Garmin | G1000 NXi: Piper PA-28-181 Archer | Garmin G1000 NXi: Piper PA-28-181 Archer Cockpit Reference Guide, G1000 PA-28-181 Archer

Garmin G1000 NXi: Piper PA-28-181 Archer Cockpit Reference Guide, G1000 PA-28-181 Archer
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Piper PA-28-181 Archer
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
NAV/COM/TRANSPONDER/AUDIO PANEL
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2698.01 or later for the
PA-28-181. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.
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Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin AT, Inc.
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Tel: 503.581.8101
Fax 503.364.2138
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Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
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Tel: 34-93-357-2608
Fax: 34-93-429-4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
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notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® G1000®, FliteCharts®, and SafeTaxi® are registered trademarks of Garmin International,
Inc. or its subsidiaries. Garmin ESP™, Garmin SVT™, and Connext™ are trademarks of Garmin
International, Inc. or its subsidiaries. These trademarks may not be used without the express
permission of Garmin.
Skywatch® and Stormscope® are registered trademarks of L-3 Communications. Ryan®, TCAD®
and Avidyne® are registered trademarks of Avidyne Corporation. CO Guardian is a trademark of
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King® and Honeywell® are registered trademarks of Honeywell International, Inc. Becker® is
a registered trademark of Becker Flugfunkwerk GmbH. NavData® is a registered trademark of
Jeppesen, Inc.; Wi-Fi® is a registered trademark of the Wi-Fi Alliance. Sirius XM Weather and
Sirius XM Satellite Radio are provided by Sirius XM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA 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 AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable 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 AOPA and, to the maximum extent allowed
by law, to release and 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 implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with 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.
Warnings, Cautions & 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 TAWS information for primary terrain or obstacle
avoidance. TAWS is intended only to enhance situational awareness.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Warnings, Cautions & Notes
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.
WARNING: Always obtain qualified instruction prior to operational use
of this equipment.
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.
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 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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Warnings, Cautions & Notes
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.
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on
the Garmin SVT display or may appear as a partial symbol.
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.
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.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Warnings, Cautions & Notes
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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Warnings, Cautions & 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
are assured compliance with all data quality requirements (DQRs) by
virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of
the Type 2 LOA is available for each database and can be viewed at http://
fly.garmin.com by selecting ‘Type 2 LOA Status.’
• 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.’
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Warnings, Cautions & Notes
NOTE: If the pilot/operator wants or needs to adjust the database,
contact Garmin Product Support to coordinate the revised DQRs.
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: 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 G1000 system power through at least one cycle in a
period of four days of continuous operation to avoid an autonomous
system reboot.
NOTE: The purpose of this Cockpit Reference Guide is to provide the
pilot a resource with which to find operating instructions on the
major features of the system more easily. It is not intended to be a
comprehensive operating guide. Complete operating procedures for the
system are found in the Pilot’s Guide for this aircraft.
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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Record of Revisions
Part Number
190-02131-00
Rev. A
Rev. B
Change Summary
Initial release
Clerical
Revision Date of Revision Affected Pages
C
October, 2016
All
190-02131-00 Rev. C
Description
Updated Bluetooth information
Updated Connext information
Updated SiriusXM information
Updated SiriusXM Weather
symbology
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
RR-13
Record of Revisions
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RR-14
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Table of Contents
FLIGHT INSTRUMENTS................................................................................................................. 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Displaying Altitude in Meters................................................................................................. 1
Setting Baro transition alert................................................................................................... 2
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 3
Turn ALL Vspeed Bugs On or Off............................................................................................. 3
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 4
ENGINE INDICATION..................................................................................................................... 5
Engine Display............................................................................................................................ 5
Engine Page................................................................................................................................ 7
Oil Pressure and Temperature Gauges................................................................................ 12
Fuel Quantity............................................................................................................................ 12
Crew Alerting System (CAS).................................................................................................. 13
NAV/COM/TRANSPONDER/AUDIO PANEL........................................................................ 15
Enter a Transponder Code..................................................................................................... 15
ADF Tuning (Optional)............................................................................................................. 15
DME Tuning............................................................................................................................... 15
Selecting a COM Radio........................................................................................................... 16
Selecting a NAV Radio............................................................................................................ 16
NAV/COM Tuning...................................................................................................................... 16
Intercom..................................................................................................................................... 16
Digital Clearance Recorder and Player............................................................................... 17
GPS NAVIGATION......................................................................................................................... 19
Direct-to Navigation............................................................................................................... 19
Activate a Stored Flight Plan................................................................................................ 20
Activate a Flight Plan Leg...................................................................................................... 20
Stop Navigating a Flight Plan............................................................................................... 21
Vertical Navigation (VNAV)................................................................................................... 21
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
i
Table of Contents
FLIGHT PLANNING....................................................................................................................... 23
Weight Planning....................................................................................................................... 23
Trip Planning............................................................................................................................. 23
Create a User Waypoint Defined by Latitude & Longitude............................................ 25
Create a User Waypoint Defined by Radials from Other Waypoints............................ 26
Create User Waypoint Defined by a Radial & Distance from Another Waypoint...... 27
Create a User Waypoint using the Map Pointer............................................................... 29
Delete a User Waypoint.......................................................................................................... 30
Create a Flight Plan................................................................................................................. 30
Import a Flight Plan from an SD Card................................................................................. 31
Insert a Waypoint in the Active Flight Plan....................................................................... 32
Insert an Along Track Offset Waypoint in the Active Flight Plan.................................. 33
Activate Parallel Track............................................................................................................ 33
Enter an Airway in a Flight Plan........................................................................................... 34
Collapse/Expand Airways in a Flight Plan.......................................................................... 34
Determine the Closest Point Along the Flight Plan to a Selected Waypoint............. 34
Create a User-Defined Hold at an Active Flight Plan Waypoint.................................... 35
Create a User-Defined Hold at the Aircraft Present Position........................................ 35
Remove a User-Defined Hold (Created at the Aircraft P.POS)....................................... 36
Remove a User-Defined Hold (Created at an Active Waypoint).................................... 36
Invert An Active Flight Plan................................................................................................... 36
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 37
Store a Flight Plan................................................................................................................... 37
Edit a Stored Flight Plan........................................................................................................ 37
Delete a Waypoint from the Flight Plan............................................................................. 38
Change the Flight Plan Comment........................................................................................ 38
Invert and Activate a Stored Flight Plan............................................................................ 39
Copy a Flight Plan.................................................................................................................... 39
Delete a Flight Plan................................................................................................................. 39
Graphical Flight Plan Creation.............................................................................................. 40
Export a Flight Plan to an SD Card...................................................................................... 40
PROCEDURES.................................................................................................................................. 41
Load and Activate a Departure Procedure........................................................................ 41
Activate a Departure Leg....................................................................................................... 41
Load an Arrival Procedure..................................................................................................... 41
Activate an Arrival Leg........................................................................................................... 42
Load and/or Activate an Approach Procedure.................................................................. 42
Activate an Approach in the Active Flight Plan................................................................ 43
Activate a Vector to Final Approach Fix............................................................................. 44
Activate a Missed Approach in the Active Flight Plan.................................................... 44
Remove a Procedure from the Active Flight Plan............................................................ 44
Temperature Compensated Altitude................................................................................... 45
ii
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Table of Contents
HAZARD AVOIDANCE................................................................................................................. 47
Customizing the Hazard Displays on the Navigation Map Page:.................................. 47
Sirius XM Weather (Optional)............................................................................................... 47
FIS-B Weather........................................................................................................................... 51
Traffic Advisory System (TAS)............................................................................................... 57
Terrain And Obstacle Proximity............................................................................................ 59
Terrain-SVT................................................................................................................................ 61
Terrain Awareness & Warning System (TAWS-B) Display (Optional)............................ 62
ADDITIONAL FEATURES............................................................................................................ 65
Synthetic Vision (Optional).................................................................................................... 65
Terminal Procedure Charts.................................................................................................... 66
Airport Directory..................................................................................................................... 69
Sirius XM Radio Entertainment............................................................................................ 69
Maintenance Logs WiFi........................................................................................................... 72
Pilot Profiles............................................................................................................................. 73
Connext Setup.......................................................................................................................... 76
ABNORMAL OPERATION.......................................................................................................... 79
Reversionary Mode................................................................................................................. 79
Abnormal COM Operation..................................................................................................... 79
Hazard Displays with Loss of GPS Position........................................................................ 79
Unusual Attitudes.................................................................................................................... 80
Dead Reckoning....................................................................................................................... 80
ANNUNCIATIONS & ALERTS.................................................................................................... 83
G1000 System Annunciations................................................................................................ 83
CAS Annunciations................................................................................................................... 85
Terrain-SVS Alerts.................................................................................................................... 86
Terrain-SVS System Status Annunciations......................................................................... 87
TAWS-B Alerts........................................................................................................................... 88
TAWS-B System Status Annunciations................................................................................ 89
GDL 69 SXM Data Link Receiver Messages........................................................................ 90
Voice Alerts............................................................................................................................... 91
System Message Advisories.................................................................................................. 91
Flight Plan Import/Export Messages................................................................................. 111
APPENDIX...................................................................................................................................... 113
PFD Softkey Map................................................................................................................... 113
Loading Updated Databases............................................................................................... 120
INDEX..........................................................................................................................................Index-1
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
EIS
Turn the BARO Knob to select the desired setting.
1)
Press the PFD Opt Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
Nav/Com/
XPDR/Audio
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
GPS Nav
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
2)
Press the ALT Units Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Procedures
Press the PFD Opt Softkey to display the second-level softkeys.
Flight
Planning
1)
Or:
4)
Hazard
Avoidance
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
2)
Press the ALT UNIT Softkey
3)
Press the METERS Softkey to turn on metric altitude readouts.
4)
Press the BACK Softkey to return to the top-level softkeys.
Annun/Alerts
Press the PFD Opt Softkey to display the second-level softkey.
Abnormal
Operation
1)
Additional
Features
DISPLAYING ALTITUDE IN METERS
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
1
SETTING BARO TRANSITION ALERT
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
1)
Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight Altitude in the BARO Transition Alert
box.
4)
Turn the small FMS Knob to turn the alert OFF or ON and press the ENT
Key.
5)
Turn the small FMS Knob to change the altitude and press the ENT Key.
6)
To cancel the selection, press the FMS Knob.
Flight
Planning
Procedures
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue 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 light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Press the OBS Softkey to select OBS Mode.
2)
Turn a 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 disable OBS Mode.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
1)
Hazard
Avoidance
CHANGE NAVIGATION SOURCES
2
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Instruments
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
GPS Nav
2)
Nav/Com/
XPDR/Audio
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
EIS
1)
Flight
Instruments
GENERIC TIMER
TURN ALL VSPEED BUGS ON OR OFF
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
Procedures
Press the TMR/REF Softkey.
Flight
Planning
1)
Hazard
Avoidance
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1) Press the TMR/REF Softkey.
Turn the large FMS Knob to highlight the OFF/BARO/TEMP COMP field to
the right of ‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to select BARO or TEMP COMP. OFF is
selected by default.
4)
Press the ENT Key or turn the FMS Knob to highlight the next field.
5)
Use the small FMS Knob to enter the desired altitude (BARO or TEMP
COMP from zero to 16,000 feet). If TEMP COMP was selected, a field for
entering the airport temperature will appear. Press the ENT Key or turn
the large FMS Knob to highlight this field, and use the small FMS Knob to
enter the temperature.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Additional
Features
2)
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
3
DISPLAYING WIND DATA
1)
Press the PFD Opt Softkey.
2)
Press the WIND Softkey to display wind data below the Selected Heading.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
4
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
EIS
Flight
Instruments
ENGINE INDICATION
ENGINE DISPLAY
EIS
1
Nav/Com/
XPDR/Audio
2
GPS Nav
3
Flight
Planning
4
Procedures
5
6
Hazard
Avoidance
7
8
Additional
Features
9
Abnormal
Operation
Engine Display when Engine Page is Displayed
1
Tachometer
(RPM)
2
Exhaust Gas Temperature Displays the exhaust gas temperature of the hottest cylinder
(EGT)
in °F
5
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Appendix
190-02131-00 Rev. C
Displays propeller speed in revolutions per minute
(rpm)
Annun/Alerts
Engine Display
3
Fuel Flow Indicator
(FFLOW GPH)
Displays fuel flow in gallons per hour (gph)
4
Oil Pressure Indicator
(OIL PSI)
Displays oil pressure in pounds per square inch (psi)
5
Oil Temperature Indicator Displays oil temperature in degrees Fahrenheit (°F)
(OIL °F)
6
Alternator Current
(ALTR AMPS)
Displays each alternator current in amperes
7
Voltage
(VOLTS)
Displays the bus voltage
8
Battery Current
(BATT AMPS)
Displays the battery current in amperes
9
Fuel Quantity Indicator
(FUEL QTY GAL)
Displays the amount of fuel in gallons (gal) for each
side of a standard fuel tank.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
EIS
6
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
EIS
Press the ENGINE Softkey or turn the large FMS Knob and select the EIS - Engine
Page.
10
EIS
11
Flight
Instruments
ENGINE PAGE
Nav/Com/
XPDR/Audio
1
2
GPS Nav
3
4
Flight
Planning
9
5
Procedures
8
6
Hazard
Avoidance
7
1
Tachometer
(RPM)
2
Exhaust Gas Temperature Displays the exhaust gas temperature in °F
(EGT °F)
3
Fuel Flow Indicator
(FFLOW GPH)
Displays fuel flow in gallons per hour (gph)
4
Oil Pressure Indicator
(OIL PSI)
Displays oil pressure in pounds per square inch (psi)
5
Oil Temperature Indicator Displays oil temperature in degrees Fahrenheit (°F)
(OIL °F)
6
Fuel Quantity Indicator
(FUEL QTY GAL)
Displays propeller speed in revolutions per minute
(rpm)
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Additional
Features
Engine Page
Displays the amount of fuel in gallons (gal) for each
side of a standard fuel tank.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
7
7
Carbon Monoxide
Displays the amount of carbon monoxide is present in
Detector
Parts Per Million (PPM)
(CO DETECTOR) (Optional)
8
Fuel Calculations Group
(FUEL CALC)
Displays calculated fuel used (GAL USED), endurance
(ENDUR), and range (in nautical miles, RANGE NM),
and fuel efficiency (in nautical miles per gallon, NMPG)
based on the displayed fuel remaining (GAL REM) and
the fuel flow totalizer
9
Engine Hours
(TACH TIME)
Displays the total time in hours the engine has been in
service
10
Exhaust Gas Temperature Displays exhaust gas temperatures for all cylinders in
(EGT °F)
°F
11
Electrical Group
(ELECTRICAL)
Displays alternator (ALTR AMPS) and battery (BATT
AMPS) currents in amperes and bus voltage (VOLTS)
Electrical
DC current for the alternator (shown in amperes) and voltage (shown in volts) for
the DC bus are shown along color-coded horizontal scales, with readouts above and
to the right of each scale. The ammeter displays the battery load in amperes (amps)
along a horizontal scale, with a white tick mark indicating zero amps. The horizontal
scales and pointers will not appear in Reversionary Mode.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
EIS
Annun/Alerts
Alternator
Current
Appendix
Bus Voltage
Index
Ammeter
Electrical Group
8
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
EIS
Nav/Com/
XPDR/Audio
Normal Operating
Temperatures
EIS
Exhaust Gas (EGT) temperature readout for each cylinder is shown at the top of the
graph. Cylinders with EGTs in the normal range appear in white. The temperature
readout is replaced with white dashes if the temperature exceeds the normal range.
Flight
Instruments
Exhaust Gas Temperature
GPS Nav
Flight
Planning
Procedures
Exhaust Gas Temperatures (Normal Range)
Hazard
Avoidance
Exceeded Operating
Temperature
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Exhaust Gas Temperatures (Exceeded Range)
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
9
Carbon Monoxide Detector (Optional)
Carbon Monoxide Detector (CO DETECTOR) is displayed on the Engine page,
below the TACH TIME. The carbon monoxide detector provides information in Parts
Per Million (PPM) and detects the amount of carbon monoxide present in PPM.
Reset the Carbon Monoxide Detector:
On the Engine Page, push CO RST softkey.
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
EIS
Flight
Planning
Carbon Monoxide Detector (CO DETECTOR)
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators
and are calculated from the last time the fuel was reset.
Fuel used (GAL USED), endurance (ENDUR), range (in nautical miles, RANGE
NM), and fuel efficiency (in nautical miles per gallon, NMPG) are calculated based on
the displayed fuel remaining (GAL REM) and the fuel flow totalizer. The calculated
range also takes into account the aircraft’s heading and the wind direction and speed.
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).
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Fuel Calculations
Index
Appendix
Annun/Alerts
Resetting the fuel totalizer:
On the Engine Page, press the RST FUEL Softkey; this resets displayed fuel
remaining (GAL REM) to the maximum fuel capacity for the aircraft and fuel
used to zero. Pressing the TABS Softkey resets the fuel remaining quantity
to the filler neck tabs quantity.
10
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
EIS
Flight
Instruments
Set Fuel Remaining
Calculated Fuel Used
EIS
Calculated Endurance
Nav/Com/
XPDR/Audio
Calculated Range
Fuel Efficiency
GPS Nav
Fuel Calculations Group
Additional
Features
Abnormal
Operation
Annun/Alerts
2)
Press the MENU Key.
3)
Highlight ‘Map Setup’ and press the ENT Key. The Map Setup Menu is
displayed.
4)
Use the small FMS Knob to select the ‘Map’ group and press the ENT Key.
5)
Highlight the ‘FUEL RNG (RSV)’ field.
Appendix
Display the Navigation Map Page (press and hold the CLR Key for 2
seconds to quickly select this map).
11
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Hazard
Avoidance
1)
190-02131-00 Rev. C
Procedures
Enabling/disabling the Fuel Range Ring and selecting a reserve
fuel time:
Flight
Planning
A map feature related to the EIS Fuel Calculations is the Fuel Range Ring, which
graphically illustrates the aircraft’s remaining range based on the endurance (ENDUR),
heading, groundspeed, and wind direction and speed. The solid green circle represents
the range until all the remaining fuel is depleted. The dashed green circle indicates
the aircraft range until only reserve fuel remains. Once on reserve fuel, the range is
indicated by a solid yellow circle.
The Fuel Range Ring shifts position in relation to the aircraft according to wind
effects. For example, more fuel is required for flying into a headwind, and the aircraft’s
decreased range in that direction is indicated by the Fuel Range Ring shifting toward
the tail of the Aircraft Symbol.
The amount of reserve fuel (only for purposes of the Fuel Range Ring) is set on the
Navigation Map Page Setup Menu in terms of remaining flight time. When enabled
the Fuel Range Ring appears on the Navigation Map Page, the Weather Data Link Page,
and PFD Inset Map.
6)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
7)
Turn the large FMS Knob to highlight the reserve fuel time, how long the
aircraft can fly after reaching the reserve fuel.
8)
Enter the desired reserve fuel time (00:00 to 23:59; hours:minutes) and
press the ENT Key.
9)
Press the FMS Knob to return to the Navigation Map Page.
OIL PRESSURE AND TEMPERATURE GAUGES
Engine oil pressure and temperature for each engine are shown along
horizontal bar indicators. Oil pressure is shown in pounds per square
inch (psi) and temperature in degrees Fahrenheit (°F). If the oil pressure
pointer enters the yellow band, a caution is issued. If the oil pressure or oil
temperature pointers enter the red band, a warning is issued.
Oil Pressure and Temperature Gauges
FUEL QUANTITY
The fuel display shows the fuel quantity in each tank in gallons (gal). Fuel
quantity for each tank is normally shown along a vertical slider scale with
corresponding readouts below each gauge. A total fuel quantity readout
is shown at the bottom of the display between the fuel quantity gauges. A
caution or warning is issued for low fuel quantity.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
EIS
Fuel Display
12
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
EIS
NOTE: Refer to the Pilot’s Operating Handbook (POH) for corrective pilot
EIS
actions.
Flight
Instruments
CREW ALERTING SYSTEM (CAS)
powered on are considered already acknowledged. They do not flash or
trigger the Master Warning or Master Caution.
Nav/Com/
XPDR/Audio
NOTE: Any CAS messages that are generated when the system is first
GPS Nav
Additional
Features
• Advisory (white) – Crew awareness required and subsequent action may
be required
Hazard
Avoidance
• Caution (amber) – Immediate crew awareness and possible future
corrective action required; Master Caution triggered
Procedures
CAS messages are grouped by criticality (warning, caution) 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:
• Warning (red) – Immediate crew awareness and action required; Master
Warning triggered
Flight
Planning
The Crew Alerting System (CAS) Display is located on the right side of the
PFD. Up to 14 messages can be displayed; when more than 14 messages accumulate, the scrolling CAS softkeys become available.
Abnormal
Operation
Annun/Alerts
CAS
Window
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
13
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
EIS
Blank Page
14
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER A TRANSPONDER CODE
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 key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
3)
Turn the large FMS Knob to select the next desired field.
4)
Turn the small FMS Knob to enter the desired number.
5)
Repeat steps 3 and 4 until the desired ADF frequency is entered.
6)
Press the ENT Key to accept the new frequency.
7)
Press the ENT Key again to transfer the frequency to the active field.
8)
Turn the large FMS Knob to select the MODE field.
9)
Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
Abnormal
Operation
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
Additional
Features
2)
Hazard
Avoidance
Press the ADF/DME Softkey.
Procedures
1)
Flight
Planning
ADF TUNING (OPTIONAL)
10) Press the ENT Key to complete the selection.
2)
Turn the large FMS Knob to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
Appendix
Press the ADF/DME Softkey.
Annun/Alerts
DME TUNING
1)
GPS Nav
2)
Nav/Com/
XPDR/Audio
Press the XPDR Softkey to display the transponder mode selection softkeys.
EIS
1)
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
15
SELECTING A COM RADIO
Transmit/Receive
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
SELECTING A NAV RADIO
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
NAV/COM TUNING
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
Receive Only
1)
Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
INTERCOM
The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.
• When the MAN SQ Annunciator is extinguished (Automatic Squelch is on),
the ICS Knob controls only the volume (pressing the ICS Knob has no effect
on the VOL/SQ selection).
• When the MAN SQ Annunciator is illuminated (Manual Squelch), the ICS
Knob controls either volume or squelch (selected by pressing the ICS Knob
and indicated by the VOL or SQ annunciation).
16
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Nav/Com/XPDR/Audio Panel
EIS
Nav/Com/
XPDR/Audio
• Pressing the PLAY Key once plays the latest recorded memory block, then returns
to normal operation.
• Pressing the MKR/MUTE Key while playing a memory block stops play.
• Pressing the PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.
Flight
Instruments
DIGITAL CLEARANCE RECORDER AND PLAYER
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
17
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
18
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
2)
3)
6)
7)
11)
12)
Abnormal
Operation
Direct-to Navigation using the PFD
1)
3)
5)
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
19
Index
6)
) on the PFD.
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘Activate?’. If no altitude constraint or course
is desired, press the ENT Key to activate. To enter an altitude constraint,
proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Appendix
4)
Press the Direct-to Key (
Annun/Alerts
2)
Additional
Features
10)
Hazard
Avoidance
9)
Procedures
8)
Flight
Planning
5)
) Key on the MFD.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
GPS Nav
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EIS
Direct-to Navigation using the MFD
EIS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the ‘Offset’ field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
GPS Nav
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
13) Turn the small FMS Knob to enter the desired course to the waypoint.
15) Press the ENT Key again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the Activate Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
14) Press the ENT Key to highlight ‘Activate?’.
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Press the ACT Leg Softkey.
Or:
Index
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3)
20
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION (VNAV)
Displayed Text
Examples
Hazard
Avoidance
5OOOFT
Cross AT or ABOVE
5,000 ft
Procedures
Altitude Constraint
Examples
Cyan Text with Pencil Icon
White Text
23OOFT
Cross AT 2,300 ft
Additional
Features
Cyan Text
3OOOFT
Cross AT or BELOW
3,000 ft
Abnormal
Operation
White Text with Altitude
Restriction Bars
Temperature Compensated
Index
21
Appendix
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Annun/Alerts
Altitudes associated with approach procedures are “auto-designated”. The system
will automatically use the altitudes loaded with the approach for giving vertical flight
path guidance outside the FAF. Note these altitudes are displayed as cyan text.
Altitudes associated with arrival procedures are “manually-designated”. This
means the system will not use the altitudes loaded with the arrival for giving vertical
flight path guidance until designated to do so by the pilot. Note that these altitudes
are initially displayed as white text. These altitudes may be “designated” by placing
the cursor over the desired altitude and pressing the ENT Key. After designation, the
text changes to cyan.
190-02131-00 Rev. C
Flight
Planning
NOTE: Temperature Compensated altitudes are depicted with a snowflake
icon.
GPS Nav
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EIS
1)
Altitudes that have been designated for use in vertical navigation may also be
made “non-designated” by placing the cursor over the desired altitude and pressing
the CLR Key. The altitude is now displayed only as a reference. It will not be used
to give vertical flight path guidance. Other displayed altitudes may change due to
re-calculations or rendered invalid as a result of manually changing an altitude to a
non-designated altitude.
White Text
Cyan Text
5OOOFT
5OOOFT
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.
Altitude is designated for use in determining
vertical guidance. A pencil icon indicates
manual designation or manual data entry.
5OOOFT
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.
5OOOFT
The system cannot use this altitude in
determining vertical guidance because of an
invalid constraint condition.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
22
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT PLANNING
EIS
All procedures apply to the MFD and the Control Unit unless otherwise stated.
Entering Weight Parameters
4)
Press the ENT Key. The cursor is now in the ‘Fuel Reserves’ field.
5)
Turn the small FMS Knob to enter the desired reserve fuel quantity.
6)
Press the FMS Knob to remove the cursor.
7)
Press the ENT Key.
Annun/Alerts
Turn the small FMS Knob to enter the desired fuel quantity.
Abnormal
Operation
3)
Additional
Features
Turn the large FMS Knob to place the cursor in the ‘Fuel On Board’ field.
Hazard
Avoidance
2)
TRIP PLANNING
2)
Turn the small FMS Knob to select the Trip Planning Page.
3)
The current ‘Page Mode’ is displayed at the top of the page: ‘Automatic’ or
‘Manual’. To change the page mode, press the Auto or Manual Softkey.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
23
Index
Turn the large FMS Knob to select the ‘Aux’ page group.
Appendix
1)
190-02131-00 Rev. C
Procedures
Press the FMS Knob to activate the cursor.
Flight
Planning
1)
GPS Nav
Entering Fuel Parameters
Nav/Com/
XPDR/Audio
The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large FMS Knob to select the ‘Aux’ page group. Turn the
small FMS Knob to select the Weight Planning Page.
1) Press the Empty WT Softkey to place the cursor in the Basic Empty Weight
field.
2) Enter the desired aircraft empty weight.
3) Press the ENT Key. The cursor is now over the ‘Pilot & Stores’ field.
4) Enter the desired weight of Pilot & Stores.
5) Press the ENT Key.
6) Continue repeating these steps until all desired weights have been entered.
Flight Planning
Flight
Instruments
4)
For Direct-to planning:
a) Press the WPTs Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
EIS
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Nav/Com/
XPDR/Audio
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
GPS Nav
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
For point-to-point planning:
Flight
Planning
a) Enter the identifier of the starting waypoint.
Procedures
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.
Hazard
Avoidance
Or:
For flight plan leg planning:
Additional
Features
a) Press the FPL Softkey (at the bottom of the display).
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
Annun/Alerts
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ will be an available option to display planning data
for the remainder of the flight plan.
Appendix
Abnormal
Operation
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
Index
5)
Turn the large FMS Knob to highlight the ‘Departure Time’ field.
NOTE: The departure time on the Trip Planning Page is used for preflight
planning. Refer to the Utility Page for the actual flight departure time.
24
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
7)
The flashing cursor moves to the ‘Ground Speed’ field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘Automatic’ page
mode, ground speed is provided by the system.
8)
The flashing cursor moves to the ‘Fuel Flow’ field Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘Automatic’ page mode, fuel flow is
provided by the system.
9)
The flashing cursor moves to the ‘Fuel on Board’ field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘Automatic’ page mode, fuel
onboard is provided by the fuel totalizer.
EIS
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the New Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘Waypoint Type’ field. If desired, the waypoint can
be made temporary (deleted automatically when the system is turned off).
If the waypoint is to remain in the system, proceed to step 7.
Annun/Alerts
1)
Appendix
25
Index
a) Turn the large FMS Knob one click to the left to highlight ‘Temporary’.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Flight
Planning
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
GPS Nav
11) The flashing cursor moves to the ‘Indicated Altitude’ field. Enter the indicated
altitude. Press the ENT Key when finished. Note that in ‘Automatic’ page
mode, indicated altitude is provided by the system.
12) The flashing cursor moves to the ‘Barometric Pressure’ field. Enter the desired
baro setting. Press the ENT Key when finished. Note that in ‘Automatic’ page
mode, the baro setting is provided by the setting entered on the PFD.
13) The flashing cursor moves to the ‘Total Air Temperature’ field. Enter the total air
temperature. Press the ENT Key when finished. Note that in ‘Automatic’ page
mode, total air temperature is provided by the system outside air temperature.
Nav/Com/
XPDR/Audio
10) The flashing cursor moves to the ‘Calibrated Airspeed’ field. Enter the calibrated
airspeed. Press the ENT Key when finished. Note that in ‘Automatic’ page
mode, calibrated airspeed is provided by the system.
190-02131-00 Rev. C
Flight
Instruments
6)
Flight Planning
7)
With the cursor in the ‘Waypoint Type’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
1)
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the New Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘Waypoint Type’ field. If desired, the waypoint can
be made temporary (deleted automatically when the system is turned off).
If the waypoint is to remain in the system, proceed to step 7.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘Waypoint Type’ field.
a) Turn the large FMS Knob one click to the left to highlight ‘Temporary’.
Abnormal
Operation
Additional
Features
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘Waypoint Type’ field.
7)
With the cursor in the ‘Waypoint Type’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Annun/Alerts
10) The cursor moves to the ‘Reference Waypoints’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
Appendix
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
b) Turn the large FMS Knob to select the desired waypoint.
Index
c) Press the ENT Key.
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
26
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Flight
Instruments
b) Turn the small FMS Knob to the right to display the ‘Nearest’ airports
to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
EIS
d) Press the ENT Key.
Or:
b) Turn the small FMS Knob to the right to display the ‘Recent’ waypoints.
GPS Nav
c) Turn the large FMS Knob to select the desired waypoint.
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Procedures
b) Turn the small FMS Knob to the right to display the ‘User’ waypoints.
Flight
Planning
Or:
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
Annun/Alerts
16) Press the FMS Knob to remove the flashing cursor.
CREATE USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the New Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Appendix
1)
Abnormal
Operation
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
Additional
Features
12) Press the ENT Key.
Hazard
Avoidance
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
27
5)
Press the ENT Key.
6)
The cursor is now in the ‘Waypoint Type’ field. If desired, the waypoint can
be made temporary (deleted automatically when the system is turned off).
If the waypoint is to remain in the system, proceed to step 7.
EIS
Flight
Instruments
Flight Planning
a) Turn the large FMS Knob one click to the left to highlight ‘Temporary’.
GPS Nav
Nav/Com/
XPDR/Audio
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘Waypoint Type’ field.
7)
With the cursor in the ‘Waypoint Type’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
Procedures
Flight
Planning
10) The cursor moves to the ‘Reference Waypoints’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Hazard
Avoidance
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Abnormal
Operation
b) Turn the small FMS Knob to the right to display the ‘Nearest’ airports
to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
Annun/Alerts
d) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘Recent’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Index
d) Press the ENT Key.
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
28
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Flight
Instruments
b) Turn the small FMS Knob to the right to display the ‘User’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Nav/Com/
XPDR/Audio
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
GPS Nav
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
2)
Press the ENT Key. The User Waypoint Information Page is displayed with
the captured position.
Procedures
Press the Joystick to activate the panning function and pan to the map
location of the desired user waypoint.
Flight
Planning
CREATE A USER WAYPOINT USING THE MAP POINTER
1)
If desired, define the type and location (i.e., LAT/LON, RAD/RAD or RAD/
DIS) of the waypoint.
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 highlight ‘Temporary’ and pressing the ENT Key to
check the box.
8)
Press the FMS Knob to remove the flashing cursor.
Appendix
5)
Annun/Alerts
Press the ENT Key to accept the selected name.
Abnormal
Operation
4)
Additional
Features
Enter a user waypoint name (up to six characters).
Hazard
Avoidance
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)
EIS
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
29
DELETE A USER WAYPOINT
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to the place the cursor in the ‘User Waypoint List’
field.
5)
Turn the small FMS Knob to highlight the desired waypoint.
6)
Press the Delete Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
CREATE A FLIGHT PLAN
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) 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).
4) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
5) The Set Runway Window is displayed and the cursor is displayed in the
‘Runway’ field. Turn the small FMS Knob to display a list of runways at the
departure airport. Turn the large FMS Knob to select the desired runway
and press the ENT Key.
6) Press the ENT Key again to accept the departure runway.
7) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint
and repeat step numbers 3 through 6 to enter the destination waypoint.
The active flight plan is modified as each waypoint is entered.
8) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
30
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the Import Softkey.
Appendix
5)
Or:
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
31
Index
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
190-02131-00 Rev. C
Annun/Alerts
Press the FMS Knob to activate the cursor.
Abnormal
Operation
4)
Additional
Features
Turn the small FMS Knob to select the Flight Plan Catalog Page.
Hazard
Avoidance
3)
Procedures
Press the FPL Key on the MFD to display the Active Flight Plan Page on the
MFD.
Flight
Planning
2)
GPS Nav
Insert the SD card containing the flight plan in the top card slot on the MFD.
Nav/Com/
XPDR/Audio
1)
EIS
IMPORT A FLIGHT PLAN FROM AN SD CARD
Flight
Instruments
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) 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) 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 departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6) The Set Runway Window is displayed and the cursor is displayed in the
‘Runway’ field. Turn the small FMS Knob to display a list of runways at the
departure airport. Turn the large FMS Knob to select the desired runway
and press the ENT Key.
7) Press the ENT Key again to accept the departure runway.
8) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint
and repeat step numbers 4 through 7 to enter the destination waypoint.
9) When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
Flight
Instruments
Flight Planning
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key to confirm the import.
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
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 a list of the 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 existing or empty
flight plan, and again press the Import Softkey.
1)
Press the FPL Key to display the active flight plan.
2)
If necessary, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5)
Enter the new flight plan waypoint by one of the following:
Hazard
Avoidance
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
Additional
Features
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Abnormal
Operation
b) Turn the small FMS Knob to the right to display the ‘Nearest’ airports
to the aircraft’s current position.
Annun/Alerts
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘Recent’ waypoints.
Index
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
32
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘User’ waypoints.
EIS
c) Turn the large FMS Knob to select the desired user waypoint.
d) Press the ENT Key.
Press the ENT Key again to “accept” the waypoint.
Nav/Com/
XPDR/Audio
6)
INSERT AN ALONG TRACK OFFSET WAYPOINT IN THE ACTIVE FLIGHT PLAN
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 OFST 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).
5)
Press the ENT Key to create the offset waypoint.
6)
Turn the small FMS Knob to enter the desired altitude for the offset.
7)
Press the FMS Knob to remove the flashing cursor.
Flight
Planning
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Hazard
Avoidance
Additional
Features
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. To remove the parallel track,
press the MENU Key, highlight ‘Cancel Parallel Track’, and press the ENT
Key.
Index
Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The
Parallel Track Window is displayed with the ‘Direction’ field highlighted.
Appendix
2)
Annun/Alerts
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Abnormal
Operation
1)
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Procedures
ACTIVATE PARALLEL TRACK
190-02131-00 Rev. C
GPS Nav
1)
33
Press the FPL Key.
2)
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. The airway is inserted before the highlighted waypoint
(as shown by the insertion point indicator). 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 press “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable 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. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
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.
COLLAPSE/EXPAND AIRWAYS IN A FLIGHT PLAN
1)
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’ and
press the ENT Key. All airways are collapsed/expanded.
DETERMINE THE CLOSEST POINT ALONG THE FLIGHT PLAN TO A SELECTED
WAYPOINT
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
GPS Nav
Nav/Com/
XPDR/Audio
EIS
1)
Flight
Planning
ENTER AN AIRWAY IN A FLIGHT PLAN
Procedures
Flight
Instruments
Flight Planning
34
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the MENU Key, highlight ‘Closest Point Of FPL’’, and press the
ENT Key. A window appears with the ‘From’ reference waypoint field
highlighted.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Enter the identifier of the reference waypoint and press the ENT Key. A
new user waypoint is created at this location and inserted into the flight
plan. The name for the new user waypoint is derived from the identifier of
the reference waypoint.
Flight
Instruments
3)
EIS
CREATE A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT
4)
Use the FMS Knobs to edit the entry 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.
Additional
Features
Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key.
The Hold At window appears with the ‘Course’ field highlighted.
Abnormal
Operation
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
CREATE A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION
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)
Use the FMS Knobs to edit the entry 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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
35
Index
2)
Appendix
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Annun/Alerts
1)
190-02131-00 Rev. C
Hazard
Avoidance
3)
Procedures
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.
Flight
Planning
2)
GPS Nav
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Nav/Com/
XPDR/Audio
1)
Flight
Planning
Procedures
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
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.
8)
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 immediately activate
the hold.
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
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.
REMOVE A USER-DEFINED HOLD (CREATED AT AN ACTIVE WAYPOINT)
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
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.
INVERT AN ACTIVE FLIGHT PLAN
Index
Appendix
6)
REMOVE A USER-DEFINED HOLD (CREATED AT THE AIRCRAFT P.POS)
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
36
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
Flight
Instruments
4)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Nav/Com/
XPDR/Audio
1)
EIS
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
Or, for a stored flight plan:
GPS Nav
a) Press the MFD FPL Key and turn the small FMS Knob to select the
Flight Plan Catalog Page.
Flight
Planning
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Press the Edit Softkey.
2)
Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in cyan directly above the
procedure’s waypoints.
Procedures
3)
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Hazard
Avoidance
Additional
Features
STORE A FLIGHT PLAN
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Annun/Alerts
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
EDIT A STORED FLIGHT PLAN
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the Edit Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Appendix
1)
190-02131-00 Rev. C
Abnormal
Operation
1)
37
EIS
Flight
Instruments
Flight Planning
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
DELETE A WAYPOINT FROM THE FLIGHT PLAN
Nav/Com/
XPDR/Audio
1)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
GPS Nav
a) Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
2)
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘Remove (Wpt Name)?’ confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the cursor.
CHANGE THE FLIGHT PLAN COMMENT
1)
Press the FPL Key to display the Active Flight Plan Page.
Or, for a stored flight plan:
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
d) Press the Edit Softkey.
a) Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
Annun/Alerts
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
Index
Appendix
d) Press the Edit Softkey.
38
2)
Press the FMS Knob to activate the cursor and turn the large FMS Knob to
highlight the comment field.
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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Flight Planning
Flight
Instruments
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Press the FPL Key for the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the Invert Softkey. ‘Invert and activate stored flight plan?’ is displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
EIS
1)
Nav/Com/
XPDR/Audio
GPS Nav
COPY A FLIGHT PLAN
Flight
Planning
Press the FPL Key for the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the Copy Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Procedures
1)
Hazard
Avoidance
Additional
Features
DELETE A FLIGHT PLAN
Press the FPL Key for the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Press the Delete Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Abnormal
Operation
1)
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
39
GRAPHICAL FLIGHT PLAN CREATION
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
3)
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor (as indicated by the insertion point indicator). Turn the large FMS
Knob to select the desired insertion point.
4)
If the pointer is placed on an existing airport, NAVAID, or user waypoint,
the waypoint name is highlighted. Press the LD WPT Softkey. The selected
waypoint is inserted at the selected point. The default user waypoint naming
is USR000, USR001, USR002, and so on. If the pointer is placed on an existing
airport, NAVAID, or user waypoint, that waypoint name is inserted.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
EXPORT 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 Active Flight Plan Page on the MFD.
3)
Turn the small FMS Knob to select the 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.
7)
Press the ENT Key to confirm the export.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
40
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EIS
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘Select Departure’.
3)
Press the ENT Key. The cursor is displayed in the ‘Departure’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘Transition’ field with a list
of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘Load?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Nav/Com/
XPDR/Audio
1)
4)
Press the ACT Leg Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘Activate’ highlighted, press the ENT Key.
Annun/Alerts
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
Abnormal
Operation
3)
Additional
Features
Press the FMS Knob to activate the cursor.
Appendix
LOAD AN ARRIVAL PROCEDURE
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘Select Arrival’.
3)
Press the ENT Key. The cursor is displayed in the ‘Arrival’ field with a list of
available arrivals.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
41
Index
1)
190-02131-00 Rev. C
Hazard
Avoidance
2)
Procedures
Press the FPL Key for the MFD to display the active flight plan.
Flight
Planning
1)
GPS Nav
ACTIVATE A DEPARTURE LEG
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Press the ENT Key.
10) With ‘Load?’ highlighted, press the ENT Key.
GPS Nav
11) The arrival becomes part of the active flight plan.
1)
Press the FPL Key to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT Leg Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘Activate’ highlighted, press the ENT Key.
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
ACTIVATE AN ARRIVAL LEG
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘Select Approach’.
3)
Select the airport and approach:
Appendix
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.
Index
Or:
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.
42
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Procedures
Flight
Instruments
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.
A list of available transitions for the selected approach procedure is now
displayed.
5)
Turn either FMS Knob to select the desired transition. The ‘VECTORS’
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
6)
Press the ENT Key. The cursor moves to the ‘Minimums’ field.
7)
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO, or
TEMP COMP.
8)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
9)
Press the ENT Key. If BARO, or OFF was selected in step 8, proceed to
step 11. If TEMP COMP was selected in step 8, the cursor moves to the
‘TEMP At....” field. Turn the small FMS Knob to enter the temperature at
the destination airport. The temperature compensated altitude minimum is
displayed below the previously enter minimum altitude value.
EIS
4)
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
Abnormal
Operation
Annun/Alerts
Selecting ‘Load?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘Activate?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
Appendix
12) Press the ENT Key.
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
2)
Turn the large FMS Knob to highlight ‘Activate Approach’.
3)
Press the ENT Key.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Press the PROC Key.
Additional
Features
11) Turn the large FMS Knob to select either ‘Load?’ or ‘Activate?’.
1)
Hazard
Avoidance
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
43
ACTIVATE A VECTOR TO FINAL APPROACH FIX
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘Activate Vector-to-Final’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
Flight
Planning
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘Activate Missed Approach’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘Activate’ highlighted, press the ENT Key.
Or:
Press the go-around button:
REMOVE A PROCEDURE FROM THE ACTIVE FLIGHT PLAN
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key. The Page Menu is displayed.
3)
Turn the FMS Knob to highlight ‘Remove <procedure type>’.
4)
Press the ENT Key. A confirmation window is displayed.
5)
With ‘OK’ highlighted, press the ENT Key.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
1)
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
44
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Procedures
A temperature compensated altitude can be computed and used for the loaded approach. A temperature compensated altitude is shown with a snowflake icon.
EIS
Nav/Com/
XPDR/Audio
Enabling temperature compensated altitude:
1) Press the FPL Key to display the active flight plan.
2) Press the MENU Key. The Page Menu is displayed.
3) Turn the FMS Knob to highlight ‘Temperature Compensation’.
4) Press the ENT Key. The Temperature Compensation Window is displayed.
Use the small FMS Knob to select the temperature at the <airport>. The
GPS Nav
5)
Flight
Instruments
TEMPERATURE COMPENSATED ALTITUDE
compensated altitude is computed as the temperature is selected.
Press the ENT Key. ‘Activate Compensation?’ is highlighted.
7)
Press the ENT Key. The compensated altitudes for the approach are
Flight
Planning
6)
Procedures
shown in the flight plan.
5)
Press the ENT Key. ‘Cancel Compensation?’ is highlighted.
6)
Press the ENT Key. The temperature compensated altitude for the
Abnormal
Operation
Press the ENT Key. The Temperature Compensation Window is displayed.
Additional
Features
4)
Hazard
Avoidance
Disabling temperature compensated altitude:
1) Press the FPL Key to display the active flight plan.
2) Press the MENU Key. The Page Menu is displayed.
3) Turn the FMS Knob to highlight ‘Temperature Compensation’.
approach is cancelled.
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
45
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
Blank Page
46
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
Customizing the Hazard Displays on the Navigation Map Page:
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
Flight
Planning
SIRIUS XM WEATHER (OPTIONAL)
GPS Nav
2)
Nav/Com/
XPDR/Audio
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Settings’
option.
EIS
1)
WARNING: Do not use data link weather information for maneuvering
If necessary, turn the small FMS Knob to select the Weather Data Link
Page. If the name of another source besides ‘(XM)’ is in the page title,
continue to Step 3.
3)
Press the MENU Key.
4)
If necessary, turn the large FMS Knob to highlight ‘Display XM Weather’
and press the ENT Key.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
2)
Appendix
If necessary, turn the large FMS Knob to select the Map Page Group.
Annun/Alerts
1)
Abnormal
Operation
Changing the Data Link Weather Source to Display Sirius XM Weather
Additional
Features
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.
Hazard
Avoidance
WARNING: Do not use the indicated data link weather product age
Procedures
in, near or around areas of hazardous weather. Information contained
within data link weather products may not accurately depict current
weather conditions.
47
Hazard Avoidance
EIS
Flight
Instruments
Displaying Sirius XM Weather on the Navigation Map Page
1)
Press the Map Opt Softkey.
2)
Press the NEXRAD or XM LTNG or METAR Softkey to display the desired
weather. Press the applicable softkey again to remove weather data from
the Navigation Map Page.
GPS Nav
Nav/Com/
XPDR/Audio
Displaying Sirius XM Weather Legends on the Navigation Map Page
1)
Press the Map Opt Softkey.
2)
Press the Legend Softkey to display or remove the legend.
Hazard
Avoidance
Procedures
Flight
Planning
Display METAR and TAF information on the Airport Information Page
1)
Turn the large FMS Knob to select the WPT Page Group.
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
4)
Press the FMS Knob to enable the cursor, then turn the small FMS Knob as
needed to FMS knob to scroll through the text.
5)
After viewing text, press the FMS Knob to disable the cursor.
Annun/Alerts
Abnormal
Operation
Additional
Features
Displaying Weather on the Weather Data Link (XM) Page
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) Page.
3)
Press the available softkeys to select the desired Sirius XM Weather product.
4)
Press the Legend Softkey to view the legends for the selected products. If
necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
Appendix
Enabling/disabling NEXRAD Animation on the Weather Data Link (XM)
Page
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) Page.
Index
3) Press the MENU Key.
4) Turn the FMS Knob to select ‘Weather Setup’ and press the ENT Key.
5) Turn the large FMS Knob to highlight the NEXRAD Animation on/off field.
6) Turn the small FMS Knob to select ‘On’ or ‘Off’ then press the ENT Key.
48
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
Flight
Instruments
Map Panning Information – Weather Data Link (XM) Page
2)
Move the Joystick to place the panning arrow on Echo Tops, Cloud Tops,
Cell Movement symbols, AIRMETs/SIGMETs, METARs, TFRs, PIREPs, AIREPs,
and County Warnings.
3)
Press the ENT Key to display pertinent information for the selected product.
GPS Nav
Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.
Nav/Com/
XPDR/Audio
Push in the Joystick to display the panning arrow.
EIS
1)
Flight
Planning
Enabling/disabling winds aloft data display in the Vertical Situation
Display (VSD):
Procedures
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key
4)
Turn the small FMS Knob to select the ‘VSD’ Group and press the ENT Key
5)
Turn the large FMS Knob to select the Winds on/off field.
6)
7)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Abnormal
Operation
NOTE: NEXRAD data cannot be displayed at the same time as terrain, echo
tops, turbulence, or icing data is displayed.
Additional
Features
Select the Navigation Map Page.
Hazard
Avoidance
1)
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
49
Hazard Avoidance
Flight
Instruments
Sirius XM Weather Products and Symbols
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
SiriusXM
Weather
Product
NEXRAD
50
Symbol
Expiration Time
(Minutes)
Broadcast Rate
(Minutes)
30
5 (U.S.)
10 (Canada)
Cloud Top (CLD
TOP)
60
Echo Top
(ECHO TOP)
30
15 (69/69A)
30 (69/69A SXM)
7.5
SiriusXM
Lightning
(LTNG)
Cell Movement
(CELL MOV)
30
5
30
1.25
SIGMETs/
AIRMETs (SIG/
AIR)
METARs
60
12
90
12
City Forecast
(CITY)
Surface
Analysis (SFC)
90
12
60
12
Freezing Levels
(FRZ LVL)
120
12
Winds Aloft
(WIND)
90
12
County
Warnings
(COUNTY)
60
5
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
90
12
90
12
180
12
No product
image
30
5
No product
image
No product
image
60
12
60
12
Hazard
Avoidance
22
Procedures
90
Flight
Planning
12
GPS Nav
60
Nav/Com/
XPDR/Audio
Broadcast Rate
(Minutes)
Symbol
EIS
Additional
Features
TAFs
Expiration Time
(Minutes)
Flight
Instruments
SiriusXM
Weather
Product
Cyclone
Warnings
(CYCLONE)
Icing Potential
(CIP and SLD)
(ICNG)
Pilot Weather
Report
(PIREPs)
Air Report
(AIREPs)
Turbulence
(TURB)
Radar
Coverage Not
Available
TFRs
Abnormal
Operation
FIS-B WEATHER
Appendix
in, near, or around areas of hazardous weather. Information contained
within data link weather products may not accurately depict current
weather conditions.
Annun/Alerts
WARNING: Do not use data link weather information for maneuvering
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
51
Flight
Instruments
Hazard Avoidance
The optional GTX 345R transponder receives Flight Information Services - Broadcast
(FIS-B) weather data from a network of UAT ground-based transceivers (GBTs).
FIS-B weather data reception requires the aircraft being within range and line-ofsight of an operating GBT broadcasting FIS-B weather data. Reception may be affected
by factors including altitude or terrain.
Reception of FIS-B weather data occurs automatically without any pilot action. FIS-B
broadcasts provide weather data in a repeating cycle which may take approximately
ten minutes to transmit all available weather data. Therefore, not all available weather
data may be available immediately upon initial FIS-B signal acquisition.
Viewing the Weather Data Link (FIS-B) Page
Turn the large FMS Knob to select the Map Page Group.
2)
Additional
Features
Turn the small FMS Knob to select the Weather Data Link (FIS-B or XM)
Page.
3)
If the page title displays a weather data link weather source other than
‘FIS-B’, such as ‘XM’, proceed to the following steps to change the data link
weather source.
4)
Press the MENU Key.
5)
Turn the small FMS Knob to select ‘Display FIS-B Weather’.
6)
Press the ENT Key. The page title will display ‘Map - Weather Data Link
(FIS-B)’ to indicate FIS-B is now the selected data link weather source.
Annun/Alerts
1)
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
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 significantly older than the
indicated weather product age.
Index
Appendix
Enabling/Disabling FIS-B Weather
52
1)
Select the 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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
5
90
10
Winds Aloft
(WIND)
90
10
SIGMETs/AIRMETs
(SIG/AIR)
60
5
no product image
30
2.5
no product image
60
10
No Radar Coverage
no product image
10
Additional
Features
Terminal Aerodrome
Forecast
Temporary Flight
Restriction (TFR)
Hazard
Avoidance
90
Procedures
2.5
Flight
Planning
30
NEXRAD Composite
(Regional)
Meteorological Aerodrome
Report
(METARs)
Pilot Weather Report
(PIREPs)
GPS Nav
15
Nav/Com/
XPDR/Audio
30
NEXRAD Composite (US)
EIS
Broadcast Rate
(Minutes)
Symbol
Flight
Instruments
Expiration Time
(Minutes)
FIS-B Weather Product
Weather Product Symbols and Data Timing
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’, 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.).
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
2)
Appendix
Select the Weather Data Link (FIS-B) Page.
Annun/Alerts
1)
Abnormal
Operation
Setting Up and Customizing the Weather Data Link (FIS-B) Page
53
Flight
Instruments
Hazard Avoidance
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Weather Data Link (FIS-B)
Page with the changed settings.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Setting Up and Customizing FIS-B Weather on the Navigation Map
Page
1)
Select the 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).
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.
Annun/Alerts
Abnormal
Operation
Additional
Features
Displaying/Removing the Weather Product Information Box on PFD
Maps
1)
On the PFD, press the Map/HSI Softkey.
2)
Press the Layout Softkey.
3)
Press the Wx LGND Softkey to display/remove the weather product
information box.
Appendix
Viewing Legends for Displayed Weather Products on the Weather Data
Link (FIS-B) Page
1)
Select the Weather Data Link (FIS-B) Page.
2)
Press the Legend Softkey to display the legends for the displayed weather
products.
Index
Or:
a) Press the MENU Key.
b) Select ‘Weather Legend’ and press the ENT Key.
54
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
To remove the Legend Window, press the Legend Softkey, the ENT or the
CLR Key, or press the FMS Knob.
EIS
Viewing Legends for Displayed Weather Products on the Navigation
Map Page
Flight
Instruments
3)
2)
Press the Map Opt Softkey.
3)
Press the Legend Softkey (available if one or more FIS-B weather products
are enabled for display).
4)
To remove the Legend Window, press the Legend Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Press the Map Opt Softkey (for the PFD Inset Map, press the INSET
Softkey). This step is not necessary on the Weather Data Link (FIS-B) Page.
2)
Press the NEXRAD Softkey.
Procedures
1)
Flight
Planning
Displaying NEXRAD Data
GPS Nav
Select the Navigation Map Page.
Nav/Com/
XPDR/Audio
1)
Displaying SIGMETs and AIRMETs
2)
Press the SIG/AIR Softkey.
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.
Additional
Features
Select the Weather Data Link (FIS-B) Page.
Hazard
Avoidance
1)
Abnormal
Operation
Displaying METAR and TAF Text
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
(FIS-B) Page.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
2)
Appendix
On the Weather Data Link (FIS-B) Page, press the METAR Softkey.
Annun/Alerts
1)
55
Hazard Avoidance
Flight
Instruments
Or:
1)
Select the Weather Information Page.
a) Turn the large FMS Knob to select the Waypoint Page Group.
GPS Nav
Nav/Com/
XPDR/Audio
EIS
b) Press 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.
Hazard
Avoidance
Procedures
Flight
Planning
Displaying Raw METAR Text on the Active Flight Plan Page
1)
Select the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint. 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.
Abnormal
Operation
Additional
Features
Displaying Winds Aloft Information
1)
Select the Weather Data Link (FIS-B) Page.
2)
Press the More WX Softkey.
3)
Press the Wind Off Softkey.
4)
Press the softkey for the desired altitude. Press the Next or PREV Softkey
to cycle through the altitude softkeys. The Wind Softkey label changes to
reflect the altitude selected.
Index
Appendix
Annun/Alerts
Enabling/Disabling Predicted Temperatures with Winds Aloft Data
56
1)
Select the Weather Data Link (FIS-B) Page.
2)
Press the MENU Key.
3)
Turn the small FMS Knob to highlight ‘Weather Setup’ and press the ENT
Key.
4)
Turn the small FMS Knob to highlight ‘Product Group 1’ and press the ENT
Key.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
Turn the small FMS Knob to highlight the Temp (•) ‘ON’ or ‘OFF’ field, then
press the ENT Key.
6)
When finished, push the FMS Knob or the CLR Key.
EIS
Displaying PIREP Text
Flight
Instruments
5)
Select the Weather Data Link (FIS-B) Page.
2)
Press the More WX Softkey.
3)
Press the PIREPS Softkey.
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 PIREP text is first displayed in a decoded fashion,
followed by the original text. Note the original text may contain additional
information not shown in the decoded version.
6)
Use the FMS Knob or the ENT Key to scroll through the PIREP text.
7)
Press the FMS Knob or the CLR Key to close the PIREP text window and
return to the Weather Data Link (FIS-B) Page.
Nav/Com/
XPDR/Audio
1)
GPS Nav
Flight
Planning
Procedures
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 INFORMATION window.
5)
Press the FMS Knob or the CLR Key to remove the INFORMATION window.
Appendix
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.
Annun/Alerts
TRAFFIC ADVISORY SYSTEM (TAS)
Abnormal
Operation
Select the Weather Data Link (XM) Page or Navigation Map Page.
Additional
Features
1)
Hazard
Avoidance
Displaying TFR Data
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
57
Flight
Instruments
Hazard Avoidance
Nav/Com/
XPDR/Audio
EIS
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. .
GPS Nav
Symbol
Description
Traffic Advisory with directional information. Points in the
direction of the intruder aircraft track.
Flight
Planning
Traffic Advisory without directional information.
Procedures
Traffic Advisory out of the selected display range. Displayed at
outer range ring at proper bearing.
Hazard
Avoidance
Proximity Advisory with directional information. Points in the
direction of the aircraft track.
Proximity Advisory without directional information.
Abnormal
Operation
Additional
Features
Non-threat traffic with directional information. Points in the
direction of the intruder aircraft track.
Non-threat traffic without directional information.
Index
Appendix
Annun/Alerts
Traffic located on the ground with directional information.
Points in the direction of the aircraft track. Ground traffic is only
displayed when ADS-B is in Surface (SURF) Mode or own aircraft
is on the ground.
Ground traffic without directional information. Ground traffic is
only displayed when ADS-B is in Surface (SURF) Mode or own
aircraft is on the ground.
Non-aircraft ground traffic. Ground traffic is only displayed
when ADS-B is in Surface (SURF) Mode or own aircraft is on the
ground.
Traffic Symbol Description
58
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
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 TAS Oper Softkey to begin displaying TAS traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the ADS-B Softkey to begin display ADS-B traffic.
5)
Press the ALT Mode Softkey to change the altitude volume. Select the
desired altitude volume by pressing the Above, Normal, Below, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
Nav/Com/
XPDR/Audio
6)
Press the Motion Softkey.
7)
Press one of the following softkeys:
REL:
Displays the motion vector relative to own aircraft
OFF:
Disables the display of the motion vector.
9)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Additional
Features
Press the TAS STBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
Hazard
Avoidance
8)
Procedures
Displays the motion vector pointing in the absolute direction.
Flight
Planning
ABS:
GPS Nav
1)
EIS
Flight
Instruments
Displaying Traffic on the Traffic Map Page
System Self Test
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Press the TAS STBY Softkey.
3)
Press the Test Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.
Abnormal
Operation
1)
2)
Press the Traffic Softkey. Traffic is now displayed on the map.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Ensure the TAS system is operating. With the Navigation Map displayed,
press the Map Opt Softkey.
Appendix
1)
Annun/Alerts
Displaying Traffic on the Navigation Map
59
TERRAIN AND OBSTACLE PROXIMITY
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
EIS
Flight
Instruments
Hazard Avoidance
GPS Nav
Nav/Com/
XPDR/Audio
Displaying Terrain and Obstacles on the Terrain Proximity Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Terrain Proximity Page.
3)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Terrain Proximity Legends
Abnormal
Operation
Terrain Proximity On-Ground
Legend
Terrain Proximity In-Air Legend
Appendix
Annun/Alerts
Displaying Relative Terrain and Obstacles on the Navigation Map
1)
With the Navigation Map displayed, press the Map Opt Softkey.
2)
Press the TER Softkey. Each softkey press cycles through to a terrain
option (Off, Topo, REL). When ‘REL’ is selected, relative terrain and obstacle
proximity will now be displayed on the map.
Displaying Relative Terrain and Obstacles in the VSD
Index
1)
60
With relative terrain display enabled on the Navigation Map Page, press the
Map Opt Softkey.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
Press the Inset Softkey.
3)
Press the VSD Softkey to enable/disable the VSD.
Flight
Instruments
2)
EIS
TERRAIN-SVT
Display Terrain on the Terrain-SVT Page
2)
Turn the small FMS Knob to select the Terrain-SVS Page.
3)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Procedures
Turn the large FMS Knob to select the Map Page Group.
Flight
Planning
1)
GPS Nav
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Nav/Com/
XPDR/Audio
NOTE: Terrain-SVT is only available when the Synthetic Vision Technology
(SVT) option is installed and the TAWS-B option has not been installed.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Terrain-SVT On-Ground Legend
Terrain-SVT In-Air Legend
Annun/Alerts
Enabling/disabling aviation data on the Terrain-SVT Page:
While the Terrain-SVT Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Appendix
1)
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
61
Hazard Avoidance
Flight
Instruments
Terrain-SVS Inhibit
Nav/Com/
XPDR/Audio
EIS
Inhibit Terrain
While the Terrain-SVS Page is displayed, press the Inhibit Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit Terrain’.
3) Press the ENT Key.
Procedures
Flight
Planning
GPS Nav
Enable Terrain SVT Alerting
While the Terrain-SVT Page is displayed, press the INHIBIT Softkey.
Or:
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable Terrain’.
3) Press the ENT Key.
TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY (OPTIONAL)
WARNING: Do not use the terrain avoidance feature as the sole means of
navigation and terrain separation. The terrain avoidance feature is only to
be used as and aid to terrain avoidance. Garmin obtains terrain database
content from third party sources and is not able to independently verify the
accuracy of the terrain data.
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the
active waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear
on the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Appendix
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Index
NOTE: TAWS-B operation is only available when the TAWS-B option is installed.
62
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Hazard Avoidance
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS System’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
EIS
1)
Flight
Instruments
Manual System Test
Nav/Com/
XPDR/Audio
If the system test passed, “TAWS System Test, OK” is heard.
Display Terrain on the TAWS-B Page
2)
Turn the small FMS Knob to select the TAWS-B Page.
3)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Flight
Planning
Turn the large FMS Knob to select the Map Page Group.
GPS Nav
1)
Procedures
Hazard
Avoidance
Additional
Features
TAWS-B On-Ground Legend
TAWS-B In-Air Legend
Abnormal
Operation
Enable/Disable Aviation Data
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Annun/Alerts
1)
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
63
Hazard Avoidance
Flight
Instruments
TAWS Inhibit
Nav/Com/
XPDR/Audio
EIS
NOTE: If TAWS-B alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Flight
Planning
GPS Nav
Inhibit TAWS
While the TAWS-B Page is displayed, press the Inhibit Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit TAWS’.
3) Press the ENT Key.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Enable TAWS
While the TAWS-B Page is displayed, press the Inhibit Softkey.
Or:
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable TAWS’.
3) Press the ENT Key.
64
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION (OPTIONAL)
Abnormal
Operation
Annun/Alerts
3)
Press the Terrain Softkey.
4)
Press the BACK Softkey to return to the previous page.
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Press the SVT Softkey.
Appendix
2)
Additional
Features
Press the PFD Opt Softkey.
Hazard
Avoidance
Displaying SVT Terrain
1)
Procedures
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Flight
Planning
•
•
•
•
•
•
•
GPS Nav
Synthetic Vision Technology (SVT) functionality is offered as an optional
enhancement to the G1000 Integrated Flight Deck System.
SVT is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the primary flight display (PFD).
SVT offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVT enhancement to the PFD, the following feature enhancements
have been added to the PFD:
Nav/Com/
XPDR/Audio
WARNING: Do not use 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.
EIS
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. 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.
65
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Pathways
2)
Press the SVT Softkey.
3)
If not already enabled, press the Terrain Softkey.
4)
Press the Pathways Softkey.
5)
Press the BACK Softkey to return to the previous page.
GPS Nav
Flight
Planning
Procedures
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
If not already enabled, press the Terrain Softkey.
4)
Press the HDG LBL Softkey.
5)
Press the BACK Softkey to return to the previous page.
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Opt Softkey.
Displaying Heading on the Horizon
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
If not already enabled, press the Terrain Softkey.
4)
Press the APT Sign Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
Abnormal
Operation
Annun/Alerts
Appendix
Index
1)
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the Detail Softkey (declutter) once removes the roads, railroads and other
man made ground features. Pressing the Detail Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
66
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Additional Features
Appendix
Index
67
Annun/Alerts
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Abnormal
Operation
190-02131-00 Rev. C
Additional
Features
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 MFD depiction shows the aircraft position on the plan view of most
approach charts and on airport diagrams.
Hazard
Avoidance
FliteCharts®
Procedures
The VFR Charts are digital representations of the Sectional Aeronautical Charts,
World 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 Aeronautical Charts are selected for display on
the G1000 as an option on the Map Page Group. The charts are only available on the
MFD map and not on other maps such as the inset or HSI map.
Flight
Planning
IFR/VFR Charts are available for US, Canada, and select European countries, and
must be purchased and downloaded at the flyGarmin website. IFR/VFR Charts are
updated every 28 days except for Canadian IFR/VFR Charts which are updated every
56 days. The only way to get multiple European countries is to purchase one of the
Regional Europe databases.
GPS Nav
IFR/VFR Charts
Nav/Com/
XPDR/Audio
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
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.
EIS
ChartView (Optional)
Flight
Instruments
the Detail Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the Detail Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. 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.
View Charts from the Navigation Map Page
EIS
Flight
Instruments
Additional Features
Nav/Com/
XPDR/Audio
1)
Press the Charts Softkey when displayed.
Or:
GPS Nav
2)
Flight
Planning
Move the map pointer to point to a desired point on the map and press the
Charts Softkey.
Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
3)
Press the GO BACK Softkey to return to the previous page.
Additional
Features
Hazard
Avoidance
Procedures
View Charts from the Active Flight Plan Page
1)
While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Press the Charts Softkey. The appropriate chart is displayed, if available for
the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Change Day/Night View
68
1)
While viewing a 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.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Additional Features
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
EIS
In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
Flight
Instruments
6)
AIRPORT DIRECTORY
Procedures
Hazard
Avoidance
SIRIUS XM RADIO ENTERTAINMENT
Selecting the XM Radio Page
3)
Press the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Annun/Alerts
Turn the small FMS Knob to select XM Radio.
Abnormal
Operation
2)
Additional
Features
The XM Radio Page provides information and control of the audio entertainment
features of the Sirius XM Satellite Radio.
Turn the large FMS Knob to select the Auxiliary Page Group.
Flight
Planning
While viewing the WPT-Airport Information Page, if necessary, press the
INFO-1 Softkey to change the softkey label to display INFO-2. Airport
information is displayed on the right half of the display.
1)
GPS Nav
View Airport Directory Information
Nav/Com/
XPDR/Audio
The Aircraft Owners and Pilots Association (AOPA) or AC-U-KWIK Airport
Directory database offers detailed information regarding services, hours of operation,
lodging options, and more for various airports. This information is viewed on the
WPT-Airport Information Page.
The Airport Directory databases are revised every 56 days. The Airport Directory is
always available for use after the expiration date. Check fly.garmin.com for the current
database.
Active Channel and Channel List
Appendix
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
Index
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69
Selecting a Category
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Press the Category Softkey on the XM Radio Page.
2) Press the CAT + and CAT - softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
Select an Available Channel within the Selected Category
1)
While on the XM Radio Page, press the Channel Softkey.
2)
Press the CH + Softkey to go down through the list in the Channel Box, or
move up the list with the CH – Softkey.
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Additional Features
Or:
Hazard
Avoidance
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
3)
With the desired channel highlighted, press the ENT Key.
Annun/Alerts
Abnormal
Operation
Additional
Features
Entering a Channel Directly
1)
While on the XM Radio Page, press the Channel Softkey.
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.
Assigning Channel Presets
Index
Appendix
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, 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.
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Additional Features
Press the SET Softkey.
4)
Press any one of the (Preset 1 - Preset 15) softkeys to assign a number
to the active channel.
Flight
Instruments
3)
With the 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 Volume Softkey is pressed, the volume can
also be adjusted using the small FMS Knob.)
Nav/Com/
XPDR/Audio
1)
EIS
Adjusting Volume
GPS Nav
Mute Sirius XM Audio
Select the XM Radio Page or XM Information Page.
2)
Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again
to unmute the audio.
Additional
Features
Entering a Scheduler Message
1) Select the AUX - Utility Page.
Hazard
Avoidance
The Scheduler feature can be used to enter and display reminder messages (e.g., Change
oil, Altimeter-Transponder, or Hot Section Inspection or Phase 1 Maintenance Check) in
the Messages Window on the PFD. Message timers set to periodic alerting automatically
reset to the original timer value once the message is displayed. When power is cycled, all
messages are retained until deleted, and message timer countdown is resumed.
Procedures
SCHEDULER
Flight
Planning
1)
Turn the large FMS Knob to highlight the first empty scheduler message
naming field.
4)
Use the FMS Knob to enter the message text to be displayed in the
Messages Window and press the ENT Key.
5)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the field next to Type.
6)
Turn the small FMS Knob to select the message type:
Appendix
3)
Annun/Alerts
Press the FMS Knob momentarily to activate the flashing cursor.
Abnormal
Operation
2)
• Event—Message issued at the specified date/time
Index
• One-time—Message issued when the message timer reaches zero
(default setting)
• Periodic—Message issued each time the message timer reaches zero
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71
EIS
Flight
Instruments
Additional Features
7)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the next field.
8)
For periodic and one-time message, use the FMS Knob to enter the timer
value (HH:MM:SS) from which to countdown and press the ENT Key.
9)
For event-based messages:
Nav/Com/
XPDR/Audio
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press
the ENT Key.
GPS Nav
b) Press the ENT Key again or use the large FMS Knob to move the cursor
to the next field.
c) Use the FMS Knob to enter the desired time (HH:MM) and press the
ENT Key.
Flight
Planning
10) Press the ENT Key again or use the large FMS Knob to move the cursor to
enter the next message.
Procedures
Deleting a Scheduler Message
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
1) Select the AUX - Utility Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the name field of the scheduler
message to be deleted.
4)
Press the CLR Key to clear the message text. If the CLR Key is pressed
again, the message is restored.
5)
Press the ENT Key while the message line is cleared to clear the message
time.
When a scheduler message is waiting, the Messages Softkey flashes. Pressing
the Messages Softkey opens the Messages Window and acknowledges the scheduler
message. Pressing the Messages Softkey again removes the Messages Window from
the display, and the scheduler message is deleted from the message queue.
MAINTENANCE LOGS WIFI
The system provides recording of CAS, CMC, exceedances, and other critical
aircraft data that occur while the aircraft is on the ground or in flight.
The Maintenance Logs feature is accessible by entering a password. No pilot
action is required. Turn the large FMS Knob on the MFD to select the AUXMaintenance WiFI Setup Page.
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Additional Features
Nav/Com/
XPDR/Audio
Creating a Profile
1) Use the FMS Knob to select the AUX - System Setup Page.
Press the FMS Knob momentarily to activate the flashing cursor.
GPS Nav
2)
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
4)
Press the ENT Key. A ‘Create Profile’ window is displayed.
Flight
Planning
5) Use the FMS Knob to enter a profile name up to 16 characters long and
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.
7)
Press the ENT Key.
Hazard
Avoidance
6)
Procedures
press the ENT Key. Pilot profile names cannot begin with a blank as the
first letter.
Additional
Features
8) With ‘CREATE’ highlighted, press the ENT Key to create the profile.
Or:
10) Press the FMS Knob to deactivate the cursor.
Selecting an Active Profile
Appendix
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Annun/Alerts
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
Abnormal
Operation
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
9)
EIS
When the system is powered on, the last selected pilot profile is shown on the MFD
power-up 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 AUX - System Setup Page in the box labeled ‘Pilot Profile’.
Flight
Instruments
PILOT PROFILES
Press the FMS Knob momentarily to activate the flashing cursor.
Index
3) Turn the large FMS Knob to highlight the active profile field in the Pilot
Profile Box.
4) Turn the small FMS Knob to display the pilot profile list and highlight the
desired profile.
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73
Additional Features
Flight
Instruments
5) Press the ENT Key. The system loads and displays the system settings for
the selected profile.
6)
Press the FMS Knob to deactivate the cursor.
EIS
Renaming a Profile
Nav/Com/
XPDR/Audio
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
GPS Nav
4)
Press the ENT Key.
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
Flight
Planning
rename.
6)
Press the ENT Key.
7) Use the FMS Knob to enter a new profile name up to 16 characters long
Procedures
and press the ENT Key.
8) With ‘RENAME’ highlighted, press the ENT Key.
Hazard
Avoidance
9)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
10) Press the FMS Knob to deactivate the cursor.
Additional
Features
Deleting a Profile
NOTE: The profile that is currently active cannot be deleted. If this is the
Annun/Alerts
Abnormal
Operation
desired profile to delete, select another profile, then delete the desired
profile.
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Appendix
3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
4)
Press the ENT Key.
5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to
Index
delete.
6)
74
Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Additional Features
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
9)
Press the FMS Knob to deactivate the cursor.
EIS
8)
Flight
Instruments
7) With ‘DELETE’ highlighted, press the ENT Key.
Importing a Profile from an SD Card
2)
Turn the FMS Knob to select the AUX - System Setup Page.
3)
Select the IMPORT Softkey.
4)
The system displays the Pilot Profile Importing Window with ‘IMPORT’
highlighted. To change the selected profile to be imported from the SD card
(shown as ‘SELECT FILE’), turn the large FMS Knob to highlight the profile
file name, then turn the small FMS Knob to highlight a profile from the list,
and press the ENT Key.
5)
If desired, the profile name to be used after profile has been imported can
be changed by turning the FMS Knob to highlight the ‘PROFILE NAME’
field, then use the large and small FMS Knobs to enter the name, and press
the ENT Key. Imported profile names cannot begin with a blank space or
be named ‘DEFAULT’, ‘GARMIN DEFAULTS’ or ‘DEFAULT SETTINGS’.
6)
With ‘IMPORT’ highlighted, press the ENT Key.
7)
If the imported profile name is the same as an existing profile on the
system, the system displays an ‘Overwrite existing file? OK or CANCEL’
prompt. Press the ENT Key to replace profile on the system with the profile
imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’
and press the ENT Key to return to the Pilot Profile Importing Window.
8)
If successful, the system displays ‘Pilot profile import succeeded.’ in the
IMPORT RESULTS window below. With ‘OK’ highlighted, press the ENT or
CLR Keys or press the FMS Knob to return to the AUX - System Setup Page.
The imported profile becomes the active profile.
GPS Nav
Insert an SD card containing the pilot profile(s) into the top card slot on the
MFD.
Nav/Com/
XPDR/Audio
1)
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
75
Additional Features
1)
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the AUX - System Setup Page.
3)
If necessary, activate the desired pilot profile to export. Only the currently
active Pilot Profile can be exported.
4)
Select the EXPORT Softkey. The system displays the Pilot Profile Exporting
Window.
5)
To export the pilot profile using the current supplied name, press the ENT
Key with ‘EXPORT’ highlighted. To change the profile file name turn the
large FMS Knob to highlight the ‘SELECT FILE’ field, then enter the new
name with the large and small FMS Knobs, then press the ENT Key. Then
press the ENT Key with ‘EXPORT’ highlighted.
6)
If the profile name to be exported is the same as an existing profile file
name on the SD card, the system displays an ‘Overwrite existing file? OK
or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD
card with the profile to be exported, or turn the FMS Knob to highlight
‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting
Window without exporting the profile.
7)
If successful, the EXPORT RESULTS window displays ‘Pilot profile export
succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the
FMS Knob to return to the AUX - System Setup Page.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Exporting a Profile to an SD Card
CONNEXT SETUP
The Connext Setup Page allows for setting up the installed optional Flight Stream
device for a Bluetooth connection between the G1000 and a mobile device running the
Garmin Pilot™ application.
The mobile device must be ‘paired’ with the G1000 in order to use the various
functions. Pairing is accomplished by first placing the G1000 in pairing mode by
displaying the Connext Setup Page. The G1000 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.
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Additional Features
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.
Flight
Instruments
Viewing the Connext Setup Page
EIS
Changing the Bluetooth Name
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.
GPS Nav
4)
Press the ENT Key. The cursor is removed and the new name is displayed.
Flight
Planning
Nav/Com/
XPDR/Audio
1)
Enabling/Disabling Flight Plan Importing from Garmin Pilot
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.
Enabling/Disabling Automatic Reconnection of a Specific Paired Device
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 G1000 to automatically connect to a previously
paired device when detected.
4)
Press the FMS Knob to remove the cursor.
Annun/Alerts
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
Abnormal
Operation
1)
Additional
Features
2)
Hazard
Avoidance
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
Procedures
1)
Appendix
Index
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Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
77
Additional Features
1)
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)
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.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Remove a Specific Paired Device from the List of Paired Devices:
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Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Additional
Features
Abnormal
Operation
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Hazard
Avoidance
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Procedures
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFD
and MFD, the emergency frequency (121.500 MHz) automatically becomes the active
frequency on both COM radios.
Flight
Planning
ABNORMAL COM OPERATION
GPS Nav
NOTE: The PA-28-181 Archer Pilot’s Operating Handbook (POH) always takes
precedence over the information found in this section.
Nav/Com/
XPDR/Audio
• PFD failure – Press the DISPLAY BACKUP Button on the audio panel to
put the MFD in reversionary mode.
• MFD failure – PFD enters reversionary mode. Reversionary display mode
can be manually activated by pressing the DISPLAY BACKUP Button on the
audio panel.
EIS
Should a system detected failure occur in either display, the G1000 automatically
enters reversionary mode. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
In the event of display failure, the display modes are as follows:
Annun/Alerts
Appendix
Loss of Hazard Functions with Loss of GPS
Position
Index
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79
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight Director
Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Extreme Pitch Indication
DEAD RECKONING
While in Enroute or Oceanic phase of flight, if the G1000 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 G1000 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.
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Abnormal Operation
EIS
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, 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.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your 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 G1000 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 compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Flight
Instruments
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 G1000 stops
navigating in GPS Mode.
Appendix
Index
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
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81
As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as yellow text on the display to denote degraded
navigation source information. This data includes the following:
• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up
to 20 minutes. Terrain Proximity, TERRAIN-SVS, and TAWS-B are also disabled.
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
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
82
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Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
G1000 SYSTEM ANNUNCIATIONS
GPS Nav
Comment
Nav/Com/
XPDR/Audio
System Annunciation
EIS
When an LRU or an LRU function fails, a large red “X” is typically displayed on
windows associated with the failed data. Refer to the PA-28-181 Archer Pilot’s Operating Handbook (POH) for additional information regarding pilot responses to these
annunciations
Flight
Planning
Attitude and Heading Reference System is aligning.
Procedures
Hazard
Avoidance
Display system is not receiving attitude information from the
AHRS.
Additional
Features
Abnormal
Operation
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).
Annun/Alerts
Display system is not receiving valid heading input from
AHRS.
Appendix
Display system is not receiving valid transponder information.
Index
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Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
83
G1000 SYSTEM ANNUNCIATIONS (CONT.)
System Annunciation
Comment
EIS
Flight
Instruments
Annunciations & Alerts
GPS Nav
Nav/Com/
XPDR/Audio
Display system is not receiving airspeed input from air data
computer.
Procedures
Flight
Planning
Display system is not receiving altitude input from the air
data computer.
Additional
Features
Hazard
Avoidance
Display system is not receiving vertical speed input from the
air data computer.
Abnormal
Operation
Display system is not receiving valid temperature
information from air data computer.
Annun/Alerts
Display system is not receiving valid ISA information from
air data computer.
A red or amber ‘X’ through any other display field (such as
engine instrumentation display) indicates that the field is not
receiving valid data.
Index
Appendix
Other Various Red and
Amber X Indications
84
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Annunciations & Alerts
The following annunciations are configured specifically for the PA-28-181 Archer
aircraft. See the PA-28-181 Archer POH for information regarding pilot responses.
EIS
Warning Annunciations
Alternator failure
Left fuel quantity in warning range
Right fuel quantity in warning range
Audio Alert
GPS Nav
START ENGD
Description
Nav/Com/
XPDR/Audio
Annunciation
Window Text
ALTR FAIL
L FUEL QTY
R FUEL QTY
Triple Chime
Starter motor energized when engine is running
Flight
Planning
Caution Annunciations
Description
Procedures
Audio Alert
Air conditioning condenser door is open
Hazard
Avoidance
Left fuel quantity in caution range
Right fuel quantity in caution range
Double Chime
Pitot heat failure
Pitot heat selected OFF
Additional
Features
Annunciation
Window Text
AC DOOR OPEN*
L FUEL QTY
R FUEL QTY
PITOT HEAT FAIL
PITOT HEAT OFF
 Optional
Flight
Instruments
CAS ANNUNCIATIONS
Abnormal
Operation
Annun/Alerts
Appendix
Index
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85
Advisory Annunciations
Annunciation
Description
Window Text
AC DOOR OPEN Air conditioning condenser door is open
AV FAN FAIL
Avionics cooling fan is inoperative
EMERG BAT ON Emergency power in use
Difference between left and right fuel quantity >
FUEL IMBAL
10 gallons
MAINT MODE Maintenance Mode has been activated
MFD FAN FAIL MFD display fan is inoperative
PFD FAN FAIL
PFD display fan is inoperative
 Optional
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
Audio Alert
Single Chime
TERRAIN-SVS ALERTS
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
MFD
Pop-Up Alert
Aural
Message
Reduced Required Terrain
Clearance Warning (RTC)
“Warning; Terrain,
Terrain”
Imminent Terrain Impact
Warning (ITI)
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
“Warning; Obstacle,
Obstacle”
Reduced Required Terrain
Clearance Caution (RTC)
“Caution; Terrain,
Terrain”
Imminent Terrain Impact
Caution (ITI)
“Caution; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
“Caution; Obstacle,
Obstacle”
Imminent Obstacle Impact
Caution (IOI)
“Caution; Obstacle,
Obstacle”
86
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Aural Message
TERRAIN TEST
None
None
“Terrain System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
Terrain System Test
Fail
TERRAIN FAIL
“Terrain System
Failure”
Terrain or Obstacle
database unavailable
or invalid,
invalid software
configuration, system
audio fault
TERRAIN FAIL
“Terrain System
Failure”
NO GPS POSITION
“Terrain System
Not Available”
None
“Terrain System
Not Available”
None
“Terrain System
Available”
System Test in
Progress
None
None
Abnormal
Operation
Annun/Alerts
None
Additional
Features
Sufficient GPS signal
received after loss
Hazard
Avoidance
Excessively degraded
GPS signal, Out of
database coverage
area
Procedures
No GPS position
Flight
Planning
MFD Terrain or
Obstacle database
unavailable or invalid.
Terrain-SVS operating
with PFD Terrain or
Obstacle databases
GPS Nav
Terrain Alerting is
disabled
Nav/Com/
XPDR/Audio
System Test Pass
EIS
TERRAIN-SVS Page
Annunciation
Alert Type
PFD/MFD Alert
Annunciation
Flight
Instruments
TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
87
Flight
Instruments
Annunciations & Alerts
TAWS-B ALERTS
MFD
Pop-Up Alert
Aural Message
“Pull Up”
Reduced Required
Terrain Clearance
Warning (RTC)
or
Imminent Terrain
Impact Warning
(ITI)
or
Reduced Required
Obstacle Clearance
Warning (ROC)
or
Imminent Obstacle
Impact Warning
(IOI)
or
Annun/Alerts
Reduced Required
Terrain Clearance
Caution (RTC)
Imminent Terrain
Impact Caution
(ITI)
Reduced Required
Obstacle Clearance
Caution (ROC)
Index
PFD/MFD
TAWS-B Page
Annunciation
Excessive Descent
Rate Warning
(EDR)
Appendix
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Alert Type
Imminent Obstacle
Impact Caution
(IOI)
88
“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain
Ahead, Pull Up”
Terrain Ahead, Pull Up; Terrain
Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”
“Obstacle, Obstacle; Pull Up, Pull
Up”
or
“Obstacle Ahead, Pull Up; Obstacle
Ahead, Pull Up”
“Obstacle Ahead, Pull Up; Obstacle
Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull
Up”
or
“Caution, Terrain; Caution, Terrain”
or
“Terrain Ahead; Terrain Ahead”
or
“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution, Terrain”
or
“Caution, Obstacle; Caution,
Obstacle”
or
“Obstacle Ahead; Obstacle Ahead”
or
“Obstacle Ahead; Obstacle Ahead”
or
“Caution, Obstacle; Caution,
Obstacle”
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
Flight
Instruments
Alert Type
Aural Message
“Too Low, Terrain”
None
None
Nav/Com/
XPDR/Audio
Altitude Callout
“500”
EIS
Premature Descent
Alert Caution
(PDA)
“Five-Hundred”
“Sink Rate”
GPS Nav
Excessive Descent
Rate Caution
(EDR)
“Don’t Sink”
or
“Too Low, Terrain”
or
Flight
Planning
Negative Climb
Rate Caution
(NCR)
PFD/MFD Alert
Annunciation
Alert Type
TAWS TEST
None
None
“TAWS System Test
OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System
Failure”
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, system
audio fault
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
System Test in Progress
System Test Pass
None
TAWS Alerting is disabled
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Appendix
190-02131-00 Rev. C
Annun/Alerts
No GPS position
None
Abnormal
Operation
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
Additional
Features
Aural Message
Hazard
Avoidance
TAWS-B Page Annunciation
Procedures
TAWS-B SYSTEM STATUS ANNUNCIATIONS
89
Alert Type
Sufficient GPS signal
received after loss
None
TAWS-B Page Annunciation
Aural Message
None
“TAWS Not
Available”
None
“TAWS Available”
GDL 69 SXM DATA LINK RECEIVER MESSAGES
Message
Message Location
CHECK ANTENNA
XM Information Page
(MFD)
Data Link Receiver antenna
error; service required
UPDATING
XM Information Page
(MFD))
Data Link Receiver updating
encryption code
NO SIGNAL
XM Information Page
Weather Datalink Page
(MFD)
Loss of signal; signal strength
too low for receiver
LOADING
XM Radio Page (MFD)
Acquiring channel audio or
information
OFF AIR
XM Radio Page (MFD)
Channel not in service
--------
XM Radio Page (MFD)
Missing channel information
WEATHER DATA LINK FAILED
Weather Datalink Page
(MFD)
No communication from Data
Link Receiver within last 5
minutes
ACTIVATION REQUIRED
XM Information Page
(MFD)
Sirius XM subscription is not
activated
DETECTING ACTIVATION
Weather Datalink Page
(MFD)
Sirius XM subscription is
activating.
WAITING FOR DATA...
Weather Datalink Page
(MFD)
Sirius XM subscription
confirmed downloading
weather data.
Flight
Planning
Procedures
Hazard
Avoidance
Description
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
PFD/MFD Alert
Annunciation
Excessively degraded
GPS signal, Out of
database coverage area
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
90
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Message
Priority
Flight
Instruments
VOICE ALERTS
Description
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Annun/Alerts
190-02131-00 Rev. C
Abnormal
Operation
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Additional
Features
The ADAHRS is using the backup GPS path.
Primary GPS path has failed. The system
should be serviced when possible.
The ADAHRS is not receiving any or any
useful GPS information. Check POH
limitations. The system should be serviced.
Hazard
Avoidance
AHRS1 GPS – AHRS1 using backup
GPS source.
Procedures
Comments
Abort approach due to loss of GPS
navigation.
The ADAHRS is reporting that the altitude
error correction is unavailable.
The ADAHRS is reporting that the airspeed
error correction is unavailable.
The ADAHRS calibration version error. The
system should be serviced.
ADAHRS configuration settings do not
match those of backup configuration
memory. The system should be serviced.
Flight
Planning
Message
ABORT APR – Loss of GPS navigation.
Abort approach.
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
AHRS1 CAL – AHRS1 calibration version
error. Srvc req’d.
AHRS1 CONFIG – AHRS1 config error.
Config service req’d.
GPS Nav
SYSTEM MESSAGE ADVISORIES
Nav/Com/
XPDR/Audio
Imminent stall is sensed by stall vane
Airspeed exceeds VNE
Warning
Aircraft has descended below the preset barometric
“Minimums, minimums”
minimum descent altitude
“Traffic”
TIS Traffic Alert
Caution
“Traffic, (distance, bearing, altitude)”
TAS Traffic Alert
“TAS System Test Passed”
TAS system initiated test passed
“TAS System Test Failed”
TAS system initiated test failed
Aircraft is one minute from Top of Descent. Issued
“Vertical track”
Advisory
only when vertical navigation is enabled.
“Traffic Not Available
Aircraft is outside TIS coverage area
“Timer Expired”
Countdown timer on the PFD has reached zero
EIS
“Stall”
“Airspeed”
91
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 SERVICE – AHRS1 Magneticfield model needs update.
Comments
The ADAHRS is not receiving backup GPS
information. The system should be serviced.
The ADAHRS is operating exclusively in noGPS mode. The system should be serviced.
The ADAHRS earth magnetic field model is
out of date. Update magnetic field model
when practical.
AHRS1 TAS – AHRS1 not receiving
The ADAHRS is not receiving true airspeed
airspeed.
from the air data computer. The ADAHRS
relies on GPS information to augment the
lack of airspeed. The system should be
serviced.
APR DWNGRADE – Approach
Use LNAV minima when approach is
downgraded.
downgraded.
ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The
than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of
ahead.
the aircraft position.
APR INACTV – Approach is not active. The system notifies the pilot that the loaded
approach is not active. Activate approach
when required.
CHECK CRS – Database course for
Selected course for LOC2 differs from
LOC2 / [LOC ID] is [CRS]°.
published localizer course by more than 10
degrees.
CNFG MODULE – PFD1 configuration The PFD1 configuration module backup
module is inoperative.
memory has failed. The system should be
serviced.
CO DET SRVC – The carbon
A failure has been detected in carbon
monoxide detector needs service.
monoxide detector has been detected. The
detector may still be available. The system
should be serviced when possible.
92
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Flight
Instruments
EIS
Message
Comments
CO DET FAIL – The carbon monoxide A failure in the carbon monoxide detector
detector is inoperative.
has been detected. The system should be
serviced.
COM1 CONFIG – COM1 config error. The COM1 configuration settings do not
Config service req’d.
match backup configuration memory. The
system should be serviced
COM1 PTT – COM1 push-to-talk key The COM1 external push-to-talk switch is
is stuck.
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 RMT XFR – COM1 remote
The COM1 transfer switch is stuck in the
transfer key is stuck.
enabled (or “pressed”) position. Press the
transfer switch again to cycle its operation.
If the problem persists, the system should be
serviced.
COM1 SERVICE – COM1 needs
The system has detected a failure in COM1.
service. Return unit for repair.
COM1 may still be usable. The system
should be serviced when possible.
COM1 TEMP – COM1 over temp.
The system has detected an over
Reducing transmitter power.
temperature condition in COM1. The
transmitter operates at reduced power. If
the problem persists, the system should be
serviced.
COM2 CONFIG – COM2 config error. The COM2 configuration settings do not
Config service req’d.
match backup configuration memory. The
system should be serviced
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
93
Message
COM2 PTT – COM2 push-to-talk key
is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
Comments
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 COM2 transfer switch is stuck in the
enabled (or “pressed”) position. Press the
transfer 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.
The system has detected an over
temperature condition in COM2. The
transmitter operates at reduced power. If
the problem persists, the system should be
serviced.
COPILOT RADIOS MUTED – Copilot
The copilot radios are set on mute.
radios are muted.
DATA LOST – Pilot stored data was
The pilot profile data was lost. System
lost. Recheck settings.
reverts to default pilot profile and settings.
The pilot may reconfigure the MFD & PFD
with preferred settings, if desired.
DB CHANGE – Database changed.
This occurs when a stored flight plan
Verify user modified procedures.
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
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
94
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Flight
Instruments
Message
DB CHANGE – Database changed.
Verify stored airways.
EIS
Comments
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.
DB MISMATCH – Navigation
The PFD and MFD have different navigation
database mismatch. Xtalk is off.
database versions or types installed. Crossfill
is off. Check the AUX-System Status Page to
determine versions or regions. Also, check
the AUX-System Status Page for a database
synchronization function not completed.
After synchronization is complete, power
must be turned off, then on.
DB MISMATCH – Obstacle database The PFD and MFD have different obstacle
mismatch.
database versions or types installed.
Check the AUX-System Status Page to
determine versions or regions. Also, check
the AUX-System Status Page for a database
synchronization function not completed.
After synchronization is complete, power
must be turned off, then on.
DB MISMATCH – Standby Navigation The PFD and MFD have different standby
database mismatch.
navigation database versions or types
installed. Check the AUX-System Status
Page to determine versions or regions.
Also, check the AUX-System Status Page
for a database synchronization function
not completed. After synchronization is
complete, power must be turned off, then
on.
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
95
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
DB MISMATCH – Terrain database
mismatch.
Comments
The PFD and MFD have different terrain
database versions or types installed.
Check the AUX-System Status Page to
determine versions or regions. Also, check
the AUX-System Status Page for a database
synchronization function not completed.
After synchronization is complete, power
must be turned off, then on.
DIG GMA1 MANIFEST – DIG GMA The digital audio controller has incorrect
1 software mismatch, communication software installed. The system should be
halted.
serviced.
DME CHECK RANGE – DME range
A failure or disagreement has been detected
disagreement. Check position sensors. in a DME receiver. Check position sensors.
FAILED PATH – A data path has
A data path connected to the GDU or the
failed.
GIA 63W has failed.
FPL TRUNC – Flight plan has been
This occurs when a newly installed
truncated.
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.
FPL WPT LOCK – Flight plan waypoint Upon power-up, the system detects that a
is locked.
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.
96
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Flight
Instruments
Message
FPL WPT MOVE – Flight plan
waypoint moved.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Nav/Com/
XPDR/Audio
190-02131-00 Rev. C
EIS
Comments
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.
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. A failure has been detected in glideslope
Return unit for repair.
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. A failure has been detected in glideslope
Return unit for repair.
receiver 2. The receiver may still be
available. The system should be serviced
when possible.
GDC1 MANIFEST – GDC1 software
The ADAHRS has incorrect software
mismatch, communication halted.
installed. The system should be serviced.
GDL59 CONFIG – GDL 59 config
GDL 59 configuration settings do not match
error. Config service req’d.
those of backup configuration memory. The
system should be serviced.
GDL59 FAIL – GDL 59 has failed.
A fault has been detected in the GDL 59.
The receiver is unavailable. The system
should be serviced.
GDL59 RTR FAIL – The GDL 59 router A fault has been detected in the GDL 59
has failed.
router. The system should be serviced.
GDL59 SERVICE – GDL 59 needs
A fault has been detected in the GDL 59.
service. Return unit for repair.
The system should be serviced.
GDL69 CONFIG – GDL 69 config
GDL 69/69A SXM configuration settings do
error. Config service req’d.
not match those of backup configuration
memory. The system should be serviced.
97
Message
GDL69 FAIL – GDL 69 has failed.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GDL69 MANIFEST – GDL software
mismatch, communication halted.
GEA1 CONFIG – GEA1 config error.
Config service req’d.
GEA1 MANIFEST – GEA1 software
mismatch, communication halted.
GEO LIMITS – AHRS1 too far North/
South, no magnetic compass.
GFC MANIFEST – GFC software
mismatch, communication halted.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA1 MANIFEST – GIA1 software
mismatch, communication halted.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
98
Comments
A failure has been detected in the GDL
69/69A or GDL 69/69A SXM. The receiver is
unavailable. The system should be serviced.
The GDL 69/69A SXM has incorrect software
installed. The system should be serviced.
The GEA1 configuration settings do not
match those of backup configuration
memory. The system should be serviced.
The #1 GEA 71 has incorrect software
installed. The system should be serviced.
The aircraft is outside geographical limits for
approved ADAHRS operation. Heading is
flagged as invalid.
Incorrect servo software is installed, or gain
settings are incorrect.
The GIA1 have an error in the audio
configuration. The system should be
serviced.
The GIA1 configuration settings do not
match backup configuration memory. The
system should be serviced.
The GIA1 and/or GIA2 temperature is too
low to operate correctly. Allow units to
warm up to operating temperature.
The GIA1 temperature is too high. If
problem persists, the system should be
serviced.
The GIA1 1 has incorrect software installed.
The system should be serviced.
The GIA1 self-test has detected a problem in
the unit. The system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Flight
Instruments
Message
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Nav/Com/
XPDR/Audio
190-02131-00 Rev. C
EIS
Comments
The GIA2 have an error in the audio
configuration. The system should be
serviced.
GIA2 CONFIG – GIA2 config error.
The GIA2 configuration settings do not
Config service req’d.
match backup configuration memory. The
system should be serviced.
GIA2 COOLING – GIA2 over
The GIA2 temperature is too high. If
temperature.
problem persists, the system should be
serviced.
GIA2 COOLING – GIA2 temperature The GIA2 temperature is too low to operate
too low.
correctly. Allow units to warm up to
operating temperature.
GIA2 MANIFEST – GIA2 software
The GIA 2 has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GIA2 SERVICE – GIA2 needs service. The GIA2 self-test has detected a problem in
Return the unit for repair.
the unit. The system should be serviced.
GMA1 AUX MANIFEST – GMA 1 AUX The digital audio controller has incorrect
software mismatch, communication
software installed. The system should be
halted.
serviced.
GMA1 CONFIG – GMA1 config error. The audio panel configuration settings do
Config service req’d.
not match backup configuration memory.
The system should be serviced.
GMA1 FAIL – GMA1 is inoperative.
The audio panel self-test has detected a
failure. The audio panel is unavailable. The
system should be serviced.
GMA1 MANIFEST – GMA1 software The audio panel has incorrect software
mismatch, communication halted.
installed. The system should be serviced.
GMA1 SERVICE – GMA1 needs
The audio panel self-test has detected a probservice. Return unit for repair.
lem 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.
99
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
GMU1 MANIFEST – GMU1 software
mismatch, communication halted.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
GRS1 MANIFEST – GRS1 software
mismatch, communication halted.
GTS CONFIG – GTS config error.
Config service req’d.
GTS MANIFEST – GTS software
mismatch, communication halted.
GTX1 MANIFEST – GTX1 software
mismatch, communication halted.
HDG FAULT – AHRS1 magnetometer
fault has occurred.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
100
Comments
The GMU 44 has incorrect software
installed. The system should be serviced.
Loss of GPS navigation due to insufficient
satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still
be available. The system should be serviced.
The ADAHRS has incorrect software
installed. The system should be serviced.
GTS 800 configuration settings do not
match those of the GDU configuration. The
system should be serviced.
The GTS has incorrect software installed.
The system should be serviced.
The transponder has incorrect software
installed. The system should be serviced.
A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The ADAHRS
uses GPS for backup mode operation. The
system should be serviced.
A GIA mismatch has been detected, where
only one is SBAS capable.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Additional
Features
The specified GDU has different software
versions installed. The system should be
serviced.
One of the terrain or obstacle databases
required for TAWS in the specified GDU is
missing or invalid.
The specified GDU’s backlight calibration
cannot be found or is invalid. The system
should be serviced.
The MFD configuration settings do not
match backup configuration memory. The
system should be serviced.
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Abnormal
Operation
190-02131-00 Rev. C
Hazard
Avoidance
MFD1 CONFIG – MFD1 config error.
Config service req’d.
Procedures
MFD1 BACKLIGHT CALIBRATION –
MFD1 calibration. Return for repair.
Flight
Planning
MFD TERRAIN DSP – MFD Terrain
awareness display unavailable.
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
GPS Nav
MANIFEST – MFD1 software
mismatch, communication halted.
MANIFEST – PFD1 software
mismatch, communication halted.
MFD SOFTWARE – MFD mismatch,
communication halted.
Nav/Com/
XPDR/Audio
LOI – GPS integrity lost. Crosscheck
with other NAVS.
LRG MAG VAR – Verify all course
angles.
EIS
LOCKED FPL – Cannot navigate
locked flight plan.
Comments
The aircraft is inside the airspace.
Data link avionics were not configured
correctly and therefore will not be able to
communicate with the ground network.
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.
GPS integrity is insufficient for the current
phase of flight.
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°.
Flight
Instruments
Message
INSIDE ARSPC – Inside airspace.
INVALID ADM – Invalid ADM: ATN
communication halted.
101
Message
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
MFD1 DB ERR – MFD1 multiple
database errors exists.
MFD1 DB ERR – MFD1 navigation
database error exists.
MFD1 DB ERR – MFD1 obstacle
database error exists.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MFD1 DB ERR – MFD1 obstacle
database missing.
102
Comments
The MFD is overheating and is reducing
power consumption by dimming the display.
If problem persists, the system should be
serviced.
The MFD detected a failure in the Airport
Directory database. Ensure that the data
card is properly inserted. Replace data card.
If problem persists, the system should be
serviced.
The MFD detected a failure in the basemap
database.
The MFD detected a failure in the ChartView
database (optional feature). Ensure that the
data card is properly inserted. data card.
If problem persists, the system should be
serviced.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure that the
data card is properly inserted. Replace data
card. If problem persists, the system should
be serviced.
The MFD detected a failure in more than
one database. If problem persists, the
system should be serviced.
The MFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system
should be serviced.
The MFD detected a failure in the obstacle
database. Ensure that the data card is
properly inserted. Replace data card. If
problem persists, the system should be
serviced.
The obstacle database is present on another
LRU, but is missing on the specified LRU.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
103
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Procedures
190-02131-00 Rev. C
Flight
Planning
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
NAV1 MANIFEST – NAV1 software
mismatch, communication halted.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
GPS Nav
MFD1 DB ERR – MFD1 terrain
database missing.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MFD1 KEYSTK – MFD1 [key name]
is stuck.
Nav/Com/
XPDR/Audio
MFD1 DB ERR – MFD1 terrain
database error exists.
EIS
MFD1 DB ERR – MFD1 terrain
database error exists.
Comments
The MFD detected a failure in the Safe
Taxi database. Ensure that the data card
is properly inserted. Replace data card. If
problem persists, the system should be
serviced.
The MFD detected a failure in the terrain
database. Ensure that the terrain card is
properly inserted in display. Replace terrain
card. If problem persists, the system should
be serviced.
The MFD detected a failure in the terrain
database. Ensure that the terrain card is
properly inserted in display. Replace terrain
card. If problem persists, the system should
be serviced.
The terrain database is present on another
LRU, but is missing on the specified LRU.
The MFD self-test has detected a problem.
The system should be serviced.
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.
The MFD voltage is low. The system should
be serviced.
NAV1 software mismatch. The system
should be serviced.
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.
Flight
Instruments
Message
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
Comments
NAV1 SERVICE – NAV1 needs service. A failure has been detected in the NAV1
Return unit for repair.
receiver. The receiver may still be available.
The system should be serviced.
NAV2 MANIFEST – NAV2 software
NAV2 software mismatch. The system
mismatch, communication halted.
should be serviced.
NAV2 RMT XFR – NAV2 remote
The remote NAV2 transfer switch is stuck in
transfer key is stuck.
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. A failure has been detected in the NAV2
Return unit for repair.
receiver. The receiver may still be available.
The system should be serviced.
NON-MAGNETIC UNITS– NonNavigation angle is not set to MAGNETIC at
magnetic NAV ANGLE display units
power-up.
are active.
NON WGS84 WPT – Do not use GPS The position of the selected waypoint [xxxx]
for navigation to [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 non-WGS84
waypoint..
PFD1 BACKLIGHT CALIBRATION –
The PFD1 backlight calibration cannot be
PFD1 calibration lost. Return for repair. found or is invalid. The system should be
serviced.
PFD1 CONFIG – PFD1 config error.
The PFD configuration settings do not match
Config service req’d.
backup configuration memory. The system
should be serviced.
PFD1 COOLING – PFD1 has poor
The PFD is overheating and is reducing
cooling. Reducing power usage.
power consumption by dimming the display.
If problem persists, the system should be
serviced.
PFD1 DB ERR – PFD1 basemap
The PFD detected a failure in the basemap
database error exists.
database.
104
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Appendix
Index
105
Annun/Alerts
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Abnormal
Operation
190-02131-00 Rev. C
Additional
Features
[PFD1, PFD2 or MFD1] CARD 1 ERR
– Card 1 is invalid.
Hazard
Avoidance
[PFD1, PFD2 or MFD1] CARD 2 REM
– Card 2 was removed. Reinsert card.
Procedures
[PFD1, PFD2 or MFD1] CARD 1 REM
– Card 1 was removed. Reinsert card.
Flight
Planning
PFD1 DB ERR – PFD1 terrain
database missing.
PFD1 KEYSTK – PFD1 [key name] is
stuck.
GPS Nav
PFD1 DB ERR – PFD1 terrain
database error exists.
Nav/Com/
XPDR/Audio
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
EIS
PFD1 DB ERR – PFD1
navigation database error exists.
Comments
The PFD detected a failure in more than one
database. If problem persists, the system
should be serviced.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system
should be serviced.
The obstacle database is present on another
LRU, but is missing on the specified LRU.
The PFD detected a failure in the Safe Taxi
database. Ensure that the data card is
properly inserted. Replace data card. If
problem persists, the system should be
serviced.
The PFD detected a failure in the terrain
database. Ensure that the terrain card is
properly inserted in display. Replace terrain
card. If problem persists, the system should
be serviced.
The terrain database is present on another
LRU, but is missing on the specified LRU.
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.
The SD card was removed from the top card
slot of the specified PFD or MFD. The SD
card needs to be reinserted.
The SD card was removed from the bottom
card slot of the specified PFD or MFD. The
SD card needs to be reinserted.
The SD card in the top card slot of the
specified PFD or MFD contains invalid data.
Flight
Instruments
Message
PFD1 DB ERR – PFD1 multiple
database errors exists.
Message
[PFD1, PFD2 or MFD1] CARD 2 ERR
– Card 2 is invalid.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD1 KEYSTK – PFD2 [key name] is
stuck.
Comments
The SD card in the bottom card slot of the
specified PFD or MFD contains invalid data.
The PFD1 voltage is low. The system should
be serviced.
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 SERVICE – PFD2 needs service. The PFD self-test has detected a problem.
Return unit for repair.
The system should be serviced.
PFD1 TERRAIN DSP – PFD1 Terrain
One of the terrain or obstacle databases
awareness display unavailable.
required for TAWS in PFD1 is missing or
invalid.
PFD1 VOLTAGE – PFD2 has low
The PFD2 voltage is low. The system should
voltage. Reducing power usage
be serviced.
PFD2 BACKLIGHT CALIBRATION –
The PFD2 backlight calibration cannot be
PFD2 calibration lost. Return for repair. found or is invalid. The system should be
serviced.
PFD2 CONFIG – PFD2 config error.
The PFD configuration settings do not match
Config service req’d.
backup configuration memory. The system
should be serviced.
PFD2 COOLING – PFD2 has poor
The PFD is overheating and is reducing
cooling. Reducing power usage.
power consumption by dimming the display.
If problem persists, the system should be
serviced.
PFD2 DB ERR – PFD2 basemap
The PFD detected a failure in the basemap
database error exists.
database.
PFD2 DB ERR – PFD2 multiple
The PFD detected a failure in more than one
database errors exists.
database. If problem persists, the system
should be serviced.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
106
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
The pilot radios are set on mute.
Index
190-02131-00 Rev. C
Procedures
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
PILOT RADIOS MUTED – Pilot
radios are muted.
PTK FAIL – Parallel track unavailable:
invalid leg type.
Flight
Planning
PFD2 SERVICE – PFD2 needs service.
Return unit for repair.
PFD2 TERRAIN DSP – PFD2 Terrain
awareness display unavailable.
GPS Nav
PFD2 DB ERR – PFD2 terrain
database missing.
PFD2 KEYSTK – PFD1 [key name] is
stuck.
Nav/Com/
XPDR/Audio
PFD2 DB ERR – PFD2 terrain
database error exists.
EIS
PFD2 DB ERR – PFD2 obstacle
database missing.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
Comments
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system
should be serviced.
The obstacle database is present on another
LRU, but is missing on the specified LRU.
The PFD detected a failure in the Safe Taxi
database. Ensure that the data card is
properly inserted. Replace data card. If
problem persists, the system should be
serviced.
The PFD detected a failure in the terrain
database. Ensure that the terrain card is
properly inserted in display. Replace terrain
card. If problem persists, the system should
be serviced.
The terrain database is present on another
LRU, but is missing on the specified LRU.
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.
The PFD self-test has detected a problem.
The system should be serviced.
One of the terrain or obstacle databases
required for TAWS in PFD2 is missing or
invalid.
The PFD2 voltage is low. The system should
be serviced.
Flight
Instruments
Message
PFD2 DB ERR – PFD2
navigation database error exists.
Invalid leg type for parallel offset.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
107
Message
PTK FAIL – Parallel track unavailable:
past IAF.
PTK FAIL – Parallel track unavailable:
bad geometry.
SCHEDULER [#] – <message>.
SLCT FREQ – Select appropriate
frequency for approach.
SLCT MAG– Select MAGNETIC NAV
ANGLE display units.
SLCT NAV – Select NAV on CDI for
approach.
SLCT NON-MAG– Select alternate
NAV ANGLE display units.
STEEP TURN – Steep turn ahead.
STRMSCP FAIL – Stormscope has
failed.
SVT DISABLED – Out of available
terrain region.
SVT DISABLED – Terrain DB
resolution too low.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
108
Comments
IAF waypoint for parallel offset has been
passed.
Bad parallel track geometry.
Message criteria entered by the user.
The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
The system notifies the pilot to set the Nav
Angle units on the Avionics Settings Screen
to Magnetic.
The system notifies the pilot to set the CDI
to the correct NAV receiver. Set the CDI to
the correct NAV receiver.
The system notifies the pilot to set the Nav
Angle units on the Avionics Settings Screen
to True.
A steep turn is 15 seconds ahead. Prepare
to turn.
Stormscope has failed. The system should
be serviced.
Synthetic Vision is disabled because the
aircraft is not within the boundaries of the
installed terrain database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (4.9 arcsecond or better) is not currently installed.
The MFD and PFD have different software
versions installed. The system should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
109
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Nav/Com/
XPDR/Audio
190-02131-00 Rev. C
EIS
Comments
TAWS is disabled because the audio
configuration is invalid. The system should
be serviced.
TERRAIN DISABLED – Terrain
TAWS is disabled because a terrain database
Awareness DB resolution too low.
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
The system is no longer receiving data from
failed.
the traffic system. The traffic device should
be serviced.
TRN AUD FAIL – Trn Awareness
Terrain Awareness audio is unavailable. The
audio source unavailable
system should be serviced.
UNABLE V WPT – Can’t reach current The current vertical waypoint can not be
vertical waypoint.
reached within the maximum flight path
angle and vertical speed constraints. The
system automatically transitions to the next
vertical waypoint.
VNV – Unavailable. Excessive
The current crosstrack exceeds the limit,
crosstrack error.
causing vertical deviation to go invalid.
VNV – Unavailable. Excessive track
The current track angle error exceeds the
angle error.
limit, causing the vertical deviation to go
invalid.
VNV – Unavailable. Parallel course
A parallel course has been selected, causing
selected.
the vertical deviation to go invalid.
VNV – Unavailable. Unsupported leg The lateral flight plan contains a procedure
type in flight plan.
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active
vertical waypoint.
WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is
-[xxxx]
the waypoint name.
Flight
Instruments
Message
TERRAIN AUD CFG – Trn Awareness
audio config error. Service req’d.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
XPDR1 ADS-B 1090 – Datalinik:
ADS-B 1090 receiver has failed.
XPDR1 ADS-B FAIL – Transponder:
XPDR1 is unable to transmit ADS-B
messages.
XPDR1 ADS-B NO POS –
Transponder: ADS-B is not transmitting
position.
XPDR1 ADS-B TRFC – Transponder:
ADS-B traffic has failed
XPDR1 ADS-B UAT – Datalink:
ADS-B in UAT receiver has failed.
XPDR1 CONFIG – XPDR1 config error.
Config service req’d.
Comments
A failure has been detected in the 1090
receiver.
ADS-B is inoperative. The transponder may
not be receiving a valid GPS position. Other
transponder functions may be available.
Service when possible.
The transponder is not able to receive
position information.
The Transponder is incapable of processing
traffic information.
A failure has been detected in the UAT
receiver.
The transponder configuration settings do
not match those of backup configuration
memory. The system should be serviced.
XPDR1 CSA FAIL - Traffic: ADS-B In ADS-B Conflict Situational Awareness (CSA)
traffic alerting has failed.
is unavailable.
XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1 or
#2 transponder.
XPDR1 FAULT – Datalink: ADSB-B in The transponder is unable to receive ADS-B
has failed.
information.
XPDR1 FIS-B WX – Datalink: FIS-B
The transponder is unable to receive FIS-B
Weather has failed.
weather information.
XPDR1 OVER TEMP - Transponder:
The system has detected an over
Transponder over temp.
temperature condition in XPDR1. The
transmitter operates at reduced power. If
the problem persists, the system should be
serviced.
XPDR1 PRES ALT –Transponder:
Unable to provide pressure altitude
ADS-B no pressure altitude.
information.
XPDR1 SRVC – XPDR1 needs service. The #1 transponder should be serviced
Return unit for repair.
when possible.
110
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Annunciations & Alerts
Comments
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.
The MFD and PFD are not communicating
with each other. The system should be
serviced.
EIS
Nav/Com/
XPDR/Audio
XTALK ERROR – A flight display
crosstalk error has occurred.
Flight
Instruments
Message
XPDR1 UNDER TEMP - Transponder:
Transponder under temp.
GPS Nav
FLIGHT PLAN IMPORT/EXPORT MESSAGES
Annun/Alerts
Appendix
Index
111
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Additional
Features
190-02131-00 Rev. C
Hazard
Avoidance
Description
A flight plan file stored on the SD card was
successfully imported as a stored flight
plan.
‘File contained user waypoints only.
The file stored on the SD card did not
User waypoints imported successfully.
contain a flight plan, only user waypoints.
No stored flight plan data was modified.’ 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.
‘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.
‘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.
Procedures
Flight Plan Import/Export Results
‘Flight plan successfully imported.’
Flight
Planning
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export Results
Description
‘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 The flight plan on the SD card contains one
locked.’
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
The flight plan file on the SD card contains
loaded.’
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.
‘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.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
112
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EIS
Map/HSI
Traffic
PFD Opt
ADF/DME
XPDR
Ident
Tmr/Ref
Nearest
Messages
Nav/Com/
XPDR/Audio
GPS Nav
CDI (FMS)
Map/HSI
Traffic
OBS
PFD Opt
ADF/DME
Ident
XPDR
Tmr/Ref
Nearest
Messages
Flight
Planning
Top Level PFD Softkeys
Procedures
Layout
Detail
Rel Ter
Traffic
NEXRAD
METAR
Lightning
Messages
Select the BACK or OFF Softkey
to return to the top-level softkeys.
Detail 2
LTNG Off
Datalink
Additional
Features
Detail 1
Map Off
Inset Map
HSI Map
Wx LGND
Traffic
Abnormal
Operation
Inset Map/HSI Softkeys
Level 2
Level 3
Adds Inset Map
HSI Map
Places Map in the HSI
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index
Inset Map
Layout
Appendix
Map Off
Displays Inset Map in PFD lower
left corner
Displays second-level softkeys for
additional Inset Map configuration
Removes Inset Map
Map/HSI
190-02131-00 Rev. C
Description
Annun/Alerts
Level 1
Hazard
Avoidance
Detail 3
Back
113
Level 1
Level 2
EIS
Flight
Instruments
Appendix
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
Detail (3)
Traffic
Hazard
Avoidance
Topo
Additional
Features
Rel Ter
Abnormal
Operation
NEXRAD
Lightning
Traffic
Description
Traffic
Traffic Displayed on inset map
Wx LGND
Displays icon and age on the Inset
Map for the selected weather products (optional)
Selects desired amount of map
detail; cycles through declutter
levels:
Detail All (No Declutter): All
map features visible
Detail-1: Declutters land data
Detail-2: Declutters land and
SUA data
Detail-3: Removes everything
except the active flight plan
Traffic information is displayed on
inset map
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes)
and elevation scale on Inset Map
Displays terrain information on
Inset Map
Displays NEXRAD weather and
coverage information on Inset Map
(optional feature)
Displays METAR flags on airport
symbols shown on the Inset Map
(optional)
Displays Sirius XM lightning information on Inset Map (optional
feature)
Toggle inset Traffic Map off/on
Index
Appendix
Annun/Alerts
METAR
Level 3
114
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
PFD Opt
Traffic
Traffic
OBS
ADF/DME
Bearing 2
Bearing 1
SVT
Ident
XPDR
Tmr/Ref
ALT Units
STD Baro
Nearest
Messages
Back
Messages
Flight
Instruments
Map/HSI
EIS
Bearing 1
(NAV2)
Bearing 2
(NAV2)
Bearing 1
(FMS)
Bearing 2
(FMS)
Bearing 1
(ADF)
Bearing 2
(ADF)
Bearing 1
(OFF)
Bearing 2
(OFF)
Meters
Select the BACK Softkey
to return to the top-level softkeys
GPS Nav
Bearing 2
(NAV1)
Nav/Com/
XPDR/Audio
Bearing 1
(NAV1)
IN
HPA
Messages
Back
Messages
Back
Messages
Flight
Planning
Back
Off
Terrain
Option 2
HDG LBL
APT Sign
Option 3
Procedures
Pathways
Option 1
Level 1
Level 2
Level 3
HDG LBL
Displays compass heading along the
Zero-Pitch line
Annun/Alerts
Terrain
Abnormal
Operation
Pathways
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes
representing the horizontal and
vertical flight path of the active flight
plan
Enables synthetic terrain depiction
Appendix
SVT
Description
Additional
Features
PFD Opt
Hazard
Avoidance
PFD Configuration Softkeys
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
115
Level 1
Level 2
Level 3
Description
APT Signs
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.
Displays softkeys to select wind data
parameters
Information not displayed
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
GPS Nav
Wind
OFF
Flight
Planning
Option 1
Option 2
Procedures
Option 3
Additional
Features
Hazard
Avoidance
DME
Abnormal
Operation
Bearing 1
Annun/Alerts
Bearing 2
Appendix
ALT Unit
Index
Meters
IN
116
Wind direction arrows with
headwind and crosswind
components
Wind direction arrow and speed
Wind direction arrow with
headwind/tailwind and crosswind
components
Press to display the DME
information window
Cycles the Bearing 1 Information
Window through NAV1/2, ADF, and
FMS/waypoint identifier and FMSderived distance information.
Cycles the Bearing 1 Information
Window through NAV2/1, ADF, and
FMS/waypoint identifier and FMSderived distance information.
Displays softkeys for setting the
altimeter and BARO settings to
metric units
When enabled, displays altimeter in
meters
Press to display the BARO setting as
inches of mercury
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
Level 2
Level 3
Description
STD Baro
ADF/DME
Map/HSI
Traffic
PFD Opt
OBS
ADF/DME
Ident
XPDR
Tmr/Ref
Nearest
GPS Nav
Toggles the HSI source through NAV
1/2 and FMS
Allows the tuning of the ADF
CDI
Nav/Com/
XPDR/Audio
OBS
EIS
Press to display the BARO setting as
hectopacals
Sets barometric pressure to 29.92 in
Hg (1013 hPa)
Turns the OBS Mode on/off
HPA
Flight
Instruments
Level 1
Messages
Flight
Planning
On
Code
Ident
Back
Messages
Back
Messages
Additional
Features
Select the BACK Softkey to return
to the top-level softkeys.
Transponder Softkeys
Level 1
Level 2
Level 3
Description
Standby
Annun/Alerts
On
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Abnormal
Operation
Displays transponder mode selection softkeys
XPDR
Hazard
Avoidance
Ident
Procedures
Select the BACK Softkey to return
to the top-level softkeys.
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
117
Level 1
Level 2
Level 3
Description
Selects Altitude Mode (selection is usually
automatic)
ALT
EIS
Flight
Instruments
Appendix
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
White (On-Ground) - Transponder does
not allow Mode A and Mode C replies, but
it does permit acquisition and extended
squitters including ADS-B out, and
replies to discretely addressed Mode S
interrogations.
VFR
Hazard
Avoidance
Code
Additional
Features
BKSP
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Removes numbers entered, one at a time
Tmr/Ref
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
Nearest
Displays Nearest Airports Window
Messages
Displays Message Window
Ident
Index
Appendix
Annun/Alerts
Ident
Abnormal
Operation
0—7
Green (Airborne) - Transponder generates
Mode A, Mode C, and Mode S replies to
interrogations, as well as transmissions
of acquisition and extended squitters
including ADS-B out.
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
118
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
Empty WT
EIS
Press the ENGINE Softkey to return
to the previous softkey level.
Tabs
DEC Fuel
INC Fuel
RST Fuel
CO RST
Nav/Com/
XPDR/Audio
Engine
Flight
Instruments
Engine
GPS Nav
Level 1
Level 2
Empty Wt
Allows you to enter
the Weight Planning
information
Appendix
Co RST
Annun/Alerts
RST Fuel
Abnormal
Operation
INC Fuel
Displays the default engine
softkey level. Press again
to return to the previous
softkey level
Resets fuel on board display
to quantities equating to
the filler neck tabs
Press to decrease fuel
quantity in 1-gallon
increments
Press to increase fuel
quantity in 1-gallon
increments
Resets remaining fuel to
zero
Resets CO counter
Additional
Features
DEC Fuel
Description
Hazard
Avoidance
Tabs
Level 4
Procedures
Engine
Level 3
Flight
Planning
MFD Softkeys at Start Up
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
119
Flight
Instruments
Appendix
LOADING UPDATED DATABASES
CAUTION: Never disconnect power to the system when loading a
Nav/Com/
XPDR/Audio
EIS
database. Power interruption during the database loading process
could result in maintenance being required to reboot the system.
NOTE: When loading database updates, the ‘DB Mismatch’ system
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
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.
All databases are updated through a single multimedia 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.
When in standby, databases are not immediately available for use, but stored
to be activated at a later time.
Databases may be loaded through Garmin Pilot and Flight Stream 510.
When loading databases through Garmin Pilot and the Flight Stream 510,
the Flight Stream 510 must be enabled on the system and inserted in the
bottom slot of the MFD.
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.
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.
120
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
Flight
Instruments
Activating Standby Databases
Manually Activating Standby Databases:
Turn the small FMS Knob and select the Databases page.
3)
Press the FMS Knob to select the first database title on the screen.
4)
Turn the small FMS Knob as necessary to select the database title.
5)
Press the ENT Key. A cyan double-sided arrow will appear indicating
that the standby database will become active. Repeat this step for the
remaining databases.
6)
Remove and reapply power to the system.
GPS Nav
2)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob and select the Aux page group on the MFD.
EIS
1)
Flight
Planning
Automatically Activating Standby Databases:
2)
Turn the small FMS Knob and select the Databases page.
3)
Press the Restart softkey. A 10 second restart countdown will appear.
4)
Press the Restart softkey again to continue with a restart of the system.
5)
Press the ENT Key to close the screen.
Hazard
Avoidance
Turn the large FMS Knob and select the Aux page group on the MFD.
Procedures
1)
Additional
Features
Basemap, SafeTaxi, Obstacle, Airport Directory,
IFR/VFR Charts, and FliteCharts or ChartView Databases
With the system OFF, remove an SD Card from the bottom SD card slot of the
MFD.
2)
Download and install the databases 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.
121
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Appendix
190-02131-00 Rev. C
Annun/Alerts
1)
Abnormal
Operation
Updating Databases:
Appendix
EIS
Flight
Instruments
8)
Nav/Com/
XPDR/Audio
9)
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 colums to show
which Standby databases will be transferred to Active at the next power
cycle.
Verify the correct database cycle information is shown in the Standby
Database column.
NOTE: The Restart Softkey is enabled only when the aircraft is on the
GPS Nav
ground.
10) Press the Restart Softkey. A 10 second restart countdown will appear.
Flight
Planning
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.
Procedures
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.
Hazard
Avoidance
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.
Abnormal
Operation
Additional
Features
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.
17) To manually activate any databases that did not transfer to the active
column:
Annun/Alerts
a) Press the FMS Knob. The first database title on the screen will be
selected.
b) Turn the small FMS Knob as necessary to select the database title.
Appendix
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.
Index
e) Verify that the standby databases transferred and are now in the active
database column.
18) Remove power from the system.
122
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
Abnormal
Operation
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Additional
Features
190-02131-00 Rev. C
Hazard
Avoidance
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 .
Procedures
9)
Flight
Planning
ground.
GPS Nav
NOTE: The Restart Softkey is enabled only when the aircraft is on the
Nav/Com/
XPDR/Audio
Updating Databases using Flight Stream 510:
1) Insert the Flight Stream 510 Multimedia Card in the bottom slot of the
MFD.
2) Press the Update softkey when the Database Update screen appears.
3) The Flight Stream 510 will enter WI-FI mode. The following screen will
appear.
4) 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.
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.
EIS
In order to load databases through Garmin Pilot and the Flight Stream 510, the Flight
Stream 510 must be enabled on the system and inserted in the bottom slot of the MFD.
The PED with Garmin Pilot must be paired with the Flight Stream 510 over Bluetooth
(refer to the Additional Features section). When there is at least one paired device
available to connect, the Flight Stream 510 will automatically connect to the system’s
preferred mobile device. The preferred device can be selected on the Aux – Databases
page from a menu list of paired devices.
Once a connection to the paired mobile device is made, Garmin Pilot makes available databases that can be transferred to the Flight Stream
510.
If any of these databases is more recent than the respective
standby database on the system, (or if there is no standby database on the system)
those databases will be automatically selected to load.
Flight
Instruments
Flight Stream 510
123
Appendix
Flight
Instruments
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.
EIS
12) Verify that the standby databases transferred and are now in the active
database column.
GPS Nav
Nav/Com/
XPDR/Audio
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.
14) To manually activate any databases that did not transfer to the active
column:
Flight
Planning
a) Press the FMS Knob. The first database title on the screen will be
selected.
b) Turn the small FMS Knob as necessary to select the database title.
Procedures
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.
Hazard
Avoidance
e) Verify that the standby databases transferred and are now in the active
database column.
15) Remove power from the system.
Additional
Features
Updating Databases from the Aux - Databases page:
1)
With the system OFF, insert the Flight Stream 510 Multimedia Card in the
Index
Appendix
Annun/Alerts
Abnormal
Operation
bottom slot of the MFD.
124
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.
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).
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Appendix
The Database Update status will appear in the Status window at the top of
the page.
ground.
Nav/Com/
XPDR/Audio
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 .
EIS
NOTE: The Restart Softkey is enabled only when the aircraft is on the
Flight
Instruments
9)
GPS Nav
11) After restarting the system, turn the large FMS Knob and select the Aux
page group on the MFD.
12) Turn the small FMS Knob and select the Databases page.
Flight
Planning
13) Verify that the standby databases transferred and are now in the active
database column.
Hazard
Avoidance
15) To manually activate any databases that did not transfer to the active
column:
Procedures
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.
b) Turn the small FMS Knob as necessary to select the database title.
d) Remove and reapply power to the system.
16) Remove power from the system.
Annun/Alerts
e) Verify that the standby databases transferred and are now in the active
database column.
Abnormal
Operation
c) Press the ENT Key. A cyan double-sided arrow will appear indicating
that the standby database will become active.
Additional
Features
a) Press the FMS Knob. The first database title on the screen will be
selected.
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
125
Magnetic Field Variation Database Update
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.
Loading the magnetic field variation database update:
1) With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed.
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
126
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Index
E
Index
Index-1
Appendix
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Annun/Alerts
Flight path marker 65
Flight Plan
Activate a Flight Plan Leg 20
Activate a Stored Flight Plan 20
Creating an Active Flight Plan 30
Edit a Stored Flight Plan 37
Invert and Activate a Stored Flight
Plan 39
Store a Flight Plan 37
Flight plan import/export messages 111
Flight Stream 76
FliteCharts® 66, 67
Abnormal
Operation
F
Additional
Features
Edit a flight plan 37
Enable Terrain 62
Endurance, calculated (ENDUR) 8, 10
Engine manifold pressure 5, 7
Export a Flight Plan 40
Hazard
Avoidance
190-02131-00 Rev. C
Procedures
Caution alerts 85
CDI 2, 16
Channel Presets 70
ChartView 66, 67
Clearance player 17
Clearance recorder 17
Closest Point 34
Flight
Planning
C
Data Link Receiver 90
DB Mismatch 120
DC bus 8
DCLTR Softkey 66
Dead Reckoning 80
DEC FUEL softkey 10
Declutter 80, 114
Designated altitudes 21, 22
Direct-to 19
DME 15, 16
DR mode 80, 81, 82
GPS Nav
Barometric Altitude Minimums 3
Barometric pressure 117
Battery
Current 8
Bluetooth 76, 77
D
Nav/Com/
XPDR/Audio
B
EIS
Activate a Flight Plan Leg 20
Active Channel 69
AC-U-KWIK 69
ADF 15, 16
AHRS 83, 92, 98, 100
Airport Directory 69
Airport Signs 65, 66
Airway
Collapse/Expand Airways 34
Load Airway 34
Along Track Offset 33
ALT 58
Altimeter setting 1, 80
Altitude mode 58
Altitude volume 58
Ammeter 8
AOPA 69
AOPA’s Airport Directory 69
Approach channel 43
Audio panel controls
NAV1, NAV2 16
Code selection softkeys 15
COM 16, 79
Crew Alerting System (CAS) 13–19
Cylinder Head Temperature (CHT) 9, 10
Flight
Instruments
A
G
H
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Nav/Com/
XPDR/Audio
Frequency Transfer 16
Fuel
Calculations 10
Display 12
Reserve 11
Fuel Range Ring 11
GPS Nav
EIS
Flight
Instruments
Index
Garmin Pilot 76, 77
Horizon heading 65
I
Import a Flight Plan 31
Inhibit 62, 64
Inhibit TAWS 64
Inhibit Terrain 62
Insertion Point Indicator 34
Inset Map 113, 114
IOI 86, 88
O
OBS 2
Obstacles 95, 100
Oil, engine
Pressure 12
Temperature 12
P
Pairing 76
Parallel Track 33
Pathways 65, 66
Procedures
Load an Arrival Procedure 41
Load and Activate a Departure Procedure 41
Load and/or Activate an Approach
Procedure 42
R
J
Reserve fuel 11
Reversionary mode 79
ROC 86, 88
Jeppesen 67
S
M
SafeTaxi® 66
SBAS 42, 62, 64, 81
Scheduler 71
SD Card 75, 76
SiriusXM lightning 114
SiriusXM Weather 48
Standby Navigation Database 122
Store Flight Plan 37
SVT 65, 108
Synthetic Vision System 65
Map panning 49
METAR 48
Missed Approach 44
MKR/MUTE 17
Mode selection softkeys 15
N
NAV 16
NAV1 2, 16
NAV2 2, 16
Navigation database 21
NEXRAD 48, 114
Index-2
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
190-02131-00 Rev. C
Index
Flight
Instruments
T
EIS
Tachometer 6, 7
TAF 48
TAS 58, 59, 92
TAWS 62, 63, 64, 88
Temperature Compensated Altitude 45
Terrain 59, 61, 62, 96, 114
Terrain-SVS 61, 62
Timer 3
Topographical data 114
Traffic 47
Traffic map page 58, 59, 60
Transponder 15, 117, 118
Trip Planning 23
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
U
User-Defined Hold 35
User Waypoint 25–30
Hazard
Avoidance
V
Additional
Features
Vector to Final 44
Vertical Navigation (VNAV)
Guidance 22
VNV 19, 80
Voice alerts 85
Abnormal
Operation
W
Annun/Alerts
WAAS 100
Warning alerts 85
Waypoint Selection Submenu 30, 31
Weight Planning Page 23
Wind data 116
WIND Softkey 56
Appendix
Index
190-02131-00 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-28-181 Archer
Index-3
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
© 2016 Garmin Ltd. or its subsidiaries
190-02131-00 Rev. C
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