Garmin G1000 Cockpit Reference Guide

®

G1000

Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Integrated Flight Deck

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 © 2007 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0636.00 or later for the Hawker
Beechcraft C90A/GT. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: [phone] Fax: [phone]

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone] Fax [phone]

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express
written permission of Garmin. Garmin hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to
be viewed for personal use, provided that such electronic or printed copy of this manual or revision
must contain the complete text of this copyright notice and provided further that any unauthorized
commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH™,
FliteCharts™, and SafeTaxi™ are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM
Satellite Radio, Inc.

September, 2007 190-00664-00 Rev. A Printed in the U.S.A.

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain
avoidance and is not certified for use in applications requiring a certified
terrain awareness system. 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 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: Traffic information shown on the G1000 Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition of
conflicting traffic.

WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only

for weather avoidance, not penetration.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

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Warnings, Cautions & Notes

WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range

weather avoidance.

WARNING: The Garmin G1000, as installed in the Hawker Beechcraft
C90A/GT 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: For safety reasons, G1000 operational procedures must be learned
on the ground.

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 and GFC 700 AFCS in Hawker Beechcraft
C90A and C90GT King Air Airplane Flight Manual Supplement. 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: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Warnings, Cautions & Notes

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.

WARNING: Because of anomalies in the earth’s magnetic field, operating
the G1000 within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.

CAUTION: The GDU 1040A PFDs and GDU 1500 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 ANTI-REFLECTIVE 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 anti-reflective 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. 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: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Warnings, Cautions & Notes

NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition

65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.

NOTE: 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.

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Warnings, Cautions & Notes

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Part Number Change Summary

190-00664-00 Initial release

Revision Date of Revision Affected Pages Description

A September, 2007 All Production release

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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

Change Navigation Sources ................................................................................................... 2

Enable/Disable OBS Mode While Navigating with GPS .................................................... 2

Generic Timer ............................................................................................................................. 2

Configure Vspeed Bugs Individually ..................................................................................... 2

Turn Vspeed Bugs On or Off by Category ............................................................................ 3

Set Barometric Minimum Descent Altitude ........................................................................ 3

Displaying Wind Data ..............................................................................................................3

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

Digital Clearance Recorder and Player ................................................................................ 6

AUTOMATIC FLIGHT CONTROL SYSTEM ............................................................................ 7

Flight Director Activation ....................................................................................................... 7

Vertical Modes ........................................................................................................................... 8

Lateral Modes ............................................................................................................................ 9

GPS NAVIGATION ........................................................................................................................ 11

Direct-to Navigation .............................................................................................................. 11

Activate a Stored Flight Plan ............................................................................................... 12

Activate a Flight Plan Leg ..................................................................................................... 12

Stop Navigating a Flight Plan .............................................................................................. 13

Vertical Navigation ................................................................................................................. 13

FLIGHT PLANNING ...................................................................................................................... 15

Weight Planning ...................................................................................................................... 15

Trip Planning ............................................................................................................................ 15

Create a New User Waypoint ............................................................................................... 17

Delete a User Waypoint ......................................................................................................... 18

Create a New Flight Plan ...................................................................................................... 18

Insert a Waypoint in the Active Flight Plan ...................................................................... 19

Enter an Airway in a Flight Plan .......................................................................................... 20

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Invert An Active Flight Plan .................................................................................................. 21

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 21

Store a Flight Plan .................................................................................................................. 22

Edit a Stored Flight Plan ....................................................................................................... 22

Delete a Waypoint from the Flight Plan ............................................................................ 22

Invert and Activate a Stored Flight Plan ........................................................................... 23

Copy a Flight Plan ................................................................................................................... 23

Delete a Flight Plan ................................................................................................................ 23

Graphical Flight Plan Creation ............................................................................................. 24

PROCEDURES ................................................................................................................................. 25

Load and Activate a Departure Procedure ....................................................................... 25

Activate A Departure Leg ..................................................................................................... 25

Load An Arrival Procedure .................................................................................................... 25

Activate An Arrival Leg ......................................................................................................... 26

Load and/or Activate an Approach Procedure ................................................................. 26

Activate An Approach in the Active Flight Plan ............................................................... 27

Activate a Vector to Final Approach Fix ............................................................................ 27

Activate A Missed Approach in the Active Flight Plan ................................................... 27

HAZARD AVOIDANCE ................................................................................................................29

Customizing the Hazard Displays on the Navigation Map ............................................ 29

XM Weather (Optional) .......................................................................................................... 29

Traffic Systems ........................................................................................................................ 31

Terrain Awareness & Warning System (TAWS) Display ................................................... 33

Airborne Color Weather Radar ............................................................................................ 35

ADDITIONAL FEATURES ........................................................................................................... 39

SafeTaxi™ ................................................................................................................................ 39

ChartView ................................................................................................................................. 39

FliteCharts™ ............................................................................................................................ 40

View Charts from the Navigation Map Page .................................................................... 40

View Charts from the Active Flight Plan Page ................................................................. 40

Change Day/Night View ........................................................................................................40

XM® Radio Entertainment .................................................................................................... 42

ANNUNCIATIONS & ALERTS ................................................................................................... 45

Comparator Annunciations ................................................................................................... 45

Reversionary Sensor Annunciations ................................................................................... 45

MFD & PFD Message Advisories .......................................................................................... 46

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Table of Contents

APPENDIX ....................................................................................................................................... 63

PFD Softkey Map .................................................................................................................... 63

MFD Softkey Map ................................................................................................................... 68

INDEX .........................................................................................................................................Index-1

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Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

Push the BARO Knob to select standard pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

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).

Or

:

Press the HPA Softkey to display the barometric pressure setting in
hectopascals.

4)

Press the BACK Softkey to return to the top-level softkeys.

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION
Window.

4)

Turn the

small

FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.

4)

Turn the

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small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

1

Flight Instruments

CHANGE NAVIGATION SOURCES

1)

Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.

2)

Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.

3)

Press the CDI Softkey a third time to return to GPS.

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)

Press the OBS Softkey to select OBS Mode.

2)

Turn a CRS Knob to select the desired course to/from the waypoint. Press 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.

GENERIC TIMER

1)

Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the
press the ENT Key. The UP/DOWN field is now highlighted.

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.

FMS Knobs to set the desired time, then

CONFIGURE VSPEED BUGS INDIVIDUALLY

1)

Press the TMR/REF Softkey.

2)

Turn the

3)

Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
speed has been changed from a default value, an asterisk appears next to
the speed).

2

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

large

FMS Knob to highlight the desired Vspeed.

190-00664-00 Rev. A

4)

Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field

5)

Turn the

6)

To remove the window, press the CLR Key or the TMR/REF Softkey.

small

FMS Knob clockwise to ON or counterclockwise to OFF.

TURN VSPEED BUGS ON OR OFF BY CATEGORY

1)

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.

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.

3)

Turn the small FMS Knob clockwise to BARO.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

To remove the window, press the CLR Key or the TMR/REF Softkey.

Flight Instruments

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.

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Flight Instruments

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NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

Tune the ADF using the remote ADF control head on the aft pedestal.

DME TUNING

1)

Press the DME Softkey.

2)

Turn the large FMS to select the DME source field.

3)

Turn the small FMS Knob to select the desired DME tuning.

4)

Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

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.

Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO

Transmit/Receive

Press the COM1 MIC, COM2 MIC
installed) on the audio panel.

Receive Only

Press the COM1, COM2
audio panel.

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, or

COM3 MIC Key (optional COM, if

, or

COM3 Key (optional COM, if installed) on the

5

Nav/Com/XPDR/Audio Panel

SELECTING A NAV RADIO

1)

Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2).

2)

Pressing the NAV1, NAV2, DME, or ADF Key selects and deselects the
navigation radio audio source. All radio keys can be selected individually or
together.

NAV/COM TUNING

1)

Press the small tuning knob to select the desired radio for tuning.

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.

DIGITAL CLEARANCE RECORDER AND PLAYER

NOTE: Only the audio for the selected
not recorded for COM3 MIC.

COM MIC

Key is recorded. Audio is

Record

1)

2)

Play

1)

2)

3)

6

Press the REC Key to begin recording.

Press the REC Key again to stop recording.

Press the PLAY Key once to play the latest recorded memory block.

Press the PLAY Key once while playing to stop.

Press the PLAY Key twice quickly while playing to begin playing the
previously recorded block.

Each subsequent two presses will skip back to

the previously recorded block.

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AUTOMATIC FLIGHT CONTROL SYSTEM

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.

NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

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.

AFCS

Control Pressed

Modes Selected

Lateral Vertical
FD Key Roll Hold (default) ROL Pitch Hold (default) PIT
AP Key Roll Hold (default) ROL Pitch Hold (default) PIT

CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch

ALT Key

Takeoff (on ground)

Go Around (in air)

TO

GA

Roll Hold (default) ROL Altitude Hold ALT

Takeoff (on ground)

Go Around (in air)TOGA

VS Key Roll Hold (default) ROL Vertical Speed VS

VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH

GPS

NAV Key

Navigation**

VOR

Pitch Hold (default) PIT

LOC

BC Key Backcourse*** BC Pitch Hold (default) PIT

GPS

APR Key Approach**

VAPP

Pitch Hold (default) PIT

LOC

HDG Key Heading Select HDG Pitch Hold (default) PIT

*Valid VNV flight plan must be entered before VNV Key press activates flight director.

**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.

BC

***The selected navigation receiver must have a valid LOC signal before

director.

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Key press activates flight

7

AFCS

VERTICAL MODES

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Selected Altitude
Capture

Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn FT

Vertical Speed

Flight Level Change,
IAS Hold

Flight Level Change,
Mach Hold

Vertical Path
Tracking

VNV Target Altitude
Capture

Glidepath

Glideslope

Takeoff (on ground)

Go Around (in air)

* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be

captured instead of VNV Target Altitude

** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude

may be used to climb/descend to the
Selected Altitude

Captures the Selected Altitude

Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude

Maintains the current aircraft airspeed
(in IAS or Mach) while the aircraft is
climbing/descending to the Selected
Altitude. Press the SPD Key to switch
between IAS and MACH.

Captures and tracks descent legs of an
active vertical profile

Captures the Vertical Navigation (VNV)
Target Altitude

Captures and tracks the WAAS
glidepath on approach

Captures and tracks the ILS glideslope
on approach

Disengages the autopilot and
commands a constant pitch angle and
wings level in the air on the ground in
preparation for takeoff

Disengages the autopilot and
commands a constant pitch angle and
wings level in the air

(default) PIT

* ALTS

VS Key VS nnnn FPM

FLC nnn KT

FLC Key

FLC M .nnn

VNV

Key

VPTH

** ALTV

GP

APR Key

GS

TO

GA

Switch

GA

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AFCS

LATERAL MODES

Lateral Mode Description Control Annunciation

Holds current aircraft roll attitude

Roll Hold

Low Bank

Heading Select

Navigation, GPS Arm/
Capture/Track

Navigation, VOR Enroute
Arm/Capture/Track

Navigation, LOC Arm/
Capture/Track
(No Glideslope)

Backcourse Arm/Capture/
Track

Approach, GPS Arm/
Capture/Track

Approach, VOR Arm/
Capture/Track

Approach, ILS Arm/
Capture/Track
(Glideslope Mode
automatically armed)

Takeoff (on ground)

Go Around (in air)

* 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.

or rolls wings level, depending
on commanded bank angle

Limits maximum commanded
roll angle

Captures and tracks Selected
Heading

Captures and tracks selected
navigation source (GPS, VOR,
LOC)

Captures and tracks a localizer
signal for backcourse approaches

Captures and tracks selected
navigation source (GPS, VOR,
LOC)

Disengages autopilot and
commands a constant pitch
angle and wings level in
preparation for takeoff

Disengages autopilot and
commands a constant pitch
angle and wings level in the air

(default) ROL

BANK

Key

HDG

Key

*

HDG

GPS

NAV

VOR

Key

LOC

BC Key BC

GPS

VAPP

APR Key

LOC

TO

GA

Switch

GA

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AFCS

Roll Hold Mode (ROL)

Bank Angle Flight Director Response

< 6 deg Rolls wings level

6 to 25 deg Maintains current aircraft roll attitude

> 25 deg Limits bank to 25 degrees

Roll Hold Mode Responses

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GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

1)

Press the Direct-to

2)

Enter the waypoint identifier.

3)

Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.

4)

If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.

5)

Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.

6)

Enter the desired altitude.

7)

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.

8)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

9)

Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.

10)

Enter the desired offset distance before (-) or after (+) the waypoint.

11)

Press the ENT Key. The ‘Activate?’ field is highlighted.

12)

Press the ENT Key to activate.

( )

Key.

GPS Navigation

Direct-to Navigation from the PFD

1)

Press the Direct-to Key

2)

Turn the large FMS Knob to place the cursor in the desired selection field.

3)

Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.

4)

Press the ENT Key.

5)

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.

6)

Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.

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( )

.

11

GPS Navigation

7)

Turn the small FMS Knob to enter the desired VNV 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 ‘VNV’ offset distance field.

11)

Turn the small FMS Knob to enter the desired target altitude offset from

the selected Direct-to.

12)

Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to

highlight the ‘COURSE’ field.

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 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
press the ENT Key.

FMS Knob to highlight ‘CANCEL’ and

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

3)

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.

4)

With ‘Activate’ highlighted, press the ENT Key.

12

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190-00664-00 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

Press the FPL Key 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.

VERTICAL NAVIGATION

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.

Large White

Text

Large Light

Blue Text

190-00664-00 Rev. A

Small Light

Blue Text

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

13

GPS Navigation

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 speed and deviation guidance. Note that these altitudes
will be displayed as blue text up to, but not including the FAF. The FAF will always be
a “reference only” altitude and cannot be designated, unless the selected approach does
not provide vertical guidance. In this case, the FAF altitude can be designated.

Altitudes that have been designated for use in vertical guidance may also be made
“non-designated” by placing the cursor over the desired altitude and pressing the CLR
Key. The altitude is now displayed only as a reference. It will not be used to give
vertical guidance. Other displayed altitudes may change due to re-calculations or
rendered invalid as a result of manually changing an altitude to a non-designated
altitude.

White Text Light Blue Text Light Blue

Subdued Text

Large Text

Small Text

14

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
speed and deviation
guidance.

Altitude is not
designated to be used
in determining vertical
speed and deviation
guidance. Altitude has
been retrieved from the
navigation database
and is provided as a
reference.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Altitude has been
entered by the pilot.
Altitude is designated
for use in giving vertical
speed and deviation
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.

Altitude is designated
for use in giving vertical
speed and deviation
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
speed and deviation
guidance.

The system cannot
use this altitude in
determining vertical
speed and deviation
guidance.

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Flight Planning

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Entering Weight Parameters

The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large
small

FMS

Knob to select the first rectangular page icon.

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.

Entering Fuel Parameters

FMS

Knob to select the ‘AUX’ page group. Turn the

1)

Press the FMS Knob to activate the cursor.

2)

Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.

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.

TRIP PLANNING

1)

Turn the large FMS Knob to select the ‘AUX’ page group.

2)

Turn the small FMS Knob to select the second rectangular page icon.

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.

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Flight Planning

4)

For Direct-to planning:

a)

Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).

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.

d)

Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.

Or:

For point-to-point planning:

a)

Enter the identifier of the starting waypoint.

b)

Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.

c)

Again, enter the identifier of the ending waypoint.

d)

Press the ENT Key to accept the waypoint.

Or:

For flight plan leg planning:

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.

c)

Turn the large FMS Knob to highlight the ‘LEG’ field.

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.

16

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.

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.

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190-00664-00 Rev. A

6)

Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.

7)

Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’
page mode, fuel flow is provided by the system.

8)

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.

9)

The flashing cursor moves to the calibrated airspeed field. Enter a calibrated
airspeed. Press the ENT Key when finished.

CREATE A NEW USER WAYPOINT

1)

Turn the large FMS Knob to select the ‘WPT’ page group.

2)

Turn the small FMS Knob to select the User WPT Information Page.

3)

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 ‘REFERENCE WAYPOINTS’ field. If desired, the
waypoint can be defined by a reference waypoint. Use one of the following
methods to enter the reference waypoint:

a)

Turn the small FMS Knob to the left to display a list of flight plan
waypoints. This list is populated only when there is an active flight
plan.

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

Flight Planning

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Flight Planning

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

7)

After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial)
field. Enter the desired radial from the reference waypoint.

8)

Press the ENT Key.

9)

The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.

10)

Press the ENT Key. The cursor is now placed for entering another reference

waypoint, if desired.

11)

Press the FMS Knob to remove the flashing cursor.

DELETE A USER WAYPOINT

1)

Turn the large FMS Knob to select the ‘WPT’ page group.

2)

Turn the small FMS Knob to select the User WPT Information Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.

5)

Turn the small FMS Knob to highlight the desired waypoint.

6)

Select the DELETE Softkey.

7)

The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.

CREATE A NEW FLIGHT PLAN

Using the MFD

1)

Press the FPL Key.

2)

Turn the small FMS Knob to display the Flight Plan Catalog Page.

3)

Select the NEW Softkey to display a blank flight plan for the first empty storage
location.

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Flight Planning

4)

Turn the small FMS Knob to display the Waypoint Information Window.

5)

Enter the identifier of the departure waypoint.

6)

Press the ENT Key.

7)

Repeat step number 4, 5, and 6 to enter the identifier for each additional
flight plan waypoint.

8)

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.

Using the PFD

NOTE: If a flight plan is active, an additional flight plan cannot be entered

using the PFD.

NOTE: After the first leg is entered (using the PFD only) it is immediately

activated.

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the small FMS Knob to enter the first letter of the destination waypoint
identifier.

4)

Turn the large FMS Knob to the right to move the cursor to the next character
position.

5)

Repeat step 3 and 4 to spell out the rest of the waypoint identifier.

6)

Press the ENT Key and the cursor is now ready for entering of the next flight
plan waypoint.

7)

Repeat steps 3 through 6 to enter the identifier for each additional flight plan
waypoint.

8)

Once all waypoints have been entered, press the FMS Knob to remove the
cursor. The new flight plan is now active.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint will be inserted before the highlighted waypoint.

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19

Flight Planning

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:

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘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.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

ENTER AN AIRWAY IN A FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan or display a stored flight
plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the waypoint before which the airway
will be entered.

4)

Enter the desired airways entry point. When the first alphanumeric key is
pressed, the Waypoint Information Window will be displayed.

5)

Press the ENT Key.

6)

Enter the desired airway identifier. When the first alphanumeric key is
pressed, the Waypoint Information Window will be displayed.

7)

Press the LD AIRWY Softkey.

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Flight Planning

8)

Turn either FMS Knob to scroll through the list of available exit points.

9)

With the desired exit point highlighted, press the ENT Key.

10)

With ‘LOAD?’ highlighted, press the ENT Key.

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

Turn the large FMS Knob to highlight ‘Invert Flight Plan’.

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.

REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT

PLAN

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or:

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.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in 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.

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Flight Planning

STORE A FLIGHT PLAN

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 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

22

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or:

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.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the waypoint to be deleted.

3)

Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.

4)

With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large

FMS Knob to highlight ‘CANCEL’ and press

the ENT Key.

5)

Once all changes have been made, press the FMS Knob to remove the
cursor.

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190-00664-00 Rev. A

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key.

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.

COPY A FLIGHT PLAN

1)

Press the FPL Key.

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.

Flight Planning

DELETE A FLIGHT PLAN

1)

Press the FPL Key.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be deleted.

5)

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.

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Flight Planning

GRAPHICAL FLIGHT PLAN CREATION

1)

Press the FPL Key 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
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.

FMS Knob to activate the cursor. Waypoints are inserted

ABOVE

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PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.

3)

Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.

4)

Turn the large FMS Knob to highlight the desired departure.

5)

Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either

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.

FMS Knob to select the desired runway.

Procedures

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired waypoint within the
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.

LOAD AN ARRIVAL PROCEDURE

1)

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.

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25

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Press the ENT Key. A list of transitions is displayed for the selected arrival.

6)

Turn either FMS Knob to select the desired transition.

7)

Press the ENT Key. A list of runways 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.

11)

The arrival will become part of the active flight plan.

ACTIVATE AN ARRIVAL LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired waypoint within the
arrival.

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg will be displayed.

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.

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 the either FMS Knob to highlight the desired approach.

The WAAS channel and ID for the selected approach procedure are
displayed in the ‘APPROACH CHANNEL’ field.

5)

Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.

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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.

7)

Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.

8)

Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.

Selecting ‘LOAD?’ will enter the selected approach procedure into the
active flight plan, but will not be currently active. Selecting ‘ACTIVATE?’
will enter the selected approach procedure into the active flight plan and
immediately activate it.

9)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.

3)

Press the ENT Key. A confirmation window will be displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Procedures

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.

3)

Press the ENT Key.

4)

A direct-to vector is established to the final approach fix.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

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.

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Procedures

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190-00664-00 Rev. A

Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page
option.

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.

XM WEATHER (OPTIONAL)

WARNING: Use of XM weather for hazardous weather penetration is not
recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.

Displaying XM Weather on the Navigation Map Page

Menu. The cursor flashes on the ‘Map Setup’

1)

Press the MAP Softkey.

2)

Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press the applicable softkey again to remove weather data from the
Navigation Map Page.

Display METAR and TAF information on the Airport Information Page

1)

Turn the large FMS Knob to select the WPT Page Group.

2)

Turn the small FMS Knob to select the Airport Information Page.

3)

Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).

Displaying Weather on the Weather Data Link Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Weather Data Link Page.

3)

Select the available softkeys to select the desired XM weather product.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

29

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.

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,
or SIGMETs.

3)

Press the ENT Key to display pertinent information for the selected product.

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.

Weather Products and Symbols

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

NEXRAD

30

Cell Movement

XM Lightning

Cloud Top

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

SIGMETs/AIRMETs

City Forecast

METARs

Freezing Levels

Surface Analysis

County Warnings

Winds Aloft

Cyclone Warnings

190-00664-00 Rev. A

Hazard Avoidance

TRAFFIC SYSTEMS

• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey will be displayed.

• If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE, TEST,
and ALT MODE Softkey will be displayed.

TAS Symbol Description

Non-Threat Traffic

(intruder is beyond 5 nm and greater than 1200’ vertical separation)

Proximity Advisory (PA)

(intruder is within 5 nm and less than 1200’ vertical separation)

Traffic Advisory (TA)

(closing rate, distance, and vertical separation meet TA criteria)

Traffic Advisory Off Scale

Traffic Symbol Description

Traffic Information Service (TIS)

NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS will not be 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.

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.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

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Hazard Avoidance

Displaying Traffic on the Navigation Map

1)

Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.

2)

Select the TRAFFIC Softkey. Traffic will now be displayed on the map.

Traffic Advisory System (TAS) (Optional)

System Self Test

1)

Set the range to 2/6 nm.

2)

Press the STANDBY Softkey.

3)

Press 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
“Skywatch System Test Passed” will be heard. If the self test fails, the
system will revert to Standby Mode and a voice alert “Skywatch System Test
Failed” will be heard.

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 second rectangular page icon.

3)

Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.

4)

Press the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.

5)

Press 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.

Displaying Traffic on the Navigation Map

1)

With the Navigation Map displayed, press the MAP Softkey.

2)

Press the TRAFFIC Softkey. Traffic will now be displayed on the map.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.

NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.

Manual System Test

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Test TAWS’.

3)

Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS Page.

When all is in working order, “TAWS System Test, OK” will be heard.

Display Terrain on the TAWS Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the TAWS 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 display a larger area or rotate counter­clockwise to display a smaller area.

190-00664-00 Rev. A

Color Terrain/Obstacle Location

Red

Yellow

Black

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Terrain/Obstacle above or within 100’
below or above aircraft altitude.

Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

33

Hazard Avoidance

Enable/Disable Aviation Data

1)

While the TAWS 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

Inhibit TAWS

While the TAWS Page is displayed, press the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

Turn the small FMS Knob to select ‘Inhibit TAWS’.

3)

Press the ENT Key.

Enable TAWS

While the TAWS Page is displayed, press the INHIBIT Softkey.

Or

:

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Enable TAWS’.

3)

Press the ENT Key.

34

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS 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.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

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.

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.

Displaying Weather on the Weather Radar Page

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.

Or

:

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.

Hazard Avoidance

Adjusting Antenna Tilt

Move the

Joystick

up or down to adjust the tilt of the antenna up or down. Moni-

tor 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.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

35

Hazard Avoidance

Adjusting Antenna Bearing

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.

Vertically Scan a Storm Cell

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.

2)

Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.

3)

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

36

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.

1)

Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.

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 Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Hazard Avoidance

Ground Mapping

1)

Select the MODE Softkey.

2)

Select the GROUND Softkey to place the radar in Ground Map Mode.

3)

Select the BACK Softkey.

4)

Press the FMS Knob to activate the cursor.

5)

Turn the large FMS Knob to place the cursor in the ‘TILT’ field.

6)

Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.

7)

Press the FMS Knob to remove the cursor.

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 FULL, 60˚, 40˚, or 20˚ scan.

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

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.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

37

Hazard Avoidance

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.

38

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Additional Features

ADDITIONAL FEATURES

NOTE: The availability of SafeTaxi™, ChartView, or FliteCharts™ in electronic
form does not preclude the requirement to carry paper charts aboard the
aircraft. See AC 120-76A for more information.

SAFETAXI™

SafeTaxi™ is an enhanced feature that gives greater map detail when zooming in on
airports at close range. The airport display on the map reveals runways with numbers,
taxiways with identifying letters/numbers, and airport landmarks including ramps,
buildings, control towers, and other prominent features. Resolution is greater at lower
map ranges. When the aircraft location is within the screen boundary, including within
SafeTaxi ranges, an airplane symbol is shown on any of the navigation map views for
enhanced position awareness.

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
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 aid in following ground control instructions by accurately displaying
the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services. This database is updated on a 56-day cycle.

CHARTVIEW

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 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.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

39

Additional Features

FLITECHARTS™

FliteCharts™ resemble the paper version of National Aeronautical Charting Office
(NACO) terminal procedures charts. The charts are displayed with high-resolution
and in color for applicable charts.

The FliteCharts database contains procedure charts for the United States only. This
database is updated on a 28-day cycle. If not updated within 180 days of the expira­tion date, FliteCharts will no longer function.

VIEW CHARTS FROM THE NAVIGATION MAP PAGE

1)

Press the SHW CHRT Softkey while viewing the navigation map. This will
display the airport diagram for the closest airport, if available.

Or

:

Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.

2)

Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs.

3)

Press the GO BACK Softkey to return to the previous page.

VIEW CHARTS FROM THE ACTIVE FLIGHT PLAN PAGE

1)

While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.

2)

Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.

3)

Press the SHW CHRT Softkey. The appropriate chart will be displayed, if
available for the item selected.

4)

Press the GO BACK Softkey to return to the previous page.

CHANGE DAY/NIGHT VIEW

1)

While viewing a terminal chart press the MENU Key to display the Page
Menu OPTIONS.

2)

Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.

40

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Additional Features

3)

Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.

4)

Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.

5)

Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.

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.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

41

Additional Features

XM® RADIO ENTERTAINMENT

The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.

Selecting the XM Radio Page

1)

Turn the large FMS Knob to select the Auxiliary Page Group.

2)

Turn the small FMS Knob to select the displayed AUX - XM Information
Page.

3)

Press the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.

Active Channel and Channel List

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.

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)

Press the CAT + and CAT - Softkeys to cycle through the categories.

Or

:

Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

1)

While on the XM Radio Page, press the CHNL Softkey.

2)

Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.

Or

:

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.

42

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Additional Features

Entering a Channel Directly

1)

While on the XM Radio Page, press the CHNL Softkey.

2)

Press the DIR CH Softkey. The channel number in the Active Channel Box
will be highlighted.

3)

Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.

4)

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

Up to 15 channels from any category can be assigned a preset number.

1)

On the XM Radio Page, with the desired channel active, press the PRESETS
Softkey to access the first five preset channels (PS1 - PS5).

2)

Press the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.

3)

Press any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.

4)

Press the SET Softkey on the desired channel number to save the channel
as a preset.

Adjusting Volume

Radio volume is controlled at each passenger station.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

43

Additional Features

Blank Page

44

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

ANNUNCIATIONS & ALERTS

COMPARATOR ANNUNCIATIONS

Comparator

Window Text

ALT MISCOMP

IAS MISCOMP

HDG MISCOMP

PIT MISCOMP

ROLL MISCOMP

ALT NO COMP
IAS NO COMP

HDG NO COMP

PIT NO COMP

ROLL NO COMP

Difference in altitude sensors is > 200 ft.

If both airspeed sensors detect < 35 knots, this is inhibited.

If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts.

If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts.

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors..

Annunciations & Alerts

Condition

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary

Sensor Window

Text

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON GPS1
BOTH ON GPS2

XSIDE ADC

XSIDE AHRS

190-00664-00 Rev. A

Both PFDs are displaying data from the number one Air Data Computer.

Both PFDs are displaying data from the number two Air Data Computer.

Both PFDs are displaying data from the number one Attitude & Heading Reference
System.

Both PFDs are displaying data from the number two Attitude & Heading Reference
System.

Both PFDs are displaying data from the number one GPS receiver.

Both PFDs are displaying data from the number two GPS receiver.

The PFD displaying this annunciation is displaying data from the cross-side Air Data
Computer.

The PFD displaying this annunciation is displaying data from the cross-side Attitude &
Heading Reference System.

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Condition

45

Annunciations & Alerts

MFD & PFD Message Advisories

Message Comments

DATA LOST

– Pilot stored data was

lost. Recheck settings.

XTALK ERROR

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

– MFD1 software

mismatch, communication halted.

PFD1 CONFIG

– PFD1 config error.

Config service req’d.

PFD2 CONFIG

– PFD2 config error.

Config service req’d.

MFD1 CONFIG

– MFD1 config error.

Config service req’d.

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

The pilot profile data was lost. System reverts
to default pilot profile and settings. The
pilot may reconfigure the MFD & PFD with
preferred settings, if desired.

The MFD and PFD are not communicating
with each other. The G1000 system should be
serviced.

The PFD and/or MFD self-test has detected
a problem. The G1000 system should be
serviced.

The PFD and/or MFD has incorrect software
installed. The G1000 system should be
serviced.

The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.

The MFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.

The MFD and PFD have different software
versions installed. The G1000 system should
be serviced.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

MFD & PFD Message Advisories (Cont.)

Message Comments

PFD1 COOLING

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

MFD1 COOLING

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

The PFD and/or MFD is overheating and is
reducing power consumption by dimming
the display. If problem persists, the G1000
system should be serviced.

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

Key is stuck.

CNFG MODULE

configuration module is inoperative.

– PFD1

The PFD1 configuration module backup
memory has failed. The G1000 system should
be serviced.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1 has low

– PFD2 has low

– MFD1 has low

The PFD1 voltage is low. The G1000 system
should be serviced.

The PFD2 voltage is low. The G1000 system
should be serviced.

The MFD voltage is low. The G1000 system
should be serviced.

Annunciations & Alerts

Database Message Advisories

Message Comments

MFD1 DB ERR

– MFD1 aviation

database error exists.

PFD1 DB ERR

– PFD1 aviation

database error exists.

PFD2 DB ERR

– PFD2 aviation

database error exists.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

The MFD and/or PFD detected a failure in
the aviation database. Attempt to reload the
aviation database. If problem persists, the
G1000 system should be serviced.

47

Annunciations & Alerts

Database Message Advisories (Cont.)

Message Comments

MFD1 DB ERR

– MFD1 basemap

database error exists.

PFD1 DB ERR

– PFD1 basemap

database error exists.

PFD2 DB ERR

– PFD2 basemap

The MFD and/or PFD detected a failure in the
basemap database.

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 terrain

– PFD1 terrain

– PFD2 terrain

The MFD and/or 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.

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 obstacle

– PFD1 obstacle

– PFD2 obstacle

The MFD and/or 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.

database error exists.

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport terrain

– PFD2 airport terrain

The MFD and/or 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.

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

The MFD and/or 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.

database error exists.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Database Message Advisories (Cont.)

Message Comments

MFD1 DB ERR

database error exists.

– MFD1 Chartview

The MFD and/or PFD detected a failure in
the ChartView 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

database error exists.

– MFD1 FliteCharts

The MFD and/or PFD detected a failure in
the FliteCharts database (optional feature).
Ensure that the data card is properly inserted.
Replace data card. If problem persists, the
G1000 system should be serviced.

DB MISMATCH

version mismatch. Xtalk is off.

– Aviation database

The PFD and MFD have different aviation
database versions installed. Crossfill is off.
Install correct aviation database version in
both displays.

DB MISMATCH

type mismatch. Xtalk is off.

– Aviation database

The PFD and MFD have different aviation
database types installed (Americas, European,
etc.). Crossfill is off. Install correct aviation
database type in both displays.

DB MISMATCH

version mismatch.

– Terrain database

The PFD and MFD have different terrain
database versions installed. Install correct
terrain database version in both displays.

DB MISMATCH

type mismatch.

– Terrain database

The PFD and MFD have different terrain
database types installed. Install correct
terrain database type in both displays.

DB MISMATCH

version mismatch.

– Obstacle database

The PFD and MFD have different obstacle
database versions installed. Install correct
obstacle database version in both displays.

DB MISMATCH

database mismatch.

– Airport Terrain

The PFD and MFD have different airport terrain
databases installed. Install correct airport
terrain database in both displays.

Annunciations & Alerts

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

49

Annunciations & Alerts

GMA 1347D Message Advisories

Message Comments

GMA1 FAIL
GMA2 FAIL

GMA XTALK

– GMA1 is inoperative. The audio panel self-test has detected a
– GMA2 is inoperative.

– GMA crosstalk error

has occurred.

GMA1 CONFIG

– GMA1 config

error. Config service req’d.

GMA2 CONFIG

– GMA2 config

error. Config service req’d.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

GMA1 SERVICE

service. Return unit for repair.

GMA2 SERVICE

service. Return unit for repair.

– GMA1 software

– GMA2 software

– GMA1 needs

– GMA2 needs

failure. The audio panel is unavailable. The
G1000 system should be serviced.

An error has occurred in transferring data
between the two GMAs. The G1000 system
should be serviced.

The audio panel configuration settings do not
match backup configuration memory. The
G1000 system should be serviced.

The audio panel has incorrect software installed.
The G1000 system should be serviced.

The audio panel self-test has detected a problem
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The G1000 system should be serviced when
possible.

GIA 63W Message Advisories

Message Comments

GIA1 CONFIG

– GIA1 config error.

Config service req’d.

GIA2 CONFIG

– GIA2 config error.

Config service req’d.

GIA1 CONFIG

– GIA1 audio config

error. Config service req’d.

GIA2 CONFIG

– GIA2 audio config

error. Config service req’d.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

The GIA1 and/or GIA2 configuration settings
do not match backup configuration memory.
The G1000 system should be serviced.

The GIA1 and/or GIA2 have an error in the
audio configuration. The G1000 system
should be serviced.

190-00664-00 Rev. A

GIA 63W Message Advisories (Cont.)

Message Comments

GIA1 COOLING

too low.

– GIA1 temperature

The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up

GIA2 COOLING

– GIA2 temperature

to operating temperature.

too low.

GIA1 COOLING

temperature.

– GIA1 over

The GIA1 and/or GIA2 temperature is too
high. If problem persists, the G1000 system

GIA2 COOLING

– GIA2 over

should be serviced.

temperature.

GIA1 SERVICE

service. Return the unit for repair.

– GIA1 needs

The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The G1000 system

GIA2 SERVICE

– GIA2 needs

should be serviced.

service. Return the unit for repair.

HW MISMATCH

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

– GIA hardware

A GIA mismatch has been detected, where
only one is WAAS capable.

mismatch. GIA2 communication
halted.

MANIFEST

mismatch, communication halted.

– GIA1 software

The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be

MANIFEST

– GIA2 software

serviced.

mismatch, communication halted.

COM1 TEMP

Reducing transmitter power.

COM2 TEMP

Reducing transmitter power.

– COM1 over temp.

– COM2 over temp.

The system has detected an over temperature
condition in COM1 and/or COM2. The
transmitter will operate at reduced power.
If the problem persists, the G1000 system
should be serviced.

COM1 SERVICE

service. Return unit for repair.

COM2 SERVICE

service. Return unit for repair.

– COM1 needs

– COM2 needs

The system has detected a failure in COM1
and/or COM2. COM1 and/or COM2 may
still be usable. The G1000 system should be
serviced when possible.

Annunciations & Alerts

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

51

Annunciations & Alerts

GIA 63W Message Advisories (Cont.)

Message Comments

COM1 PTT

is stuck.

COM2 PTT

is stuck.

– COM1 push-to-talk key

– COM2 push-to-talk key

The COM1 and/or COM2 external push­to-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.

COM1 RMT XFR

transfer key is stuck.

COM2 RMT XFR

transfer key is stuck.

– COM1 remote

– COM2 remote

The COM1 and/or 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.

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

GPS NAV LOST

– Loss of GPS

navigation. Insufficient satellites.

GPS NAV LOST

– Loss of GPS

navigation. Position error.

GPS NAV LOST

– Loss of GPS

navigation. GPS fail.

ABORT APR

– Loss of GPS

navigation. Abort approach.

APR DWNGRADE

– Approach

downgraded.

TRUE APR

– True north approach.

Change HDG reference to TRUE.

GPS integrity is insufficient for the current
phase of flight.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS
navigation.

Use LNAV minima when approach is
downgraded.

Displayed after passing the first waypoint of
a true north approach when the nav angle is
set to ‘AUTO’.

GPS1 SERVICE

service. Return unit for repair.

GPS2 SERVICE

service. Return unit for repair.

– GPS1 needs

– GPS2 needs

A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be
serviced.

52

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

GIA 63W Message Advisories (Cont.)

Message Comments

NAV1 SERVICE

service. Return unit for repair.

NAV2 SERVICE

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 needs

– NAV2 needs

– NAV1 remote

– NAV2 remote

A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be
serviced.

The remote NAV1 and/or NAV2 transfer
switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle
its operation. If the problem persists, the
G1000 system should be serviced.

G/S1 FAIL

G/S2 FAIL

G/S1 SERVICE

Return unit for repair.

G/S2 SERVICE

Return unit for repair.

– G/S1 is inoperative. A failure has been detected in glideslope

– G/S2 is inoperative.

– G/S1 needs service.

receiver 1 and/or receiver 2. The G1000
system should be serviced.

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may

– G/S2 needs service.

still be available. The G1000 system should
be serviced when possible.

Annunciations & Alerts

GEA 71 Message Advisories

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

GEA2 CONFIG

– GEA2 config error.

Config service req’d.

MANIFEST

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

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 #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.

53

Annunciations & Alerts

GTX 33 Message Advisories

Message Comments

XPDR1 CONFIG

– XPDR1 config

error. Config service req’d.

XPDR2 CONFIG

– XPDR2 config

error. Config service req’d.

MANIFEST

– GTX1 software

mismatch, communication halted.

MANIFEST

– GTX2 software

mismatch, communication halted.

XPDR1 SRVC

– XPDR1 needs

service. Return unit for repair.

XPDR2 SRVC

– XPDR2 needs

service. Return unit for repair.

XPDR1 FAIL

XPDR2 FAIL

– XPDR1 is inoperative. There is no communication with the #1

– XPDR2 is inoperative. There is no communication with the #2

The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.

The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.

The transponder has incorrect software
installed. The G1000 system should be
serviced.

The transponder has incorrect software
installed. The G1000 system should be
serviced.

The #1 transponder should be serviced when
possible.

The #2 transponder should be serviced when
possible.

transponder.

transponder.

GRS 77 Message Advisories

Message Comments

AHRS1 TAS

– AHRS1 not receiving

airspeed.

AHRS2 TAS

– AHRS2 not receiving

airspeed.

54

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

The #1 AHRS is not receiving true airspeed
from the air data computer. The AHRS relies
on GPS information to augment the lack
of airspeed. The G1000 system should be
serviced.

The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.

190-00664-00 Rev. A

GRS 77 Message Advisories (Cont.)

Message Comments

AHRS1 GPS

GPS source.

– AHRS1 using backup

The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000
system should be serviced when possible.

AHRS2 GPS

GPS source.

– AHRS2 using backup

The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000
system should be serviced when possible.

AHRS1 GPS

any GPS information.

– AHRS1 not receiving

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

any GPS information.

The #2 AHRS is not receiving any or any
useful GPS information. Check AFMS
limitations. The G1000 system should be
serviced.

AHRS1 GPS

backup GPS information.

– AHRS1 not receiving

The #1 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.

AHRS2 GPS

– AHRS2 not receiving

backup GPS information.

The #2 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.

AHRS1 GPS

exclusively in no-GPS mode.

– AHRS1 operating

The #1 AHRS is operating exclusively in
no-GPS mode. The G1000 system should be
serviced.

AHRS2 GPS

exclusively in no-GPS mode.

– AHRS2 operating

The #2 AHRS is operating exclusively in
no-GPS mode. The G1000 system should be
serviced.

AHRS MAG DB

model database version mismatch.

AHRS1 SRVC

field model needs update.

– AHRS magnetic

– AHRS1 Magnetic-

The #1 AHRS and #2 AHRS magnetic model
database versions do not match.

The #1 AHRS earth magnetic field model is
out of date. Update magnetic field model
when practical.

Annunciations & Alerts

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

55

Annunciations & Alerts

GRS 77 Message Advisories (Cont.)

Message Comments

AHRS2 SRVC

– AHRS2 Magnetic-

field model needs update.

GEO LIMITS

– AHRS1 too far North/

South, no magnetic compass.

GEO LIMITS

– AHRS2 too far North/

South, no magnetic compass.

MANIFEST

– GRS1 software

mismatch, communication halted.

MANIFEST

– GRS2 software

mismatch, communication halted.

GMU 44 Message Advisories

Message Comments

HDG FAULT

– AHRS1 magnetometer

fault has occurred.

HDG FAULT

– AHRS2 magnetometer

fault has occurred.

MANIFEST

– GMU1 software

mismatch, communication halted.

MANIFEST

– GMU2 software

mismatch, communication halted.

The #2 AHRS earth magnetic field model is
out of date. Update magnetic field model
when practical.

The aircraft is outside geographical limits
for approved AHRS operation. Heading is
flagged as invalid.

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.

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.

The GMU 44 has incorrect software installed.
The G1000 system should be serviced.

GDL 69A Message Advisories

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

56

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

190-00664-00 Rev. A

GDL 69A Message Advisories (Cont.)

Message Comments

GDL69 FAIL

– GDL 69 has failed. A failure has been detected in the GDL

69. The receiver is unavailable. The G1000
system should be serviced

MANIFEST

mismatch, communication halted.

– GDL software

The GDL 69 has incorrect software installed.
The G1000 system should be serviced.

GDC 74B Message Advisories

Message Comments

ADC1 ALT EC

correction is unavailable.

ADC2 ALT EC

– ADC1 altitude error

– ADC2 altitude error

GDC1 or GDC2 is reporting that the altitude
error correction is unavailable.

correction is unavailable.

ADC1 AS EC

correction is unavailable.

ADC2 AS EC

– ADC1 airspeed error

– ADC2 airspeed error

GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.

correction is unavailable.

MANIFEST

mismatch, communication halted.

MANIFEST

– GDC1 software

– GDC2 software

The GDC 74B has incorrect software installed.
The G1000 system should be serviced.

mismatch, communication halted.

Annunciations & Alerts

GCU 475 Message Advisories

Message Comments

GCU CNFG

– GCU config error.

Config service req’d.

GCU FAIL

MANIFEST

– GCU is inoperative. A failure has been detected in the GCU 475.

– GCU software

mismatch, communication halted.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

GCU 475 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The GCU 475 is unavailable.
The GCU 475 has incorrect software installed.

The G1000 system should be serviced.

57

Annunciations & Alerts

GCU 475 Message Advisories (Cont.)

Message Comments

GCU KEYSTK

– GCU [key name] Key

is stuck.

GMC 710 Message Advisories

Message Comments

GMC CONFIG

– GMC config error.

Config service req’d.

GMC FAIL

MANIFEST

– GMC is inoperative. A failure has been detected in the GMC 710.

– GMC software

mismatch, communication halted.

GMC KEYSTK

– GMC [key name]

Key is stuck.

A key is stuck on the GCU 475 bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

Error in the configuration of the GMC 710.

The GMC 710 is unavailable.
The GMC 710 has incorrect software

installed. The G1000 system should be
serviced.

A key is stuck on the GMC 710 bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

GWX 68 Alert Messages

Message Comments

GWX CONFIG

– GWX config error.

Config service req’d.

GWX FAIL

GWX SERVICE

– GWX is inoperative. The GDU is not receiving status packet from

– GWX needs

service. Return unit for repair.

MANIFEST

– GWX software

mismatch, communication halted.

58

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.

the GWX 68 or the GWX 68 is reporting a
fault. The GWX 68 radar system should be
serviced.

A failure has been detected in the GWX 68.
The GWX 68 may still be usable.

The GWX 68 has incorrect software installed.
The G1000 system should be serviced.

190-00664-00 Rev. A

GWX 68 Alert Messages (Cont.)

Message Comments

WX ALERT

– Possible severe weather

ahead.

Miscellaneous Message Advisories

Message Comments

FPL WPT LOCK

waypoint is locked.

– Flight plan

Upon power-up, the G1000 system detects that a
stored flight plan waypoint is locked. This occurs
when an aviation database update eliminates an
obsolete waypoint. The flight plan cannot find
the specified waypoint and flags this message.
This can also occur with user waypoints in a flight
plan that is deleted.

Remove the waypoint from the flight plan if
it no longer exists in any database, or update
the waypoint name/identifier to reflect the new
information.

FPL WPT MOVE

waypoint moved.

– Flight plan

The system has detected that a waypoint
coordinate has changed due to a new aviation
database update. Verify that stored flight plans
contain correct waypoint locations.

TIMER EXPIRD

expired.

DB CHANGE

changed. Verify user modified
procedures.

– Timer has

– Database

The system notifies the pilot that the timer has
expired.

This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an aviation database
update. Verify that the user-modified procedures
in stored flight plans are correct and up to date.

DB CHANGE

changed. Verify stored airways.

– Database

This occurs when a stored flight plan contains
an airway that is no longer consistent with the
aviation database. This alert is issued only after
an aviation database update. Verify use of
airways in stored flight plans and reload airways
as needed.

Annunciations & Alerts

The GWX 68 indicates severe weather within
±10 degrees of the aircraft heading at a
range of 80 to 320 nm.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

59

Annunciations & Alerts

Miscellaneous Message Advisories (Cont.)

Message Comments

FPL TRUNC

been truncated.

– Flight plan has

This occurs when a newly installed aviation
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.

LOCKED FPL

navigate locked flight plan.

– Cannot

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.

WPT ARRIVAL

waypoint -[xxxx]

STEEP TURN

ahead.

INSIDE ARSPC

airspace.

ARSPC AHEAD

ahead less than 10 minutes.

– Arriving at

– Steep turn

– Inside

– Airspace

Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.

A steep turn is 15 seconds ahead. Prepare to turn.

The aircraft is inside the airspace.

Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
minutes.

ARSPC NEAR

and ahead.

ARSPC NEAR

– less than 2 nm.

APR INACTV

active.

– Airspace near

– Airspace near

– Approach is not

Special use airspace is near and ahead of the
aircraft position.

Special use airspace is within 2 nm of the aircraft
position.

The system notifies the pilot that the loaded
approach is not active. Activate approach when
required.

SLCT FREQ

frequency for approach.

– Select appropriate

The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.

SLCT NAV

for approach.

– Select NAV on CDI

The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct
NAV receiver.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Miscellaneous Message Advisories (Cont.)

Message Comments

PTK FAIL

unavailable: bad geometry.

PTK FAIL

unavailable: invalid leg type.

PTK FAIL

unavailable: past IAF.

UNABLE V WPT

current vertical waypoint.

– Parallel track

– Parallel track

– Parallel track

– Can’t reach

Bad parallel track geometry.

Invalid leg type for parallel offset.

IAF waypoint for parallel offset has been passed.

The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system will automatically
transition to the next vertical waypoint.

VNV

– Unavailable. Unsupported

leg type in flight plan.

The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to
the active vertical waypoint. This will prevent
vertical guidance to the active vertical waypoint.

VNV

– Unavailable. Excessive

crosstrack error.

VNV

– Unavailable. Excessive

track angle error.

VNV

– Unavailable. Parallel course

selected.

NO WGS84 WPT

– Non WGS 84

waypoint for navigation -[xxxx]

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 selected waypoint [xxxx] does not use the
WGS 84 datum. Cross-check position with
alternate navigation sources.

TRAFFIC FAIL

failed.

STRMSCP FAIL

failed.

FAILED PATH

failed.

SCHEDULER [#]

– Traffic device has

The G1000 is no longer receiving data from the
traffic system. The traffic device should be serviced.

– Stormscope has

Stormscope has failed. The G1000 system
should be serviced.

– A data path has

A data path connected to the GDU or the GIA
63/63W has failed.

– <message>. Message criteria entered by the user.

Annunciations & Alerts

190-00664-00 Rev. A

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61

Annunciations & Alerts

Miscellaneous Message Advisories (Cont.)

Message Comments

MAG VAR WARN

magnetic variance. Verify all course
angles.

– Large

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°.

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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

PFD SOFTKEY MAP

ALERTS

Select the BACK Softkey to return to
the top-level softkeys.

STRMSCP

ALERTS

ALERTS

Appendix

APPENDIX

Top Level PFD Softkeys

INSET

OFF

DCLTR (3)

190-00664-00 Rev. A

Inset Map Softkeys

Displays Inset Map in PFD lower left corner

Removes Inset Map

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

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

63

Appendix

Select the BACK Softkey to
return to the top level softkeys.

BACK

ADC2

ADC1

AHRS1

AHRS2

ALERTS

ALERTS

TRAFFIC

TOPO

TERRAIN

STRMSCP

NEXRAD

XM LTNG

Displays traffic information on Inset Map

Displays topographical data (e.g., coast­lines, terrain, rivers, lakes) and elevation
scale on Inset Map

Displays terrain information on Inset Map

Press to display the Stormscope lightning
data on the Inset Map (within a 200 nm
radius of the aircraft)

Displays NEXRAD weather and coverage
information on Inset Map (optional feature)

Displays XM lightning information on Inset
Map (optional feature)

Sensor Softkeys

SENSOR

64

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

ADC1

ADC2

AHRS1

AHRS2

Displays softkeys for selecting the #1 and
#2 AHRS and Air Data Computers

Selects the #1 Air Data Computer

Selects the #2 Air Data Computer

Selects the #1 AHRS

Selects the #2 AHRS

190-00664-00 Rev. A

PFD Configuration Softkeys

Select the BACK Softkey to
return to the top-level softkeys

FD FRMT

ALT UNIT

METERS IN HPA

SNGL CUE

X POINT

R

ALERTS

ALERTS

ALERTS

ALERTS

ALERTS

HSI FRMT

360 HSI

ARC HSI

ALERTS

(optional)

Appendix

PFD

190-00664-00 Rev. A

FD FRMT

DFLTS

WIND

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Displays second-level softkeys for ad­ditional PFD configurations

Displays the softkeys for selecting the

SNGL CUE

two flight director formats

Selects the single cue flight director
format

X POINTR

Selects the cross pointer flight director
format

Resets PFD to default settings, including
changing units to standard

Displays softkeys to select wind data
parameters

OPTN 1

Longitudinal and lateral components

65

Appendix

DME

BRG1

HSI FRMT

BRG2

ALT UNIT

OPTN 2

OPTN 3

OFF

360 HSI

ARC HSI

METERS

Total direction and speed

Total direction with head and crosswind
speed 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 for setting the altimeter
and BARO settings to metric units

When enabled, displays altimeter in
meters

66

IN

Press to display the BARO setting as
inches of mercury

HPA

Press to display the BARO setting as
hectopacals

STD BARO

Sets barometric pressure to 29.92 in Hg
(1013 hPa)

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Transponder Softkeys

Select the BACK Softkey to return
to the top-level softkeys.

Select the BACK Softkey to return
to the previous level softkeys.

ALERTS

ALERTS

ALERTS

Appendix

XPDR

XPDR1

XPDR2

STBY

ON

ALT

GND

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)

Selects Mode A (transponder replies to
interrogations)

Selects Mode C – Altitude Reporting Mode
(transponder replies to identification and
altitude interrogations)

Manually selects Ground Mode, the tran­sponder does not allow Mode A and
Mode C replies, but it does permit acquisi­tion squitter and replies to discretely ad­dressed Mode S interrogations.

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

67

Appendix

MAP

DCLTR

TRAFFIC

TOPO

BACK

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

Select the BACK Softkey on
this level to return to the top
softkey level.

NEXRAD

XM LTNG

(optional)(optional)

SHW CHRT

CHKLIST

(optional)(optional)

AIRWAYS

AIRWY LO

AIRWAY HI

AIRWY ON

STRMSCP

VFR

CODE

IDENT

TMR/REF

NRST

MSG

MFD SOFTKEY MAP

0 — 7

BKSP

Automatically enters the VFR code (1200 in
the U.S.A. only)

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 Messages Window

MAP

68

TRAFFIC

TOPO

MFD Softkeys

Enables second-level Navigation Map softkeys

Displays traffic information on Navigation Map

Displays topographical data (e.g., coastlines, terrain,
rivers, lakes) and elevation scale on Navigation Map

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Appendix

DCLTR (3)

SHW CHRT

CHKLIST

TERRAIN

AIRWAYS

STRMSCP

NEXRAD

XM LTNG

BACK

Displays terrain information on Navigation Map

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

Displays Stormscope weather and coverage
information on Navigation Map (optional feature)

Displays NEXRAD weather and coverage informa­tion on Navigation Map (optional feature)

Displays XM lightning information on Navigation
Map (optional feature)

Returns to top-level softkeys

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

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

69

Appendix

Blank Page

70

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Index

A

Activate a flight plan 12
Active Channel 42
ADF 5, 6, 66
AHRS 54, 55, 56, 57, 58
Airways 20, 69
Air Data Computer 45
Alert messages 58, 59
ALT 32
Altitude mode 32
Altitude volume 32
Antenna stabilization 37
Antenna tilt 35
APR Softkey 40
Attitude & Heading Reference System

45

Audio panel controls

NAV1, NAV2 6

B

Barometric Altitude Minimums 3
Barometric pressure 66
Bearing line 36, 37

C

CDI 1, 2, 6, 60
Channel Presets 43
ChartView 39, 49
Clearance Recorder 6
Code selection softkeys 5
COM 5, 6

D

Database Updates 69
DCLTR Softkey 39
Declutter 63, 69
Direct-to 11
DME 5, 6

E

Edit a flight plan 22

F

Flight Director 7, 10
FliteCharts™ 39, 40
Frequency Transfer 6

G

Gain 36
Ground mapping 37

H

HF 5
Horizontal scan 36

I

Inhibit 34
Inhibit TAWS 34
Inset Map 63, 64

J

Jeppesen 39

L

Lightning 64

M

Map panning 30
Message advisories 46 – 50, 53 – 62
METAR
MISCOMP 45
Mode S 67
Mode selection softkeys 5
Multi Function Display (MFD)

29

Softkeys

68

190-00664-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Index-1

Index

N

NACO 40
NAV 6
NAV1 2, 6
NAV2

2, 6
Navigation database 13, 14
NEXRAD 29, 30, 64, 69
NOTAM Softkey 40

O

OBS 2
Obstacles 49, 51
Overspeed Protection 8

P

PIT 45
Play 6
Playback 6

R

RADIO softkey 42

S

SafeTaxi™ 39
Sector scan 37
Sensor 45
STAB

37
Standby 35
STAR Softkey 40
Store Flight Plan 21
Stormscope lightning data 64

TAWS-B
Terrain 33, 49, 64, 68, 69
Tilt line 35
Topographical data 64, 68
Traffic 29, 31, 64, 68
Traffic advisory
Traffic map page 31, 32
Transponder 5, 67, 68

33

31

V

Vertical deviation guidance 14
Vertical speed guidance 14
VNV 11, 12, 61
Vspeed 2

W

WAAS 26, 51
WATCH 37
Weather Attenuated Color Highlight 37
Weather data link page 29
Weather radar 35
Wind data 65
WX Softkey 40

X

XM lightning 64, 69
XM weather 29
XPDR Softkey 5

T

TAF 29
TAS

32, 54

TAWS 33, 34

Index-2

Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

190-00664-00 Rev. A

Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282

Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138

Garmin (Europe) Ltd
Liberty House, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251

Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099

www.garmin.com

© 2007 Garmin Ltd. or its subsidiaries

190-00664-00 Rev. A