Card 2 was removed.
Reinsert card.
MFD1 DB ERR – MFD1
Safe Taxi database error
exists.
The MFD detected a failure in the Safe Taxi
database. Ensure the data card is properly
programmed if present. If problem persists, the
system should be serviced.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
190–02362–00 Rev. A
Appendix
The obstacle database is present on another LRU,
MFD1 DB ERR – MFD1
obstacle database missing. but is missing on the specified LRU.
249
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Message Advisory
Comments
MFD1 DB ERR – MFD1
terrain database error
exists.
The MFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1
terrain database missing.
The terrain database is present on another LRU, but
is missing on the specified LRU.
MFD1 VOLTAGE – MFD1
has low voltage. Reducing
power usage
The MFD voltage is low. The system should be
serviced.
MFD1 COOLING – MFD1
has poor cooling.
Reducing power usage.
The MFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
MFD1 KEYSTK – MFD
[key name] Key is stuck.
A key is stuck on the MFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
MFD1 MANIFEST –
MFD1 software mismatch,
communication halted.
The MFD has incorrect software installed. The
system should be serviced.
MFD1 SERVICE – MFD1
needs service. Return unit
for repair.
The MFD self-test has detected a problem. The
system should be serviced.
NAV1 RMT XFR – NAV1
remote transfer key is
stuck.
The remote NAV1 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the system should be serviced.
NAV1 SERVICE – NAV1
needs service. Return unit
for repair.
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
NAV2 RMT XFR – NAV2
remote transfer key is
stuck.
The remote NAV2 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the system should be serviced.
NAV2 SERVICE – NAV2
needs service. Return unit
for repair.
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
NO WGS84 WPT – Non
WGS 84 waypoint for
navigation -[xxxx]
The position of the selected waypoint [xxxx] is not
calculated based on the WGS84 map reference
datum and may be positioned in error as displayed.
Do not use GPS to navigate to the selected nonWGS84 waypoint.
250
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Appendix
Comments
The PFD detected a failure in the basemap database.
PFD1 DB ERR – PFD1
navigation database error
exists.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
PFD1 DB ERR – PFD1
obstacle database error
exists.
The PFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Hazard
Avoidance
PFD1 DB ERR – PFD1
basemap database error
exists.
Flight
Management
The PFD configuration settings do not match backup
configuration memory. The system should be
serviced.
Audio Panel
and CNS
PFD1 CONFIG – PFD1
config error. Config
service req’d.
EIS
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
Flight
Instruments
Message Advisory
PFD1 COOLING – PFD1
has poor cooling.
Reducing power usage.
AFCS
The obstacle database is present on another LRU,
PFD1 DB ERR – PFD1
obstacle database missing. but is missing on the specified LRU.
PFD1 KEYSTK – PFD1
[key name] Key is stuck.
A key is stuck on the PFD bezel. Attempt to free the
stuck key by pressing it several times. The system
should be serviced if the problem persists.
PFD1 MANIFEST – PFD1
software mismatch,
communication halted.
The PFD has incorrect software installed. The system
should be serviced.
PFD1 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified PFD. The SD card needs to be
reinserted.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The terrain database is present on another LRU, but
is missing on the specified LRU
Appendix
PFD1 DB ERR – PFD1
terrain database missing.
Annunciations
& Alerts
The PFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Abnormal
Operation
PFD1 DB ERR – PFD1
terrain database error
exists.
Additional
Features
PFD1 DB ERR – PFD1 Safe The PFD detected a failure in the Safe Taxi database.
Taxi database error exists. Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
251
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Message Advisory
Comments
PFD1 CARD 2 REM– Card The SD card was removed from the bottom card slot
of the specified PFD. The SD card needs to be
2 was removed. Reinsert
reinserted.
card.
PFD1 CARD 1 REM ERR –
Card 1 is invalid.
The SD card in the top card slot of the specified PFD
contains invalid data.
PFD1 CARD 2 ERR – Card The SD card in the bottom card slot of the specified
PFD contains invalid data.
2 is invalid.
PFD1 SERVICE – PFD1
needs service. Return unit
for repair.
The PFD self-test has detected a problem. The
system should be serviced.
PFD1 VOLTAGE – PFD1
has low voltage. Reducing
power usage
The PFD1 voltage is low. The system should be
serviced.
PILOT RADIOS MUTED –
Pilot radios are muted.
The pilot radios are set on mute
PFD2 COOLING – PFD2
has poor cooling.
Reducing power usage.
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
PFD2 CONFIG – PFD2
config error. Config
service req’d.
The PFD configuration settings do not match backup
configuration memory. The system should be
serviced.
PFD2 DB ERR – PFD2
basemap database error
exists.
The PFD detected a failure in the basemap database.
PFD2 DB ERR – PFD2
navigation database error
exists.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should be
serviced.
PFD2 DB ERR – PFD2
obstacle database error
exists.
The PFD detected a failure in the obstacle database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
The obstacle database is present on another LRU,
PFD2 DB ERR – PFD2
obstacle database missing. but is missing on the specified LRU.
PFD2 DB ERR – PFD2 Safe The PFD detected a failure in the Safe Taxi database.
Taxi database error exists. Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
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Appendix
Comments
A key is stuck on the PFD bezel. Attempt to free the
stuck key by pressing it several times. The system
should be serviced if the problem persists.
PFD2 MANIFEST – PFD2
software mismatch,
communication halted.
The PFD has incorrect software installed. The system
should be serviced.
PFD2 CARD 1 REM –
Card 1 was removed.
Reinsert card.
The SD card was removed from the top card slot of
the specified PFD. The SD card needs to be
reinserted.
Hazard
Avoidance
PFD2 KEYSTK – PFD2
[key name] Key is stuck.
Flight
Management
The terrain database is present on another LRU, but
is missing on the specified LRU
Audio Panel
and CNS
PFD21 DB ERR – PFD2
terrain database missing.
EIS
The PFD detected a failure in the terrain database.
Ensure the data card is properly programmed if
present. If problem persists, the system should be
serviced.
Flight
Instruments
Message Advisory
PFD2 DB ERR – PFD2
terrain database error
exists.
PFD2 CARD 2 REM– Card The SD card was removed from the bottom card slot
of the specified PFD. The SD card needs to be
2 was removed. Reinsert
reinserted.
card.
The SD card in the top card slot of the specified PFD
contains invalid data.
AFCS
PFD2 CARD 1 REM ERR –
Card 1 is invalid.
PTK FAIL – Parallel track
unavailable: bad
geometry.
Bad parallel track geometry.
PTK FAIL – Parallel track
unavailable: invalid leg
type.
Invalid leg type for parallel offset.
PTK FAIL – Parallel track
unavailable: past IAF.
IAF waypoint for parallel offset has been passed.
REGISTER GFDS – Data
services are inoperative,
register w/Connext.
The system is not registered with Connext, or its
current registration data has failed authentication.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
The PFD1 voltage is low. The system should be
serviced.
Appendix
PFD2 VOLTAGE – PFD2
has low voltage. Reducing
power usage
Annunciations
& Alerts
The PFD self-test has detected a problem. The
system should be serviced.
Abnormal
Operation
PFD2 SERVICE – PFD2
needs service. Return unit
for repair.
Additional
Features
PFD2 CARD 2 ERR – Card The SD card in the bottom card slot of the specified
PFD contains invalid data.
2 is invalid.
253
Comments
SLCT FREQ – Select
appropriate frequency for
approach.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.
SLCT NAV – Select NAV
on CDI for approach.
The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct NAV
receiver.
STEEP TURN – Steep turn
ahead.
A steep turn is 15 seconds ahead. Prepare to turn.
STRMSCP FAIL –
Stormscope has failed.
Stormscope has failed. The system should be
serviced.
SVT DISABLED – Out of
available terrain region.
Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
database.
SVT DISABLED – Terrain
DB resolution too low.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second or
better) is not currently installed.
SW MISMATCH – GDU
software version
mismatch. Xtalk is off.
The MFD and PFDs have different software versions
installed. The system should be serviced.
SYSTEM CONFIG –
SYSTEM config error.
Config service req’d.
The system configuration has changed unexpectedly.
The system should be serviced.
TCAS FAIL –TCAS system
is inoperative.
The TCAS system has failed. The system should be
serviced.
TERRAIN AUD CFG –Trn
Awareness audio config
error. Service req’d
TAWS is disabled because the audio configuration is
invalid. The system should be serviced.
TERRAIN DISABLED –
Terrain Awareness DB
resolution too low.
TAWS is disabled because a terrain database of
sufficient resolution (4.9 arc-second or better) is not
currently installed.
TIMER EXPIRD – Timer
has expired.
The system notifies the pilot that the timer has
expired.
TRAFFIC FAIL – Traffic
device has failed.
The system is no longer receiving data from the
traffic system. The traffic device should be serviced.
TCAS FAIL - TCAS system
is inoperative.
The TCAS or TAS system is not operational.
Index
Appendix
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Message criteria entered by the user.
Abnormal
Operation
Message Advisory
SCHEDULER [#] –
Annunciations
& Alerts
Flight
Instruments
Appendix
254
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
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Appendix
Comments
UNABLE V WPT – Can’t
reach current vertical
waypoint.
The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system automatically
transitions to the next vertical waypoint.
EIS
Terrain Awareness audio is unavailable. The system
should be serviced.
Flight
Instruments
Message Advisory
TRN AUD FAIL – Trn
Awareness audio source
unavailable
Audio Panel
and CNS
The current track angle error exceeds the limit,
VNV– UNAVAILABLE.
Excessive track angle error. causing the vertical deviation to go invalid.
WPT ARRIVAL – Arriving
at waypoint -[xxxx]
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
WX ALERT – Possible
severe weather ahead.
The GWX 68 indicates severe weather within ±10
degrees of the aircraft heading at a range of 80 to
320 nm.
XPDR1 ADS-B 1090 –
Datalinik: ADS-B 1090
receiver has failed.
A failure has been detected in the 1090 receiver.
XPDR1 ADS-B FAIL –
Transponder: XPDR1 is
unable to transmit ADS-B
messages.
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when possible.
XPDR1 ADS-B NO POS –
Transponder: ADS-B is not
transmitting position.
The transponder is not able to receive position
information.
Annunciations
& Alerts
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
Abnormal
Operation
VNV– UNAVAILABLE.
Unsupported leg type in
flight plan.
Additional
Features
A parallel course has been selected, causing the
vertical deviation to go invalid.
AFCS
VNV– UNAVAILABLE.
Parallel course selected.
Hazard
Avoidance
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
Flight
Management
VNV– UNAVAILABLE.
Excessive crosstrack error.
190–02362–00 Rev. A
A failure has been detected in the UAT receiver.
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
XPDR1 ADS-B UAT –
Datalink: ADS-B in UAT
receiver has failed.
Appendix
The Transponder is incapable of processing traffic
XPDR1 ADS-B TRFC –
Transponder: ADS-B traffic information.
has failed
255
Message Advisory
XPDR1 CONFIG – XPDR1
config error. Config
service req’d.
Comments
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
XPDR1 CSA FAIL - Traffic: ADS-B Conflict Situational Awareness (CSA) is
unavailable.
ADS-B In traffic alerting
has failed.
XPDR1 FAIL – XPDR1 is
inoperative.
There is no communication with the #1 or #2
transponder.
XPDR1 FAULT – Datalink:
ADSB-B in has failed.
The transponder is unable to receive ADS-B
information.
XPDR1 FIS-B WX –
Datalink: FIS-B Weather
has failed.
The transponder is unable to receive FIS-B weather
information.
XPDR1 OVER TEMP Transponder: Transponder
over temp.
The system has detected an over temperature
condition in XPDR1. The transmitter operates at
reduced power. If the problem persists, the system
should be serviced.
XPDR1 PRES ALT –
Transponder: ADS-B no
pressure altitude.
Unable to provide pressure altitude information.
XPDR1 SRVC – XPDR1
needs service. Return unit
for repair.
The #1 transponder should be serviced when
possible.
XPDR1 UNDER TEMP Transponder: Transponder
under temp.
The system has detected an under temperature
condition in XPDR1. The transmitter operates at
reduced power. If the problem persists, the system
should be serviced.
XTALK ERROR – A flight
display crosstalk error has
occurred.
The MFD and PFDs are not communicating with
each other. The system should be serviced.
Loading Updated Databases
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Index
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
256
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190–02362–00 Rev. A
Appendix
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
257
Index
190–02362–00 Rev. A
Appendix
The AOPA or AC-U-KWIK Airport Directory provides data on airports and heliports
throughout the U.S. or worldwide, respectively. The AOPA Directory offers detailed
information for over 5,300 U. S. airports, along with the names and phone numbers of
thousands of FBOs. These databases are updated every 56 days. The AC-U-KWIK
Annunciations
& Alerts
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the data,
but cannot guarantee the accuracy and completeness of the data.
Abnormal
Operation
The obstacle database contains data for obstacles, such as towers, that pose a potential
hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is
very important to note that not all obstacles are necessarily charted and therefore may not
be contained in the obstacle database. This database is updated on a 56-day cycle.
Additional
Features
The terrain database contains the terrain mapping data. These databases are updated
periodically and have no expiration date.
AFCS
The basemap database contains data for the topography and land features, such as
rivers, lakes, and towns. It is updated only periodically, with no set schedule. There is no
expiration date.
Hazard
Avoidance
The navigation database contains the aeronautical data used by the system for the flight
management and flight planning functions. Included is detailed data for waypoints,
procedures (arrivals, departures, approaches), and airways. The navigation database is
updated every 28 days.
Flight
Management
In some cases it may be necessary to obtain an unlock code from Garmin in order to
make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database features.
Audio Panel
and CNS
The cycles and dates for both standby and active databases are displayed on the “Aux –
Databases” page on the MFD. Any active databases with expiration dates in the past will
be highlighted with amber text. When an expired active database has a standby database
that is ready to become effective, a cyan double-sided arrow will be displayed between the
database cycles. When this arrow is visible, it indicates that the standby and active
databases in that row will be switched on the next power cycle, activating the current
standby database. Databases can also be manually selected (or deselected) by highlighting
a list item and pressing the ENT key, provided a valid, verified standby database is
present.
EIS
Databases may be loaded through Garmin Pilot and Flight Stream 510. When loading
databases through Garmin Pilot and the Flight Stream 510, it must be enabled on the
system and the multimedia card inserted in the bottom SD slot of the MFD.
Flight
Instruments
NOTE: When loading database updates, the ‘DB Mismatch’ system messages
will be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the Aux Database Page.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Directory offers detailed information for more than 8,000 airports with runways longer
than 3,000 feet worldwide.
The SafeTaxi database contains detailed airport diagrams for selected airports. These
diagrams aid in following ground control instructions by accurately displaying the aircraft
position on the map in relation to taxiways, ramps, runways, terminals, and services. This
database is updated on a 56-day cycle.
The FliteCharts database contains procedure charts for the United States only. This
database is updated on a 28-day cycle. If not updated within 180 days of the expiration
date, FliteCharts will no longer function.
The ChartView database is updated on a 14-day cycle. If the ChartView database is not
updated within 70 days of the expiration date, ChartView will no longer function. The
ChartView database must be purchased directly from Jeppesen, but can be update d at
jeppesen.com or flygarmin.com.
The IFR/VFR charts database contains VFR and IFR raster charts. The VFR Charts are
digital representations of the Sectional Aeronautical Charts and Terminal Area Charts. The
IFR Charts include both IFR High (designed for navigation at or above 18,000 ft) and IFR
Low (designed for navigation below 18,000 ft). IFR/VFR Charts are updated every 28 days
except for Canadian IFR/VFR Charts which are updated every 56 days.
Database Updates Using A Supplemental Data (SD) Card
Additional
Features
AFCS
All databases are updated through a single SD card in the bottom slot of the MFD.
When the card is inserted, the databases on the card will be copied to standby and
synchronized across all powered, configured units. After update, the card is removed
and the databases are stored on the system. When in standby, databases are not
immediately available for use, but stored to be activated at a later time.
Abnormal
Operation
Database updates can be obtained by following the instructions detailed in the
‘Aviation Databases’ section of the Garmin website (fly.garmin.com). Once the updated
files have been downloaded from the website, a PC equipped with an appropriate SD
card reader is used to unpack and program the new databases onto an existing
Supplemental Data Card. Equipment required to perform the update is as follows:
• Windows-compatible PC computer
Annunciations
& Alerts
• SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or
equivalent
• Updated database obtained from the Garmin website
Appendix
• Supplemental SD Cards
Index
In some cases it may be necessary to obtain an unlock code from Garmin in order to
make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database
features.
258
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190–02362–00 Rev. A
Appendix
With the system OFF, remove an SD Card from the bottom SD card slot of the
MFD.
2)
Download the databases and install them on an SD card.
3)
Put the SD Card in the bottom SD card slot of the MFD.
4)
Turn the system ON.
5)
Press the ENT Key or the right most softkey on MFD display to acknowledge the
startup screen.
6)
Turn the large FMS Knob to select the Aux page group on the MFD.
7)
Turn the small FMS Knob to select the Database page group on the MFD.
8)
Monitor the Sync Status on the Database page. Wait for all databases to
complete syncing, indicated by ‘Sync Complete’ being displayed. A cyan double
arrow will appear between the Standby and Active columns to show which
Standby databases will be transferred to Active at the next power cycle.
EIS
1)
Flight
Instruments
Updating Databases using an SD Card:
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
9)
Appendix
Figure 60 Databases Page before Activation of Standby Databases
Verify the correct database cycle information is shown in the Standby Database
column.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
259
Index
NOTE: The Restart Softkey is enabled only when the aircraft is on the ground.
10) Press the Restart Softkey. A 10 second restart countdown will appear.
11) Press the Restart Button in the display window to continue with the restart of
the system, or remove power from the system if the Restart Softkey is
diminished.
Figure 61 Database Restart
12) Remove the SD card from the bottom slot of the MFD.
13) After restarting the system, turn the large FMS Knob and select the Aux page
group on the MFD.
14) Turn the small FMS Knob and select the Databases page.
15) Verify that the standby databases transferred and are now in the active
database column.
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
Index
Figure 62 Databases Page with Updated Databases
16) To view database information for an individual display, press and then turn the
FMS Knob to select the database, and then press the Details Softkey. Press the
ENT Key or the FMS Knob to exit.
260
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
b)
Turn the small FMS Knob as necessary to select the database title.
c)
Press the ENT Key. A cyan double-sided arrow will appear indicating that
the standby database will become active.
d)
Remove and reapply power to the system.
e)
Verify that the standby databases transferred and are now in the active
database column.
Audio Panel
and CNS
Press the FMS Knob. The first database title on the screen will be selected.
18) Remove power from the system.
2)
Press the Update softkey when the Database Update screen appears.
Hazard
Avoidance
Insert the Flight Stream Multimedia Card in the bottom slot of the MFD.
Flight
Management
Updating Databases from any MFD page (except the Aux Databases page):
1)
EIS
a)
Flight
Instruments
17) To manually activate any databases that did not transfer to the active column:
AFCS
3)
The Flight Stream 510 will enter WI-FI mode. The following screen will appear.
Additional
Features
Figure 63 Database Update Available
Abnormal
Operation
Put the mobile device in WI-FI mode (refer to the Additional Features section).
5)
Connect the mobile device to the Flight Stream 510 WI-FI (refer to the
Additional Features section). The ‘WI-FI Not Connected’ screen will close when
the WI-FI connection is established.
6)
When the transfer is complete, the following screen will appear.
Appendix
4)
Annunciations
& Alerts
Figure 64 Starting Database Transfer
Index
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
261
EIS
Flight
Instruments
Appendix
7)
Press the Close softkey.
8)
When an existing database is expired and a new one is ready to become active,
a ‘Database Expired’ window will appear. Continue to the next step to restart
the system.
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
Figure 65 Database Transfer Complete
NOTE: The Restart Softkey is enabled only when the aircraft is on the ground.
9)
Select the Restart Softkey to restart the system and load the updated
database(s), or remove power from the system if the Restart Softkey is
diminished.
10) After restarting the system, turn the large FMS Knob and select the Aux page
group on the MFD.
11) Turn the small FMS Knob and select the Databases page.
12) Verify that the standby databases transferred and are now in the active
database column.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Figure 66 Database Expired
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Appendix
Flight
Instruments
EIS
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
Figure 67 Databases Page with Updated Databases
13) To view database information for an individual display, press and then turn the
FMS Knob to select the database, and then press the Details Softkey. Press the
ENT Key or the FMS Knob to exit.
AFCS
14) To manually activate any databases that did not transfer to the active column:
Additional
Features
b)
Turn the small FMS Knob as necessary to select the database title.
c)
Press the ENT Key. A cyan double-sided arrow will appear indicating that
the standby database will become active.
d)
Remove and reapply power to the system.
e)
Verify that the standby databases transferred and are now in the active
database column.
Annunciations
& Alerts
Press the FMS Knob. The first database title on the screen will be selected.
Abnormal
Operation
a)
Updating Databases from the Aux - Databases page:
2)
Turn the large FMS Knob to select the Aux page group on the MFD.
3)
Turn the small FMS Knob to select the Database page group on the MFD.
4)
Press the Device Softkey.
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
With the system OFF, insert the Flight Stream Multimedia Card in the bottom
slot of the MFD.
Appendix
1)
263
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
Appendix
5)
The Aux - Databases page will show the databases connected to the mobile
device in place of the active databases on the system. Databases selected to
load will be indicated by a cyan arrow.
6)
Press the Update softkey. The Flight Stream 510 will enter WI-FI mode.
7)
Put the mobile device in WI-FI mode (refer to the Additional Features section).
8)
Connect the mobile device to the Flight Stream 510 WI-FI (refer to the
Additional Features section).
9)
The Database Update status will appear in the Status window at the top of the
page.
NOTE: The Restart Softkey is enabled only when the aircraft is on the ground.
10) Select the Restart Softkey to restart the system and load the updated
database(s), or remove power from the system if the Restart Softkey is
diminished .
11) After restarting the system, turn the large FMS Knob and select the Aux page
group on the MFD.
13) Verify that the standby databases transferred and are now in the active
database column.
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
12) Turn the small FMS Knob and select the Databases page.
Figure 68 Databases Page with Updated Databases
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190–02362–00 Rev. A
Appendix
Flight
Instruments
14) To view database information for an individual display, press and then turn the
FMS Knob to select the database, and then press the Details Softkey. Press the
ENT Key or the FMS Knob to exit.
15) To manually activate any databases that did not transfer to the active column:
Turn the small FMS Knob as necessary to select the database title.
c)
Press the ENT Key. A cyan double-sided arrow will appear indicating that
the standby database will become active.
d)
Remove and reapply power to the system.
e)
Verify that the standby databases transferred and are now in the active
database column.
Flight
Management
b)
Audio Panel
and CNS
Press the FMS Knob. The first database title on the screen will be selected.
EIS
a)
16) Remove power from the system.
Magnetic Field Variation Database Update
Hazard
Avoidance
A copy of the current magnetic field variation database (MV DB) is included with the
navigation database. At startup, the system compares this version of the MV DB with that
presently being used by the AHRS. If the system determines the MV DB needs to be
updated, a prompt is displayed on the Navigation Map Page.
AFCS
Additional
Features
Figure 69 Magnetic Field Variation Database Update Prompt
Loading the magnetic field variation database update:
Abnormal
Operation
Annunciations
& Alerts
With ‘OK’ highlighted, as shown in the Magnetic Field Variation Database
Update Prompt figure, press the ENT Key on the MFD. A progress monitor is
displayed as shown in Figure 70. When the upload is complete, the system is
ready for use.
Appendix
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
Figure 70 Uploading Database
265
Map Symbols
This section discusses the types of land and aviation symbols that can be displayed.
Each listed type of symbol can be turned on or off, and the maximum range to display
each symbol can be set. The decluttering of the symbols from the map using the Detail
Softkey is also discussed.
EIS
Flight
Instruments
Appendix
Land Symbols
Audio Panel
and CNS
The following items are configured on the land menu:
Default
Range
(nm)
Max Range (nm)
User Waypoint
25
40
Highways and
Roads
N/A
N/A
Interstate
Highway
(Freeway)
50
400
International
Highway
(Freeway)
50
400
US Highway
(National
Highway)
15
150
State Highway
(Local Highway)
2.5
100
4
25
Railroads
(RAILROAD)
7.5
25
Large City (>
200,000)
100
1000
Medium City (>
50,000)
50
400
Small City (>
5,000)
25
100
State/Province
400
1000
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Land Symbols
N/A
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Local Road
(Local Road)
Symbol
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Appendix
Max Range (nm)
River/Lake
75
100
Latitude/
Longitude (LAT/
LON)
1
1000
Symbol
Flight
Instruments
Default
Range
(nm)
Land Symbols
EIS
Audio Panel
and CNS
Table 24 Land Symbol Information
Aviation Symbols
Max Range
(nm)
Large Airport (Longest
Runway >8100 ft)
100
1000
Medium Airport (8100 ft
> Longest Runway
>5000 ft)
50
400
25
150
1.5
5
7.5
150
N/A
N/A
Intersection (INT)
25
40
Non-directional Beacon
(NDB)
25
50
VOR
50
250
N/A
N/A
25
1000
Symbols
Taxiways (SafeTaxi)
See Additional Features
Visual Reporting Point
(VRP)
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
Index
N/A
Appendix
VOR Compass Rose
On/Off
N/A
Annunciations
& Alerts
Missed Approach
Preview On/Off (Missed
APR)
Abnormal
Operation
Runway Extension
Additional
Features
(Medium Airport if it has
a tower frequency)
AFCS
Small Airport (Longest
Runway < 5000 ft)
Hazard
Avoidance
Default
Range
(nm)
Aviation Symbols
Flight
Management
The following items are configured on the aviation menu:
267
Flight
Instruments
Appendix
Default
Range
(nm)
Max Range
(nm)
Temporary Flight
Restriction (TFR)
250
1000
VNAV Constraints
1000
1000
Symbols
EIS
Aviation Symbols
Audio Panel
and CNS
Table 25 Aviation Symbol Information
Airspace Symbols
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
The following items are configured on the airspace menu:
268
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
Appendix
Max Range
(nm)
Smart Airspace On/Off
N/A
N/A
N/A
Airspace Altitude Labels
(Airspace ALT LBL) On/Off:
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
Class B Airspace/TMA (CLASS
B/TMA)
50
150
Class C Airspace/TCA (CLASS
C/TCA)
50
100
Class D Airspace (CLASS D)
10
100
Alert/Prohibited/Restricted/
Warning Areas (RESTRICTED)
50
100
Military Operations Area
[MOA(MILITARY)]
50
250
Other/Air Defense Interdiction
Zone (OTHER/ADIZ)
50
250
Altitude Label (ceiling/floor)
• Class C Airspace
• Class D Airspace
Altitude Label (ceiling)
Flight
Management
Altitude Label (ceiling/floor)
Audio Panel
and CNS
• Class B Airspace
EIS
Default
Range
(nm)
Flight
Instruments
Symbol
Airspace Symbols
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Table 26 Airspace Symbol Information
Appendix
All navigation maps can display land, aviation and airspace symbols. Symbol types
(e.g. runway extensions, railroads) can be removed individually. The range sets the
maximum range at which items appear on the display. For example, enabling “Runway
Extension” displays a dashed line on the map extending from each runway of an airport
in the flight plan when the range is set at or below the value of the map settings option.
Annunciations
& Alerts
Symbol Setup
ARTCC Frequency or FSS Frequency
Index
Map Pointer (when panning)
190–02362–00 Rev. A
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
269
Flight
Instruments
Appendix
Measuring Pointer
EIS
User Waypoint
Vertical Navigation Along Track Waypoint
Audio Panel
and CNS
Unanchored Flight Path Waypoint
Flight
Management
Parallel Track Waypoint
Top of Descent (TOD)
Displayed when aircraft GPS location is valid, but heading is
invalid.
Bottom of Descent (BOD)
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Navigating using Dead Reckoning
270
Garmin G1000 NXi Cockpit Reference Guide for the Piper M350
190–02362–00 Rev. A
INDEX
Audio Panel
and CNS
Flight
Management
B
EIS
Bearing Pointers
Selecting bearing display and changing
sources:.............................................. 5
Blue-Select Mode................................. 22
Hazard
Avoidance
C
AFCS
Appendix
Index
I-1
Annunciations
& Alerts
D
Databases
Information.....................................160
Updating from any MFD Page......... 261
Updating from the Aux - Databases
Page............................................... 263
Updating Using an SD Card.... 258, 259
Dead Reckoning Mode....................... 167
Abnormal
Operation
COM Tuning Failure............................161
Command Bar Format
Changing the Command Bar Format...1
Comparator Annunciations.................163
Crew Alerting System (CAS)
Advisory Messages..................177, 234
CAS Annunciations................. 174, 231
CAS Message Prioritization..... 172, 230
Caution Messages...................176, 233
Display Inhibits........................174, 232
Warning Messages..................175, 232
Crew Profile....................................... 216
Import/Export Messages..................216
Additional
Features
Abnormal GPS Conditions.................. 162
Airport
Nearest Airport Information on MFD. 34
Nearest Airport Information on PFD.. 34
Select & Review by ID, name, or
location............................................ 33
Viewing Destination..........................34
Viewing Runway Information............ 34
Airspace
Changing altitude buffer distance..... 41
Reviewing Information...................... 29
Selecting and Viewing Alert
Information.......................................42
Turning On or Off Alert..................... 42
Turning Smart Airspace On/Off..........42
Airway
Displaying and Removing.................. 32
Selecting Range................................ 32
Along Track Offset
Entering Offset Distance................... 61
Altimeter
Selecting the altitude display units...... 1
Altimeter Baro Transition Alerts
Setting the Baro Transition Alerts........ 3
Altimeter Barometric Sync
Synchronizing the altimeter barometric
pressure settings................................. 2
Altimeter Overlays
Enabling altitude units overlays........... 2
Altimeter Selected Altitude
Setting the Selected Altitude...............2
Altitude Constraint
Chart................................................ 69
Deleting a Manual Entry....................71
Deleting Database-Generated........... 70
Entering/Modifying........................... 70
Invalid Causes................................... 69
Modifying system calculated............. 71
Reverting Manual back to Original.... 71
Annunciations.................................... 171
Power Up........................................159
Approach
Activating a Loaded With Vectors to
Final..................................................78
Activating a Previously Loaded.......... 78
Loading Into Active FP Using PROC Key
.........................................................76
Removing from Active FP.................. 78
Arrival
Loading into Active FP with PROC Key
.........................................................75
Removing from Active FP.................. 75
Auto-designation..................................67
Auto-Tuning
COM................................................ 15
NAV..................................................16
Flight
Instruments
A
Departure
Loading Into Active FP using PROC Key
.........................................................74
Removing from Active FP.................. 74
Direct-To
Cancelling.........................................45
Manual Course Selection.................. 44
Direct-To Destination
Entering waypoint, facility, or city......43
Selecting Active Flight Plan Waypoint 43
Selecting Nearest, Recent, or User
Waypoint.......................................... 44
DME
Displaying the DME Information
Window............................................. 5
DME Pairing......................................... 18
E
Electronic Stability and Protection (ESP)....
154
Emergency Frequency.........................161
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
INDEX
F
Flight Plan
Activating Leg...................................59
Activating Pending............................50
Activating Stored on MFD................. 55
Adding Airway..................................53
Adding Waypoint to Active............... 52
Changing View................................. 62
Closest Point in Active FP to a WPT... 63
Collapsing/Expanding Airways in Active
.........................................................63
Creating Active................................. 46
Creating/Adding User Waypoints to
Active............................................... 52
Deleting Active................................. 60
Deleting Airway from Active............. 60
Deleting All Pending......................... 51
Deleting Pending.............................. 51
Deleting Procedure from Active.........61
Deleting Waypoint from Active......... 60
Ignore Pending Transfer from Wireless
.........................................................49
Import/Export Messages..................214
Inverting Active.................................59
Inverting/Activating Stored on MFD...56
Previewing Pending Transfer from
Wireless............................................ 49
Storing Active from Page or Window 55
Storing Pending................................ 49
Frequency Spacing................................16
G
Index
Appendix
Annunciations
& Alerts
Global Positioning System (GPS)
Dead Reckoning Mode....................167
I-2
INDEX
Abnormal
Operation
Annunciations
& Alerts
Appendix
OBS Mode
Enabling/disabling OBS Mode while
navigating a GPS flight plan................ 5
Additional
Features
Magnetic Field Variation Database Update
.......................................................... 265
Manual Tuning
COM................................................ 15
NAV..................................................16
O
AFCS
M
Hazard
Avoidance
L
Landing Gear Indicator......................... 12
Line Replaceable Units (LRU)
Failure.............................................171
Flight
Management
Intercom...............................................20
Intercom Modes................................... 21
Intersection
Selection...........................................35
Navigation
Dead Reckoning Mode....................167
Navigation Data Bar
Changing a Field...............................27
Navigation Map
Auto North Up..................................27
Changing Orientation....................... 27
Configuring Automatic Zoom........... 28
Decluttering......................................31
Panning............................................ 28
Setting Topographic Display.............. 30
Setting up Additional Group Items.... 33
Setting up Land, Aviation or Airspace31
Non-Directional Beacon (NDB)
Selection...........................................35
Normal Operating Mode.....................160
Audio Panel
and CNS
I
N
EIS
Holding
Creating User-Defined at Active FP WPT
.........................................................64
Creating User-Defined at Direct-To WPT
.........................................................65
Creating User-Defined at Present
Position.............................................64
Exiting Active FP User-Defined Hold...66
Removing Active FP User-Defined Hold
.........................................................66
Removing Off-Route User-Defined Hold
.........................................................66
HSI CDI Sync
Synchronizing the CDIs....................... 4
HSI FMS CDI Setting
Changing the selected FMS CDI setting
...........................................................5
HSI Navigation Angles
Changing the navigation angle true/
magnetic setting................................. 4
HSI Navigation Sources
Changing navigation sources.............. 4
Map
Airspace Symbols............................ 268
Aviation Symbols............................ 267
Land Symbols..................................267
Symbol Setup..................................269
Minimum Descent Altitude/Decision
Height Alerting
Setting the Minimum Descent Altitude/
Decision Height and bug.....................7
Missed Approach
Activating in Active FP.......................79
Modifying Vspeed Bugs
Enabling/disabling or modifying
Individual Vspeed Reference Bugs....... 1
Multi Function Display (MFD)
Power Up........................................159
Softkeys..........................................226
Flight
Instruments
H
P
I-3
Index
Parallel Track
Activating......................................... 62
Cancelling.........................................62
Primary Flight Display (PFD)
Map Decluttering..............................32
Power Up........................................159
Setting Topographic Display.............. 30
Softkeys..........................................219
Procedure Loading
Available Procedures at Airport......... 72
Into Active FP from Information Page 73
R
RAIM
Predicting at Present Position............ 83
Predicting at Waypoint......................82
Reversionary Mode............................. 161
Reversionary Sensor Annunciations.....164
Runway
Selection...........................................33
S
Satellite-Based Augmentation System
(SBAS)
Disabling...........................................84
Softkeys
Function......................................... 219
Multi Function Display (MFD).......... 226
Primary Flight Display (PFD)............. 219
Speaker................................................ 20
Split-PA Mode...................................... 20
SVT in Reversionary Mode.................. 166
SVT Operation
Activating and deactivating Horizon
Headings............................................ 8
Activating and deactivating Pathways. 7
Activating and deactivating Wire
Obstacles on SVT................................ 8
Activating and deactivationg Airport
Signs...................................................8
Enabling and disabling SVT................. 7
Enabling and disabling SVT Field of
View on the Navigation Map...............8
SVT Troubleshooting...........................165
SVT Unusual Attitudes........................ 167
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
INDEX
I-4
T
Temperature Compensation Altitude
Cancelling.........................................79
Manually Activating.......................... 79
Temperature Displays
Changing temperature display units....6
Transponder Code Entry....................... 19
Transponder Mode Selection................ 18
Trip Statistics
Calculations via Manual Data Entry... 82
Selecting Automatic or Manual Page
Mode................................................81
Selecting Flight Plan and Leg.............82
Selecting Flight Plan or Waypoint Mode
.........................................................81
U
User Waypoint
Creating from Information Page........37
Creating from Map Pages................. 38
Selection...........................................36
V
Vertical Navigation
Waypoint Manual Designation.......... 69
Vertical Navigation (VNV)
Activating Direct-To...........................67
Altitude Constraints.......................... 67
Enabling/Disabling Guidance.............66
Entering Along-Track Offset for WPT.45
Modifying VS TGT and FPA............... 67
Removing Altitude Constraint........... 46
Vertical Situation Display (VSD)
Disabling...........................................72
Enabling........................................... 71
VHF Omni-directional Range (VOR)
Selection...........................................36
Visual Reporting Point (VRP)
Selection...........................................36
Voice Alerts................................ 193, 235
Vspeed Bugs
Enabling/disabling Individual Vspeed
Reference Bugs................................... 1
INDEX
Flight
Instruments
W
EIS
Waypoint
Reviewing Information...................... 29
Selecting for Waypoint Mode............82
Wind Data
Displaying wind data...........................6
Audio Panel
and CNS
Flight
Management
Hazard
Avoidance
AFCS
Additional
Features
Abnormal
Operation
Annunciations
& Alerts
Appendix
Index
I-5
Index
Appendix
Annunciations
& Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Audio Panel
and CNS
EIS
Flight
Instruments
INDEX
BLANK PAGE
I-6
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