Garmin | G1000: Beechcraft King Air 200/B200 | Garmin G1000: Beechcraft King Air 200/B200 G1000 Cockpit Reference Guide for KingAir 200/B200 Series - SSV 0985.08

Garmin G1000: Beechcraft King Air 200/B200 G1000 Cockpit Reference Guide for KingAir 200/B200 Series - SSV 0985.08
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Beechcraft 200/B200 Series
FLIGHT INSTRUMENTS
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2011, 2013, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.08 or later for the
Beechcraft 200 and B200. Some differences in operation may be observed when comparing
the information in this manual to earlier or later software versions.
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“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
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consequential damages that result from the use or inability to use the software or related
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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.
March, 2016
190-00929-05 Rev. B
Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (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: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
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.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Warnings, Cautions & Notes
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be significantly older than the indicated weather
product age.
WARNING: Do not rely on information from the 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 the documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: The Garmin G1000 system, as installed in this aircraft, has a very
high degree of functional integrity. However, the pilot must recognize that
providing monitoring and/or self-test capability for all conceivable system
failures is not practical. Although unlikely, it may be possible for erroneous
operation to occur without a fault indication shown by the G1000. It is
thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the
cockpit.
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Warnings, Cautions & Notes
WARNING: 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 Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
G1000 Integrated Avionics System in the Airplane Flight Manual. Thoroughly
practice basic operation prior to actual use. During flight operations, carefully
compare indications from the G1000 to all available navigation sources,
including the information from other NAVAIDs, visual sightings, charts, etc.
For safety purposes, always resolve any discrepancies before continuing
navigation.
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
WARNING: Do not use the system to attempt to penetrate a thunderstorm.
The illustrations in this guide are only examples. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding any thunderstorm identified as severe of giving
intense radar echo by at least 20 miles.
WARNING: Because of variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications (GRS 77 installations only). North of 72° North latitude
at all longitudes. South of 70° South latitude at all longitudes. North of 65°
North latitude between longitude 75° W and 120° W. (Northern Canada).
North of 70° North latitude between longitude 70° W and 128° W. (Northern
Canada). North of 70° North latitude between longitude 85° E and 114° E.
(Northern Russia). South of 55° South latitude between longitude 120° E
and 165° E. (Region south of Australia and New Zealand).
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Warnings, Cautions & Notes
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: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
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: 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Warnings, Cautions & Notes
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: When operating the G1000 in DG Free Mode (GRS 7800 installations
only), the heading information used by some system components (e.g. GTS
8000, AFCS, and GWX) will be different from the heading displayed on the
GDU by an amount equal to the difference between the current Magnetic
Field Variation Database (MV DB) value, and the MV DB value when DG Free
Mode was activated. Due to the convergence of isogonic lines, this condition
is most noticeable at or near the North and South poles.
NOTE: System navigation utilities may not reliably calculate range and
bearing information when the aircraft is operating north of 80° North latitude
or south of 80° South latitude. This may result in the system displaying small
gaps in racetrack holding pattern depictions (GRS 7800 installations only).
NOTE: The Terrain Awareness and Warning System (TAWS) may not operate
reliably north of 89º North latitude and south of 89º South latitude. This is
due to limitations present within the Terrain database and the system’s ability
to process the data representing the affected areas (GRS 7800 installations
only).
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 G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Pilot’s Guide for this aircraft.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Warnings, Cautions & Notes
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.’
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 ‘Report An Aviation Data
Error Report.’
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Record of Revisions
Part Number
190-00929-00
190-00929-01
190-00929-02
190-00929-03
190-00929-04
190-00929-05 Rev. B
Change Summary
Initial release
Added Synthetic Vision System
Added TAWS-A
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Added other GDU 10.00 parameters
Added GDU 11.12 changes
Added GTS 820/850
Added Electronic Stabilization & Protection
Iridium Telephone and Data Link
Added Worldwide Weather
Added other GDU 12.01 parameters
Added METAR and WX LGND softkeys
Updated XM weather product symbols
Updated Iridium registration procedure
Updated SiriusXM product references
Added GDU 13.06 parameters
Added GRS 7800, GTS 8000, GTX 3000, GRA 5500
Added Pilot Profiles
Added Temperature Compensated Altitude
Added User-defined Holds
Added TCAS II
Removed Reports Page
Added DG Mode
Changed GFDS to Connext
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
RR-1
Record of Revisions
Part Number
190-00929-05
Rev. A
Change Summary
Updated Softkey Map
Added GDU 13.31 parameters
Updated Support for SiriusXM Weather Service
Updated Warnings, Cautions, and Notes
Updated System Messages
Revision Date of Revision Affected Pages
B
March, 2016
All
RR-2
Description
Clerical
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
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
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Synchronize CDI......................................................................................................................... 1
Selecting DG Mode (GRS 7800 Installations Only):............................................................ 2
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 3
Configure Vspeed Bugs Individually...................................................................................... 3
Turn Vspeed Bugs On or Off by Category............................................................................. 3
Set Barometric/Radar Altimeter Minimum Descent Altitude.......................................... 4
Testing the Radar Altimeter.................................................................................................... 4
Displaying Wind Data............................................................................................................... 4
NAV/COM/TRANSPONDER/AUDIO PANEL.......................................................................... 5
ADF Tuning (Optional)............................................................................................................... 5
DME Tuning................................................................................................................................. 5
Enter a Transponder Code....................................................................................................... 5
Selecting a COM Radio............................................................................................................. 5
Selecting a NAV Radio.............................................................................................................. 6
NAV/COM Tuning........................................................................................................................ 6
Intercom....................................................................................................................................... 6
Passenger Address (PA) System.............................................................................................. 7
Clearance Recorder and Player.............................................................................................. 7
AUTOMATIC FLIGHT CONTROL SYSTEM............................................................................. 9
Flight Director Activation........................................................................................................ 9
Vertical Modes.......................................................................................................................... 10
Lateral Modes........................................................................................................................... 11
Suspected Autopilot Malfunction........................................................................................ 12
Overpowering Autopilot Servos.......................................................................................... 12
GPS NAVIGATION......................................................................................................................... 13
Direct-to Navigation............................................................................................................... 13
Activate a Stored Flight Plan................................................................................................ 14
Activate a Flight Plan Leg...................................................................................................... 14
Stop Navigating a Flight Plan............................................................................................... 15
Vertical Navigation (VNAV)................................................................................................... 15
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
i
Table of Contents
FLIGHT PLANNING....................................................................................................................... 19
Weight Planning....................................................................................................................... 19
Trip Planning............................................................................................................................. 19
Create a User Waypoint Defined by Latitude & Longitude............................................ 21
Create a User Waypoint Defined by Radials from Other Waypoints............................ 22
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 24
Delete a User Waypoint.......................................................................................................... 25
Create a Flight Plan................................................................................................................. 26
Import a Flight Plan from an SD Card................................................................................. 27
Insert a Waypoint in the Active Flight Plan....................................................................... 27
Enter an Airway in a Flight Plan........................................................................................... 28
User-Defined Holding Patterns............................................................................................. 29
Invert An Active Flight Plan................................................................................................... 31
Remove a Departure, Arrival, Appr, or Airway from a Flight Plan............................... 31
Store a Flight Plan................................................................................................................... 32
Edit a Stored Flight Plan........................................................................................................ 32
Delete a Waypoint from the Flight Plan............................................................................. 32
Invert and Activate a Stored Flight Plan............................................................................ 33
Copy a Flight Plan.................................................................................................................... 33
Delete a Flight Plan................................................................................................................. 33
Graphical Flight Plan Creation.............................................................................................. 34
Export a Flight Plan to an SD Card...................................................................................... 34
PROCEDURES.................................................................................................................................. 35
Load and Activate a Departure Procedure........................................................................ 35
Activate A Departure Leg...................................................................................................... 35
Load An Arrival Procedure..................................................................................................... 35
Activate An Arrival Leg.......................................................................................................... 36
Load and/or Activate an Approach Procedure.................................................................. 36
Activate An Approach in the Active Flight Plan................................................................ 37
Activate a Vector to Final Approach Fix............................................................................. 37
Activate A Missed Approach in the Active Flight Plan.................................................... 38
Temperature Compensated Altitude................................................................................... 38
HAZARD AVOIDANCE................................................................................................................. 41
Customizing the Hazard Displays on the Navigation Map............................................. 41
STORMSCOPE® (Optional)...................................................................................................... 41
SiriusXM Satellite Weather (Optional)................................................................................ 43
Connext Weather (Optional)................................................................................................. 46
Airborne Color Weather Radar............................................................................................. 58
Traffic Avoidance Systems..................................................................................................... 61
Traffic Collision Avoidance System (TCAS II) (Optional)................................................. 63
Terrain Awareness & Warning System................................................................................ 65
ii
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Table of Contents
ADDITIONAL FEATURES............................................................................................................ 69
Synthetic Vision........................................................................................................................ 69
Terminal Procedure Charts.................................................................................................... 70
Airport Directory..................................................................................................................... 72
Satellite Telephone and Data Link Services...................................................................... 73
WI-FI Connections.................................................................................................................... 86
SiriusXM™ Radio Entertainment........................................................................................... 89
Pilot Profiles............................................................................................................................. 91
Electronic Stability & Protection (ESP™)........................................................................... 94
ANNUNCIATIONS & ALERTS.................................................................................................... 97
WARNING Annunciation......................................................................................................... 97
Advisory Annunciations......................................................................................................... 97
Message Advisory Alerts........................................................................................................ 97
Comparator Annunciations.................................................................................................... 98
Reversionary Sensor Annunciations.................................................................................... 98
AFCS Alerts................................................................................................................................ 99
TAWS-A Alerts......................................................................................................................... 100
TAWS-B Alerts......................................................................................................................... 103
Additional Voice Alerts......................................................................................................... 106
System Message Advisories................................................................................................ 107
Flight Plan Import/Export Messages................................................................................. 134
Pilot Profile Import/Export Messages............................................................................... 135
APPENDIX...................................................................................................................................... 137
PFD Softkey Map................................................................................................................... 137
MFD Navigation Page Softkey Map.................................................................................. 148
Loading Updated Databases............................................................................................... 150
INDEX..........................................................................................................................................Index-1
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
iii
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Nav/Com/
XPDR/Audio
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
AFCS
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Flight
Planning
1)
GPS Nav
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
Procedures
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
4)
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION
Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
Annun/Alerts
Select the AUX-SYSTEM SETUP Page on the MFD.
Additional
Features
1)
SYNCHRONIZE CDI
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Select the AUX-SYSTEM SETUP Page on the MFD.
Appendix
1)
1
SELECTING DG MODE (GRS 7800 INSTALLATIONS ONLY):
NOTE: When operating the G1000 in DG Free Mode (GRS 7800 installations
only), the heading information used by some system components (e.g. GTS
8000, AFCS, and GWX) will be different from the heading displayed on the
GDU by an amount equal to the difference between the current Magnetic
Field Variation Database (MV DB) value, and the MV DB value when DG Free
Mode was activated. Due to the convergence of isogonic lines, this condition
is most noticeable at or near the North and South poles.
1)
Press the PFD Softkey.
2)
Press the HDG MODE Softkey.
3)
Press the DG FREE Softkey to activate DG mode. Press the DG SLAVE
Softkey to deactivate DG mode.
Pressing the HDG- or HDG+ softkey to slew the heading
counterclockwise or clockwise.
•
Pressing the HDG SYNC softkey to synchronize the heading to the
current selected heading.
•
Pressing the TRACK SYNC softkey to synchronize the heading to the
current track.
Annun/Alerts
1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes
the NAV1 standby frequency in the upper left corner of the PFD to light
blue, indicating this is the frequency selected for tuning.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or
LOC2. This changes the NAV2 standby frequency in the upper left corner of
the PFD to light blue, indicating this is the frequency selected for tuning.
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 a
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
•
CHANGE NAVIGATION SOURCES
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Instruments
2)
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.
AFCS
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.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
GENERIC TIMER
GPS Nav
CONFIGURE VSPEED BUGS INDIVIDUALLY
Flight
Planning
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Hazard
Avoidance
4)
Procedures
speed has been changed from a default value, an asterisk appears next to
the speed).
Press the TMR/REF Softkey.
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.
Annun/Alerts
1)
Additional
Features
TURN VSPEED BUGS ON OR OFF BY CATEGORY
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
3
SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE
1) Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select BARO, TEMP COMP, or RAD ALT. OFF
is selected by default. Press the ENT Key or turn the large FMS Knob to
highlight the next field.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet for BARO, or from zero to 2,500 for RAD ALT).
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS
Knob to highlight the next field and then enter the destination airport
temperature (-59˚C to 59˚C). The temperature compensated altitude
minimum is displayed below the previously enter minimum altitude value.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
TESTING THE RADAR ALTIMETER
1)
Select the AUX-SYSTEM STATUS Page on the MFD.
2)
Select the RA TEST Softkey. ‘RA TEST’ is displayed to the left of the Radar
Altitude window. The Radar Altitude window displays 50 feet, indicating a
properly functioning system.
3)
Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.
DISPLAYING WIND DATA
1)
Press the PFD 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
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
Nav/Com/
XPDR/Audio
ADF TUNING (OPTIONAL)
Tune the ADF using the remote ADF control head.
DME TUNING
2)
Turn the large FMS 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.
GPS Nav
Press the DME Softkey.
AFCS
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the XPDR1 or XPDR2 Softkey to select the active transponder.
3)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
4)
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.
Procedures
1)
Flight
Planning
ENTER A TRANSPONDER CODE
Hazard
Avoidance
Additional
Features
SELECTING A COM RADIO
Annun/Alerts
Transmit/Receive
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
Appendix
Receive Only
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
5
SELECTING A NAV RADIO
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.
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
Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.
The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.
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.
During manual squelch operation, pressing the ICS Knob switches between volume
and squelch adjustment, lighting the associated annunciator beneath the knob. When
the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When
the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
1)
GPS Nav
NAV/COM TUNING
Flight
Planning
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Nav/Com/XPDR/Audio Panel
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
PA Key is enabled on both audio panels. PA messages are one way from the flight deck
to the passengers.
Flight
Instruments
PASSENGER ADDRESS (PA) SYSTEM
CLEARANCE RECORDER AND PLAYER
AFCS
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
of recording time have been reached, the recorder begins recording over the stored
memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicate when play is in progress. The PLAY annunciator extinguishes after playback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
block, play is halted.
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
GPS Nav
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
7
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
AFCS
AFCS
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
Nav/Com/
XPDR/Audio
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT DIRECTOR ACTIVATION
Modes Selected
Lateral
Vertical
AP Key
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
CWS Button
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
GA Switch
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on ground)
Go Around (in air)
TO
GA
ALT Key
Roll Hold (default)
ROL
Altitude Hold
ALT
VS Key
Roll Hold (default)
ROL
Vertical Speed
VS
VNV Key
Roll Hold (default)
ROL
Vertical Path Tracking*
VPTH
NAV Key
Navigation**
GPS
VOR
LOC
Pitch Hold (default)
PIT
BC Key
Backcourse***
BC
Pitch Hold (default)
PIT
APR Key
Approach**
GPS
VAPP
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT
GP
GS
HDG Key
Heading Select
HDG
Pitch Hold (default)
PIT
Appendix
PIT
Annun/Alerts
Pitch Hold (default)
Additional
Features
ROL
Hazard
Avoidance
Roll Hold (default)
Procedures
FD Key
Flight
Planning
Control Pressed
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
Index
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV or APR Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
190-00929-05 Rev. B
GPS Nav
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
9
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
AFCS
VERTICAL MODES
Vertical Mode
Description
Control
Annunciation
Pitch Hold
Holds the current aircraft pitch attitude; may
be used to climb/descend to the Selected
Altitude
(default)
PIT
Selected Altitude
Armed
AFCS armed to capture the altitude displayed in
the Selected Altitude window
*
ALTS
Altitude Hold
Holds the current Altitude Reference
ALT Key
ALT
nnnnn ft
Vertical Speed
Maintains the current aircraft vertical speed;
may be used to climb/descend to the Selected
Altitude
VS Key
VS
nnnn fpm
FLC
nnn kt
FLC
M .nnn
Flight Level Change, Maintains the current aircraft airspeed (in
IAS or Mach) while the aircraft is climbing/
IAS Hold
descending to the Selected Altitude. Press
Flight Level Change, the SPD Key to switch between IAS and
Mach Hold
MACH.
FLC Key
VNAV
Captures and tracks the VNAV flight path
VNV Key
VPTH
VNAV Target
Altitude Armed
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window
**
ALTV
Glidepath
Captures and tracks the SBAS glidepath on
approach
Glideslope
Captures and tracks the ILS glideslope on
approach
Takeoff (on ground)
Disengages the autopilot and commands a
constant pitch angle and wings level in the
air on the ground in preparation for takeoff
Go Around (in air)
Disengages the autopilot and commands a
constant pitch attitude and wings level in
the air
Level
Commands 0° pitch attitude
GP
APR Key
GS
TO
GA
Switch
GA
Activated
only by
the ESP
function
LVL
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be
captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude
10
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
AFCS
Lateral Mode
Description
Control
Annunciation
(default)
ROL
Low Bank
Limits maximum commanded roll
angle
BANK
Key
*
Heading Select
Captures and tracks Selected
Heading
HDG Key
HDG
Navigation, GPS Arm/
Capture/Track
NAV Key
LOC
Captures and tracks a localizer
signal for backcourse approaches
BC Key
Approach, GPS Arm/Capture/
Track
LOC
Commands wings level attitude
GA
Switch
GA
LVL
Index
Activated
only by
the ESP
function
Appendix
Disengages autopilot and
commands a constant pitch angle
and wings level in the air
TO
Annun/Alerts
Disengages autopilot and commands
a constant pitch angle and wings
level in preparation for takeoff
Additional
Features
Level
Hazard
Avoidance
VAPP
APR Key
Track
(Glideslope Mode
automatically armed)
Go Around (in air)
BC
GPS
Approach, VOR Arm/Capture/
Track
Captures and tracks selected
Approach, ILS Arm/Capture/ navigation source (GPS, VOR, LOC)
Takeoff (on ground)
VOR
Procedures
Backcourse Arm/Capture/
Track
Captures and tracks selected
navigation source (GPS, VOR, LOC)
Flight
Planning
Navigation, LOC Arm/
Capture/Track
(No Glideslope)
GPS
GPS Nav
Navigation, VOR Enroute
Arm/Capture/Track
AFCS
Holds current aircraft roll attitude
or rolls wings level, depending on
commanded bank angle
Nav/Com/
XPDR/Audio
Roll Hold
Flight
Instruments
LATERAL MODES
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
11
SUSPECTED AUTOPILOT MALFUNCTION
NOTE: Consult the aircraft documentation for the location of circuit breakers
as well as specifics that may supplement or amplify this procedure.
If an autopilot failure or trim failure is suspected to have occurred, perform the
following steps:
1)
Firmly grasp the control wheel.
2)
Press and hold the AP DISC Switch. The autopilot will disconnect and
power is removed from the trim motor. Power is also removed from all
primary servo motors and engaged solenoids. Note the visual and aural
alerting indicating autopilot disconnect.
3)
Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4)
Pull the appropriate circuit breaker(s) to electrically isolate the servo and
solenoid components.
5)
Release the AP DISC Switch.
OVERPOWERING AUTOPILOT SERVOS
In the context of this discussion, “overpowering” refers to any pressure or force
applied to the pitch controls when the autopilot is engaged. A small amount of
pressure or force on the pitch controls can cause the autopilot automatic trim to run
to an out-of-trim condition. Therefore, any application of pressure or force to the
controls should be avoided when the autopilot is engaged.
Overpowering the autopilot during flight will cause the autopilot’s automatic trim
to run, resulting in an out-of-trim condition or cause the trim to hit the stop if the
action is prolonged. In this case, larger than anticipated control forces are required
after the autopilot is disengaged.
The following steps should be added to the preflight check:
1) Check for proper autopilot operation and ensure the autopilot can be
overpowered.
2) Note the forces required to overpower the autopilot servo clutches.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
AFCS
12
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
1)
3)
5)
7)
9)
11)
Direct-to Navigation from the PFD
2)
3)
5)
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
13
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
1)
Additional
Features
12)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
6)
GPS Nav
4)
) Key on the Control Unit.
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 (-) or after (+) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
2)
Press the Direct-to (
Nav/Com/
XPDR/Audio
Direct-to Navigation from the MFD
Nav/Com/
XPDR/Audio
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’.
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance field.
AFCS
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
13) Turn the small FMS Knob to enter the desired course to the waypoint.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the Control Unit 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)
Select the ACTIVE 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.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
Appendix
Annun/Alerts
ACTIVATE A FLIGHT PLAN LEG
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)
Select 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)
14
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
GPS Navigation
Press the FPL Key on the Control Unit to display the Active Flight Plan Page.
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.
AFCS
VERTICAL NAVIGATION (VNAV)
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
Flight
Planning
NOTE: Temperature Compensated (TEMP COMP) altitudes are depicted as
slanted text.
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.
Procedures
Hazard
Avoidance
Large White
Text
Large Light
Blue Text
Additional
Features
Small Light
Blue Text
Annun/Alerts
Small Light
Blue Subdued
Text
Small White Text
with Altitude
Restriction Bar
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
15
Flight
Instruments
GPS Navigation
Cross AT or ABOVE 5,000 ft
Cross AT or BELOW 3,000 ft
Altitudes associated with arrival and approach procedures are “auto-designated”.
This means the system will automatically use the altitudes loaded with the arrival or
approach for giving vertical flight path guidance outside the FAF. Note that these altitudes will be displayed as small light blue text.
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 flight
path vertical 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.
The system updates vertical path guidance continuously using ground speed and
the calculated distance to the Bottom of Descent (BOD). Due to turn anticipation
guidance (turn-smoothing), distance to the BOD can be affected by course changes
greater than approximately 5 degrees. Ground speed can be affected by factors such as
shifts in wind direction, aircraft power management, pitch angle, and course changes.
Abrupt and/or substantial changes to either the distance to the BOD, ground speed, or
both can cause similarly abrupt/substantial changes in vertical path guidance.
Because of turn-smoothing, changes to both distance to the BOD and ground speed
tend to be more extreme when the BOD is also a waypoint that marks a large course
change. These speed and distance changes will be accounted for in the computed
required vertical path and reflected in the vertical guidance indications.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Cross AT 2,300 ft
16
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
GPS Navigation
Light Blue Text
Light Blue
Subdued Text
Small Text Altitude is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.
Altitude is designated for
use in giving vertical flight
path guidance. Altitude
has been retrieved from
the navigation database
or has been entered by
the pilot and matches a
published altitude in the
navigation database.
The system
cannot use
this altitude in
determining
vertical flight
path guidance.
GPS Nav
The system
cannot use
this altitude in
determining
vertical flight
path guidance.
AFCS
Altitude has been entered
by the pilot. Altitude is
designated for use in
giving vertical flight path
guidance. Altitude does
not match the published
altitude in navigation
database or no published
altitude exists.
Nav/Com/
XPDR/Audio
Large Text Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.
Flight
Instruments
White Text
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
17
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
GPS Navigation
Blank Page
18
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT PLANNING
Nav/Com/
XPDR/Audio
All procedures apply to the MFD and the Control Unit unless otherwise stated.
Entering Weight Parameters
3)
Turn the small FMS Knob to enter the desired fuel quantity.
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.
Additional
Features
Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.
Annun/Alerts
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, select the AUTO or MANUAL
Softkey.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
19
Index
Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page
group.
Appendix
1)
190-00929-05 Rev. B
Hazard
Avoidance
2)
Procedures
Press the FMS Knob to activate the cursor.
Flight
Planning
1)
GPS Nav
Entering Fuel Parameters
AFCS
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) Select 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) Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
Nav/Com/
XPDR/Audio
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
GPS Nav
Or:
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Flight
Planning
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.
Procedures
d) Press the ENT Key to accept the waypoint.
Or:
For flight plan leg planning:
Hazard
Avoidance
a) Select 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.
Additional
Features
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
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’ will display 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
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Index
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.
20
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
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 onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
Hazard
Avoidance
Additional
Features
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
Procedures
12) The flashing cursor moves to the barometric setting (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.
Flight
Planning
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
GPS Nav
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
AFCS
7)
Nav/Com/
XPDR/Audio
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Flight
Instruments
6)
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
190-00929-05 Rev. B
Appendix
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
Annun/Alerts
1)
21
Flight Planning
Flight
Instruments
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
AFCS
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 LAT/LON (latitude and longitude).
9)
Press the ENT Key.
Procedures
Flight
Planning
GPS Nav
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select 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
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Annun/Alerts
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.
Appendix
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:
Index
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.
c) Press the ENT Key.
22
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Flight
Instruments
Or:
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Hazard
Avoidance
c) Turn the large FMS Knob to select the desired waypoint.
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
12) Press the ENT Key.
Additional
Features
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
Appendix
16) Press the FMS Knob to remove the flashing cursor.
Annun/Alerts
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.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
23
Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select 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.
GPS Nav
1)
Nav/Com/
XPDR/Audio
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
AFCS
Flight
Instruments
Flight Planning
Flight
Planning
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Hazard
Avoidance
Procedures
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.
Additional
Features
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:
Annun/Alerts
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.
c) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
24
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Instruments
Or:
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Procedures
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Hazard
Avoidance
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
Additional
Features
DELETE A USER WAYPOINT
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)
Select the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
25
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
Turn the large FMS Knob to select the ‘WPT’ page group.
Annun/Alerts
1)
190-00929-05 Rev. B
Flight
Planning
d) 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.
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
Procedures
Flight
Planning
GPS Nav
AFCS
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. The
active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
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) Select 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) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) 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.
26
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
2)
Press the FPL Key on the Control Unit 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 either FMS Knob to highlight an empty or existing flight plan.
6)
Select the IMPORT Softkey.
AFCS
Insert the SD card containing the flight plan in the top card slot on the
MFD.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
IMPORT A FLIGHT PLAN FROM AN SD CARD
GPS Nav
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
Or:
8)
Press the ENT Key.
Hazard
Avoidance
Turn the small FMS Knob to highlight the desired flight plan for importing.
Procedures
7)
Flight
Planning
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 select the IMPORT Softkey.
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Additional
Features
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint will be 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:
Appendix
Press the FPL Key on the Control Unit to display the active flight plan.
Annun/Alerts
1)
a) Enter the user waypoint identifier, facility, or city.
Index
b) Press the ENT Key.
Or:
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
27
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
ENTER AN AIRWAY IN A FLIGHT PLAN
1)
Press the FPL Key on the Control Unit.
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. 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 select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”(required on
the PFD). 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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
28
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
A holding pattern can be defined at any active flight plan waypoint, or at the aircraft
present position.
Nav/Com/
XPDR/Audio
AFCS
NOTE: System navigation utilities may not reliably calculate range and
bearing information when the aircraft is operating north of 80° North latitude
or south of 80° South latitude. This may result in the system displaying small
gaps in racetrack holding pattern depictions (GRS 7800 installations only).
Flight
Instruments
USER-DEFINED HOLDING PATTERNS
Creating a user-defined hold at an active flight plan waypoint:
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The
HOLD AT window appears with the course field highlighted.
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 ‘DIST’ 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.
Procedures
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the Length mode highlighted.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
29
Index
2)
Appendix
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
(MFD) or the Active Flight Plan Window (PFD).
Annun/Alerts
1)
Additional
Features
Creating a user-defined hold at the aircraft present position:
Hazard
Avoidance
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
190-00929-05 Rev. B
Flight
Planning
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
(MFD) or the Active Flight Plan Window (PFD).
GPS Nav
1)
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
3)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
4)
Use the FMS Knobs to edit the length, and press the ENT Key.
5)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
6)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
7)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate
the hold.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Creating a User-Defined Hold at a Direct-To Waypoint:
1)
Press a Direct-to Key on the Control Unit and set up the Direct To
waypoint as desired, but select ‘HOLD?’ instead of ‘ACTIVATE?’ when
finished.
2)
Use the FMS Knobs to edit the 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 ‘DIST’ 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.
Annun/Alerts
10) Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the Direct To
with the user-defined hold defined at the Direct To waypoint.
Exiting a user-defined hold inserted into the active flight plan:
Index
Appendix
Press the SUSP Softkey. The system will provide guidance to follow the
holding pattern to the inbound course and resume automatic waypoint
sequencing.
30
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
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.
Nav/Com/
XPDR/Audio
1)
Press the MENU Key to display the PAGE MENU with the cursor on the
‘Cancel Direct-To NAV’ selection.
3)
Press the ENT Key. The holding pattern is removed.
Flight
Planning
2)
Procedures
INVERT AN ACTIVE FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
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.
Additional
Features
Press the FPL Key to display the active flight plan.
Hazard
Avoidance
1)
Press the FPL Key on the Control Unit to display the active flight plan. Press
the FMS Knob to activate the cursor.
Appendix
Or:
Annun/Alerts
REMOVE A DEPARTURE, ARRIVAL, APPR, OR AIRWAY FROM A FLIGHT PLAN
1)
GPS Nav
Press a Direct To Key to display the DIRECT TO Window (PFD or MFD).
AFCS
Removing a user-defined hold at an off-route direct-to:
1)
Flight
Instruments
Removing a user-defined hold inserted into the active flight plan:
a) Turn the small FMS Knob to select the Flight Plan Catalog Page.
b) Press the FMS Knob to activate the cursor.
Index
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Select the EDIT Softkey.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
31
Hazard
Avoidance
Procedures
Flight
Planning
Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
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.
1)
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
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.
EDIT A STORED FLIGHT PLAN
1)
Press the FPL Key on the Control Unit 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)
Select the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
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
1)
Annun/Alerts
Additional
Features
2)
STORE A FLIGHT PLAN
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or:
Appendix
a) 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.
Index
d) Select the EDIT Softkey.
2)
32
Turn the large FMS Knob to highlight the waypoint to be deleted.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Flight Planning
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.
AFCS
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Press the FPL Key on the Control Unit.
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)
Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be
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.
GPS Nav
1)
Hazard
Avoidance
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)
Select 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.
Additional
Features
Press the FPL Key on the Control Unit.
Press the FMS Knob to activate the cursor.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
3)
Appendix
Turn the small FMS Knob to select the Flight Plan Catalog Page.
Annun/Alerts
DELETE A FLIGHT PLAN
2)
Procedures
1)
Press the FPL Key on the Control Unit.
Flight
Planning
COPY A FLIGHT PLAN
1)
Nav/Com/
XPDR/Audio
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
Flight
Instruments
3)
33
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Select 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.
1)
Press the FPL Key on the Control Unit to display the Active Flight Plan Page.
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. Turn the large FMS Knob to select the desired insertion point.
4)
Select the LD WPT Softkey. The selected waypoint will be inserted at the
selected point. The default user waypoint naming is USR000, USR001, USR002,
and so on.
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 on the Control Unit 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)
Select the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
GRAPHICAL FLIGHT PLAN CREATION
34
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
Nav/Com/
XPDR/Audio
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 will be active
when the flight plan is active.
Flight
Planning
2)
GPS Nav
Press the PROC Key.
AFCS
1)
Procedures
ACTIVATE A DEPARTURE LEG
Hazard
Avoidance
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the departure.
4)
Select the ACT LEG Softkey. A confirmation window showing the selected
leg will be displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Annun/Alerts
Press the FPL Key to display the active flight plan.
Additional
Features
1)
LOAD AN ARRIVAL PROCEDURE
Appendix
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.
4)
Turn the large FMS Knob to highlight the desired arrival.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
35
Index
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
Procedures
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 is 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.
AFCS
11) The arrival will become part of the active flight plan.
1)
Press the FPL Key on the Control Unit to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the arrival.
4)
Select 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
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
ACTIVATE AN ARRIVAL LEG
Index
Appendix
Annun/Alerts
Additional
Features
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.
36
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Procedures
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, TEMP
COMP or optional RAD ALT.
9)
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.
AFCS
8)
Nav/Com/
XPDR/Audio
Press the ENT Key. The cursor moves to the MINIMUMS field.
Flight
Instruments
7)
GPS Nav
10) Press the ENT Key. If BARO, or OFF was selected 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.
Flight
Planning
11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Procedures
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.
Hazard
Avoidance
13) 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.
Annun/Alerts
Press the PROC Key.
Additional
Features
1)
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.
Appendix
1)
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
37
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
Nav/Com/
XPDR/Audio
Flight
Instruments
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window will be displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Or:
5)
After activating the missed approach procedure, and the CDI has changed
to TERM mode sensitivity, another approach procedure may be loaded.
TEMPERATURE COMPENSATED ALTITUDE
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Press the go-around button.
Additional
Features
Altitudes Displayed Without
Temperature Compensation
Altitudes Displayed With
Temperature Compensation
Appendix
Annun/Alerts
Enabling temperature compensated altitude:
1)
From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Use the small FMS Knob to select the temperature at the <airport>. The
Index
compensated altitude is computed as the temperature is selected.
5)
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
shown in the flight plan.
38
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Procedures
Flight
Instruments
Disabling temperature compensated altitude:
From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
5)
Press the ENT Key. The temperature compensated altitude at the FAF
Nav/Com/
XPDR/Audio
1)
AFCS
is cancelled.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
39
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Procedures
Blank Page
40
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
Flight
Planning
2)
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.
Appendix
Displaying Stormscope Lightning Data on the Navigation Map Page
2)
Select the STRMSCP Softkey. Select the STRMSCP Softkey again to
remove Stormscope Lightning Data from the Navigation Map Page.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Select the MAP Softkey.
Annun/Alerts
WARNING: Do not rely on information from the 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 the documentation from the lightning detection system
manufacturer for detailed information about the system.
Additional
Features
STORMSCOPE® (OPTIONAL)
Hazard
Avoidance
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
Procedures
1)
1)
GPS Nav
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
AFCS
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.
Nav/Com/
XPDR/Audio
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.
41
Hazard Avoidance
Flight
Instruments
Lightning Age
Strike is less than 6 seconds old
Symbol
Nav/Com/
XPDR/Audio
Strike is between 6 and 60 seconds old
AFCS
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Procedures
Flight
Planning
GPS Nav
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
1)
Press the MENU Key (with the Navigation Map Page displayed).
2)
Turn either FMS Knob to highlight ‘Map Setup’.
3)
Press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’.
5)
Press the ENT Key.
6)
Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7)
Turn the small FMS Knob to display the ‘Cell/Strike’ window.
8)
Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
9)
Push the FMS Knob to return to the Navigation Map Page.
Additional
Features
Hazard
Avoidance
Clear Stormscope Lightning Data from the Navigation Map Page
1)
Press the MENU Key (with the Navigation Map Page displayed).
2)
Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
Annun/Alerts
after the execution of each turn. This is to ensure that the strike and/or cell
positions are depicted accurately in relation to the nose of the aircraft.
1)
Turn the large FMS Knob until the Map Page group is selected.
2)
Turn the small FMS Knob select the Stormscope Page.
Index
Appendix
Stormscope Page
42
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Flight
Instruments
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Select the Stormscope Page.
2)
Select the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Select the CELL Softkey to display ‘CELL’ data or select the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.
GPS Nav
Change the Viewing Mode Between 360˚ and 120˚
Select the Stormscope Page.
2)
Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select
the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to
display a 120˚ viewing area.
SIRIUSXM SATELLITE WEATHER (OPTIONAL)
2)
Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.
Additional
Features
Select the MAP Softkey.
Hazard
Avoidance
Displaying SiriusXM Weather on the Navigation Map Page
Procedures
Select the CLEAR Softkey to remove all Stormscope lightning data from the
display.
Flight
Planning
1)
1)
AFCS
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Nav/Com/
XPDR/Audio
1)
Display METAR and TAF information on the Airport Information Page
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Appendix
Turn the large FMS Knob to select the WPT Page Group.
Annun/Alerts
1)
Displaying Weather on the Weather Data Link Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
1)
43
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
4)
Select 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.
AFCS
Map Panning Information – Weather Data Link Page
1)
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
SIGMETs, PIREPs or AIREPs.
3)
Press the ENT Key to display pertinent information for the selected product.
Flight
Planning
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.
SiriusXM Weather Products and Symbols
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Select the available softkeys to select the desired SiriusXM weather product.
Weather Product
Symbol
Expiration Time
(Minutes)
Refresh Rate
(Minutes)
5 (U.S.)
10 (Canada)
Next-generation Radar
(NEXRAD)
30
Cloud Top
60
Echo Top
30
7.5
SiriusXM Lightning
30
5
Cell Movement
30
12
SIGMETs/AIRMETs
60
12
15 (69/69A)
30 (69/69A SXM)
Index
Appendix
3)
44
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
12
Freezing Levels
120
12
Winds Aloft
90
12
County Warnings
60
5
Cyclone Warnings
60
12
Icing Potential (CIP and
SLD)
90
22
Pilot Weather Report
(PIREPs)
90
12
Air Report (AIREPs)
90
12
Turbulence
180
12
no product image
30
5
no product image
60
12
no product image
60
12
Radar Coverage
Temporary Flight
Restrictions
Terminal Aerodrome
Reports
Appendix
90
Annun/Alerts
Surface Analysis
Additional
Features
12
Hazard
Avoidance
60
Procedures
City Forecast
Flight
Planning
12
GPS Nav
90
AFCS
Meteorological Aerodrome
Report (METARS)
Nav/Com/
XPDR/Audio
Refresh Rate
(Minutes)
Symbol
Flight
Instruments
Expiration Time
(Minutes)
Weather Product
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
45
CONNEXT WEATHER (OPTIONAL)
NOTE: The availability of specific Garmin Connext Weather products varies by
region. For product coverage information, refer to fly.garmin.com/fly-garmin/
gfds-weather.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
Weather data is provided when the pilot initiates either a manual or automatic
Connext data request on the Weather Data Link (CNXT) Page on the MFD. No
weather data is displayed until the first Connext Weather Data Request is made.
A subscriber account must be established prior to receiving Connext Weather
products. Contact Garmin Flight Data Services at https://fly.garmin.com/fly-garmin/
support/applications/satelliteservices/ or by calling 1-866-739-5687 in the United
States or (011) 913-440-1135. The following information is required to register for
Connext Weather services: G1000 System ID, GSR56 (GSR1) Serial Number(s), Tail
Number, Serail/Airframe Number, Country of Registration, Aircraft Manufacturer, and
Aircraft Model.
1)
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the
System ID and GSR1 Serial Number in the AIRFRAME field.
Activating Connext Weather Registration:
After a subscriber account has been established, the system must be activated
for data link features such as reporting services or Connext Weather. Activation is
accomplished by entering the required access code. This process is only performed
when initially setting up the system for Connext services.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Registering with Garmin Flight Data Services
46
1)
Ensure the aircraft is outside with a clear view of the sky.
2)
Turn the large FMS Knob to select the MAP Page group.
3)
Turn the small FMS Knob to select the MAP-WEATHER DATA LINK (CNXT)
Page.
4)
Press the MENU Key. If necessary, select ‘Display Connext Weather’.
5)
Press ENT Key. The ‘CONNEXT REGISTRATION’ Window is now displayed.
6)
Using the FMS Knob enter the access code obtained from Garmin Flight
Data Services in the ACCESS CODE field.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Press the ENT Key. REGISTER will now be highlighted.
8)
Press the ENT Key. System registration is complete when ‘REGISTERED’ is
displayed in the STATUS field.
Nav/Com/
XPDR/Audio
Accessing Connext Weather Products
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link (CNXT) Page.
Continuous
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
60
Appendix
Continuous
Annun/Alerts
30
Additional
Features
30
Hazard
Avoidance
60
Procedures
Broadcast
Rate
(Minutes)
U.S.: 3*
Canada: 3*†
Europe: 15
Australia: 15ˆ
Flight
Planning
30
Infrared Satellite
(IR SAT)
Data Link Lightning
(DL LTNG)
SIGMETs/AIRMETs
(SIG/AIR)
190-00929-05 Rev. B
Expiration
Time
(Minutes)
GPS Nav
Radar Precipitation
(PRECIP)
Symbol
AFCS
When a weather product is selected for display on the Weather Data Link (CNXT)
Page, a box containing a symbol for the product and its age (in minutes) are shown
in the upper right. If weather data has not been requested, ‘N/A’ is shown next to the
product symbol instead of age. The age of the weather product is based on the time
difference between when the data was assembled on the ground and the current GPS
time. Weather products are updated continuously or refreshed at specific intervals
(defined in the Broadcast Rate column in the following table).
If for any reason, a weather product is not refreshed within the defined Expiration
Time intervals, the data is considered expired and is removed from the display. The
age of the expired product is replaced by dashes. If more than half of the expiration
time has elapsed, the color of the product age readout changes to yellow.
The refresh rate represents the interval at which the Garmin Connext groundbased servers make available the most current known weather data. It does not
necessarily represent the rate at which new content is received from weather sources.
Garmin Connext Weather
Product
Flight
Instruments
7)
47
Garmin Connext Weather
Product
Symbol
Meteorological Aerodrome Report
(METARs)
Winds Aloft
(WIND)
Pilot Weather Report
(PIREPs)
Temporary Flight Restrictions
no product image
(TFRs)
Terminal Aerodrome Reports
no product image
(TAFs)
Expiration
Time
(Minutes)
Broadcast
Rate
(Minutes)
90
Continuous
90
Continuous
90
Continuous
60
Continuous
60
Continuous
* The composite precipitation image is updated every 3 minutes, but individual radar sites may take
between 3 and 10 minutes to provide new data.
†
Canadian radar precipitation data provided by Environment Canada.
ˆ Australian radar precipitation data provided by the Australia Bureau of Meteorology
Setting Up and Customizing the Connext Weather Data Link (CNXT)
Page
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
Additional
Features
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’,
and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Weather Data Link (CNXT)
Page with the changed settings.
Index
Appendix
1)
Annun/Alerts
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
48
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Press the MENU Key.
5)
Highlight the desired default(s) to restore (all or for selection) and press
ENT Key.
AFCS
Select the Weather Data Link (CNXT) Page.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
Restoring Default Connext Weather Data Link Page (CNXT) Settings
Viewing Legends for Displayed Connext Weather Products
Select the Weather Data Link (CNXT) Page.
2)
Select the LEGEND Softkey to display the legends for the displayed
weather products.
GPS Nav
1)
Flight
Planning
Or:
a) Press the MENU Key.
b) Select ‘Weather Legend’ and press the ENT Key.
4)
To remove the Legend Window, select the LEGEND Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Connext Weather Data Requests
Annun/Alerts
Requesting Connext Weather Data Manually
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Turn the large FMS Knob to highlight the desired coverage option(s)
and press the ENT Key to check or uncheck one of more of the following
coverage selections:
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Select the Weather Data Link (CNXT) Page.
Appendix
1)
Additional
Features
The Connext Data Request window provides the flight crew with the options to
define the requested weather coverage area(s), choose automatic weather update
intervals (if desired), and the ability to send or cancel weather data requests. The
window also displays the status of the Connext data request process.
Hazard
Avoidance
Turn the FMS Knob to scroll through the legends if more are available than
fit in the window.
Procedures
3)
49
Hazard Avoidance
Flight
Instruments
• PRESENT POSITION – Requests data based on current location.
Nav/Com/
XPDR/Audio
• DESTINATION – Requests data based on active flight plan
destination (if the flight plan contains no destination, dashes ‘------” are
displayed.)
AFCS
• FPL – Requests data based on active flight plan. Turn the small
FMS Knob to select the desired flight plan look-ahead distance
option (or choose ‘REMAINING FPL’ to request the remainder of the
flight plan).
• WAYPOINT – Requests data based on any valid waypoint.
Turn the large FMS Knob highlight to the ‘DIAMETER / RTE WIDTH’
distance field and turn the small FMS Knob to select the desired diameter
and route width of the request, then press the ENT Key.
6)
Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted. Press
the ENT Key to initiate the request immediately or press the FMS Knob to
return to the Connext Data Link Page without requesting data.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
5)
During a Connext Data Request, the REQUEST STATUS window initially displays
“Contacting Connext...”. Once a connection is established, the REQUEST STATUS
window displays “Receiving Wx Data... Time Remaining:” with an estimated data
transfer time (either in minutes or seconds). If desired, the Connext Data Request
window may be closed while the data request is processing by pressing the FMS
Knob; the data request will continue to process in the background. Connext Data
Requests typically take between 1 to 4 minutes to complete depending on the size of
the selected weather coverage area(s), the amount of weather activity present (such as
precipitation), and the Iridium signal strength.
The system retrieves all available Garmin Connext weather products within
the selected coverage area(s) during an initial Connext Data Request. Enabling or
disabling the display of the weather product does not affect which weather products
are retrieved during a Connext Data Request.
To reduce data usage during subsequent requests, the system retains previously
retrieved textual weather products such as METARs and TAFs, so long as they have
not expired. The system also retrieves any new textual weather products matching the
current coverage area, and all graphical weather products during each data request.
If the Connext Data Request was successful, the REQUEST STATUS window (if
shown) indicates ‘OK’. Refer to the Abnormal Operations discussion later in this
section for more information on the messages received if the request is unsuccessful,
with possible causes.
50
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Connext Comm Error [7]
Hazard
Avoidance
Connext Comm Error [8]
Procedures
Connext Comm Error [6]
Flight
Planning
Connext Comm Error [5]
GPS Nav
Connext Comm Error [4]
AFCS
Connext Comm Error [2]
The system has disabled automatic weather data
requests due to excessive errors. Automatic weather
data requests have stopped. Send a manual weather
data request to resume automatic updates.
The system will attempt another automatic weather
data request after an error occurred during the
previous request. Timer counts down until the next
automatic request occurs.
A communications error has occurred with the GIA,
GSR 56 or GDL 59. The system should be serviced.
This occurs if multiple automatic weather data
requests have recently failed, or the GIA is off-line.
The Iridium or Garmin Connext services are not
accessible. Check Iridium signal strength. If this error
persists, the system should be serviced.
A communications error has occurred. It this error
persists, the system should be serviced.
A weather data transfer has timed out. Check
Iridium signal strength and re-send the Connext Data
Request.
A server error has occurred or invalid data received.
Nav/Com/
XPDR/Audio
Auto update retry: ## Seconds
Description
Flight
Instruments
Weather Request Status
Message
Auto requests inhibited
Send manual request to reset.
There is a problem with the Garmin Connext
registration. Contact Garmin Connext at 1-866739-5687 in the United States or 913-440-1135 for
assistance.
Connext Server Temporarily Inop The Garmin Connext weather data server is
temporarily out of service, but is expected to return to
service in less than 30 minutes.
Connext Server Inop
The Garmin Connext weather data server will be out
of service for at least 30 minutes.
Additional
Features
Connext Login Invalid
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
51
Weather Request Status
Message
Invalid Coverage Area
No Connext Subscription
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
Request Cancelled
The weather data request coverage area does not
contain at least one of the following: a waypoint, a
flight plan, or a flight plan destination. Verify at least
one of the coverage options is enabled and contains
required criteria, then re-send the data request.
The system is not be currently subscribed to the
Garmin Connext Weather service, or the access code
is incorrect. Verify the access code. Contact Garmin
Connext at 1-866-739-5687 in the United States or
913-440-1135 for assistance.
The weather data request area exceeds size limits.
Reduce weather coverage area and re-send data
request.
The user has cancelled a weather data request.
Requested area too large.
Reduce coverage area.
The size of the weather data request has exceeded
limits. Reduce the size of the coverage area and try
the weather data request again.
Request Failed - Try Again
The weather data request timed-out. Re-send data
request.
The data link is busy. Retry request later.
Transfer Preempted
Abnormal Weather Data Request Status Messages
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Reduce Request Area
Description
1)
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
With the ‘CANCEL REQ’ option highlighted, press the ENT Key. The
REQUEST STATUS window indicates ‘Request Canceled’.
5)
Press the FMS Knob to return to the Weather Data Link (CNXT) Page.
Index
Appendix
Annun/Alerts
Cancelling Connext Data Request in Progress:
52
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Flight
Instruments
Enabling Automatic Connext Data Requests
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Choose the desired weather coverage options.
5)
Turn the large FMS Knob to select the ‘UPDATE RATE’ setting. Then turn
the small FMS Knob to highlight the desired automatic update frequency
(OFF, 5 Min, 10 Min, 15 Min, 20 Min, 25 Min, 30 Min, 45 Min, or 60 Min),
then press the ENT Key.
6)
The ‘SEND REQ” button is highlighted and a countdown timer is displayed
in the ‘REQUEST STATUS’ based on the currently selected update rate.
Press the ENT Key to immediately send an immediate Connext Data
Request.
Nav/Com/
XPDR/Audio
1)
Flight
Planning
Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
This step is not necessary on the Connext Weather Data Link Page.
2)
Select the PRECIP Softkey.
53
Index
Radar data shown represents lowest level, base reflectivity, of radar returns. The
display of the information is color-coded to indicate the weather severity level. All
weather product legends can be viewed on the Connext Weather Data Link Page. For
the Precipitation legend, select the LEGEND Softkey when Precipitation is selected
for display.
Appendix
1)
Annun/Alerts
Displaying Precipitation Weather Information
Additional
Features
NOTE: Precipitation data cannot be displayed on the Navigation Map Page
at the same time as terrain.
Hazard
Avoidance
Precipitation
Precipitation data is not real-time. The lapsed time between collection, processing,
and dissemination of radar images can be significant and may not reflect the current
radar synopsis. Due to the inherent delays and the relative age of the data, it should
be used for long-range planning purposes only.
Procedures
Connext Weather Products
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
GPS Nav
Press the FMS Knob to return to the Connext Weather Data Link Page.
190-00929-05 Rev. B
AFCS
Or:
Hazard Avoidance
Infrared Satellite
Infrared Satellite (IR SAT) data depicts cloud top temperatures from satellite imagery.
Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes.
Displaying Cloud Tops information
1)
Select the Weather Data Link (CNXT) Page.
2)
Select the IR SAT Softkey.
To display the Infrared Satellite legend, select the LEGEND Softkey when Infrared
Satellite data is selected for display.
Data Link Lightning
Lightning data shows the approximate location of cloud-to-ground lightning strikes.
A strike icon represents a strike that has occurred within a two-kilometer region. Neither
cloud-to-cloud nor the exact location of the lightning strike is displayed.
If the aircraft is also equipped with an on-board lightning detection system (e.g., L-3
WX-500 Stormscope®), only one lightning product may be enabled for display at a time.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Precipitation Limitations
Radar images may have certain limitations:
• Radar base reflectivity does not provide sufficient information to determine cloud
layers or precipitation characteristics (wet hail vs. rain). For example, it is not
possible to distinguish between wet snow, wet hail, and rain.
• Radar base reflectivity is sampled at the minimum antenna elevation angle. An
individual radar site cannot depict high altitude storms at close ranges. It has
no information about storms directly over the site.
• When zoomed in to a range of 30 nm, each square block on the display represents
an area of four square kilometers.
The following may cause abnormalities in displayed radar images:
• Ground clutter
• Strobes and spurious radar data
• Sun strobes (when the radar antenna points directly at the sun)
• Interference from buildings or mountains, which may cause shadows
• Metallic dust from military aircraft, which can cause alterations in radar scans
54
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
1)
Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
This step is not necessary on the Connext Weather Data Link Page.
The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring
within the coverage area of the Connext data request.
GPS Nav
Displaying SIGMETs and AIRMETs
Select the Weather Data Link (CNXT) Page.
2)
Select the SIG/AIR Softkey.
3)
To view the text of the SIGMET or AIRMET, press the RANGE Knob and move
the Map Pointer over the icon.
Hazard
Avoidance
METARs and TAFs
Displaying METAR and TAF text
Press the RANGE Knob and pan to the desired airport.
3)
Press the ENT Key. The Weather Information Page is shown with METAR
and TAF text.
Appendix
2)
Annun/Alerts
METAR and TAF text are displayed on the WPT-Weather Information Page. TAF
information is displayed in its raw form when it is available.
Additional
Features
NOTE: METAR information is only displayed within the installed navigation
database service area.
On the Weather Data Link (CNXT) Page, select the METAR Softkey.
Procedures
4) Press the ENT key.
To display the SIGMET and AIRMET legend on the Weather Data Link (CNXT)
Page, select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display.
Flight
Planning
1)
1)
AFCS
SIGMETs and AIRMETs
Nav/Com/
XPDR/Audio
2) Select the DL LTNG Softkey.
To display the Data Link Lightning legend on the Weather Data Link (CNXT) Page,
select the LEGEND Softkey when Data Link Lightning is selected for display.
Flight
Instruments
Displaying Data Link Lightning information
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
55
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
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 Connext Weather Data
Link Page.
Or:
1)
Select the Weather Information Page.
AFCS
a) Turn the large FMS Knob to select the Waypoint Page Group.
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
GPS Nav
b) Select the WX Softkey to select the Weather Information Page.
To display the METAR legend on the Weather Data Link (CNXT) Page, select the
LEGEND Softkey when METARs are selected for display.
Winds Aloft
Winds Aloft data shows the forecasted wind speed and direction at the surface and
at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000
feet MSL.
1)
Select the Weather Data Link (CNXT) Page.
2)
Select the MORE WX Softkey.
3)
Select the WIND Softkey.
4)
Select the desired altitude level: SFC (surface) up to 42,000 feet. Select
the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND
Softkey label changes to reflect the altitude selected.
To display the Winds Aloft legend on the Weather Data Link (CNXT) Page, select
the LEGEND Softkey when Winds Aloft is selected for display.
Index
Appendix
Annun/Alerts
Additional
Features
Displaying Winds Aloft data
56
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Displaying PIREP text
3)
Select the PIREPS Softkey.
4)
Press the RANGE Knob 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,
then as raw text.
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 Connext Weather Data Link Page.
Hazard
Avoidance
To display the PIREP or AIREP legend, select the LEGEND Softkey when PIREPs
or AIREPs are selected for display. The PIREP color is determined by the type (routine
or urgent).
Procedures
Select the MORE WX Softkey.
Flight
Planning
2)
GPS Nav
Select the Weather Data Link (CNXT) Page.
AFCS
1)
Nav/Com/
XPDR/Audio
Pilot Weather Reports (PIREPs) describe in-flight weather encountered by pilots.
A PIREP may contain unforecast adverse weather conditions, such as low in-flight
visibility, icing conditions, wind shear, turbulence, and type of aircraft flown. PIREPs
are issued as either Routine (UA) or Urgent (UUA).
Flight
Instruments
PIREPs
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
57
AIRBORNE COLOR WEATHER RADAR
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
AFCS
CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Radar Page.
3)
Select the MODE Softkey.
4)
If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.
Procedures
Flight
Planning
GPS Nav
Displaying Weather on the Weather Radar Page
Hazard
Avoidance
Or:
Index
Appendix
Annun/Alerts
Additional
Features
If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.
5)
Turn the Joystick to select the desired range.
6)
If desired, select the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Move the Joystick up or down to adjust the tilt of the antenna up or down.
Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
58
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.
4)
Turn the Joystick to adjust the range.
5)
To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.
Adjusting Gain
2)
Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.
3)
Press the FMS Knob to remove the cursor.
4)
Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
59
Index
190-00929-05 Rev. B
Appendix
Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
Annun/Alerts
1)
Additional
Features
WARNING: Changing the gain in Weather Mode will cause precipitation
intensity to be displayed as a color not representative of the true intensity.
Remember to return the gain setting to ‘Calibrated’ for viewing the actual
intensity of precipitation.
Hazard
Avoidance
3)
Procedures
Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.
Flight
Planning
2)
GPS Nav
1) While in the Horizontal Scan view, move the Joystick to place the Bearing
Line on the desired storm cell, or other area, to be vertically scanned.
AFCS
Vertically Scan a Storm Cell
Nav/Com/
XPDR/Audio
Move the Joystick right or left to adjust the azimuth position of the antenna right
or left. Monitor the displayed bearing value in the BEARING field.
When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Bearing Line’.
3) Press the ENT Key.
Flight
Instruments
Adjusting Antenna Bearing
Hazard Avoidance
Nav/Com/
XPDR/Audio
Flight
Instruments
Ground Mapping
Select the MODE Softkey.
2)
Select the GROUND Softkey to place the radar in Ground Map Mode.
3)
Select the BACK Softkey.
Procedures
Flight
Planning
GPS Nav
AFCS
Sector Scan
1)
While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.
2)
Press the FMS Knob to display the cursor.
3)
Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
4)
Turn the small FMS Knob to select a scan angle.
5)
If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
6)
Press the FMS Knob to remove the cursor.
Antenna Stabilization
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
1)
1)
To activate or deactivate the antenna stabilization, select the MODE
Softkey.
2)
Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the WATCH® feature, select the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Weather Alert
To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating
and deactivating will also enable or inhibit the alert on the PFD.
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system will automatically switch to Standby Mode.
60
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Procedures
Hazard
Avoidance
Description
Flight
Planning
Traffic Symbol
GPS Nav
• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey will be displayed.
• If a Traffic Advisory System (TAS) or Traffic Collision Avoidance System (TCAS
I) is configured, a STANDBY, OPERATE or NORMAL, TEST, and ALT MODE
Softkey will be displayed.
• If a Traffic Collision Avoidance System (TCAS II) is configured, an REL, ABS,
TFC STBY, TA ONLY, TA/RA, TEST, and ALT RNG Softkey will be displayed.
AFCS
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.
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
TRAFFIC AVOIDANCE SYSTEMS
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Additional
Features
Proximity Advisory (PA)(TAS only, not available with TIS)
(intruder is within 5 nm and less than 1200’ vertical separation)
Annun/Alerts
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Traffic Advisory Off Scale
Appendix
Resolution Advisory (RA)(TCAS II only)
(Potential collision area is within 15 to 35 seconds)
Resolution Advisory Off Scale (TCAS II only)
Index
Traffic Symbol Description
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
61
Hazard Avoidance
Flight
Instruments
Traffic Information Service (TIS)
Nav/Com/
XPDR/Audio
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Procedures
Flight
Planning
GPS Nav
AFCS
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ will be displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural alert.
Hazard
Avoidance
Displaying Traffic on the Navigation Map
1)
Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Additional
Features
Traffic Advisory System (TAS) or Traffic Collision Avoidance System
(TCAS I, GTS 850/855 only) (Optional)
Index
Appendix
Annun/Alerts
System Self Test
62
1)
Set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
Self test will take approximately eight seconds to complete. When
completed successfully, traffic symbols will be displayed and a voice alert
appropriate for the installed system will be heard indicating the test passed
(see Annunciations & Alerts section). If the self test fails, the system will
revert to Standby Mode and a voice alert appropriate for the installed
system will be heard indicating the test failed.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
Flight
Instruments
Displaying Traffic on the Traffic Map Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the second rectangular page icon.
3)
Select the OPERATE or NORMAL Softkey to begin displaying traffic.
‘OPERATING’ is displayed in the Traffic Mode field.
4)
Select the ALT MODE Softkey to change the altitude display volume.
Select the desired altitude volume by selecting the BELOW, NORMAL,
ABOVE, or UNREST (unrestricted) Softkey. The selection is displayed in the
Altitude Mode field.
5)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ will be displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
7)
Select the FLT ID Softkey (GTS 800/820/825/850/855 only) to enable or
disable Flight ID displayed with the intruder information.
Nav/Com/
XPDR/Audio
1)
GPS Nav
Flight
Planning
With the Navigation Map displayed, select the MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Procedures
1)
Hazard
Avoidance
TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS II) (OPTIONAL)
System Test
3)
Select the TEST Softkey. A test pattern of traffic symbols is displayed on
the Traffic Page and inset map on the PFD. The VSI will display red with
a green climb indication from 0 to 2000 feet per min. The self test takes
approximately eight seconds to complete, after which a voice alert “TCAS
System Test OK” is heard. In the event the system test fails, a voice alert
“TCAS System Test Failed” is heard and a visual annunciation ‘TCAS FAIL’
appears on the PFD. In addition, a yellow visual annunciation ‘FAILED’
appears in the center of the Traffic Map Page.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Turn the small FMS Knob to select the Traffic Map Page.
Appendix
2)
Annun/Alerts
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
NOTE: If the system is configured to use TIS or TAS, the optional TCAS II is
not available for use.
1)
AFCS
Displaying Traffic on the Navigation Map
63
Hazard Avoidance
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA/RA’ or
‘TA ONLY’ respectively, is displayed in the TCAS Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘TFC STBY’ will be displayed in the TCAS Mode field.
5)
Select the ABS (absolute) or REL (relative) Softkey to display intruder
altitude as an absolute altitude or an altitude relative to own aircraft
altitude.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Procedures
Flight
Planning
Changing the Altitude Range
1)
On the Traffic Page, select the ALT RNG Softkey.
2)
Select one of the following Softkeys:
Hazard
Avoidance
NORMAL: Displays non-threat and proximity traffic from 2700 feet above
the aircraft to 2700 feet below the aircraft. Typically used during enroute
phase of flight.
Additional
Features
ABOVE: Displays non-threat and proximity traffic from 9900 feet above the
aircraft to 2700 feet below the aircraft. Typically used during climb phase
of flight.
BELOW: Displays non-threat and proximity traffic from 2700 feet above the
aircraft to 9900 feet below the aircraft. Typically used during descent phase
of flight.
Annun/Alerts
UNREST (unrestricted): All traffic is displayed.
3)
To return to the Traffic Page, select the BACK Softkey.
1)
Ensure TCAS II system is operating. With the Navigation Map displayed,
select the MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Index
Appendix
Displaying Traffic on the Navigation Map
64
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Hazard Avoidance
Flight
Instruments
TERRAIN AWARENESS & WARNING SYSTEM
TAWS-A (Optional)
Procedures
Manual System Test
While the TAWS-A 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-A Page.
Hazard
Avoidance
1)
Additional
Features
When all is in working order, “TAWS System Test, OK” is heard.
Displaying the TAWS-A Page
2)
Turn the small FMS Knob to select the TAWS-A Page.
3)
If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.
Appendix
Turn the large FMS Knob to select the Map Page Group.
Annun/Alerts
1)
Flight
Planning
NOTE: The Terrain Awareness and Warning System (TAWS) may not operate
reliably north of 89º North latitude and south of 89º South latitude. This is
due to limitations present within the Terrain database and the system’s ability
to process the data representing the affected areas (GRS 7800 installations
only).
GPS Nav
NOTE: TAWS operation is only available when the system is configured for
a TAWS-A installation.
AFCS
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Nav/Com/
XPDR/Audio
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
65
Hazard Avoidance
Flight
Instruments
Color
Nav/Com/
XPDR/Audio
Red
Terrain/Obstacle Location
Terrain/Obstacle above or within 100’ below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’ below aircraft altitude.
GPS Nav
AFCS
Enable/Disable Aviation Data
1)
While the TAWS-A 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.
Flight
Planning
Inhibiting/Enabling FLTA and PDA Alerting
1)
Select the TAWS-A Page.
2)
Select the TAWS INH Softkey to inhibit or enable TAWS-A (choice
dependent on current state).
Procedures
Overriding Flaps-based FIT Alerting
1)
Select the TAWS-A Page.
2)
Select the FLAP OVR Softkey.
Additional
Features
Hazard
Avoidance
Inhibiting/Enabling GPWS Alerting
1)
Select the TAWS-A Page.
2)
Select the GPWS INH Softkey to inhibit or enable GPWS alerts (choice
dependent on current state).
Annun/Alerts
Inhibiting/Enabling GSD Alerting
1)
Select the TAWS-A Page.
2)
Select the GS INH or GP INH Softkey to inhibit or enable GSD alerts
(softkey choice dependent on present GSD alert type).
Index
Appendix
NOTE: Only available during a GSD alert.
66
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Hazard Avoidance
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
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.
Hazard
Avoidance
While the TAWS-B Page is displayed, press the MENU Key.
Procedures
1)
When all is in working order, “TAWS System Test, OK” is heard.
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.
Appendix
2)
Annun/Alerts
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
Display Terrain and Obstacles on the TAWS-B Page
1)
Flight
Planning
Manual System Test
GPS Nav
NOTE: The Terrain Awareness and Warning System (TAWS) may not operate
reliably north of 89º North latitude and south of 89º South latitude. This is
due to limitations present within the Terrain database and the system’s ability
to process the data representing the affected areas (GRS 7800 installations
only).
AFCS
NOTE: TAWS operation is only available when the system is configured for
a TAWS-B installation.
Nav/Com/
XPDR/Audio
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Flight
Instruments
TAWS-B
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
67
Hazard Avoidance
Flight
Instruments
Color
Red
Nav/Com/
XPDR/Audio
Yellow
Black
Terrain/Obstacle Location
Terrain/Obstacle above or within 100’ below current aircraft altitude.
Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.
Terrain/Obstacle is more than 1000’ below aircraft altitude.
GPS Nav
AFCS
Enable/Disable Aviation Data
1)
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.
TAWS Inhibit
Flight
Planning
NOTE: If TAWS 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.
Procedures
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Additional
Features
Hazard
Avoidance
Or:
1)
Press the MENU Key.
2)
Turn the small FMS Knob to select ‘Inhibit TAWS’.
3)
Press the ENT Key.
Enable TAWS
Annun/Alerts
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Appendix
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.
Index
Displaying Terrain and Obstacles on the Navigation Map
68
1)
With the Navigation Map displayed, select the MAP Softkey.
2)
Select the TERRAIN Softkey. Terrain and obstacles will now be displayed
on the map.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
Hazard
Avoidance
Additional
Features
Annun/Alerts
Displaying SVT Terrain
2)
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
Appendix
Press the PFD Softkey.
Procedures
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
1)
Flight
Planning
•
•
•
•
•
•
•
GPS Nav
Synthetic Vision Technology (SVT) functionality is offered as an optional
enhancement to the G1000 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).
In addition to SVT enhancement to the PFD, the following features have been
added to the PFD:
AFCS
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.
Nav/Com/
XPDR/Audio
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 the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
69
Additional Features
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Pathways
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
Flight
Planning
GPS Nav
AFCS
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
1)
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
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 DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
70
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Flight
Planning
Procedures
Hazard
Avoidance
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 moving map in the plan
view of most approach charts and on airport diagrams.
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.
GPS Nav
FliteCharts®
AFCS
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.
Nav/Com/
XPDR/Audio
ChartView
Flight
Instruments
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR 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.
View Charts from the Navigation Map Page
Annun/Alerts
1)
Select the SHW CHRT Softkey when displayed.
Or:
Select 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)
Select the GO BACK Softkey to return to the previous page.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
71
Index
2)
Appendix
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
Additional Features
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
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)
Select the SHW CHRT Softkey. The appropriate chart will be displayed, if
available for the item selected.
4)
Select the GO BACK Softkey to return to the previous page.
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)
Hazard
Avoidance
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
6)
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.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
Procedures
Flight
Planning
GPS Nav
1)
Additional
Features
Change Day/Night View
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.
Index
Appendix
Annun/Alerts
AIRPORT DIRECTORY
72
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Flight
Instruments
View Airport Directory Information
Nav/Com/
XPDR/Audio
While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. Airport
Directory information is displayed on the right half of the display.
SATELLITE TELEPHONE AND DATA LINK SERVICES
2)
Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the
System ID and GSR1 Serial Number in the AIRFRAME field.
Additional
Features
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the large FMS Knob to select the MAP Page group.
3)
Turn the small FMS Knob to select the MAP-WEATHER DATA LINK (CNXT)
Page.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
73
Index
Ensure the aircraft is outside with a clear view of the sky.
Appendix
1)
Annun/Alerts
Activating Connext Weather Registration:
After a subscriber account has been established, the system must be activated
for data link features such as reporting services or Connext Weather. Activation is
accomplished by entering the required access code. This process is only performed
when initially setting up the system for Connext services.
190-00929-05 Rev. B
Hazard
Avoidance
1)
Procedures
A subscriber account must be established prior to receiving Connext Weather
products. Contact Garmin Flight Data Services at https://fly.garmin.com/fly-garmin/
support/applications/satelliteservices/ or by calling 1-866-739-5687 in the United
States or (011) 913-440-1135. The following information is required to register for
Connext Weather services: G1000 System ID, GSR56 (GSR1) Serial Number(s), Tail
Number, Serial/Airframe Number, Country of Registration, Aircraft Manufacturer, and
Aircraft Model.
Flight
Planning
Registering with Garmin Flight Data Services
GPS Nav
Operation of these features in the cockpit is accomplished through the AUXTELEPHONE, AUX-TEXT MESSAGING, and AUX-WI-FI SETUP Pages. For operation
using the cabin handset, consult the instructions provided with the handset.
AFCS
NOTE: Separate accounts must be established to access the Iridium satellite
network for voice/SMS and low speed data transmission, and high speed data
transmission for the maintenance reports.
5)
Turn the large FMS Knob to hightlight ‘Register With Connext’.
6)
Press the ENT Key. The ‘CONNEXT REGISTRATION’ Window is now
displayed.
7)
Using the FMS Knob enter the access code obtained from Garmin Flight
Data Services in the ACCESS CODE field.
8)
Press the ENT Key. REGISTER will now be highlighted.
9)
Press the ENT Key. System registration is complete when ‘REGISTERED’ is
displayed in the STATUS field.
Disable/Enable Telephone and Low Speed Data Services:
Procedures
Hazard
Avoidance
Additional
Features
Press the MENU Key. If necessary, select ‘Display Connext Weather’.
Iridium telephone and data communications may be turned on or off by performing
these simple steps.
1)
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the AUX-TELEPHONE Page.
3)
Press the MENU Key. The Page Menu window is now displayed.
4)
Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list.
5)
Press the ENT Key. The Iridium transceiver is now disabled.
6)
To enable the Iridium transceiver, repeat steps 1 through 4, then select
‘Enable Iridium Transceiver’.
Telephone Communication
The pilot or copilot can place and answer calls on the Iridium satellite network as well
as to or from the telephone handset in the cabin. Calls can also be answered or made from
the cabin phone, however, only actions initiated from the cockpit phone will be discussed
here. See the cabin handset user guide for more information. Control and monitoring of
telephone functions are accomplished through the AUX-TELEPHONE Page.
Viewing the Telephone Page
1)
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the AUX - TELEPHONE or AUX - TEXT
MESSAGING Page.
3)
If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page.
Index
Appendix
Annun/Alerts
4)
Disable/Enable Iridium Transceiver
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
74
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
External
Phone
Flight
Instruments
Internal
Phone
Description
Nav/Com/
XPDR/Audio
Phone is Idle
Phone is ringing
AFCS
Phone has a dial tone (off hook) or connected to
another phone
GPS Nav
Phone dialed is busy
Flight
Planning
Phone is dialing another phone
Procedures
Phone has failed
Hazard
Avoidance
Phone status not known
Phone is disabled
Additional
Features
Phone is reserved for data transmission
Annun/Alerts
Calling other phone or incoming call from other phone
Appendix
Other phone is on hold
Index
Phones are connected
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
75
Incoming Calls
When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up
alert will be displayed. If the call is from the cabin, CABIN will be displayed. If the
incoming call is an Iridium network call, IRIDIUM will be displayed. The pop-up alert
may be inhibited at times, such as during takeoff. In addition to the pop-up alert, a
ringing phone symbol will be displayed to the right of the MFD page title. Also, the
voice alert “Incoming Call” will be heard on the selected cockpit audio.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
GPS Nav
Answer an Incoming Call in the Cockpit
1)
Press the TEL Key on the appropriate audio panel.
2)
Select the ANSWER Softkey on the MFD.
Or:
1)
Press the TEL Key on the appropriate audio panel.
2)
Press the MENU Key to display the Page Menu.
3)
Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’.
4)
Press the ENT Key.
Selecting the IGNORE Softkey will extinguish the pop-up window and leave the
call unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page
allowing additional call information to be viewed before answering.
Mute Incoming Call Alerts
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
While viewing the AUX-TELEPHONE Page
1)
With the AUX-TELEPHONE Page displayed, press the MENU Key on the
MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Mute Incoming Call Alerts’.
3)
Press the ENT Key. The voice and pop-up alert will not be displayed now
when an incoming call is received.
Voice calls can be made from the cockpit to the handset in the cabin, or to an
external phone through the Iridium Satellite Network.
Index
Appendix
Outgoing Calls
76
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Press the TEL Key on the appropriate audio panel.
2)
Select the DIAL Softkey on the MFD.
3)
Press the ENT Key. The cursor will move from ‘CABIN’ to ‘OK’.
4)
Press the ENT Key again. The cabin phone will now ring.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
Make a Call to the Cabin:
To exit the call, select the HANGUP Softkey.
AFCS
Make an External Call from the Cockpit
Press the TEL Key on the appropriate audio panel.
2)
Select the DIAL Softkey on the MFD.
3)
Turn the small FMS Knob to select ‘IRIDIUM’.
4)
Press the ENT Key. The cursor has now moved to the phone number entry
field.
5)
Enter the desired number string ( typically, country code + area code +
phone number) by selecting the number softkeys on the MFD, pressing the
numeric keys on the MFD Controller, or turning the FMS knobs. The GSR 56
may be configured by an authorized repair facility to automatically enter a
default county code when the dialing window is displayed. To replace the
default country code, move the cursor to the first (furthest left) number in
the dialing window and enter the desired country code.
6)
Press the ENT Key. ‘OK’ is highlighted.
7)
Press the ENT Key. The system will begin calling the number.
GPS Nav
1)
Additional
Features
Annun/Alerts
Or:
Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’.
3)
Press the ENT Key.
Appendix
2)
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Select the HOLD Softkey again to resume the call.
190-00929-05 Rev. B
Hazard
Avoidance
Select the HOLD Softkey on the MFD.
Press the MENU Key to display the Page Menu.
Procedures
Placing The Cockpit Phone on Hold
1)
Flight
Planning
To exit the call, select the HANGUP Softkey.
77
Transferring a Call from the Cockpit
From the cockpit phone, a external call can be transferred to the cabin phone,
or a call with the cabin phone can be transferred to an external phone, or (when
two Iridium Transceivers are installed) an external call can be transferred to another
external phone.
1) Select the TRANS Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’.
c) Press the ENT Key.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
2)
Press the ENT Key. The cursor now highlights the phone number entry
field.
3)
Enter the phone number as discussed earlier for making an external call on
the Iridium satellite network.
4)
Press the ENT Key. ‘OK’ is now highlighted.
5)
Press the ENT Key again to place the call.
Making a Conference Call from the Cockpit
Hazard
Avoidance
1)
Select the CONF Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’.
2)
Press the ENT Key. The cursor now highlights the phone number entry
field.
3)
Enter the phone number as discussed earlier for making an external call on
the Iridium satellite network.
4)
Press the ENT Key. ‘OK’ is now highlighted.
5)
Press the ENT Key again to place the call.
Index
Appendix
Annun/Alerts
c) Press the ENT Key.
78
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Viewing the Text Messaging Page
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the AUX - TELEPHONE or AUX - TEXT
MESSAGING Page.
3)
If necessary, select the SMS Softkey to display the AUX-TEXT MESSAGING
Page.
Flight
Planning
Description
GPS Nav
Message Symbol
AFCS
1)
Nav/Com/
XPDR/Audio
Messages may be sent to an email address or text message capable cellular telephone.
Message length is limited to 160 characters, including the email address.
The text messaging user interface is mainly through the AUX-TEXT MESSAGING
Page.
Flight
Instruments
Text Messaging (SMS)
Received text message that has not been opened
Procedures
Received text message that has been opened
Hazard
Avoidance
Saved text message, draft not sent
Additional
Features
System is sending text message
Annun/Alerts
Text message has been sent
System failed to send text message
Appendix
Predefined text message
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
79
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Viewing a Text Message When Received
When viewing MFD pages other than the AUX-TEXT MESSAGING Page, a pop-up
alert will be displayed when a new text message is received.
Select the VIEW Softkey to view the message. Selecting the IGNORE Softkey will
extinguish the pop-up window and leave the text message unopened. Selecting the
IGNR ALL Softkey will extinguish the pop-window and ignore all future incoming
text messages. Selecting the SMS Softkey will display the AUX-TEXT MESSAGING
Page.
The pop-up alerts may be enabled or disabled through the Page Menu.
Procedures
Flight
Planning
GPS Nav
Enable/Disable Incoming Text Message Pop-Up Alerts
1)
With the AUX-TEXT MESSAGING Page displayed, press the MENU Key on
the MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Disable New Message
Popups’ or ‘Enable New Message Popups’.
3)
Press the ENT Key. The pop-up alert will not be displayed when an
incoming text message is received.
Reply to a Text Message
Hazard
Avoidance
While viewing the text message, select the REPLY Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Reply To Message’.
c) Press the ENT Key.
Annun/Alerts
Sending a Text Message
1)
While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey.
Or:
Appendix
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Draft New Message’.
Index
c) Press the ENT Key.
80
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Additional Features
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
4)
Enter the desired message using any combination of entry methods as
described in step 2.
5)
Press the ENT Key.
6)
Select the SEND Softkey to send the message immediately, or select the
SAVE Softkey to save the message in Outbox for sending at a later time.
Select the CANCEL Softkey to delete the message.
AFCS
3)
Nav/Com/
XPDR/Audio
The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the
‘TO’ field. Enter the desired telephone number or email address. Entry can
be accomplished through the alphanumeric keys on the MFD Controller,
or combination of the FMS Knob on the controller and softkeys on the
MFD. The FMS Knob is used to enter letters and numbers, or numbers
can be entered from the MFD by selecting the NUMBERS Softkey. Select
the CAP LOCK Softkey to create upper and lower case alpha characters.
Special characters can be accessed by selecting the SYMBOLS Softkey.
Flight
Instruments
2)
GPS Nav
Flight
Planning
Predefined Text Messages
Procedures
Time and effort can be saved in typing text messages that are used repeatedly by
saving these messages as a predefined message.
Create a Predefined Text Message
2)
Turn either FMS Knob to select ‘Edit Predefined Messages’.
3)
Press the ENT Key. The PREDEFINED MESSSAGES view is now displayed.
4)
Select the NEW Softkey.
Additional
Features
While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to
display the Page Menu.
Hazard
Avoidance
1)
Annun/Alerts
Or:
a) Press the MENU Key to display the Page Menu.
Appendix
b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined
Message’.
c) Press the ENT Key. The PREDEFINED SMS TEXT MESSAGE Window is
now displayed.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
81
5)
The cursor is displayed in the ‘TITLE’ field. Enter the desired message title.
Entry can be accomplished through the alphanumeric keys on the MFD
Controller, or combination of the FMS Knob on the controller and softkeys
on the MFD. The FMS Knob is used to enter letters and numbers, or
numbers can be entered from the MFD by selecting the NUMBERS Softkey.
Select the CAP LOCK Softkey to create upper and lower case alpha
characters. Special characters can be accessed by selecting the SYMBOLS
Softkey.
6)
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
7)
Enter the desired message using any combination of entry methods as
described in step 5.
8)
Press the ENT Key.
9)
Select the SAVE Softkey. The new predefined message is now shown in
the displayed list. Selecting the CANCEL Softkey will delete the message
without saving.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
10) Press the MENU Key to display the Page Menu.
Procedures
11) Turn either FMS Knob to place the cursor on ‘Stop Editing Predefined
Message’.
12) Press the ENT Key.
1)
While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey.
2)
The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the
‘TO’ field. Enter the desired telephone number or email address. Entry can
be accomplished through the alphanumeric keys on the MFD Controller, or
combination of the FMS Knob on the controller and softkeys on the MFD.
The FMS Knob is used to enter letters and numbers, or numbers can be
entered from the MFD by selecting the NUMBERS Softkey. Select the CAP
LOCK Softkey to create upper and lower case alpha characters. Special
characters can be accessed by selecting the SYMBOLS Softkey.
3)
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
4)
Select the PREDEFD Softkey. The PREDEFINED MESSAGE MENU Window is
displayed.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Send a Predefined Text Message
82
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
7)
Press the ENT Key.
8)
Select the SEND Softkey to transmit the message.
Nav/Com/
XPDR/Audio
Press the ENT Key. The predefined message text is inserted into the
message field. If desired, the message can be edited by using the FMS
Knobs.
Flight
Instruments
6)
Text Message Boxes
Flight
Planning
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the INBOX Softkey.
GPS Nav
Show Inbox Messages
AFCS
Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The
Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to
be sent later are stored as Drafts. Each text message box may be viewed separately, or
together in any combination.
Or:
Procedures
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’.
Hazard
Avoidance
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Show Outbox Messages
Additional
Features
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the OUTBOX Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Appendix
Show Draft Messages
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the DRAFTS Softkey.
Index
Or:
190-00929-05 Rev. B
Annun/Alerts
b) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
83
Additional Features
Flight
Instruments
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’.
AFCS
Nav/Com/
XPDR/Audio
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Arranging Text Messages
The viewed messages may be listed according to the date/time the message was
sent or received, the type of message (read, unread, sent, unsent, etc.), or by message
address.
GPS Nav
View Messages Sorted by Message Date/Time:
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the TIME Softkey.
Flight
Planning
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’.
Procedures
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
Hazard
Avoidance
View Messages Sorted by Message Type
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the TYPE Softkey.
Additional
Features
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Type’.
Annun/Alerts
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
View Messages Sorted by Address:
Appendix
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the ADDRESS Softkey.
Index
Or:
84
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Additional Features
Flight
Instruments
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Address’.
Nav/Com/
XPDR/Audio
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
Viewing The Content of a Text Message
While viewing the AUX-TEXT MESSAGING Page, select the desired message box.
2)
Press the FMS Knob to activate the cursor.
3)
Turn either FMS Knob to select the desired message.
4)
Select the VIEW Softkey.
AFCS
1)
GPS Nav
Or:
Press the ENT Key.
Flight
Planning
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘View Selected Message’.
5)
Procedures
c) Press the ENT Key.
To close the text message, select the CLOSE Softkey.
Or:
Hazard
Avoidance
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Close Message’.
Additional
Features
c) Press the ENT Key.
Mark Selected Message As Read
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the MRK READ Softkey.
Annun/Alerts
1)
Appendix
Or:
a) Press the MENU Key to display the Page Menu.
Index
b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message
As Read’.
c) Press the ENT Key. The message symbol now indicates the message
has been opened.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
85
Additional Features
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Mark All Messages As Read
1)
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Mark All New Messages As
Read’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With cursor highlighting ‘YES’, press the ENT Key. The message symbols
now indicate all the message have been opened.
Flight
Planning
GPS Nav
Delete a Message
1)
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the DELETE Softkey.
Or:
b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’.
c) Press the ENT Key.
WI-FI CONNECTIONS
The system can connect to a IEEE 802.11g compatible network provided the
aircraft is on the ground and located within range of the network. The system is
capable of WEP64, WEP128,WPA-PSK, and WPA2-PSK encryption formats. WPAEnterprise and WPA2-Enterprise are not supported. Connections that require web
proxies, captive portals, or other elements that require user credentials, including a
username and password or a redemption or access code; or require action such as
accepting a user agreement, are not supported.
Control and monitoring of Wi-Fi functions are accomplished through the AUXWI-FI SETUP Page.
View the Wi-Fi Setup Page
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
a) Press the MENU Key to display the Page Menu.
86
1)
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the AUX - WI-FI SETUP Page.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Select the AVAIL Softkey on the MFD. A list of available networks will
be displayed in the AVAILABLE NETWORKS window. Signal strength is
shown for each network, as well as security requirements and whether the
network has been saved in the system’s memory.
2)
If necessary, select the RESCAN Softkey to have the system scan again for
available networks.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
Set Up a New Wi-Fi Connection
AFCS
Or:
a) Press the MENU Key to display the Page Menu.
GPS Nav
b) Turn either FMS Knob to place the cursor on ‘Rescan Available
Networks’.
c) Press the ENT Key.
Press the FMS Knob to place the cursor in the list of networks.
4)
Turn either FMS Knob to select the desired network.
5)
Select the CONNECT Softkey.
Flight
Planning
3)
Procedures
Or:
a) Press the MENU Key to display the Page Menu.
Hazard
Avoidance
b) Turn either FMS Knob to place the cursor on ‘Connect To Selected
Network’.
c) Press the ENT Key.
Press the ENT Key. ‘OK’ will be highlighted.
8)
Press the ENT Key again.
9)
The SAVE SETTINGS window is now displayed with the cursor highlighting
‘SAVE CONNECTION’.
10) The selected network can be saved to system memory to make reconnection easier at a later time.
Appendix
7)
Annun/Alerts
If the network is secured, a window will be displayed in order to enter
the necessary passcode. Use the FMS Knobs to enter the desired alpha
numeric characters. Select the CAP LOCK Softkey to enter upper case
letters. If there is no security associated with the network, proceed to step
9.
Additional
Features
6)
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
87
Additional Features
Flight
Instruments
To connect the selected network without saving:
a) Turn the large FMS Knob to move the cursor to highlight ‘CONNECT’.
b) Press the ENT Key.
Nav/Com/
XPDR/Audio
To save and connect the selected network:
a) Press the ENT Key. A checkmark is placed in the checkbox and the
cursor moves to the airport field.
AFCS
b) Using the FMS Knobs, enter an airport identifier to be associated with
the saved network. This aids in identifying the network later in the
event of duplicate network names.
GPS Nav
c) Press the ENT Key. The cursor moves to ‘CONNECT’.
d) Press the ENT Key again to connect to the selected network.
1)
While viewing list of saved networks, press the FMS Knob to activate the
cursor.
2)
Turn either FMS Knob to highlight the network to be edited.
3)
Pressing the ENT Key at this point will check or uncheck the AUTO
CONNECT checkbox. When a checkmark is present, the system will
automatically connect to the network when within range.
4)
Select the EDIT Softkey. The cursor now appears in the CONNECTION
SETTINGS window.
5)
Turn the large FMS Knob to select the network attribute to be edited.
6)
Turn the small FMS Knob to begin editing the field.
7)
When the entry is complete, press the ENT Key.
8)
Turn the large FMS Knob or press the ENT Key until ‘SAVE’ is highlighted.
9)
Press the ENT Key.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Edit a Saved Network
88
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Additional Features
Flight
Instruments
Disconnect a Wi-Fi Network
Select the DISCNCT Softkey.
Or:
Nav/Com/
XPDR/Audio
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Disconnect From
Network’.
AFCS
c) Press the ENT Key.
Delete a Saved Wi-Fi Network:
While viewing the list of saved networks, press the FMS Knob to activate
the cursor.
2)
Turn either FMS Knob to highlight the network to be deleted.
3)
Select the DELETE Softkey. The selected network is removed from the list.
GPS Nav
1)
Procedures
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM™ Satellite Radio.
Flight
Planning
SIRIUSXM™ RADIO ENTERTAINMENT
Selecting the XM Radio Page
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Additional
Features
Turn the large FMS Knob to select the Auxiliary Page Group.
Hazard
Avoidance
1)
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.
Annun/Alerts
Active Channel and Channel List
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
89
Selecting a Category
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the CATGRY Softkey on the XM Radio Page.
2) Select 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
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
1)
While on the XM Radio Page, select the CHNL Softkey.
2)
Select the CH + Softkey to move down through the list in the Channel Box,
or move up the list with the CH – Softkey.
Or:
Procedures
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
Additional
Features
Hazard
Avoidance
Entering a Channel Directly
1)
While on the XM Radio Page, select the CHNL Softkey.
2)
Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Select 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, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).
2) Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Selecting the
MORE Softkey repeatedly cycles through the preset channels.
90
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Additional Features
Select the SET Softkey.
4)
Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
Flight
Instruments
3)
Nav/Com/
XPDR/Audio
Adjusting Volume
Radio volume is controlled at each passenger station.
AFCS
PILOT PROFILES
Creating a profile:
GPS Nav
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
4)
Flight
Planning
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
Press the ENT Key. A ‘Create Profile’ window is displayed.
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:
9)
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
Annun/Alerts
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
Appendix
Selecting an active profile:
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
Press the FMS Knob momentarily to activate the flashing cursor.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
2)
91
Additional Features
Flight
Instruments
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
Nav/Com/
XPDR/Audio
desired profile.
5) Press the ENT Key. The system loads and displays the system settings for
the selected profile.
AFCS
Renaming a profile:
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
GPS Nav
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.
4)
Press the ENT Key.
Flight
Planning
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
rename.
6)
Press the ENT Key.
Procedures
7) Use the FMS Knob to enter a new profile name up to 16 characters long
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.
Additional
Features
Deleting a profile:
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Annun/Alerts
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
Appendix
delete.
6)
Press the ENT Key.
7) With ‘DELETE’ highlighted, press the ENT Key.
Index
8)
92
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
1)
2) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
3)
Press the IMPORT softkey. If the correct Pilot Profile file is selected; with
‘IMPORT’ highlighted press the ENT Key.
AFCS
Or:
Nav/Com/
XPDR/Audio
Insert the SD card containing the Pilot Profile into the top card slot on the
MFD.
Flight
Instruments
Importing a profile:
If the SD card contains more than one Pilot Profile:
GPS Nav
a) Turn the large FMS Knob to highlight the select file field in the Pilot
Profile Importing Box.
b) Turn the small FMS Knob to display the pilot profile list and highlight
the desired profile to import and press the ENT Key.
Flight
Planning
c) With ‘IMPORT’ highlighted, press the ENT Key.
4)
Procedures
“Pilot profile import succeeded.” is shown in the import results box. Press
the ENT Key. The imported profile becomes the active Pilot Profile.
Exporting a profile:
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
2) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
4)
Press the EXPORT softkey.
5)
With ‘EXPORT’ highlighted press the ENT Key.
6)
“Pilot profile export succeeded.” is shown in the export results box. Press
the ENT Key to exit the Pilot Profile Exporting Box.
Annun/Alerts
Activate the desired Pilot Profile to export. Only the active Pilot Profile can
be exported.
Additional
Features
3)
Hazard
Avoidance
1)
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
93
ELECTRONIC STABILITY & PROTECTION (ESP™)
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo, Mmo,
and/or angle of attack) beyond the normal flight parameters. Enhanced stability for each
condition is provided by applying a force to the appropriate control surface to return the
aircraft to the desired flight envelope. This is perceived by the pilot as resistance to control
movement in the undesired direction when the aircraft approaches a steep attitude, high
airspeed, or when a stall is imminent.
As the aircraft deviates further from the desired attitude, angle of attack, or airspeed
continues to increase, the force increases (up to an established maximum) to encourage
control movement in the direction necessary to return to the desired attitude and/or
airspeed range. Except in the case of high airspeed, when maximum force is reached, force
remains constant up to the maximum engagement limit. Above the maximum engagement
limit, forces are no longer applied. There is no maximum engagement related to a high
airspeed condition.
When ESP has been engaged for more than ten seconds (cumulative; not necessarily
consecutive seconds) of a 20-second interval, the autopilot is automatically engaged with
the flight director in Level Mode in the pitch and/or roll axis, bringing the aircraft into
level flight. An aural “Engaging Autopilot” alert is played and the flight director mode
annunciation will indicate ‘LVL’ for vertical and lateral modes.
The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering
(CWS) or Autopilot Disconnect (AP/YD DISC TRIM INTRPT) switch. Upon releasing the
CWS or AP/YD DISC TRIM INTRPT switch, ESP force will again be applied, provided
aircraft attitude, angle of attack and/or airspeed are within their respective engagement
limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit.
ESP can be enabled or disabled on the AUX-SYSTEM SETUP 2 Page on the MFD.
To enable or disable ESP:
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
94
1)
Turn the large FMS Knob to select the AUX Page Group.
2)
Turn the small FMS Knob to select the SYSTEM SETUP 1 Page.
3)
If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
6)
Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7)
Press the FMS Knob to remove the cursor.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Additional Features
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the onside Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing
where ESP will disengage as roll attitude decreases to within the desirable roll attitude
range.
Once engaged, ESP force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force
is intended to encourage pilot input that returns the airplane to a more normal roll
attitude. As roll attitude decreases, ESP will disengage at 30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
Flight
Instruments
Roll Engagement
Pitch Engagement
Annun/Alerts
Appendix
95
Index
Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of
the aircraft. When the high airspeed condition is remedied, ESP force is no longer
applied.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Additional
Features
High Airspeed Protection
190-00929-05 Rev. B
Hazard
Avoidance
If the Angle of Attack Protection feature is available in the current installation,
ESP force may be applied if the compatible lift computer determines a stall warning
condition is imminent. In this condition, the Pitch Limit Indicator will be initially
displayed 4° below this computed pitch attitude. When pitch attitude equals that
indicated by the Pitch Limit Indicator, ESP will engage, applying a force in the direction
necessary to lower the nose of the aircraft.
Procedures
Angle of Attack Protection
Flight
Planning
ESP engages at 20° nose-up and 17° nose-down. Once ESP is engaged, it will apply
opposing force between 15° and 50° nose-up and between 12° and 50° nose-down.
Maximum opposing force is applied between 25° and 50° nose-up and between 22°
and 50° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP engage and disengage limits in
these nose-up/nose-down conditions.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Blank Page
96
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
WARNING ANNUNCIATION
Aural Alert
“Airspeed” is heard once when an altitude-notUNDERSPEED critcal flight director mode is active. “Airspeed”
PROTECT ACTIVE - repeats every five seconds when an altitudecritical flight director mode is active.
AFCS
UNDERSPEED
PROTECT ACTIVE
Alerts Window
Text
Nav/Com/
XPDR/Audio
Annunciation
Window Text
GPS Nav
ADVISORY ANNUNCIATIONS
Alerts Window Text
AVN FAN 2 FAIL
AVN FAN 2 FAIL - Avionics cooling fan #2 is inoperative.
PFD 1 FAN FAIL
PFD 2 FAN FAIL
PFD 1 FAN FAIL - PFD #1 cooling fan is inoperative.
MFD FAN FAIL
MFD FAN FAIL - MFD cooling fan is inoperative.
Procedures
AVN FAN 1 FAIL - Avionics cooling fan #1 is inoperative.
Flight
Planning
Annunciation
Window Text
AVN FAN 1 FAIL
PFD FAN FAIL - PFD #2 cooling fan is inoperative.
Hazard
Avoidance
MESSAGE ADVISORY ALERTS
Alerts Window Message
Additional
Features
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
190-00929-05 Rev. B
Annun/Alerts
*ESP DEGRADE – ESP AOA mode is inoperative.
ESP DEGRADE – ESP IAS mode is inoperative.
ESP FAIL – ESP is inoperative.
ESP OFF – ESP selected off.
ESP CONFIG – ESP config error. Config service req’d.
TAWS GEAR FAULT – Landing Gear detected in the DOWN position.
TAWS FLAP FAULT – Flaps detected in the LDG position.
WOW FAULT – Miscompare between weight on wheels inputs.
WOW INVALID – Weight on wheels inputs invalid.
YD OFF – AP engaged without Yaw Damper.
*only available when compatible lift computer is installed.
97
COMPARATOR ANNUNCIATIONS
Comparator Window
Text
ALT MISCOMP
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
If either airspeed sensor detects > 35 knots, and the difference in sensors
is > 10 kts.
Procedures
Flight
Planning
GPS Nav
AFCS
If either airspeed sensor detects > 80 knots, and the difference in
sensors is > 7 kts.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..
REVERSIONARY SENSOR ANNUNCIATIONS
Annun/Alerts
Additional
Features
Hazard
Avoidance
Condition
Reversionary Sensor
Window Text
Condition
BOTH ON ADC1
BOTH ON ADC2
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON AHRS1
Both PFDs are displaying data from the number one Attitude & Heading
Reference System.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
Index
Appendix
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
98
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one GPS receiver.
Both PFDs are displaying data from the number two GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
Nav/Com/
XPDR/Audio
USING AHRS2
USING GPS1
USING GPS2
Condition
Flight
Instruments
Reversionary Sensor
Window Text
PFD1 is displaying data from the #2 GPS.
Condition
Annunciation Description
Roll Failure
Roll axis control failure.
Pitch Trim Axis
Control Failure
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
System Failure
AP and MET are unavailable. FD may still be available.
Flight
Planning
Pitch axis control failure.
GPS Nav
Pitch Failure
Procedures
YD axis control failure.
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
Hazard
Avoidance
Yaw Damper/
Ruddar Boost
Failure
Elevator Mistrim
Up
AFCS
AFCS ALERTS
A condition has developed causing the roll servo to provide
a sustained left force.
Aileron Mistrim
Right
A condition has developed causing the roll servo to provide
a sustained right force.
Rudder Mistrim
Left
A condition has developed causing the yaw servo to
provide a sustained force.
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force.
Preflight Test
Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Preflight system test has failed.
Appendix
Aileron Mistrim
Left
Annun/Alerts
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
Additional
Features
Elevator Mistrim
Down
99
TAWS-A ALERTS
Alert Type
Reduced Required Terrain
Clearance Warning (RTC)
PFD/MFD
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Voice Message
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
Imminent Terrain Impact
Warning (ITI)
Reduced Required Obstacle
Clearance Warning (ROC)
Imminent Obstacle Impact
Warning (IOI)
Excessive Descent Rate
Warning (EDR)
“<whoop><whoop>
Pull Up”
Excessive Closure Rate
Warning (ECR)
“<whoop><whoop>
Pull Up”
Reduced Required Terrain
Clearance Caution (RTC)
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”
Imminent Terrain Impact
Caution (ITI)
Reduced Required Obstacle
Clearance Caution (ROC)
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
100
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Voice Message
or
“Obstacle Ahead;
Obstacle Ahead”
or
“Caution, Obstacle;
Caution, Obstacle”
Excessive Descent Rate
Caution (EDR)
“Sink Rate”
Excessive Closure Rate
Caution (ECR)
“Terrain, Terrain”
or
“Don’t Sink”
or
“Too Low, Terrain”
Flight Into Terrain Gear
Caution (FIT)
“Too Low, Gear”
Flight Into Terrain Flaps
Caution (FIT)
“Too Low, Flaps”
Flight Into Terrain Takeoff
Caution (FIT)
“Too Low, Terrain”
or
“Glide Slope”
or
“Glide Path”
None
“Five-Hundred”
“Four-Hundred”
“Three-Hundred”
“Two-Hundred”
“One-Hundred”
(depends on approach type)
Altitude Voice Callout
(VCO)
(all are configurable, except
“Five-Hundred”)
None
Annun/Alerts
or
Additional
Features
Glide Slope Deviation
Caution (GSD)
Hazard
Avoidance
“Too Low, Terrain”
Procedures
Flight Into Terrain High
Speed Caution (FIT)
Flight
Planning
Negative Climb Rate
Caution (NCR)
GPS Nav
“Too Low, Terrain”
AFCS
Premature Descent Alert
Caution (PDA)
Nav/Com/
XPDR/Audio
Imminent Obstacle Impact
Caution (IOI)
MFD Map Page
Pop-Up Alert
Flight
Instruments
PFD/MFD
TAWS Page
Annunciation
Alert Type
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
101
Flight
Instruments
Annunciations & Alerts
TAWS-A System Status Annunciations
PFD/MFD
Additional TAWS-A Page
TAWS-A Page
Annunciation
Annunciation
Voice
Message
TAWS System Fail
TAWS FAIL
“TAWS System
Failure”
System Test in progress
TAWS TEST
None
System Test pass
None
None
“TAWS System
Test OK”
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
None
TERRAIN DATABASE FAILURE
None
None
“GPWS System
Failure”
NO GPS
POSITION
“TAWS Not
Available”
“TAWS
Available” when
sufficient GPS
signal is received.
None
“TAWS Not
Available”
“TAWS
Available”
when aircraft
enters database
coverage area.
GPWS System Fail,
Radar Altimeter invalid,
Altitude or Vertical
Speed unavailable
No GPS position,
excessively degraded
GPS signal
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Alert Type
Index
Appendix
Annun/Alerts
Out of database
coverage area
102
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Flight
Instruments
TAWS-A Alert Type Availability Under Various Conditions
TAWS-A Alert Type Available
FIT
GSD VCO
No
No
No
No
No
No
No
No
No
No
No
No
Yes
Yes
Yes
Yes
*No
**Yes
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
**Yes
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
No
No
No
No
**Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
#Yes
Yes
Yes
GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being
received.
**
VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available.
#
Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is
displayed.
190-00929-05 Rev. B
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
103
Index
Imminent Terrain Impact
Warning (ITI)
Voice Message
Appendix
Reduced Required Terrain
Clearance Warning (RTC)
MFD Map Page
Pop-Up Alert
Annun/Alerts
PFD/MFD
TAWS Page
Annunciation
Alert Type
Additional
Features
TAWS-B ALERTS
Hazard
Avoidance
*
Procedures
No
Flight
Planning
No
GPS Nav
No
AFCS
No
Nav/Com/
XPDR/Audio
TAWS-A
Status
RTC ITI ROC IOI PDA EDR ECR NCR
Annunciation
Displayed
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Alert Type
Reduced Required Obstacle
Clearance Warning (ROC)
Imminent Obstacle Impact
Warning (IOI)
PFD/MFD
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Voice Message
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
Excessive Descent Rate
Warning (EDR)
Reduced Required Terrain
Clearance Caution (RTC)
Imminent Terrain Impact
Caution (ITI)
Reduced Required Obstacle
Clearance Caution (ROC)
Imminent Obstacle Impact
Caution (IOI)
“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”
Premature Descent Alert
Caution (PDA)
“Too Low, Terrain”
Excessive Descent Rate
Caution (EDR)
“Sink Rate”
or
“Don’t Sink”
or
“Too Low, Terrain”
Index
Negative Climb Rate
Caution (NCR)
104
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Voice
Message
TAWS FAIL
“TAWS System
Failure”
System Test in progress
TAWS TEST
None
AFCS
TAWS System Fail
None
None
“TAWS System
Test OK”
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
None
TERRAIN DATABASE FAILURE
None
NO GPS
POSITION
“TAWS Not
Available”
“TAWS
Available”
when sufficient
GPS signal is
received.
None
“TAWS Not
Available”
“TAWS
Available”
when aircraft
enters database
coverage area.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Out of database
coverage area
GPS Nav
System Test pass
No GPS position,
excessively degraded
GPS signal
Nav/Com/
XPDR/Audio
PFD/MFD
Additional TAWS-A Page
TAWS-A Page
Annunciation
Annunciation
Alert Type
Flight
Instruments
TAWS-B System Status Annunciations
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
105
Flight
Instruments
Annunciations & Alerts
ADDITIONAL VOICE ALERTS
Voice Alert
Nav/Com/
XPDR/Audio
“Minimums”
“Vertical track”
The aircraft is one minute from Top of Descent. Issued only
when vertical navigation is enabled.
“Airspeed”
The aircraft is in an underspeed condition. See the AFCS
section for more details.
“Engaging autopilot”
The ESP system is engaging the autopilot. See the AFCS
section for more details.
“Traffic”
Played when a Traffic Advisory (TA) is issued with the
TIS system, the optional GTS 800/820/825 TAS system,
or the optional GTS 850/855 TCAS I system. See the
Hazard Avoidance section for additional details on GTS
800/820/825/850/855 voice alerts.
“TIS Not Available”
The aircraft is outside the Traffic Information Service (TIS)
coverage area.
“Traffic, Traffic”
Played when a Traffic Advisory (TA) is issued with the
optional SKY 497/SKY899 TAS system, or the optional KTA
870 TAS system. See the Skywatch PG or KTA 870 PG for
additional details on voice alerts.
Played for each subsequent TA (KTA 870 only).
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
The aircraft has descended below the preset minimum
descent altitude or decision altitude.
“Traffic”
Played when the optional traffic system passes a pilotinitiated self test.
“Traffic Advisory System Test Passed” - SKY 497 TAS
“SKYWATCH System Test Passed” - SKY 899 TAS
- KTA 870 TAS
“TAS System Test OK”
- GTS 800/820/825 TAS
“TAS System Test Passed”
- GTS 850 TCAS I
“TCAS System Test Passed”
- GTS 855 TCAS I
“TCAS One System Test Passed”
- GTS 8000 TCAS II
“TCAS Two System Test Passed”
Index
Appendix
Annun/Alerts
Description
106
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Description
GPS Nav
Intruder relative altitude (GTS 800/820/825/850/855 only)
Abort approach due to loss of GPS navigation.
GDC1 is reporting that the altitude error
correction is unavailable. The G1000 system
should be serviced.
GDC1 is reporting that the airspeed error
correction is unavailable. The G1000 system
should be serviced.
The GDC1 should be serviced.
Annun/Alerts
Appendix
ADC1 SERVICE – ADC1 needs
service. Return unit for repair.
Comments
Additional
Features
ADC1 AS EC – ADC1 airspeed
error correction is unavailable.
Hazard
Avoidance
SYSTEM MESSAGE ADVISORIES
Message
ABORT APR – Loss of GPS
navigation. Abort approach.
ADC1 ALT EC – ADC1 altitude
error correction is unavailable.
Procedures
“Less than one mile”,
Intruder distance (GTS 800/820/825/850/855 only)
“One Mile” through “Ten Miles”, or
“More than ten miles”
Flight
Planning
“High”, “Low”, “Same Altitude” (if
within 200 feet of own altitude), or
“Altitude not available”
Intruder bearing (GTS 800/820/825/850/855 only)
AFCS
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
Nav/Com/
XPDR/Audio
Played when the optional traffic system fails a pilot-initiated
self test.
“Traffic Advisory System Test Failed” - SKY 497 TAS
“SKYWATCH System Test Failed” - SKY 899 TAS
- KTA 870 TAS
“TAS System Test Fail”
- GTS 800/820/825 TAS
“TAS System Test Failed”
- GTS 850 TCAS I
“TCAS System Test Failed”
- GTS 855 TCAS I
“TCAS One System Test Failed”
- GTS 8000 TCAS II
“TCAS Two System Test Failed”
Flight
Instruments
Voice Alert
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
107
Message
ADC2 ALT EC – ADC2 altitude
error correction is unavailable.
ADC2 AS EC – ADC2 airspeed
error correction is unavailable.
ADC2 SERVICE – ADC2 needs
service. Return unit for repair.
Comments
GDC2 is reporting that the altitude error
correction is unavailable. The G1000 system
should be serviced.
GDC2 is reporting that the airspeed error
correction is unavailable. The G1000 system
should be serviced.
The GDC2 should be serviced.
AHRS MAG DB – AHRS magnetic
model database version mismatch.
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
The #1 AHRS calibration version error. The system
should be serviced.
AHRS1 CONFIG – AHRS1 config
error. Config service req’d.
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 GPS – AHRS1 not receiving
any GPS information.
The #1 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be
serviced.
AHRS1 GPS – AHRS1 using
The #1 AHRS is using the backup GPS path.
backup GPS source.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
AHRS1 SERVICE – AHRS1 needs
A failure has been detected in the #1 AHRS or #2
service. Return unit for repair.
AHRS. The system should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
108
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
The #1 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
AHRS2 GPS – AHRS2 not receiving The #1 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be
serviced.
AHRS2 GPS – AHRS2 using
The #1 AHRS is using the backup GPS path.
backup GPS source.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
AHRS2 SERVICE – AHRS2 needs
A failure has been detected in the #1 AHRS or #2
service. Return unit for repair.
AHRS. The system should be serviced.
AHRS2 SRVC – AHRS2 Magnetic- The #1 AHRS earth magnetic field model is out
field model needs update.
of date. Update magnetic field model when
practical.
Flight
Planning
AHRS2 GPS – AHRS2 operating
exclusively in no-GPS mode.
AHRS2 GPS – AHRS2 not receiving
any GPS information.
GPS Nav
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
AFCS
AHRS2 CONFIG – AHRS2 config
error. Config service req’d.
Nav/Com/
XPDR/Audio
Comments
The #1 AHRS earth magnetic field model is out
of date. Update magnetic field model when
practical.
AHRS1 TAS – AHRS1 not receiving The #1 AHRS is not receiving true airspeed from
valid airspeed.
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.
AHRS2 CAL – AHRS2 calibration
The #1 AHRS calibration version error. The system
version error. Srvc req’d.
should be serviced.
Flight
Instruments
Message
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
109
Message
Comments
AHRS2 TAS – AHRS2 not receiving The #1 AHRS is not receiving true airspeed from
valid airspeed.
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.
APR ADVISORY – SBAS VNAV not
SBAS VNAN not available. Check GPS sensor.
available. Using Baro VNAV.
APR DWNGRADE – Approach
Vertical guidance generated by SBAS is
downgraded.
unavailable, use LNAV only minimums..
APPR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
ARSPC AHEAD – Airspace ahead Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the special use airspace
within 10 minutes.
ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near –
Special use airspace is within 2 nm of the aircraft
less than 2 nm.
position.
BARO MISMATCH – Correct baro
mismatch for VNAV guidance.
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
CNFG MODULE – PFD1
configuration module is
inoperative.
COM1 CONFIG – COM1 config
error. Config service req’d.
Altimeter setting is not the same on PFD1 and
PFD2. Synchronize settings for VNAV guidance.
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
The PFD1 configuration module backup memory
has failed. The G1000 system should be
serviced.
COM1 configuration settings do not match
backup configuration memory. The system
should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
110
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190-00929-05 Rev. B
Annunciations & Alerts
Additional
Features
Annun/Alerts
Appendix
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 G1000 system should
be serviced.
Hazard
Avoidance
COM2 software mismatch. The system should be
serviced.
Procedures
COM2 MANIFEST – COM2
software mismatch, communication
halted.
COM2 PTT – COM2 push-to-talk
key is stuck.
Flight
Planning
COM2 CONFIG – COM2 config
error. Config service req’d.
GPS Nav
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
The COM1 external push-to-talk switch is stuck
in the enable (or “pressed”) position. Press the
PTT switch again to cycle its operation.
If the problem persists, the G1000 system should
be serviced.
The COM1 transfer switch is stuck in the enabled
(or “pressed”) position. Press the transfer switch
again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
The system has detected a failure in COM1.
COM1 may still be usable. The G1000 system
should be serviced when possible.
The system has detected an over temperature
condition in COM1. The transmitter operates
at reduced power. If the problem persists, the
G1000 system should be serviced.
COM2 configuration settings do not match
backup configuration memory. The system
should be serviced.
AFCS
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM1 software mismatch. The system should be
serviced.
Nav/Com/
XPDR/Audio
COM1 RMT XFR – COM1 remote
transfer key is stuck.
Comments
Flight
Instruments
Message
COM1 MANIFEST – COM1
software mismatch, communication
halted.
COM1 PTT – COM1 push-to-talk
key is stuck.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
111
Message
COM2 RMT XFR – COM2 remote
transfer key is stuck.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts
lost. Recheck settings.
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 contains
Verify stored airways.
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 CHANGE – Database changed. This occurs when a stored flight plan contains a
Verify user modified procedures.
procedure that is no longer consistent with the
navigation database. 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
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
Comments
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 G1000 system should be serviced.
The system has detected a failure in COM2.
COM2 may still be usable. The G1000 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
G1000 system should be serviced.
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Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
DB MISMATCH – Standby
Navigation database mismatch.
AFCS
DB MISMATCH – Obstacle
database mismatch.
Nav/Com/
XPDR/Audio
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
Annun/Alerts
Appendix
Comments
The PFDs and MFD have different airport terrain
database versions or regions 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.
The PFDs and MFD have different navigation
database versions or regions 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.
The PFDs and MFD have different obstacle
database versions or regions 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.
The PFDs and MFD have different standby
navigation database versions or regions 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.
Flight
Instruments
Message
DB MISMATCH – Airport Terrain
database mismatch.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
113
Message
Comments
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
mismatch.
database versions or regions 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.
FAILED PATH – A data path has
failed.
FPL TRUNC – Flight plan has been
truncated.
FPL WPT LOCK – Flight plan
waypoint is locked.
FPL WPT MOVE – Flight plan
waypoint moved.
A data path connected to the GDU or the GIA
63/W has failed.
This occurs when a newly installed navigation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
Upon power-up, the G1000 system detects that
a stored flight plan waypoint is locked. This
occurs when an navigation database update
eliminates an obsolete waypoint. The flight plan
cannot find the specified waypoint and flags
this message. This can also occur with user
waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database,
Or - update the waypoint name/identifier to
reflect the new information.
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
114
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Annunciations & Alerts
The GDC1 has incorrect software installed. The
system should be serviced.
Hazard
Avoidance
The GDC2 has incorrect software installed. The
system should be serviced
Annun/Alerts
GDL 59 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
Appendix
GCU1 MANIFEST – GCU software
mismatch, ommunication halted.
GDC1 MANIFEST – GDC1
software mismatch, communication
halted.
GDC2 MANIFEST – GDC2
software mismatch, communication
halted.
GDL59 CONFIG – GDL 59 config
error. Config service req’d.
Procedures
GCU KEYSTK – GCU [keyname]
Key is stuck
Flight
Planning
GCU FAIL – GCU is inoperative.
Additional
Features
GCU CNFG – GCU Config error.
Config service req’d.
GPS Nav
G/S2 SERVICE – G/S2 needs
service. Return unit for repair
AFCS
G/S2 FAIL – G/S2 is inoperative.
Nav/Com/
XPDR/Audio
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
Comments
A failure has been detected in glideslope receiver
1. The G1000 system should be serviced.
A failure has been detected in glideslope receiver
1. The receiver may still be available. The system
should be serviced when possible.
A failure has been detected in glideslope receiver
2. The G1000 system should be serviced.
A failure has been detected in glideslope receiver
2. The receiver may still be available. The system
should be serviced when possible.
GCU 477 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GCU 477. The
GCU 477 is unavailable.
A key is stuck on the GCU 477 bezel. Attempt
to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.
The GCU 477 has incorrect software installed.
The G1000 system should be serviced.
Flight
Instruments
Message
G/S1 FAIL – G/S1 is inoperative.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
115
Message
GDL59 FAIL – GDL 59 has failed.
Comments
A failure has been detected in the GDL 59. The
receiver is unavailable. The system should be
serviced.
GDL59 MANIFEST – GDL59
The GDL 59 has incorrect software installed. The
software mismatch, communication system should be serviced.
halted.
GDL59 RTR FAIL – The GDL 59
router has failed.
GDL59 SERVICE – GDL 59 needs
service. Return unit for repair.
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
A failure has been detected in the GDL 59 router.
The system should be serviced.
A failure has been detected in the GDL 59. The
system should be serviced.
GDL 69/69A/69 SXM configuration settings
do not match those of backup configuration
memory. The G1000 system should be serviced.
GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL
69/69A/69 SXM. The receiver is unavailable.
The G1000 system should be serviced
GDL69 MANIFEST – GDL software The GDL 69/69A/69 SXM has incorrect software
mismatch, communication halted. installed. The G1000 system should be serviced.
GEA1 CONFIG – GEA1 config
error. Config service req’d.
GEA2 CONFIG – GEA2 config
error. Config service req’d.
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass.
GEO LIMITS – AHRS2 too far
North/South, no magnetic compass.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
The GEA1 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
The GEA2 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
as invalid.
The GIA1 has an error in the audio configuration.
The G1000 system should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
116
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190-00929-05 Rev. B
Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
117
AFCS
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Nav/Com/
XPDR/Audio
190-00929-05 Rev. B
Flight
Instruments
Message
Comments
GIA1 CONFIG – GIA1 config error. The GIA1 configuration settings do not match
Config service req’d.
backup configuration memory. The G1000
system should be serviced.
GIA1 COOLING – GIA1 over
The GIA1 temperature is too high. If problem
temperature.
persists, the G1000 system should be serviced.
GIA1 COOLING – GIA1
The GIA1 temperature is too low to operate
temperature too low.
correctly. Allow units to warm up to operating
temperature.
GIA1 MANIFEST – GIA1 software The GIA1 has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
GIA1 SERVICE – GIA1 needs
The GIA1 self-test has detected a problem in the
service. Return the unit for repair. unit. The G1000 system should be serviced.
GIA2 CONFIG – GIA2 audio config The GIA2 h an error in the audio configuration.
error. Config service req’d.
The G1000 system should be serviced.
GIA2 CONFIG – GIA2 config error. The GIA2 configuration settings do not match
Config service req’d.
backup configuration memory. The G1000
system should be serviced.
GIA2 COOLING – GIA2 over
The GIA2 temperature is too high. If problem
temperature.
persists, the G1000 system should be serviced.
GIA2 COOLING – GIA2
The GIA2 temperature is too low to operate
temperature too low.
correctly. Allow units to warm up to operating
temperature.
GIA2 MANIFEST – GIA2 software The GIA 2 has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
GIA2 SERVICE – GIA2 needs
The GIA2 self-test has detected a problem in the
service. Return the unit for repair. unit. The G1000 system should be serviced.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data
has occurred.
between the two GMAs. The G1000 system
should be serviced.
GMA1 CONFIG – GMA1
The audio panel configuration settings do not
configuration error. Config service match backup configuration memory. The
req’d.
G1000 system should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The G1000
system should be serviced.
GMA1 MANIFEST – GMA1 software The audio panel has incorrect software installed. The
G1000 system should be serviced.
mismatch. Communication halted.
The audio panel self-test has detected a problem in
GMA1 SERVICE – GMA1 needs
the unit. Certain audio functions may still be availservice. Return unit for repair.
able, and the audio panel may still be usable. The
G1000 system should be serviced when possible.
GMA2 CONFIG – GMA2
The audio panel configuration settings do not
configuration error. Config service match backup configuration memory. The
req’d.
G1000 system should be serviced.
GMA2 FAIL – GMA2 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The G1000
system should be serviced.
GMA2 MANIFEST – GMA2 software The audio panel has incorrect software installed. The
G1000 system should be serviced.
mismatch. Communication halted.
The audio panel self-test has detected a problem in
GMA2 SERVICE – GMA2 needs
the unit. Certain audio functions may still be availservice. Return unit for repair.
able, and the audio panel may still be usable. The
G1000 system should be serviced when possible.
GMC CNFG – GMC Config error.
Error in the configuration of the GMC 710.
Config service req’d.
GMC FAIL – GMC is inoperative.
A failure has been detected in the GMC 710.
The GMC 710 is unavailable.
GMC KEYSTK – GMC [keyname]
A key is stuck on the GCMC 710 bezel. Attempt
Key is stuck
to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.
GMC MANIFEST – GMC software The GMC 710 has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
118
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Annunciations & Alerts
Annun/Alerts
Appendix
The #1 AHRS has incorrect software installed.
The G1000 system should be serviced.
The #2 AHRS has incorrect software installed.
The G1000 system should be serviced.
Additional
Features
A failure has been detected in the GRA. The
system should be serviced.
The GRA temperature is too high. If the problem
persists, the system should be serviced.
Hazard
Avoidance
GRS1 MANIFEST – GRS1 software
mismatch, communication halted.
GRS2 MANIFEST – GRS2 software
mismatch, communication halted.
The GRA has incorrect software installed. The
system should be serviced.
Procedures
GRA1 MANIFEST – GRA1
software mismatch, communication
halted.
GRA1 SERVICE – GRA1 needs
service. Return unit for repair.
GRA1 TEMP – GRA1 over
temperature.
Flight
Planning
GRA1 CAL – GRA1 calibration
error. Service req’d.
GRA1 CONFIG – GRA1 config
error. Config service req’d.
GPS Nav
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
A failure has been detected in GPS receiver #1.
The system should be serviced.
A failure has been detected in the GPS1 receiver.
The receiver may still be available. The G1000
system should be serviced.
A failure has been detected in GPS receiver #2.
The system should be serviced.
A failure has been detected in the GPS2 receiver.
The receiver may still be available. The G1000
system should be serviced.
A calibration error has been detected in the GRA.
The system should be serviced.
The GRA configuration settings do not match
those of backup configuration memory. The
system should be serviced.
AFCS
GPS2 FAIL – GPS2 is inoperative.
Loss of GPS navigation due to position error.
Nav/Com/
XPDR/Audio
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
Comments
Loss of GPS navigation due to insufficient
satellites.
Flight
Instruments
Message
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS1 FAIL – GPS1 is inoperative.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
119
Message
GSD1 CONFIG – GSD1 config
error. Config service req’d.
GSD1 COOLING – GSD1
temperature too low.
GSD1 MANIFEST – GSD1 software
mismatch. Communication halted.
GSD1 SERVICE – GSD1 needs
service. Return unit for repair.
GSR1 FAIL – GSR1 has failed.
Comments
GSD1 and the CDU have different copies of the
GSD1 configuration.
GSD1 is reporting a low temperature condition.
GSD1 has incorrect software installed. The
system should be serviced.
GSD1 is reporting an internal error condition.
The GSD may still be usable.
A failure has been detected in the #1 GSR 56.
The system should be serviced.
GTS CONFIG – GTS Config error.
The GTS and GDU have different copies of the
Config service req'd.
GTS configuration, or the Mode S address is
invalid. The G1000 system should be serviced.
GTS MANIFEST – GTS software
The GTS has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
GTX1 MANIFEST – GTX1 software The transponder has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
GTX2 MANIFEST – GTX2 software The transponder has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
GWX CONFIG – GWX config error. GWX 68/70 configuration settings do not match
Config service req’d.
those of the GDU configuration. The G1000
system should be serviced.
GWX FAIL – GWX is inoperative.
The GDU is not recieving status packet from the
GWX 68/70 or the GWX 68/70 is reporting a
fault. The GWX 68/70 radar system should be
serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
120
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190-00929-05 Rev. B
Annunciations & Alerts
HDG FAULT – AHRS2
magnetometer fault has occurred.
Hazard
Avoidance
Additional
Features
LOCKED FPL – Cannot navigate
locked flight plan.
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan.
Update flight plan with current waypoint.
GPS integrity is insufficient for the current phase
of flight.
Appendix
The aircraft is inside the special use airspace.
Annun/Alerts
INSIDE ARSPC – Inside airspace.
LOI – GPS integrity lost.
Crosscheck with other NAVS.
Procedures
A GIA mismatch has been detected, where only
one is SBAS capable. The G1000 system should
be serviced.
Flight
Planning
HOLD EXPIRED – Holding EFC
time expired.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
GPS Nav
A fault has occurred in the #1 GMU 44. Heading
is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
A fault has occurred in the #2 GMU 44. Heading
is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
Expect Further Clearance (EFC) time has expired
for the User Defined Hold.
AFCS
HDG FAULT – AHRS1
magnetometer fault has occurred.
Nav/Com/
XPDR/Audio
Comments
The GWX 68/70 has incorrect software installed.
The G1000 system should be serviced.
A failure has been detected in the GWX 68/70.
The GWX 68/70 may still be usable.
Flight
Instruments
Message
GWX MANIFEST – GWX software
mismatch, communication halted.
GWX SERVICE – Needs service.
Return unit for repair.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
121
Message
MAG VAR – Large magnetic
variance. Verify all course angles.
MANIFEST – GDC1 software
mismatch, communication halted.
MANIFEST – GDC2 software
mismatch, communication halted.
MANIFEST – GEA1 software
mismatch, communication halted.
MANIFEST – GEA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
MANIFEST – GMU1 software
mismatch, communication halted.
MANIFEST – GMU2 software
mismatch, communication halted.
MANIFEST – MFD1 software
mismatch. Communication halted.
MANIFEST – PFD1 software
mismatch. Communication halted.
MANIFEST – PFD2 software
mismatch. Communication halted.
MFD1 CONFIG – MFD1
configuration error. Config service
req’d.
Comments
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°.
The GDC 74B has incorrect software installed.
The G1000 system should be serviced.
The #1 GEA 71 has incorrect software installed.
The G1000 system should be serviced.
The #2 GEA 71 has incorrect software installed.
The G1000 system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
The GMU 44 has incorrect software installed.
The G1000 system should be serviced.
The MFD has incorrect software installed. The
G1000 system should be serviced.
The PFD has incorrect software installed. The
G1000 system should be serviced.
The MFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
122
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190-00929-05 Rev. B
Annunciations & Alerts
Flight
Instruments
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Message
Comments
MFD1 COOLING – MFD1 has poor The MFD is overheating and is reducing power
cooling. Reducing power usage.
consumption by dimming the display. If
problem persists, the G1000 system should be
serviced.
MFD1 DB ERR – MFD1 Airport
The MFD detected a failure in the Airport
Directory database error exists.
Directory database. Ensure the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
MFD1 DB ERR – MFD1 airport
The MFD detected a failure in the airport terrain
terrain database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
MFD1 DB ERR – MFD1 airport
The airport terrain database is present on
terrain database missing.
another LRU, but is missing on the specified LRU.
Ensure that the terrain card is properly inserted
in the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
MFD1 DB ERR – MFD1 basemap The MFD detected a failure in the basemap
database error exists.
database. The G1000 system should be serviced.
MFD1 DB ERR – MFD1 Chartview The MFD detected a failure in the Chartview
database error exists.
database (optional feature). Ensure that the
data card is properly inserted. Replace data
card. If problem persists, the G1000 system
should be serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD detected a failure in the FliteCharts
database error exists.
database (optional feature). Ensure that the
data card is properly inserted. Replace data
card. If problem persists, the G1000 system
should be serviced.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
123
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
Comments
MFD1 DB ERR – MFD1 navigation The MFD detected a failure in the navigation
database error exists.
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
MFD1 DB ERR – MFD1 obstacle
The MFD detected a failure in the obstacle
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
MFD1 DB ERR – MFD1 obstacle
The obstacle database is present on another
database missing.
LRU, but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
MFD1 DB ERR – MFD1 Safe Taxi
The MFD detected a failure in the Safe Taxi
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
MFD1 DB ERR – MFD1 terrain
The MFD detected a failure in the terrain
database error exists.
database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, the G1000 system should be
serviced.
MFD1 DB ERR – MFD1 terrain
The terrain database is present on another LRU,
database missing.
but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
MFD1 KEYSTK – MFD1 [key name] A key is stuck on the MFD bezel. Attempt to free
Key is stuck
the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
124
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Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage.
Comments
The MFD self-test has detected a problem. The
G1000 system should be serviced.
The specified GDU has different software
versions installed. The system should be
serviced.
The MFD voltage is low. The G1000 system
should be serviced.
Flight
Instruments
Message
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MFD1 SOFTWARE – MFD1
mismatch, communication halted.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
System has updated the active navigation
database from the standby navigation database.
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 G1000 system should
be serviced.
NAV1 SERVICE – NAV1 needs
A failure has been detected in the NAV1 receiver.
service. Return unit for repair.
The receiver may still be available. The G1000
system should be serviced.
NAV2 MANIFEST – NAV2 software NAV2 software mismatch. The system should be
mismatch, communication halted. 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 G1000 system should
be serviced.
NAV2 SERVICE – NAV2 needs
A failure has been detected in the NAV2 receiver.
service. Return unit for repair.
The receiver may still be available. The G1000
system should be serviced.
GPS Nav
NAV DB UPDATED – Active
navigation database updated.
NAV1 MANIFEST – NAV1 software
mismatch, communication halted.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
125
Message
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
Comments
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to the
selected non-WGS84 waypoint.
PFD1 CONFIG – PFD1
configuration error. Config service
req’d.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
The PFD is overheating and is reducing power
consumption by dimming the display. If
problem persists, the G1000 system should be
serviced.
The PFD detected a failure in the airport terrain
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
Ensure that the terrain card is properly inserted
in the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
The PFD detected a failure in the basemap
database. The G1000 system should be serviced.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
The PFD detected a failure in the obstacle
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 basemap
database error exists.
PFD1 DB ERR – PFD1
navigation database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
126
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190-00929-05 Rev. B
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Comments
The obstacle database is present on another
LRU, but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
PFD1 DB ERR – PFD1 Safe Taxi
The PFD detected a failure in the Safe Taxi
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
PFD1 DB ERR – PFD1 terrain
The PFD detected a failure in the terrain
database error exists.
database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, the G1000 system should be
serviced.
PFD1 DB ERR – PFD1 terrain
The terrain database is present on another LRU,
database missing.
but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
PFD1 KEYSTK – PFD1 [key name] A key is stuck on the PFD bezel. Attempt to free
Key is stuck.
the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
[PFD1, PFD2, or MFD1] BKLT CAL The PFD1, PFD2 and/or MFD backlight
INV – calibration lost or mismatch. calibration cannot be found or is invalid. The
Return for repair.
system should be serviced.
[PFD1, PFD2, or MFD1] CARD 1
The SD card in the top card slot of the specified
ERR – Card 1 is invalid.
PFD or MFD contains invalid data.
[PFD1, PFD2, or MFD1] CARD 2
The SD card in the bottom card slot of the
ERR – Card 2 is invalid.
specified PFD or MFD contains invalid data.
Flight
Instruments
Message
PFD1 DB ERR – PFD1 obstacle
database missing.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
127
Message
[PFD1, PFD2, or MFD1] CARD
1 REM – Card 1 was removed.
Reinsert card.
[PFD1, PFD2, or MFD1] CARD
2 REM – Card 2 was removed.
Reinsert card.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD1 SOFTWARE – PFD1
mismatch, communication halted.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage.
PFD2 CONFIG – PFD2
configuration error. Config service
req’d.
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
PFD2 DB ERR – PFD2 airport
terrain database error exists.
PFD2 DB ERR – PFD2 airport
terrain database missing.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
PFD2 DB ERR – PFD2 basemap
database error exists.
128
Comments
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 PFD1 self-test has detected a problem. The
G1000 system should be serviced.
The specified GDU has different software
versions installed. The system should be
serviced.
The PFD1 voltage is low. The G1000 system
should be serviced.
The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
The PFD is overheating and is reducing power
consumption by dimming the display. If
problem persists, the G1000 system should be
serviced.
The PFD detected a failure in the airport terrain
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
Ensure that the terrain card is properly inserted
in the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
The PFD detected a failure in the basemap
database. The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
AFCS
PFD2 DB ERR – PFD2 obstacle
database missing.
Nav/Com/
XPDR/Audio
PFD2 DB ERR – PFD2 obstacle
database error exists.
Comments
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
The PFD detected a failure in the obstacle
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the G1000 system should be serviced.
The obstacle database is present on another
LRU, but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
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 G1000 system should be serviced.
Flight
Instruments
Message
PFD2 DB ERR – PFD2
navigation database error exists.
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
129
Message
PFD2 DB ERR – PFD2 terrain
database error exists.
PFD2 DB ERR – PFD2 terrain
database missing.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
PFD2 KEYSTK – PFD2 [key name]
Key is stuck
PFD2 SERVICE – PFD2 needs
service. Return unit for repair.
PFD2 SOFTWARE – PFD2
mismatch, communication halted.
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage.
PTK FAIL – Parallel track
unavailable: bad geometry.
PTK FAIL – Parallel track
unavailable: invalid leg type.
PTK FAIL – Parallel track
unavailable: past IAF.
Comments
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 G1000 system should be
serviced.
The terrain database is present on another LRU,
but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
A key is stuck on the PFD bezel. Attempt to free
the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
The PFD2 self-test has detected a problem. The
G1000 system should be serviced.
The specified GDU has different software
versions installed. The system should be
serviced.
The PFD2 voltage is low. The G1000 system
should be serviced.
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been passed.
REGISTER CONNEXT – Data
The GDL 59 is not registered with Garmin Flight
services are inoperative, register w/ Data Services, or its current registration data has
CONNEXT.
failed authentication.
130
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Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
131
Procedures
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Flight
Planning
190-00929-05 Rev. B
TAWS is disabled because a terrain database of
sufficient resolution (9 arc-second or better) is
not currently installed.
One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD
or MFD is missing or invalid.
The system notifies the pilot that the timer has
expired.
The system is no longer receiving data from
the traffic system. The traffic device should be
serviced.
GPS Nav
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
TIMER EXPIRD – Timer has
expired.
TRAFFIC FAIL – Traffic device has
failed.
Terrain audio alerts are not configured properly.
The system should be serviced
AFCS
TERRAIN AUD CFG – Trn
Awareness audio config error.
Service req’d.
TERRAIN DISABLED – Terrain
Awareness DB resolution too low.
Nav/Com/
XPDR/Audio
Comments
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.
SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to the
approach.
correct NAV receiver. Set the CDI to the correct
NAV receiver.
STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to
turn.
STRMSCP FAIL – Stormscope has Stormscope has failed. The G1000 system
failed.
should be serviced.
SVT – SVT DISABLED: Out of
Synthetic Vision is disabled because the aircraft
available terrain region.
is not within the boundaries of the installed
terrain database.
SVT – SVT DISABLED: Terrain DB
Synthetic Vision is disabled because a terrain
resolution too low.
database of sufficient resolution (9 arc-second or
better) is not currently installed.
Flight
Instruments
Message
SCHEDULER [#] – <message>.
SLCT FREQ – Select appropriate
frequency for approach.
Message
TRN AUD FAIL – Trn Awareness
audio source unavailable.
TRUE APR – True north approach.
Change HDG reference to TRUE.
Comments
The audio source for terrain awareness is offline.
Check GIA1 or GIA 2.
Displayed after passing the first waypoint of a
true north approach when the nav angle is set to
‘AUTO’.
UNABLE RNP – Estimated
position error exceeds RNP.
UNABLE RNP APR – GPS
integerity lost. Check GPS sensors.
The estimated GPS position error exceeds the
RNP limits. Check GPS sensors.
The estimated GPS position error exceeds the
requirements for the current approach. Check
GPS sensor
The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.
User magnetic variation mode was selected
during previous operation and is still active
(checked at power-up.)
UNABLE V WPT – Can’t reach
current vertical waypoint.
USER MAG VAR – User magnetic
variation is active.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Excessive
track angle error.
VNV – Unavailable. Parallel course
selected.
VNV – Unavailable. Unsupported
leg type in flight plan.
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
A parallel course has been selected, causing the
vertical deviation to go invalid.
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
132
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when possible.
XPDR1 CONFIG – XPDR1 config
The transponder configuration settings do not
error. Config service req’d.
match those of backup configuration memory. The
G1000 system should be serviced.
XPDR1 CONFIG – XPDR1 config
The transponder configuration settings do not
error. Config service req’d.
match those of backup configuration memory. The
G1000 system should be serviced.
XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1 or #2
transponder.
XPDR1 SRVC – XPDR1 needs
The #1 transponder should be serviced when
service. Return unit for repair.
possible.
XPDR2 ADS-B FAIL – XPDR2 is
ADS-B is inoperative. The transponder may not be
unable to transmit ADS-B messages. receiving a valid GPS position. Other transponder
functions may be available. Service when possible.
XPDR2 CONFIG – XPDR2 config
The transponder configuration settings do not
error. Config service req’d.
match those of backup configuration memory. The
G1000 system should be serviced.
XPDR2 FAIL – XPDR2 is inoperative. There is no communication with the #2
transponder.
XPDR2 SRVC – XPDR2 needs
The #2 transponder should be serviced when
service. Return unit for repair.
possible.
XTALK ERROR – A flight display
The MFD and PFD are not communicating with
crosstalk error has occurred.
each other. The G1000 system should be serviced.
AFCS
XPDR1 ADS-B FAIL – XPDR1 is
unable to transmit ADS-B messages.
Nav/Com/
XPDR/Audio
Comments
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
The GWX 68/70 indicates severe weather within
±10 degrees of the aircraft heading at a range
of 80 to 320 nm.
Flight
Instruments
Message
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
WX ALERT – Possible severe
weather ahead.
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
133
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
‘Flight plan successfully imported.’
Description
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints only. User The file stored on the SD card did not contain a flight plan,
waypoints imported successfully. No
only user waypoints. These waypoints have been saved to the
stored flight plan data was modified.’
system user waypoints. No flight plans stored in the system
have been modified.
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported from the SD
card.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported
from the SD card, however others had errors and were not
imported. A partial stored flight plan now exists in the
system.
‘File contained user waypoints only.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
‘Too many points. Flight plan truncated.’ The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.
‘Some waypoints not loaded. Waypoints
locked.’
The flight plan on the SD card contains one or more
waypoints that the system cannot find in the navigation
database. The flight plan has been imported, but must be
edited within the system before it can be activated for use.
‘User waypoint database full. Not all
loaded.’
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD
card have been imported. Any flight plan user waypoints
that were not imported are locked in the flight plan. The
flight plan must be edited within the system before it can be
activated for use.
‘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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
134
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190-00929-05 Rev. B
Annunciations & Alerts
Description
Flight
Instruments
Flight Plan Import/Export
Results
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.
AFCS
PILOT PROFILE IMPORT/EXPORT MESSAGES
Pilot Profile Import/Export Results
Nav/Com/
XPDR/Audio
‘Flight plan successfully exported.’
Description
GPS Nav
Displayed if the SD card does not have one or
more valid pilot profile filenames.
‘Overwrite existing profile?’
Displayed if the profile name matches the name
of existing profile.
‘Profile name invalid. Enter a different profile
name.’
Displayed if the profile name is invalid.
‘All available pilot profiles in use. Delete a
profile before importing another.’
Displayed if the maximum number for pilot
profiles has been reached.
‘Pilot profile import failed.’
Displayed if the importing operation fails for any
other reason.
‘Pilot profile import succeeded.’
Displayed if the importing operation succeeds.
‘Overwrite existing file?’
Displayed if the filename matches the name of an
existing file on the SD card.
‘Pilot profile export failed.’
Displayed if the export operation fails.
‘Pilot profile export succeeded.’
Displayed if the export operation succeeds.
Flight
Planning
‘No pilot profile plan files found to import.’
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
135
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Blank Page
136
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
Nav/Com/
XPDR/Audio
ALERTS
AFCS
GPS Nav
Top Level PFD Softkeys
(optional)
(optional)
(optional)
WX LGND
(optional)
ALERTS
(optional)
(optional)
PRECIP
or
DL LTNG
(optional)
or
METAR
STRMSCP
Select the BACK Softkey
to return to the top-level softkeys.
TRFC-2
Level 2
INSET or
TRFC/MAP
Appendix
OFF
Description
Pressing the INSET Softkey Displays Inset Map
in the PFD lower left corner. The TRFC/MAP
Softkey is displayed when the TCAS II option
is installed. Pressing the TRFC/MAP Softkey
displays the Inset Map showing Traffic Map Page.
Removes Inset Map
Annun/Alerts
Level 1
Additional
Features
Inset Map Softkeys
Hazard
Avoidance
TRFC-1
ALERTS
Procedures
(optional)
XPDR/TRC
or
Flight
Planning
TRFC/MAP
or
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
137
Level 1
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Level 2
Description
Selects desired amount of map detail; cycles
DCLTR
through declutter levels:
(3)
DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the active
flight plan
WX LGND Displays icon and age on the Inset Map for the
selected weather products (optional)
TRAFFIC Displays traffic information on Inset Map
Displays topographical data (e.g., coastlines,
TOPO
terrain, rivers, lakes) and elevation scale on Inset
Map
TERRAIN Displays terrain information on Inset Map
STRMSCP Press to display the Stormscope lightning data
on the Inset Map (within a 200 nm radius of the
aircraft)
Displays NEXRAD weather and coverage
NEXRAD
information on Inset Map (optional)
or
PRECIP
Additional
Features
XM LTNG
or
Annun/Alerts
DL LTNG
Displays Worldwide Weather lightning
information on Inset Map (optional)
Displays METAR flags on airport symbols shown on
the Inset Map (optional)
Index
Appendix
METAR
Displays Worldwide Weather precipitation on
Inset Map (optional)
Displays XM lightning information on Inset Map
(optional)
138
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Appendix
AHRS1
BACK
AHRS2
ALERTS
Select the BACK Softkey to
return to the top level softkeys.
Level 1
Level 2
AFCS
Sensor Softkeys
Description
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Flight
Planning
ADC2
GPS Nav
ADC1
Displays softkeys for selecting the #1 and #2 AHRS
and Air Data Computers
Selects the #1 Air Data Computer
SENSOR
Nav/Com/
XPDR/Audio
ADC2
ADC1
Flight
Instruments
ALERTS
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
139
Flight
Instruments
Appendix
DME
SYN VIS
ALERTS
HDG MODE ALT UNIT
Nav/Com/
XPDR/Audio
HSI FMT
ALERTS
GPS Nav
AFCS
Select the BACK Softkey
to return to the top-level softkeys
DG FREE DG SLAVE
HDG +
360 HSI
ARC HSI
HDG -
HDG SYNC
Flight
Planning
METERS
TRK SYNC
IN
HPA
BACK
ALERTS
BACK
ALERTS
ALERTS
PATHWAY
SYN TERR HRZN HDG APTSIGNS
ALERTS
PFD Configuration Softkeys
Level 1
Level 2
Level 3
PFD
SYN VIS
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
ALERTS
PATHWAY
Appendix
SYN TERR
Description
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
Index
HRZN HDG Displays compass heading along the
Zero-Pitch line
140
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Appendix
Level 2
Level 3
APTSIGNS
OPTN 2
OFF
BRG2
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
141
Index
DG SLAVE
Appendix
DG FREE
Annun/Alerts
HDG
MODE
Additional
Features
360 HSI
ARC HSI
Hazard
Avoidance
HSI FRMT
Procedures
DME
BRG1
Flight
Planning
OPTN 3
GPS Nav
OPTN 1
AFCS
WIND
Nav/Com/
XPDR/Audio
DFLTS
Description
Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings, including
changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrow and speed
Wind direction arrow with digital
direction and speed
Longitudinal and lateral components
Information not displayed
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information, and ADF/
frequency.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information, and ADF/
frequency.
Displays softkeys to select DG Modes
(GRS 7800 installations only)
Allows the DG to enter FREE mode.
Slaves the DG to the AHRS.
Flight
Instruments
Level 1
Level 1
Level 2
Level 3
HDG HDG +
HDG SYNC
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
AFCS
TRK SYNC
GPS Nav
ALT UNIT
METERS
Flight
Planning
IN
Procedures
HPA
STD BARO
Description
Slews heading counterclockwise.
Slews heading clockwise.
Synchronizes heading to the selected
heading.
Synchronizes heading to the current
track.
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
Press to display the BARO setting as
hectopacals
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
Hazard
Avoidance
ALERTS
Additional
Features
ALERTS
Annun/Alerts
Select the BACK Softkey to return
to the top-level softkeys.
ALERTS
Appendix
Select the BACK Softkey to return
to the previous level softkeys.
Index
Transponder Softkeys
142
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Appendix
Level 2
XPDR
XPDR2
STBY
Flight
Planning
Procedures
Hazard
Avoidance
143
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
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 (if equipped).
Automatically enters the VFR code (1200 in
the U.S.A. only)
Annun/Alerts
190-00929-05 Rev. B
Additional
Features
White (On-Ground) - Transponder does
not allow Mode A or Mode C replies
to interrogations, , but it does permit
acquisition and extended squitters
including ADS-B out (if equipped), and
replies to discretely addressed Mode S
interrogations.
VFR
GPS Nav
ALT
Green (Airborne) - Transponder generates
Mode A and Mode S replies, as well as
transmission of acquisition and extended
squitters, including ADS-B out (if
equipped).
Selects Altitude Mode (selection is usually
automatic)
AFCS
ON
Description
Displays transponder mode selection
softkeys
Selects the #1 transponder as active
Selects the #2 transponder as active
Selects Standby Mode (transponder does
not reply to any interrogations)
White (On-Ground) - Transponder
generates Mode A and Mode S replies, as
well as transmission of acquisition and
extended squitters, including ADS-B out (if
equipped).
Nav/Com/
XPDR/Audio
XPDR1
Level 3
Flight
Instruments
Level 1
Level 1
Level 2
Level 3
Description
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
Removes numbers entered, one at a time
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
Displays Nearest Airports Window
Displays Alerts Window
CODE
0—7
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
BKSP
AFCS
IDENT
NRST
ALERTS
Flight
Planning
GPS Nav
TMR/REF
TRFC/MAP SENSOR
PFD
OBS
CDI
(optional)
DME
XPDR/TFC
IDENT
TMR/REF
NRST
ALERTS
Procedures
Press the BACK Softkey to return
to the top-level softkeys.
MODE
TCAS
CODE
BACK
IDENT
ALERTS
Hazard
Avoidance
Selecting BACK returns to the
previous softkey level.
REL
ABS
ALT RNG
TEST
BACK
ALERTS
Selecting BACK returns to the
previous softkey level.
Additional
Features
ABOVE
NORMAL BELOW
UNREST
BACK
ALERTS
Selecting BACK returns to the
previous softkey level.
Annun/Alerts
STBY
ON
ALT
TA ONLY
BACK
TA/RA
ALERTS
Selecting BACK returns to the
previous softkey level.
Appendix
0
1
2
3
4
5
6
7
IDENT
BKSP
BACK
ALERTS
Index
Transponder/Traffic Softkeys with TCAS II Option
144
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Appendix
Level 2
Level 3
XPDR2
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Green (Airborne) Transponder generates Mode A
and Mode S replies, as well as
transmission of acquisition and
extended squitters, including
ADS-B out (if equipped).
Flight
Planning
ON
GPS Nav
STBY
AFCS
MODE
Description
Displays the transponder and
TCAS II selection softkeys
Selects the #1 transponder as
active
Selects the #2 transponder as
active
Displays transponder mode
selection softkeys
Selects transponder Standby
Mode (transponder does not
reply to any interrogations).
When the transponder is set to
standby, the TCAS II system is
also set to standby.
White (On-Ground) Transponder generates Mode A
and Mode S replies, as well as
transmission of acquisition and
extended squitters, including
ADS-B out (if equipped).
Nav/Com/
XPDR/Audio
XPDR1
Level 4
Flight
Instruments
Level 1
XPDR/TFC
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
145
Level 1
Level 2
Level 3
ALT
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Level 4
Description
Selects Altitude Mode
(selection is usually automatic)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
White (On-Ground) Transponder does not allow
Mode A or Mode C replies
to interrogations, , but it
does permit acquisition and
extended squitters including
ADS-B out (if equipped), and
replies to discretely addressed
Mode S interrogations.
Additional
Features
TA ONLY
Annun/Alerts
TA/RA
BACK
Appendix
REL
Index
TCAS
ABS
146
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 (if
equipped).
Activates the TCAS II system
in TA Only Mode and set the
transponder to ALT
Activates the TCAS II system
in TA/RA Mode and sets the
transponder to ALT
Returns to the previous softkey
level
Displays the TCAS control
softkeys
Displays intruder altitude as
altitude relative to own aircraft
altitude
Displays intruder MSL altitude
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Appendix
Level 2
Level 3 Level 4
ALT RNG
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
BKSP
Procedures
IDENT
Flight
Planning
0—7
GPS Nav
CODE
AFCS
BACK
Nav/Com/
XPDR/Audio
TEST
Description
Displays the altitude display
range softkeys
Displays non-threat traffic from
ABOVE
9900 feet above the aircraft to
2700 feet below the aircraft.
Typically used during climb
phase of flight.
NORMAL Displays non-threat traffic from
2700 feet above the aircraft to
2700 feet below the aircraft.
Typically used during enroute
phase of flight.
BELOW Displays non-threat traffic from
2700 feet above the aircraft to
9900 feet below the aircraft.
Typically used during descent
phase of flight.
UNREST All traffic is displayed
Activates Test Mode and
displays test intruder symbols
Returns to the previous softkey
level
Displays transponder code
selection softkeys 0-7
Use numbers to enter code
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
Flight
Instruments
Level 1
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
147
Level 1
IDENT
Level 2
Level 3
Level 4
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
NRST
ALERTS
MFD NAVIGATION PAGE SOFTKEY MAP
(optional)
DCLTR
MAP
SHW CHRT
CHKLIST
DCLTR-1
Procedures
Flight
Planning
GPS Nav
AFCS
TMR/REF
Description
Activates the Special Position
Identification (SPI) pulse for
18 seconds, identifying the
transponder return on the ATC
screen
Displays Timer/References
Window
Displays Nearest Airports
Window
Displays Alerts Window
DCLTR-2
Hazard
Avoidance
DCLTR-3
TRAFFIC
PROFILE
TOPO
(optional)
TERRAIN
AIRWAYS
(optional)
STRMSCP
(optional)
(optional)
PRECIP
or
NEXRAD
DL LTNG
or
XM LTNG
Select the BACK Softkey
on this level to return to the
top softkey level.
(optional)
(optional)
METAR
LEGEND
BACK
Additional
Features
AIRWY ON
AIRWY LO
Appendix
Annun/Alerts
AIRWAY HI
MFD Softkeys
Level 1
Level 2
MAP
Index
TRAFFIC
Description
Enables second-level Navigation Map softkeys
Displays traffic information on Navigation Map
148
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Index
Displays Connext precipitation on the Navigation
Map (optional)
XM LTNG Displays XM lightning information on the
Navigation Map (optional)
or
Procedures
Level 2
Additional
Features
Annun/Alerts
BACK
Hazard
Avoidance
LEGEND
Flight
Planning
METAR
Displays Connext lightning information on the
Navigation Map (optional)
Displays METAR flags on airport symbols shown on
the Navigation Map (optional)
Displays the legend for the selected weather
products. Available only when NEXRAD, XM
LTNG, and/or METAR softkeys are selected.
Returns to top-level softkeys
GPS Nav
DL LTNG
AFCS
PRECIP
Nav/Com/
XPDR/Audio
Description
Displays topographical data (e.g., coastlines, terrain,
TOPO
rivers, lakes) and elevation scale on Navigation Map
TERRAIN Displays terrain information on Navigation Map
AIRWAYS Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed
STRMSCP Displays Stormscope weather and coverage
information on Navigation Map (optional feature)
NEXRAD Displays NEXRAD weather and coverage
information on the Navigation Map (optional)
or
Flight
Instruments
Level 1
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
149
Level 1
DCLTR (3)
SHW
CHRT
CHKLIST
Description
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the active
flight plan
When available, displays optional airport and
terminal procedure charts
When available, displays optional checklists
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
Annun/Alerts
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
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.
Index
Appendix
Level 2
LOADING UPDATED DATABASES
Database information is obtained from third party sources. Inaccuracies in the data
may be discovered from time to time. Garmin communicates this information by issuing a Database Alert. These notifications are available on http://fly.garmin.com.
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 http://fly.garmin.com
and select “Aviation Data Error Report”.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
150
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Appendix
AFCS
GPS Nav
Flight
Planning
With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
2)
Update the Garmin databases on the MFD card.
3)
Insert the MFD database card into the bottom card slot of the MFD.
4)
Apply power to the system, check that the databases are initialized
and displayed on the power-up screen. When updating the terrain and
FliteCharts databases, a ‘Verifying’ message may be seen. If this message is
present, wait for the system to finish loading before proceeding to step 5.
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete syncing, indicated by ‘Complete’ being displayed.
9)
Remove and reapply power to the system.
Hazard
Avoidance
1)
Procedures
Loading Garmin Database Updates
Additional
Features
Annun/Alerts
Appendix
Index
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Nav/Com/
XPDR/Audio
Error Message
Description
Canceled
Database synchronization has been canceled by removing the
bottom SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
190-00929-05 Rev. B
Flight
Instruments
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error
message is displayed, the problem must be corrected before synchronization can be
completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
151
Appendix
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct
database cycle information is shown for each database for each display.
Loading the Jeppesen Navigation Database as the Active Navigation
Database
NOTE: Loading the Jeppesen navigation database as the active database
prior to its effective date will result in the expiration date on the power-up
screen and the effective date on the AUX-System Status Page being displayed
in yellow.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
11) Turn the small FMS Knob to select the System Status Page.
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
1)
With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2)
Turn the system ON. A prompt is displayed in the upper left corner of the
display:
3)
4)
Press the NO Softkey to proceed to loading the active database.
A prompt similar to the following is displayed. Press the YES Softkey to update
the active navigation database.
5)
After the update completes, the display starts in normal mode.
6)
Turn the system OFF and remove the SD card from the top card slot.
7)
Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD).
8)
Apply power to the system and press the ENT Key to acknowledge the startup
screen.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
Appendix
10) Turn the small FMS Knob to select the System Status Page.
Index
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify
the correct active navigation database cycle information is shown for each
display.
152
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190-00929-05 Rev. B
Appendix
Nav/Com/
XPDR/Audio
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Flight
Instruments
Loading the Jeppesen Navigation Database as the Standby Navigation
Database
With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
2)
Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
3)
Turn the system ON. A prompt is displayed.
4)
Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
5)
After the navigation database files are copied to the bottom SD card, press
any key to continue, as instructed.
Again, press any key to continue as instructed on the display.
Flight
Planning
8)
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
Procedures
9)
Press the ENT Key to acknowledge the startup screen.
GPS Nav
7)
AFCS
1)
Hazard
Avoidance
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Appendix
NOTE: During the synchronization process, version differences between
standby navigation databases will exist. This will result in the system
displaying a ‘DB Mismatch’ alert for the standby navigation databases. This
alert will remain until the next power cycle.
Annun/Alerts
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
Additional
Features
11) Turn the small FMS Knob to select the System Status Page.
13) Turn system power OFF.
Index
14) Remove the SD card from the top card slot of the MFD.
15) Turn system power ON.
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
153
Appendix
Flight
Instruments
16) Press the ENT Key to acknowledge the startup screen.
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
18) Turn the small FMS Knob to select the System Status Page.
Magnetic Field Variation Database Update
At startup, the system compares this version of the MV DB with that presently being
used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs
to be updated, a prompt is displayed on the Navigation Map Page, as shown in the
following figure. Note, in the following example, GRS1 is the first AHRS to indicate
an update is available. In actuality, this is dependent on which AHRS is the first to
report status to the system. GRS2 may be displayed before GRS1. The order is not
important, only that both AHRS be updated.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
19) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Verify the correct standby navigation database cycle information is shown
for each display.
GRS1 Magnetic Field Variation Database Update Prompt
Index
Appendix
Annun/Alerts
Additional
Features
Loading the magnetic field variation database update:
1) With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key on the
MFD. A progress monitor is displayed as shown in the following figure.
154
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Appendix
Flight
Instruments
Nav/Com/
XPDR/Audio
AFCS
Uploading Database to GRS1
GPS Nav
2)
When the upload is complete, the prompt for the next GRS upload is
displayed, as seen in the following figure.
Flight
Planning
Procedures
GRS2 Magnetic Field Variation Database Update Prompt
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed as shown in the following figure. When the upload is complete,
the system is ready for use.
Hazard
Avoidance
3)
Additional
Features
Annun/Alerts
Appendix
Uploading Database to GRS2
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
155
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Blank Page
156
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Index
F
FD 99
Flight Director 9
Flight path marker 69
FliteCharts® 70, 71
Frequency Transfer 6
Hazard
Avoidance
G
Additional
Features
Gain 59
H
Annun/Alerts
HF 5
Horizon heading 69
Horizontal scan 59
I
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index-1
Index
Inhibit 68
Inhibit TAWS 68
Inset Map 137, 138
IOI 100, 101, 104
Iridium satellite network 73, 74, 78
Appendix
190-00929-05 Rev. B
Edit a flight plan 32
ESP 94, 95
Procedures
CDI 1, 2, 6, 131
Cell 42, 43
Cell mode 43
Channel Presets 90
E
Flight
Planning
C
DB Mismatch 150, 153
DCLTR Softkey 70
Declutter 138, 150
DG Mode 2
Direct-to 13
DME 5, 6
GPS Nav
Barometric Altitude Minimums 4
Barometric pressure 142
Bearing line 59, 60
D
AFCS
B
Nav/Com/
XPDR/Audio
Access code 46, 74
Activate a flight plan 14
Active Channel 89
Active database 152
Active Navigation Database 152
AC-U-KWIK 72
ADF 5, 6, 141
Advisory alerts 97
AHRS 108, 109, 110, 115, 116, 118,
121
Air Data Computer 98
Airport Directory 72
Airport Signs 69, 70
Airways 149
ALT 63
Altitude mode 63
Altitude volume 63
Antenna stabilization 60
Antenna tilt 58
AOPA 72
AOPA’s Airport Directory 72
AP 99
Attitude & Heading Reference System
98
Audio panel controls
NAV1, NAV2 6
ChartView 70, 71
CLD TOP Softkey 54
Code selection softkeys 5
COM 5, 6
Flight
Instruments
A
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
J
R
Jeppesen 71
RADIO softkey 89
Register 47, 74
Resolution Advisory 61
ROC 100, 104
L
Level Mode 94
Lightning 42, 43, 44, 138
Low speed data 73, 74
M
Map panning 44
Message advisories 107
MET 99
METAR 43
Minimums 106
MISCOMP 98
Mistrim 99
Mode selection softkeys 5
Multi Function Display (MFD)
Softkeys 148
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
N
NAV 6
NAV1 2, 6
NAV2 6
Navigation database 15, 17, 134
NEXRAD 43, 138, 149
NEXRAD Softkey 53
O
OBS 2
Obstacles 113, 121
Overspeed Protection 10
P
Pathways 69, 70
PIREP 57
PIT 98
Predefined message 81, 82
Index-2
S
SafeTaxi® 70
SBAS 10, 36, 68
Sector scan 60
Sensor 98
STAB 60
Standby 58
Standby Navigation Database 153
Store Flight Plan 32
Stormscope lightning data 41, 42, 43,
138
Strike 42
Strike mode 43
SVT 69
SVT Terrain 69
Synchronization 151
SYNC Status 153
Synthetic vision (SVS) 131
Synthetic Vision System 69
System ID 46, 73
T
TAF 43, 55
TAS 62, 63, 109, 110
TAWS 65, 66, 67, 68, 100, 101, 102,
103, 105
TAWS-B 65, 67
TCAS II 62, 63, 64, 137, 144, 145, 146
TCAS II System Test Fail 107
TCAS II System Test Passed 106
TCAS I System Test Fail 107
TCAS I System Test Passed 106
Telephone 74
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Index
X
Flight
Instruments
XM lightning 138, 149
XM WX weather 44
XPDR Softkey 5
Nav/Com/
XPDR/Audio
AFCS
TEMP COMP 15
Terrain 65, 67, 100, 101, 103, 104,
114, 138, 149
Text messaging 79, 80, 81, 83
Tilt line 58
Topographical data 138, 149
Traffic 41, 62, 64, 138, 148
Traffic Advisory (TA) 62, 106, 107
Traffic map page 62, 63, 64
Transponder 5, 143, 144, 145, 147,
148
GPS Nav
U
User-Defined Holding Pattern 30
Flight
Planning
V
Procedures
vertical path guidance 16
Vertical speed guidance 17
Vertical track 106
VNAV 132
VNV 13
Vspeed 3
Hazard
Avoidance
W
Additional
Features
WAAS 121
WATCH® 60
Waypoint Selection Submenu 26
Weather Attenuated Color Highlight 60
Weather data link page 43
Weather radar 58
Wi-Fi 86, 87, 89
Wind data 141
Winds Aloft 56
WIND Softkey 56
Annun/Alerts
Appendix
Index
190-00929-05 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index-3
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-05 Rev. B
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 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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Salem, OR 97302, U.S.A.
p: 503.581.8101 f: 503.364.2138
Garmin (Europe) Ltd.
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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
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www.garmin.com
© 2011, 2013, 2016 Garmin Ltd. or its subsidiaries
190-00929-05 Rev. B
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