Garmin C90A-GT Reference Guide

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G1000

Cockpit Reference Guide for the Hawker Beechcraft C90A/GT

Integrated Flight Deck

System Software 0636.02 or later

FLIGHT INSTRUMENTS

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

This manual reﬂects the operation of System Software version 0636.02 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: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138

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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.

March, 2009 190-00664-01 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 avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data Computer, or other altimeters in the aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.

WARNING: Trafﬁc information shown on system displays 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

190-00664-01 Rev. A

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: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration.

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/GT 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.

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

Warnings, Cautions & Notes

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.”

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 PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is speciﬁed as safe for antireﬂective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reﬂect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment.

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

190-00664-01 Rev. A

Warnings, Cautions & Notes

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.

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.

NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to ﬁnd operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft.

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Warnings, Cautions & Notes

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Record of Revisions

Part Number Change Summary

190-00664-00

Initial release at GDU 8.10

190-00664-01

Added Synthetic Vision System Added GDU 9.14 parameters

Revision Date of Revision Affected Pages Description

A March, 2009 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

Activate ADS-B Transmit ......................................................................................................... 5

Selecting a COM Radio ............................................................................................................ 5

Selecting a NAV Radio ............................................................................................................. 6

NAV/COM Tuning ....................................................................................................................... 6

Intercom ...................................................................................................................................... 6

Passenger Address (PA) System ............................................................................................. 7

Clearance Recorder and Player .............................................................................................7

AUTOMATIC FLIGHT CONTROL SYSTEM ............................................................................ 9

Flight Director Activation ....................................................................................................... 9

Vertical Modes ......................................................................................................................... 10

Lateral Modes .......................................................................................................................... 11

GPS NAVIGATION ........................................................................................................................ 13

Direct-to Navigation .............................................................................................................. 13

Activate a Stored Flight Plan ............................................................................................... 14

Activate a Flight Plan Leg ..................................................................................................... 14

Stop Navigating a Flight Plan .............................................................................................. 15

Vertical Navigation (VNAV)................................................................................................... 15

FLIGHT PLANNING ...................................................................................................................... 17

Weight Planning ...................................................................................................................... 17

Trip Planning ............................................................................................................................ 17

Create a New User Waypoint Deﬁned by Latitude & Longitude ................................. 19

Create a New User Waypoint Deﬁned by Radials from Other Waypoints ................. 20

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Table of Contents

Create a New User Waypoint Deﬁned by a Radial & Distance from Another

Waypoint ................................................................................................................................... 22

Delete a User Waypoint ......................................................................................................... 23

Create a New Flight Plan ...................................................................................................... 24

Import a Flight Plan from an SD Card ................................................................................ 25

Insert a Waypoint in the Active Flight Plan ...................................................................... 25

Enter an Airway in a Flight Plan .......................................................................................... 26

Invert An Active Flight Plan .................................................................................................. 27

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 27

Store a Flight Plan .................................................................................................................. 27

Edit a Stored Flight Plan ....................................................................................................... 28

Delete a Waypoint from the Flight Plan ............................................................................ 28

Invert and Activate a Stored Flight Plan ........................................................................... 28

Copy a Flight Plan ................................................................................................................... 29

Delete a Flight Plan ................................................................................................................ 29

Graphical Flight Plan Creation ............................................................................................. 29

Export a Flight Plan to an SD Card ..................................................................................... 30

PROCEDURES ................................................................................................................................. 31

Load and Activate a Departure Procedure ....................................................................... 31

Activate A Departure Leg ..................................................................................................... 31

Load An Arrival Procedure .................................................................................................... 31

Activate An Arrival Leg ......................................................................................................... 32

Load and/or Activate an Approach Procedure ................................................................. 32

Activate An Approach in the Active Flight Plan ............................................................... 33

Activate a Vector to Final Approach Fix ............................................................................ 33

Activate A Missed Approach in the Active Flight Plan ................................................... 33

HAZARD AVOIDANCE ................................................................................................................35

Customizing the Hazard Displays on the Navigation Map ............................................ 35

STORMSCOPE® (Optional) ..................................................................................................... 35

XM Weather (Optional) .......................................................................................................... 37

Trafﬁc Systems ........................................................................................................................ 38

Terrain Awareness & Warning System (TAWS) Display ................................................... 40

Airborne Color Weather Radar ............................................................................................ 42

ADDITIONAL FEATURES ........................................................................................................... 47

Synthetic Vision ....................................................................................................................... 47

Terminal Procedure Charts ...................................................................................................48

XM® Radio Entertainment..................................................................................................... 50

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

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Table of Contents

ANNUNCIATIONS & ALERTS ................................................................................................... 53

Advisory Annunciations......................................................................................................... 53

Comparator Annunciations ................................................................................................... 53

Reversionary Sensor Annunciations ................................................................................... 54

AFCS Alerts ............................................................................................................................... 54

TAWS Alerts .............................................................................................................................. 55

Aural Alerts .............................................................................................................................. 57

Flight Plan Import/Export Messages .................................................................................. 58

MFD & PFD Message Advisories .......................................................................................... 59

Database Message Advisories ............................................................................................. 60

GMA 1347D Message Advisories ......................................................................................... 63

GIA 63W Message Advisories ............................................................................................... 64

GEA 71 Message Advisories .................................................................................................. 67

GTX 33 Message Advisories .................................................................................................. 67

GRS 77 Message Advisories .................................................................................................. 68

GMU 44 Message Advisories ................................................................................................ 70

GDL 69A Message Advisories ............................................................................................... 70

GWX 68 Alert Messages ......................................................................................................... 71

GDC 74B Message Advisories ............................................................................................... 71

GCU 475 Message Advisories ............................................................................................... 72

GMC 710 Message Advisories .............................................................................................. 72

Miscellaneous Message Advisories ..................................................................................... 73

APPENDIX ....................................................................................................................................... 77

PFD Softkey Map .................................................................................................................... 77

MFD Softkey Map ................................................................................................................... 82

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

Press the PFD Softkey to display the second-level softkeys.

Press the ALT UNIT Softkey.

Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).

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

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

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Select the AUX-SYSTEM SETUP Page on the MFD.

Press the FMS Knob to activate the cursor.

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

Turn the

small

FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

Select the AUX-SYSTEM SETUP Page on the MFD.

Press the FMS Knob to activate the cursor.

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

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

Additional

Features Annun/Alerts Appendix Index

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

Instruments

Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning.

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

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Press the OBS Softkey to select OBS Mode.

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.

Flight

PlanningProcedures

Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

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

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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.

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.

CONFIGURE VSPEED BUGS INDIVIDUALLY

Press the TMR/REF Softkey.

Turn the

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).

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

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

large

FMS Knob to highlight the desired Vspeed.

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Flight Instruments

Turn the

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

Press the TMR/REF Softkey.

Press the MENU Key.

Turn the FMS Knob to highlight the desired option.

Press the ENT Key. Press the TMR/REF Softkey to remove the window.

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

Press the TMR/REF Softkey.

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

Turn the small FMS Knob clockwise to BARO.

Press the ENT Key.

Use the small FMS Knob to enter the desired altitude.

Press the ENT Key.

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

DISPLAYING WIND DATA

Press the PFD Softkey.

Press the WIND Softkey to display wind data below the Selected Heading.

Press one of the OPTN softkeys to change how wind data is displayed.

To remove the Wind Data Window, press the OFF Softkey.

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Additional

Features Annun/Alerts Appendix Index

Flight Instruments

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

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Hazard

Avoidance

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

190-00664-01 Rev. A

Nav/Com/XPDR/Audio Panel

NAV/COM/TRANSPONDER/AUDIO PANEL

Instruments

Flight

ADF TUNING (OPTIONAL)

Tune the ADF using the remote ADF control head.

DME TUNING

Press the DME Softkey.

Turn the large FMS to select the DME source ﬁeld.

Turn the small FMS Knob to select the desired Nav radio.

Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

Press the XPDR Softkey to display the transponder mode selection softkeys.

Press the XPDR1 or XPDR2 Softkey to select the active transponder.

Press the CODE Softkey to display the transponder code selection softkeys, for digit entry.

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.

ACTIVATE ADS-B TRANSMIT

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Press the XPDR Softkey to display the transponder mode selection softkeys.

Press the ADS-B TX Softkey to enable transmission of three-dimensional aircraft position and aircraft heading.

Press the ADS-B TX Softkey again to disable transmission.

SELECTING A COM RADIO

Transmit/Receive

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

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, or

COM3 MIC Key (optional COM, if

Nav/Com/XPDR/Audio Panel

Receive Only

Flight

Instruments

Press the COM1, COM2 audio panel.

SELECTING A NAV RADIO

Nav/Com/

XPDR/AudioAFCSGPS Nav

To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).

Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together.

NAV/COM TUNING

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

Flight

PlanningProcedures

blue box highlights the radio frequency to be tuned.

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.

Press the Frequency Transfer Key to place the frequency into the active frequency ﬁeld.

, or

COM3 Key (optional COM, if installed) on the

INTERCOM

Hazard

Avoidance

Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may

FeaturesAnnun/AlertsAppendixIndex

Additional

select or deselect the intercom.

The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin. The annunciator is lit when the cabin intercom is active on either Audio Panel.

The MAN SQ Key allows either automatic or manual control of the intercom squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated by the MAN SQ annunciator.

During manual squelch operation, pressing the ICS Knob switches between volume and squelch adjustment, lighting the associated annunciator beneath the knob. When the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.

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Nav/Com/XPDR/Audio Panel

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels. PA messages are one way from the ﬂight deck to the passengers.

CLEARANCE RECORDER AND PLAYER

NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded audio to the Copilot.

Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block.

The PLAY Key controls the play function. The PLAY annunciator is illuminated to indicate when play is in progress. The PLAY annunciator extinguishes after playback is ﬁnished.

Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation. Pressing the PLAY Key again during play of a memory block stops play. If a COM input signal is detected during play of a recorded memory block, play is halted.

Pressing the PLAY Key twice within one-half second while audio is playing plays the previous block of recorded audio. Each subsequent two presses of the PLAY Key within one-half second backtracks through the recorded memory blocks to reach and play any recorded block.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

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

Nav/Com/XPDR/Audio Panel

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

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Avoidance

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

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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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

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

Takeoff (on ground)

Go Around (in air)TOGA

Takeoff (on ground)

Go Around (in air)TOGA

A LT Key Roll Hold (default) ROL Altitude Hold A LT

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

APR Key Approach**

GPS

VAPP

LOC

Pitch Hold (default)

Glidepath

Glideslope

PIT GP GS

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

APR

Key press activates ﬂight director.

***The selected navigation receiver must have a valid LOC signal before BC Key press activates ﬂight

director.

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Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

AFCS

VERTICAL MODES

Flight

Instruments

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Nav/Com/

XPDR/AudioAFCSGPS Nav

Selected Altitude Armed

Altitude Hold Holds the current Altitude Reference ALT Key A LT nnnnn f T

Vertical Speed

Flight Level Change, IAS Hold

Flight

PlanningProcedures

Flight Level Change, Mach Hold

VNAV

VNAV Target

Hazard

Altitude Armed

Avoidance

Glidepath

FeaturesAnnun/AlertsAppendixIndex

Additional

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 VNAV Target Altitude

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

may be used to climb/descend to the Selected Altitude

AFCS armed to capture the altitude displayed in the Selected Altitude window

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 the VNAV ﬂight path

AFCS armed to capture the altitude displayed in the VNAV Target Altitude window

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 attitude and wings level in the air

(default) PIT

* ALTS

VS Key VS nnnn f p m

FLC nnn k T

FLC Key

FLC M .nnn

VNV

Key

** ALTV

APR Key

Switch

VPTH

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

190-00664-01 Rev. A

AFCS

LATERAL MODES

Instruments

Flight

Lateral Mode Description Control Annunciation

Roll Hold

Holds current aircraft roll attitude or rolls wings level, depending

(default) ROL

XPDR/Audio AFCS GPS Nav

Nav/Com/

on commanded bank angle

Low Bank

Heading Select

Navigation, GPS Arm/ Capture/Track

Navigation, VOR Enroute Arm/Capture/Track

Navigation, LOC Arm/ Capture/Track

Limits maximum commanded roll angle

Captures and tracks Selected Heading

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

BANK

Key

HDG

Key

NAV

Key

HDG

GPS

VOR

LOC

Planning Procedures

Flight

(No Glideslope) Backcourse Arm/Capture/

Track Approach, GPS Arm/

Capture/Track Approach, VOR Arm/

Capture/Track Approach, ILS Arm/

Capture/Track (Glideslope Mode

Captures and tracks a localizer signal for backcourse approaches

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

BC Key BC

VAPP

APR Key

GPS

LOC

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

automatically armed)

Disengages autopilot and

Takeoff (on ground)

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

Switch

Disengages autopilot and

Go Around (in air)

commands a constant pitch

angle and wings level in the 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.

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

AFCS

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

190-00664-01 Rev. A

GPS NAVIGATION

GPS Navigation

Instruments

Flight

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

Press the Direct-to

Enter the waypoint identiﬁer.

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

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

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

Enter the desired altitude.

Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9.

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

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

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 on the Control Unit.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Direct-to Navigation from the PFD

Press the Direct-to Key

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

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

Press the ENT Key.

The cursor is now ﬂashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 6.

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

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

( )

on the PFD.

GPS Navigation

Turn the small FMS Knob to enter the desired altitude.

Flight

Instruments

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

10)

Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance ﬁeld.

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 ‘CRS’ 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.

Flight

PlanningProcedures

ACTIVATE A STORED FLIGHT PLAN

Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired ﬂight plan

Hazard

Avoidance

Select the ACTIVE Softkey. The conﬁrmation window is now displayed.

With ‘OK’ highlighted, press the ENT Key to activate the ﬂight plan. To cancel the ﬂight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and

FeaturesAnnun/AlertsAppendixIndex

Additional

press the ENT Key.

ACTIVATE A FLIGHT PLAN LEG

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.

Select the ACT LEG Softkey.

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.

With ‘Activate’ highlighted, press the ENT Key.

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

190-00664-01 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

Press the FPL Key on the Control Unit to display the Active Flight Plan Page.

Press the MENU Key to display the Page Menu Window.

Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the ﬂight plan. This will not delete the stored ﬂight plan, only the active ﬂight plan.

VERTICAL NAVIGATION (VNAV)

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

Small Light

Blue Text

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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

190-00664-01 Rev. A 15

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

Additional

Features Annun/Alerts Appendix Index

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

Flight

Instruments

or approach for giving vertical ﬂight path guidance outside the FAF. Note that these altitudes will be displayed as small light blue text.

Altitudes that have been designated for use in vertical navigation may also be made

Nav/Com/

“non-designated” by placing the cursor over the desired altitude and pressing the CLR

XPDR/AudioAFCSGPS Nav

Key. The altitude is now displayed only as a reference. It will not be used to give ﬂight path vertical guidance. Other displayed altitudes may change due to re-calculations or rendered invalid as a result of manually changing an altitude to a non-designated altitude.

White Text Light Blue Text Light Blue

Subdued Text

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

Large Text

Small Text

Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical ﬂight path guidance.

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

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

Altitude is designated for use in giving vertical ﬂight path guidance. Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database.

The system cannot use this altitude in determining vertical ﬂight path guidance.

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

190-00664-01 Rev. A

Flight Planning

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD and the Control Unit 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 Weight Planning Pge.

Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight ﬁeld.

Enter the desired aircraft empty weight.

Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ ﬁeld.

Enter the desired weight of Pilot & Stores.

Press the ENT Key.

Continue repeating these steps until all desired weights have been entered.

Entering Fuel Parameters

FMS

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Press the FMS Knob to activate the cursor.

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

Turn the small FMS Knob to enter the desired fuel quantity.

Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ ﬁeld.

Turn the small FMS Knob to enter the desired reserve fuel quantity.

Press the FMS Knob to remove the cursor.

Press the ENT Key.

TRIP PLANNING

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

Turn the small FMS Knob to select the Trip Planning Page.

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

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Flight Planning

For Direct-to planning:

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

Or:

For point-to-point planning:

Or:

For ﬂight plan leg planning:

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

If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’.

Press the ENT Key and the ﬂashing cursor moves to the ending waypoint ﬁeld.

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

Enter the identiﬁer of the starting waypoint.

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

Again, enter the identiﬁer of the ending waypoint.

Press the ENT Key to accept the waypoint.

Select the FPL Softkey (at the bottom of the display).

Turn the small FMS Knob to select the desired ﬂight plan (already stored in memory), by number.

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

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.

NOTE: The page mode must be set to ‘MANUAL’ to perform the following steps.

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.

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

190-00664-01 Rev. A

Flight Planning

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

The ﬂashing cursor moves to the ground speed (GS) ﬁeld. Enter the ground speed. Press the

ENT

Key when ﬁnished. Note that in ‘automatic’ page

mode, ground speed is provided by the system.

The ﬂashing cursor moves to the fuel ﬂow ﬁeld. Enter the fuel ﬂow. Press the ENT Key when ﬁnished. Note that in ‘AUTOMATIC’ page mode, fuel ﬂow is provided by the system.

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.

10)

The ﬂashing cursor moves to the calibrated airspeed (CALIBRATED AS) ﬁeld.

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

11)

The ﬂashing cursor moves to the altitude (IND ALTITUDE) ﬁeld. Enter the

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

12)

The ﬂashing cursor moves to the barometric setting (PRESSURE) ﬁeld. Enter

the desired baro setting. Press the ENT Key when ﬁnished. Note that in ‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered on the PFD.

13)

The ﬂashing cursor moves to the air temperature (TOTAL AIR TEMP) ﬁeld. Enter

the desired air temperature. Press the ENT Key when ﬁnished. Note that in ‘AUTOMATIC’ page mode, air temperature is provided by the system outside air temperature.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

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

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

Select the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

190-00664-01 Rev. A 19

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

Flight Planning

The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. If desired, the waypoint

Flight

Instruments

can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.

Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key to place a check-mark in the box.

The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. Turn the small FMS Knob to display a list of waypoint types.

Turn the small FMS Knob to select LAT/LON (latitude and longitude).

Press the ENT Key.

CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER

WAYPOINTS

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

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

Select the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.

Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.

Press the ENT Key to place a check-mark in the box.

The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. Turn the small FMS Knob to display a list of waypoint types.

Turn the small FMS Knob to select RAD/RAD (radial/radial).

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ ﬁeld. With the ﬁrst

waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

When a ﬂight plan is active, turning the small FMS Knob to the left will display a list of the ﬂight plan waypoints.

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

190-00664-01 Rev. A

Flight Planning

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

Repeat step 10 to enter the next waypoint name.

14)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld for the

second waypoint. Enter the desired radial from the reference waypoint.

15)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

16)

Press the FMS Knob to remove the ﬂashing cursor.

190-00664-01 Rev. A 21

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

Flight Planning

CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

ANOTHER WAYPOINT

Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page group.

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

Select the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.

Press the ENT Key to place a check-mark in the box.

The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. Turn the small FMS Knob to display a list of waypoint types.

Turn the small FMS Knob to select RAD/DIS (radial/distance).

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ ﬁeld. With the ﬁrst

waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

When a ﬂight plan is active, turning the small FMS Knob to the left will display a list of the ﬂight plan waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

190-00664-01 Rev. A

Flight Planning

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

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

distance from the reference waypoint.

14)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

15)

Press the FMS Knob to remove the ﬂashing cursor.

DELETE A USER WAYPOINT

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

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

Press the FMS Knob to activate the cursor.

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

Turn the small FMS Knob to highlight the desired waypoint.

Select the DELETE Softkey.

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

190-00664-01 Rev. A 23

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

Additional

Features Annun/Alerts Appendix Index

Flight Planning

CREATE A NEW FLIGHT PLAN

Flight

Using the MFD

Instruments

Press the FPL Key on the Control Unit.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

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

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

Enter the identiﬁer of the departure waypoint.

Press the ENT Key.

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

When all waypoints have been entered, press the FMS Knob to return to the

Flight

PlanningProcedures

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.

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

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

activated.

Press the FPL Key on the PFD.

Press the FMS Knob to activate the cursor.

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

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

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

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

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

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

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

190-00664-01 Rev. A

Flight Planning

IMPORT A FLIGHT PLAN FROM AN SD CARD

Insert the SD card containing the ﬂight plan in the top card slot on the MFD.

Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.

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

Press the FMS Knob to activate the cursor.

Turn either FMS Knob to highlight an empty or existing ﬂight plan.

Select the IMPORT Softkey.

If an empty ﬂight plan is selected, a list of the available ﬂight plans on the SD card will be displayed.

Or:

If an existing ﬂight plan is selected, an ‘Overwrite existing ﬂight plan? OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the selected ﬂight plan and see a list of the available ﬂight plans on the SD card. If overwriting the existing ﬂight plan is not desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select another existing or empty ﬂight plan, and again select the IMPORT Softkey.

Turn the small FMS Knob to highlight the desired ﬂight plan for importing.

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Press the FPL Key on the Control Unit to display the active ﬂight plan.

Press the FMS Knob to activate the cursor.

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

Turn the small FMS Knob. The Waypoint Information Window is now displayed.

Enter the new ﬂight plan waypoint by one of the following:

Enter the user waypoint identiﬁer, facility, or city.

Press the ENT Key.

Or:

190-00664-01 Rev. A 25

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

Additional

Features Annun/Alerts Appendix Index

Flight Planning

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

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

ENTER AN AIRWAY IN A FLIGHT PLAN

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

is displayed.

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Press the FPL Key on the Control Unit.

Press the FMS Knob to activate the cursor (not required on the PFD).

Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time.

Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey, or press the MENU Key and select “Load Airway”(required on the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when an acceptable airway entry waypoint has been chosen (the waypoint ahead of the cursor position).

Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown ﬁrst in the list, followed by “all” altitude airways, and then high altitude airways.

Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted.

Press the ENT Key. The system returns to editing the ﬂight plan with the new airway inserted.

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Flight Planning

INVERT AN ACTIVE FLIGHT PLAN

Press the FPL Key to display the active ﬂight plan.

Press the MENU Key to display the Page Menu.

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

Press the ENT Key. The original ﬂight plan remains intact in its ﬂight plan catalog storage location.

With ‘OK’ highlighted, press the ENT Key to invert the ﬂight plan.

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

PLAN

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

Or:

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

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired ﬂight plan.

Select the EDIT Softkey.

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.

Press the CLR Key to display a conﬁrmation window.

With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

STORE A FLIGHT PLAN

After creating a ﬂight plan on either the PFD or MFD, it may be saved by pressing the MENU Key.

Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.

With ‘OK’ highlighted, press the ENT Key to store the ﬂight plan.

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Flight Planning

EDIT A STORED FLIGHT PLAN

Flight

Instruments

Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turn the large FMS Knob to highlight the desired ﬂight plan.

Select the EDIT Softkey.

Turn the large FMS Knob to place the cursor in the desired location.

Enter the changes, then press the ENT Key.

Press the FMS Knob to return to the Flight Plan Catalog Page.

DELETE A WAYPOINT FROM THE FLIGHT PLAN

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

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PlanningProcedures

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Avoidance

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Additional

activate the cursor.

Or:

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

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired ﬂight plan.

Select the EDIT Softkey.

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

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

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.

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

INVERT AND ACTIVATE A STORED FLIGHT PLAN

Press the FPL Key on the Control Unit.

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

Press the FMS Knob to activate the cursor.

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190-00664-01 Rev. A

Flight Planning

Turn the large FMS Knob to highlight the desired ﬂight plan.

Select the INVERT Softkey. ‘Invert and activate stored ﬂight plan?’ will be displayed.

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

Press the FPL Key on the Control Unit.

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

Press the FMS Knob to activate the cursor.

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

Select the COPY Softkey. A ‘Copy to ﬂight plan #?’ conﬁrmation window is displayed.

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.

DELETE A FLIGHT PLAN

Press the FPL Key on the Control Unit.

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

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XPDR/Audio AFCS GPS Nav

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Avoidance

Hazard

Press the FMS Knob to activate the cursor.

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

Select the DELETE Softkey. A ‘Delete ﬂight plan #?’ conﬁrmation window is displayed.

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.

GRAPHICAL FLIGHT PLAN CREATION

Press the FPL Key on the Control Unit to display the Active Flight Plan Page.

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.

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Flight Planning

The default insertion point is at the end of the ﬂight plan. If the selected

Flight

Instruments

waypoint is to be placed anywhere other than the end of the ﬂight plan, press the FMS Knob to activate the cursor. Waypoints are inserted the cursor. Turn the large FMS Knob to select the desired insertion point.

Select the LD WPT Softkey. The selected waypoint will be inserted at the

Nav/Com/

XPDR/AudioAFCSGPS Nav

selected point. The default user waypoint naming is USR000, USR001, USR002, and so on.

To change the user waypoint name, follow the procedure for modifying a user waypoint.

EXPORT A FLIGHT PLAN TO AN SD CARD

Insert the SD card into the top card slot on the MFD.

Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD.

Flight

PlanningProcedures

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

Press the FMS Knob to activate the cursor.

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

Select the EXPORT Softkey.

Press the ENT Key to conﬁrm the export.

ABOVE

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

190-00664-01 Rev. A

PROCEDURES

Procedures

Instruments

Flight

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

Press the PROC Key.

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

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

Turn the large FMS Knob to highlight the desired departure.

Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway.

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

Turn the large FMS Knob to highlight the desired transition.

Press the ENT Key.

With ‘LOAD?’ highlighted, press the ENT Key. The departure will be active when the ﬂight plan is active.

ACTIVATE A DEPARTURE LEG

Press the FPL Key to display the active ﬂight plan.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure.

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

With ‘ACTIVATE’ highlighted, press the ENT Key.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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Avoidance

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Additional

Features Annun/Alerts Appendix Index

LOAD AN ARRIVAL PROCEDURE

Press the PROC Key.

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

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

Turn the large FMS Knob to highlight the desired arrival.

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Procedures

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

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turn either FMS Knob to select the desired transition.

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

Turn the large FMS Knob to highlight the desired runway.

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

Press the FPL Key on the Control Unit to display the active ﬂight plan.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the TO waypoint of the desired leg

Flight

PlanningProcedures

within the arrival.

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

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

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FeaturesAnnun/AlertsAppendixIndex

Additional

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.

Press the PROC Key.

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

Press the ENT Key. A list of available approaches for the destination airport is displayed.

Turn either FMS Knob to highlight the desired approach.

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

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.

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190-00664-01 Rev. A

Procedures

Press the ENT Key. The cursor moves to the MINIMUMS ﬁeld.

If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small

FMS

Knob in the

direction of the green arrow to change the display from OFF to BARO.

Press the

FMS

ENT

Key. The cursor moves to the altitude ﬁeld. Turn the small

Knob to enter the published DA/MDA for the selected approach

procedure.

10)

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

highlighted.

11)

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

Selecting ‘LOAD?’ enters the selected approach procedure into the active ﬂight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the selected approach procedure into the active ﬂight plan and is immediately activated.

12)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

Press the PROC Key.

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

Press the ENT Key.

Instruments

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

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Avoidance

Hazard

ACTIVATE A VECTOR TO FINAL APPROACH FIX

Press the PROC Key.

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

Press the ENT Key.

The ﬁnal approach course becomes the active leg.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Press the PROC Key.

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

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

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the go-around button.

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Procedures

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

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HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option.

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.

Press the small FMS Knob to return to the Navigation Map Page.

STORMSCOPE® (OPTIONAL)

WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation.

Displaying Stormscope Lightning Data on the Navigation Map Page

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Press the MAP Softkey.

Select the STRMSCP Softkey. Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page.

Lightning Age Symbol

Strike is less than 6 seconds old

Strike is between 6 and 60 seconds old

Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old

Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode

With the Weather Group selected, press the ENT Key. The cursor ﬂashes on ‘STRMSCP LTNG’.

Turn the large FMS Knob to select ‘STRMSCP MODE’.

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Turn the small FMS Knob to display the ‘Cell/Strike’ window.

Flight

Instruments

Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.

Push the FMS Knob to return to the Navigation Map Page.

Clear Stormscope Lightning Data from the Navigation Map Page

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the MENU Key (with the Navigation Map Page displayed).

Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ ﬁeld and press the ENT Key.

NOTE:

after the execution of each turn. This is to ensure that the strike and/or cell

If heading input is lost, strikes and/or cells must be cleared manually

positions are depicted accurately in relation to the nose of the aircraft.

Stormscope Page

Flight

PlanningProcedures

Turn the large FMS Knob until the Map Page group is selected.

Turn the small FMS Knob select the Stormscope Page.

Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’

Select the Stormscope Page.

Select the MODE Softkey. The CELL and STRIKE Softkeys are displayed.

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Avoidance

Select the CELL Softkey to display ‘CELL’ data or select the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page.

FeaturesAnnun/AlertsAppendixIndex

Additional

NOTE: “Cell mode” uses a clustering program to identify clusters of electrical

activity that indicate cells.

Change the Viewing Mode Between 360˚ and 120˚

Select the Stormscope Page.

Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to display a 120˚ viewing area.

Select the CLEAR Softkey to remove all Stormscope lightning data from the display.

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Hazard Avoidance

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

Select the MAP Softkey.

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

Display METAR and TAF information on the Airport Information Page

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

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

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

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

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

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

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.

Instruments

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XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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Avoidance

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Additional

Features Annun/Alerts Appendix Index

Map Panning Information – Weather Data Link Page

Push in the Joystick to display the panning arrow.

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs.

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

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Hazard Avoidance

information but allows the user to press the ENT Key and select that

Flight

Instruments

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turbulence PIREPs

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Icing Potential

AIREPs

NEXRAD

Cloud Top

Cell Movement

XM Lightning

SIGMETs/AIRMETs

City Forecast

METARs

Cyclone Warnings

Freezing Levels

Surface Analysis

Winds Aloft

TRAFFIC SYSTEMS

Flight

PlanningProcedures

• IfTrafcinformationService(TIS)iscongured,aSTANDBY, OPERATE, and TNA MUTE Softkey will be displayed.

• IfaTrafcAdvisorySystem(TAS)iscongured,aSTANDBY, NORMAL, TEST, and ALT MODE Softkey will be displayed.

Trafﬁc Symbol Description

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

Proximity Advisory (PA)(TAS only, not available with TIS)

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

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

Non-Threat Trafﬁc

Trafﬁc Advisory (TA)

County Warnings

Trafﬁc Symbol Description

Trafﬁc Information Service (TIS)

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

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

Trafﬁc Advisory Off Scale

190-00664-01 Rev. A

Hazard Avoidance

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

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

Turn the small FMS Knob to select the Trafﬁc Map Page.

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

Select the STANDBY Softkey to place the system in the Standby Mode. ‘STANDBY’ will be displayed in the Trafﬁc Mode ﬁeld.

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Select the TNA MUTE Softkey to mute the “Trafﬁc Not Available” aural alert.

Displaying Trafﬁc on the Navigation Map

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

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

Instruments

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Planning Procedures

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Avoidance

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Trafﬁc Advisory System (TAS) (Optional)

System Self Test

Set the range to 2/6 nm.

Select the STANDBY Softkey.

Select the TEST Softkey.

Self test will take approximately eight seconds to complete. When completed successfully, trafﬁc symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed (see Annuciations & Alerts section). If the self test fails, the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed.

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Displaying Trafﬁc on the Trafﬁc Map Page

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

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

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

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

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

Select the STANDBY Softkey to place the system in the Standby Mode. ‘STANDBY’ will be displayed in the Trafﬁc Mode ﬁeld.

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Displaying Trafﬁc on the Navigation Map

With the Navigation Map displayed, select the MAP Softkey.

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

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

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FeaturesAnnun/AlertsAppendixIndex

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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

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

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

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

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

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Display Terrain on the TAWS-B Page

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

Turn the small FMS Knob to select the TAWS-B Page.

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.

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Color Terrain/Obstacle Location

Red

Yellow

Black

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Enable/Disable Aviation Data

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

Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.

Press the ENT Key.

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TAWS Inhibit

Inhibit TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

Press the MENU Key.

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

Press the ENT Key.

Enable TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

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

Flight

Instruments

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

Press the ENT Key.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

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.

Flight

PlanningProcedures

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

Hazard

Avoidance

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

Turn the small FMS Knob to select the Weather Radar Page.

FeaturesAnnun/AlertsAppendixIndex

Additional

Select the MODE Softkey.

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.

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.

Turn the Joystick to select the desired range.

If desired, select the VERTICAL Softkey for vertical scanning.

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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:

Press the MENU Key

Turn the large FMS Knob to select ‘Show Tilt Line’.

Press the ENT Key.

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:

Press the MENU Key

Turn the large FMS Knob to select ‘Show Bearing Line’.

Press the ENT Key.

Vertically Scan a Storm Cell

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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.

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

Move the Joystick right or left to move the scanned “slice” a few degrees right or left.

Turn the Joystick to adjust the range.

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

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.

190-00664-01 Rev. A 43

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

Additional

Features Annun/Alerts Appendix Index

Hazard Avoidance

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

Flight

Instruments

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the FMS Knob to remove the cursor.

Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be displayed in the ‘GAIN’ ﬁeld.

Ground Mapping

Select the MODE Softkey.

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

Select the BACK Softkey.

Sector Scan

Flight

PlanningProcedures

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.

Press the FMS Knob to display the cursor.

Turn the large FMS Knob to place the cursor in the SECTOR SCAN ﬁeld.

Hazard

Avoidance

Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.

If desired, readjust the Bearing Line with the Joystick to change the center of the Sector Scan.

Press the FMS Knob to remove the cursor.

FeaturesAnnun/AlertsAppendixIndex

Additional

Antenna Stabilization

To activate or deactivate the antenna stabilization, select the MODE Softkey.

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.

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

190-00664-01 Rev. A

Hazard Avoidance

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating and deactivating will also enable or inhibit the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon landing the system will automatically switch to Standby Mode.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00664-01 Rev. A 45

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

Additional

Features Annun/Alerts Appendix Index

Hazard Avoidance

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

190-00664-01 Rev. A

Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION

WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and trafﬁc avoidance. SVS is intended as an aid to situational awareness only and may not provide the accuracy and/or ﬁdelity upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or trafﬁc.

WARNING: Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing.

Synthetic Vision System (SVS) functionality is offered as an optional enhancement to the G1000 system.

SVS is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot’s perspective. SVS information is shown on the primary ﬂight display (PFD).

In addition to SVS enhancement to the PFD, the following features have been added to the PFD:

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Trafﬁc

• Airport Signs

• Runway Display

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Displaying SVS Terrain

Press the PFD Softkey.

Press the SYN VIS Softkey.

Press the SYN TERR Softkey.

Press the BACK Softkey to return to the previous page.

190-00664-01 Rev. A 47

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

Additional Features

Displaying Pathways

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the PATHWAY Softkey.

Press the BACK Softkey to return to the previous page.

Displaying Heading on the Horizon

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the HRZN HDG Softkey.

Press the BACK Softkey to return to the previous page.

Flight

PlanningProcedures

Displaying Airport Signs

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the APTSIGNS Softkey.

Hazard

Avoidance

Press the BACK Softkey to return to the previous page.

TERMINAL PROCEDURE CHARTS

FeaturesAnnun/AlertsAppendixIndex

Additional

NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in

electronic form, it is still advisable to carry another source of charts on-board the aircraft.

SafeTaxi

SafeTaxi® is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport. The airport display on the map reveals runways with numbers, taxiways identiﬁers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. The aircraft symbol provides situational awareness while taxiing.

Selecting the DCLTR Softkey (declutter) once removes the taxiway markings and airport identiﬁcation labels. Selecting the DCLTR Softkey twice removes VOR station

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

190-00664-01 Rev. A

Additional Features

ID, the VOR symbol, and intersection names if within the airport plan view. Selecting the DCLTR Softkey a third time removes the airport runway layout, unless the airport in view is part of an active route structure. Selecting 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 most approach charts and on airport diagrams.

The ChartView database is updated on a 14-day cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView will no longer function.

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. Current aircraft position is not displayed on FliteCharts.

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

View Charts from the Navigation Map Page

Select the SHW CHRT Softkey when displayed.

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

Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS are only available with ChartView.

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

190-00664-01 Rev. A 49

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

Additional Features

View Charts from the Active Flight Plan Page

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

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

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

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

Change Day/Night View

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

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

Flight

PlanningProcedures

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

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

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

Hazard

Avoidance

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.

FeaturesAnnun/AlertsAppendixIndex

Additional

Press the FMS Knob when ﬁnished to remove the Chart Setup Menu.

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

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

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

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

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

190-00664-01 Rev. A

Additional Features

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.

Select the CATGRY Softkey on the XM Radio Page.

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

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

Press the ENT Key.

Select an Available Channel within the Selected Category

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

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

Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels.

With the desired channel highlighted, press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Entering a Channel Directly

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

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

Using the numeric keys, enter the desired channel number.

Press the ENT Key to activate the selected channel.

190-00664-01 Rev. A 51

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

Additional Features

Assigning Channel Presets

Flight

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

Instruments

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

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

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

Adjusting Volume

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

Radio volume is controlled at each passenger station.

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

190-00664-01 Rev. A

ANNUNCIATIONS & ALERTS

ADVISORY ANNUNCIATIONS

Annunciation

Window Text

AVN FAN 1 FAIL

AVN FAN 2 FAIL

PFD 1 FAN FAIL PFD #1 cooling fan is inoperative. PFD 2 FAN FAIL

MFD FAN FAIL

Avionics cooling fan #1 is inoperative.

Avionics cooling fan #2 is inoperative.

PFD #2 cooling fan is inoperative.

MFD cooling fan is inoperative..

Annunciations & Alerts

Alerts Window Text

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

COMPARATOR ANNUNCIATIONS

Comparator Window

Text

ALT MISCOMP

IAS MISCOMP

HDG MISCOMP

PIT MISCOMP ROL MISCOMP

ALT NO COMP

IAS NO COMP

HDG NO COMP

PIT NO COMP ROL 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..

Condition

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 53

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

Annunciations & Alerts

REVERSIONARY SENSOR ANNUNCIATIONS

Flight

Reversionary

Instruments

Sensor Window

Text

BOTH ON ADC1

Nav/Com/

XPDR/AudioAFCSGPS Nav

BOTH ON ADC2

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON GPS1 BOTH ON GPS2

USING ADC1 USING ADC2

Flight

PlanningProcedures

USING AHRS1 USING AHRS2

USING GPS1 USING GPS2

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.

PFD2 is displaying data from the #1 Air Data Computer.

PFD1 is displaying data from the #2 Air Data Computer.

PFD2 is displaying data from the #1 AHRS.

PFD1 is displaying data from the #2 AHRS.

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

Condition

AFCS ALERTS

Hazard

Avoidance

Condition Annunciation Description

Pitch Failure Pitch axis control failure.

FeaturesAnnun/AlertsAppendixIndex

Additional

Roll Failure Roll axis control failure.

Pitch Trim Axis Control Failure

Yaw Damper Failure

System Failure AP and MET are unavailable. FD may still be available.

Elevator Mistrim Up

Elevator Mistrim Down

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

If annunciated when AP is engaged, a failure has occurred in the pitch trim system.

YD control failure.

A condition has developed causing the pitch servo to provide a sustained force in the nose up direction.

A condition has developed causing the pitch servo to provide a sustained force in the nose down direction.

190-00664-01 Rev. A

Annunciations & Alerts

Condition Annunciation Description

Aileron Mistrim Left

Aileron Mistrim Right

Rudder Mistrim Left

Rudder Mistrim Right

Preﬂight Test Performing preﬂight system test. Upon completion of the

A condition has developed causing the roll servo to provide a sustained left force.

A condition has developed causing the roll servo to provide a sustained right force.

A condition has developed causing the yaw servo to provide a sustained force.

test, the aural alert will be heard.

Preﬂight system test has failed.

TAWS ALERTS

Alert Type

Excessive Descent Rate Warning (EDR)

Reduced Required Terrain Clearance Warning (RTC)

Imminent Terrain Impact Warning (ITI)

Reduced Required Obstacle Clearance Warning (ROC)

PFD/MFD TAWS-B Page Annunciation

MFD

Pop-Up Alert

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up; Ter-

rain Ahead, Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 55

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

Annunciations & Alerts

Flight

Alert Type

Instruments

Imminent Obstacle Impact Warning

Nav/Com/

(IOI)

XPDR/AudioAFCSGPS Nav

Reduced Required Terrain Clearance Caution (RTC)

Imminent Terrain Impact Caution (ITI)

Flight

PlanningProcedures

Reduced Required Obstacle Clearance Caution (ROC)

Imminent Obstacle

Hazard

Avoidance

Impact Caution (IOI)

FeaturesAnnun/AlertsAppendixIndex

Additional

Premature Descent Alert Caution (PDA)

Altitude Callout “500”

Excessive Descent Rate Caution (EDR)

Negative Climb Rate Caution (NCR)

PFD/MFD TAWS-B Page Annunciation

MFD

Pop-Up Alert

Aural Message

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

“Caution, Terrain; Caution,

“Terrain Ahead; Terrain

“Caution, Terrain; Caution,

“Caution, Obstacle; Cau-

tion, Obstacle”

“Obstacle Ahead; Obstacle

“Caution, Obstacle;

Caution, Obstacle”

“Too Low, Terrain”

None None “Five-Hundred”

“Don’t Sink”

“Too Low, Terrain”

Terrain”

Ahead”

Terrain”

Ahead”

“Sink Rate”

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

190-00664-01 Rev. A

Annunciations & Alerts

TAWS System Status Annunciations

PFD/MFD

Alert Type

TAWS-B Page

Annunciation

TAWS System Test Fail None “TAWS System Failure”

TAWS Alerting is disabled None None

No GPS position or excessively degraded GPS signal

System Test in progress None None

System Test pass None None Chime

MFD

Pop-Up Alert

Aural Message

None “TAWS Not Available”

“TAWS Available” will be heard when sufﬁcient GPS signal is re-established.

AURAL ALERTS

Aural Alert Description

“Minimums” The aircraft has descended below the preset minimum descent altitude or

decision altitude.

“Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical

navigation is enabled.

“Trafﬁc” Played when a Trafﬁc Advisory (TA) is issued with the TIS system.

“Trafﬁc Not Available” The aircraft is outside the Trafﬁc Information Service (TIS) coverage area.

“Trafﬁc, Trafﬁc” Played when ﬁrst Trafﬁc Advisory (TA) is issued with an optional TAS system.

“Trafﬁc” for each subsequent TA.

“Trafﬁc Advisory System Test Passed”

“Trafﬁc Advisory System Test Failed”

“Skywatch System Test Passed”

“Skywatch System Test Failed”

Played when the optional KTA 870 or Skywatch HP TAS system passes a pilot-initiated self test.

Played when the optional KTA 870 or Skywatch HP TAS system fails a pilotinitiated self test.

Played when the optional SKY497 TAS system passes a pilot-initiated self test (optional).

Played when the optional SKY497 TAS system fails a pilot-initiated self test (optional).

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 57

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

Annunciations & Alerts

FLIGHT PLAN IMPORT/EXPORT MESSAGES

Flight

In some circumstances, some messages may appear in conjunction with others.

Instruments

Flight Plan Import/

Export Results

‘Flight plan successfully

Nav/Com/

XPDR/AudioAFCSGPS Nav

imported.’

‘File contained user waypoints only. User waypoints imported successfully. No stored ﬂight plan data was modiﬁed.’

‘No ﬂight plan ﬁles found to import.’

‘Flight plan import failed.’ Flight plan data was not successfully imported from the SD card.

‘Flight plan partially imported.’

Flight

PlanningProcedures

‘File contained user waypoints only.’

‘Too many points. Flight plan truncated.’

‘Some waypoints not loaded.

Hazard

Avoidance

Waypoints locked.’

‘User waypoint database full.

FeaturesAnnun/AlertsAppendixIndex

Additional

Not all loaded.’

‘One or more user waypoints renamed.’

‘Flight plan successfully exported.’

‘Flight plan export failed.’ The stored ﬂight plan was not successfully exported to the SD card.

A ﬂight plan ﬁle stored on the SD card was successfully imported as a stored ﬂight plan.

The ﬁle stored on the SD card did not contain a ﬂight plan, only user waypoints. These waypoints have been saved to the system user waypoints. No ﬂight plans stored in the system have been modiﬁed.

The SD card contains no ﬂight plan data.

Some ﬂight plan waypoints were successfully imported from the SD card, however others had errors and were not imported. A partial stored ﬂight plan now exists in the system.

The ﬁle stored on the SD card did not contain a ﬂight plan, only user waypoints. One or more of these waypoints did not import successfully.

The ﬂight plan on the SD card contains more waypoints than the system can support. The ﬂight plan was imported with as many waypoints as possible.

The ﬂight plan on the SD card contains one or more waypoints that the system cannot ﬁnd in the navigation database. The ﬂight plan has been imported, but must be edited within the system before it can be activated for use.

The ﬂight plan ﬁle on the SD card contains user waypoints. The quantity of stored user waypoints has exceeded system capacity, therefore not all the user waypoints on the SD card have been imported. Any ﬂight plan user waypoints that were not imported are locked in the ﬂight plan. The ﬂight plan must be edited within the system before it can be activated for use.

One or more imported user waypoints were renamed when imported due to naming conﬂicts with waypoints already existing in the system.

The stored ﬂight plan was successfully exported to the SD card.

The SD card may not have sufﬁcient available memory or the card may have been removed prematurely.

Description

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

190-00664-01 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Message Comments

DATA LOST

lost. Recheck settings.

– Pilot stored data was

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

XTALK ERROR

crosstalk error has occurred.

PFD1 SERVICE

– A ﬂight display

– PFD1 needs

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

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

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

service. Return unit for repair.

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

– MFD1 software

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

mismatch, communication halted.

PFD1 CONFIG

Conﬁg service req’d.

– PFD1 conﬁg error.

The PFD conﬁguration settings do not match backup conﬁguration memory. The system

PFD2 CONFIG

– PFD2 conﬁg error.

should be serviced.

Conﬁg service req’d.

MFD1 CONFIG

error. Conﬁg service req’d.

– MFD1 conﬁg

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

SW MISMATCH

version mismatch. Xtalk is off.

– GDU software

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 59

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

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Flight

Instruments

PFD1 COOLING

cooling. Reducing power usage.

Nav/Com/

PFD2 COOLING

XPDR/AudioAFCSGPS Nav

cooling. Reducing power usage.

MFD1 COOLING

Message Comments

– PFD1 has poor

The PFD and/or MFD is overheating and is

– PFD2 has poor

reducing power consumption by dimming the display. If problem persists, the system should

– MFD1 has poor

be serviced.

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

Flight

Key is stuck.

PlanningProcedures

CNFG MODULE

conﬁguration module is inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

Hazard

Avoidance

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

FeaturesAnnun/AlertsAppendixIndex

Additional

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

– PFD1

– PFD1 has low

– PFD2 has low

– MFD1 has low

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

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

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

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

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

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.

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 system should be serviced.

190-00664-01 Rev. A

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 system should be serviced.

database error exists.

MFD1 DB ERR

– MFD1 terrain

database missing.

PFD1 DB ERR

– PFD1 terrain

database missing.

PFD2 DB ERR

– PFD2 terrain

The terrain database is present on another LRU, but is missing on the speciﬁed LRU.

database missing.

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 system should be serviced.

database error exists.

MFD1 DB ERR

– MFD1 obstacle

database missing.

PFD1 DB ERR

– PFD1 obstacle

database missing.

PFD2 DB ERR

– PFD2 obstacle

The obstacle database is present on another LRU, but is missing on the speciﬁed LRU.

database missing.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 61

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

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

Instruments

MFD1 DB ERR

terrain database error exists.

Nav/Com/

PFD1 DB ERR

XPDR/AudioAFCSGPS Nav

terrain database error exists.

PFD2 DB ERR

Message Comments

– MFD1 airport

The MFD and/or PFD detected a failure in the

– PFD1 airport

airport terrain database. Ensure that the data card is properly inserted. Replace data card. If

– PFD2 airport

problem persists, the system should be serviced.

terrain database error exists.

MFD1 DB ERR

– MFD1 airport

terrain database missing.

PFD1 DB ERR

– PFD1 airport

terrain database missing.

PFD2 DB ERR

Flight

terrain database missing.

PlanningProcedures

MFD1 DB ERR

– PFD2 airport

– MFD1 Safe Taxi

database error exists.

PFD1 DB ERR

– PFD1 Safe Taxi

database error exists.

PFD2 DB ERR

database error exists.

Hazard

Avoidance

MFD1 DB ERR

– PFD2 Safe Taxi

– MFD1 Chartview

database error exists.

FeaturesAnnun/AlertsAppendixIndex

Additional

The airport terrain database is present on another LRU, but is missing on the speciﬁed LRU.

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 system should be serviced.

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

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

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

DB MISMATCH

database version mismatch. Xtalk is off.

– Aviation

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

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

190-00664-01 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

DB MISMATCH

database type mismatch. Xtalk is off.

– Aviation

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

DB MISMATCH

version mismatch.

– Terrain database

The PFDs and MFD have different terrain database versions installed. Install correct terrain database version in all displays.

DB MISMATCH

type mismatch.

– Terrain database

The PFDs and MFD have different terrain database types installed. Install correct terrain database type in all displays.

DB MISMATCH

database version mismatch.

– Obstacle

The PFDs and MFD have different obstacle database versions installed. Install correct obstacle database version in all displays.

DB MISMATCH

database mismatch.

– Airport Terrain

The PFDs and MFD have different airport terrrain databases installed. Install correct airport terrain database in all displays.

GMA 1347D MESSAGE ADVISORIES

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Message Comments GMA1 FAIL GMA2 FAIL

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

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

GMA XTALK

has occurred.

– GMA crosstalk error

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

GMA1 CONFIG

error. Conﬁg service req’d.

– GMA1 conﬁg

The audio panel conﬁguration settings do not match backup conﬁguration memory. The system

GMA2 CONFIG

– GMA2 conﬁg

should be serviced.

error. Conﬁg service req’d.

190-00664-01 Rev. A 63

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

Additional

Features Annun/Alerts Appendix Index

Annunciations & Alerts

GMA 1347D MESSAGE ADVISORIES (CONT.)

Flight

Instruments

Message Comments

MANIFEST – GMA1 software

mismatch, communication halted.

Nav/Com/

MANIFEST – GMA2 software

XPDR/AudioAFCSGPS Nav

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

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

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

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

Flight

PlanningProcedures

Conﬁg service req’d.

– GIA1 conﬁg error.

The GIA1 and/or GIA2 conﬁguration settings do not match backup conﬁguration memory. The

GIA2 CONFIG

– GIA2 conﬁg error.

system should be serviced.

Conﬁg service req’d.

GIA1 CONFIG

error. Conﬁg service req’d.

GIA2 CONFIG

Hazard

Avoidance

error. Conﬁg service req’d.

GIA1 COOLING

temperature too low.

FeaturesAnnun/AlertsAppendixIndex

Additional

GIA2 COOLING

– GIA1 audio conﬁg

– GIA2 audio conﬁg

– GIA1

– GIA2

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

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

temperature too low.

GIA1 COOLING

temperature.

– GIA1 over

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

GIA2 COOLING

– GIA2 over

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 system should be

GIA2 SERVICE

– GIA2 needs

serviced.

service. Return the unit for repair.

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

190-00664-01 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

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.

MANIFEST

– GIA1 software

– GIA2 software

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

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

COM1 TEMP

Reducing transmitter power.

COM2 TEMP

Reducing transmitter power.

COM1 SERVICE

service. Return unit for repair.

– GFC software

– COM1 over temp.

– COM2 over temp.

– COM1 needs

Incorrect servo software is installed, or gain settings are incorrect.

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

The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable.

COM2 SERVICE

– COM2 needs

The system should be serviced when possible.

service. Return unit for repair.

COM1 PTT

key is stuck.

COM2 PTT

key is stuck.

– COM1 push-to-talk

– COM2 push-to-talk

The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced.

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 system should be serviced.

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

GPS integrity is insufﬁcient for the current phase of ﬂight.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 65

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

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

Instruments

GPS NAV LOST

Message Comments

– Loss of GPS

navigation. Insufﬁcient satellites.

Nav/Com/

GPS NAV LOST

XPDR/AudioAFCSGPS Nav

– 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

Flight

Change HDG reference to TRUE.

PlanningProcedures

GPS1 SERVICE

– True north approach.

– GPS1 needs

service. Return unit for repair.

GPS2 SERVICE

– GPS2 needs

service. Return unit for repair.

NAV1 SERVICE

Hazard

Avoidance

service. Return unit for repair.

NAV2 SERVICE

service. Return unit for repair.

FeaturesAnnun/AlertsAppendixIndex

Additional

NAV1 RMT XFR

– NAV1 needs

– NAV2 needs

– NAV1 remote

transfer key is stuck.

NAV2 RMT XFR

– NAV2 remote

transfer key is stuck.

G/S1 FAIL

G/S2 FAIL

– G/S1 is inoperative.

– G/S2 is inoperative.

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.

Vertical guidance generated by WAAS is unavailable, use LNAV only minimums.

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

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

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

A failure has been detected in glideslope receiver 1 and/or receiver 2. The system should be serviced.

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

190-00664-01 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

G/S1 SERVICE

service. Return unit for repair.

G/S2 SERVICE

service. Return unit for repair.

– G/S1 needs

– G/S2 needs

A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The system should be serviced when possible.

GEA 71 MESSAGE ADVISORIES

Message Comments

GEA1 CONFIG

Conﬁg service req’d.

– GEA1 conﬁg error.

The GEA1 conﬁguration settings do not match those of backup conﬁguration memory. The system should be serviced.

GEA2 CONFIG

Conﬁg service req’d.

– GEA2 conﬁg error.

The GEA2 conﬁguration settings do not match those of backup conﬁguration memory. The system should be serviced.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

– GEA1 software

– GEA2 software

The #1 GEA 71 has incorrect software installed. The system should be serviced.

The #2 GEA 71 has incorrect software installed. The system should be serviced.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

GTX 33 MESSAGE ADVISORIES

Message Comments

XPDR1 CONFIG

error. Conﬁg service req’d.

– XPDR1 conﬁg

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

XPDR2 CONFIG

error. Conﬁg service req’d.

– XPDR2 conﬁg

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

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

190-00664-01 Rev. A 67

– GTX1 software

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

– GTX2 software

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

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

Additional

Features Annun/Alerts Appendix Index

Annunciations & Alerts

GTX 33 MESSAGE ADVISORIES (CONT.)

Flight

Instruments

XPDR1 SRVC

Message Comments

– XPDR1 needs

service. Return unit for repair.

Nav/Com/

XPDR/AudioAFCSGPS Nav

XPDR2 SRVC

– XPDR2 needs

service. Return unit for repair.

XPDR1 FAIL

– XPDR1 is

inoperative.

XPDR2 FAIL

– XPDR2 is

inoperative.

GRS 77 MESSAGE ADVISORIES

The #1 transponder should be serviced when possible.

The #2 transponder should be serviced when possible.

There is no communication with the #1 transponder.

There is no communication with the #2 transponder.

Flight

PlanningProcedures

AHRS1 TAS

– AHRS1 not receiving

valid airspeed.

AHRS2 TAS

– AHRS2 not receiving

valid airspeed.

Hazard

Avoidance

AHRS1 GPS

GPS source.

FeaturesAnnun/AlertsAppendixIndex

Additional

AHRS2 GPS

GPS source.

AHRS1 GPS

any GPS information.

AHRS2 GPS

any GPS information.

Message Comments

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

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

– AHRS1 using backup

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

– AHRS2 using backup

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

– AHRS1 not receiving

The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced.

– AHRS2 not receiving

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

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

190-00664-01 Rev. A

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES (CONT.)

Message Comments

AHRS1 GPS

backup GPS information.

AHRS2 GPS

backup GPS information.

AHRS1 GPS

exclusively in no-GPS mode.

AHRS2 GPS

exclusively in no-GPS mode.

AHRS MAG DB

model database version mismatch.

AHRS1 SRVC

ﬁeld model needs update.

AHRS2 SRVC

ﬁeld model needs update.

GEO LIMITS

North/South, no magnetic compass.

– AHRS1 not receiving

– AHRS2 not receiving

– AHRS1 operating

– AHRS2 operating

– AHRS magnetic

– AHRS1 Magnetic-

– AHRS2 Magnetic-

– AHRS1 too far

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

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

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

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

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.

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

GEO LIMITS

– AHRS2 too far

as invalid.

North/South, no magnetic compass.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

– GRS1 software

– GRS2 software

The #1 AHRS has incorrect software installed. The system should be serviced.

The #2 AHRS has incorrect software installed. The system should be serviced.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 69

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

Annunciations & Alerts

GMU 44 MESSAGE ADVISORIES

Flight

Instruments

HDG FAULT

Message Comments

– AHRS1

magnetometer fault has occurred.

Nav/Com/

XPDR/AudioAFCSGPS Nav

HDG FAULT

– AHRS2

magnetometer fault has occurred.

MANIFEST

– GMU1 software

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

Flight

PlanningProcedures

– GMU2 software

GDL 69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

– GDL 69 conﬁg

error. Conﬁg service req’d.

Hazard

Avoidance

GDL69 FAIL

FeaturesAnnun/AlertsAppendixIndex

Additional

MANIFEST

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

– GDL software

mismatch, communication halted.

A fault has occurred in the #1 GMU 44. Heading is ﬂagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced.

A fault has occurred in the #2 GMU 44. Heading is ﬂagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced.

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

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

receiver is unavailable. The system should be serviced

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

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

190-00664-01 Rev. A

Annunciations & Alerts

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 recieving status packet from the

– GWX needs

service. Return unit for repair.

MANIFEST

– GWX software

mismatch, communication halted.

WX ALERT

– Possible severe

weather ahead.

GDC 74B MESSAGE ADVISORIES

Message Comments

ADC1 ALT EC

– ADC1 altitude error

correction is unavailable.

ADC2 ALT EC

– ADC2 altitude error

correction is unavailable.

ADC1 AS EC

– ADC1 airspeed error

correction is unavailable.

ADC2 AS EC

– ADC2 airspeed error

correction is unavailable.

MANIFEST

– GDC1 software

mismatch, communication halted.

MANIFEST

– GDC2 software

mismatch, communication halted.

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

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 system should be serviced.

Possible severe weather detected within +/- 10 degrees of the aircraft heading at a range of 80 to 320 nm.

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

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

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 71

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

Annunciations & Alerts

GCU 475 MESSAGE ADVISORIES

Flight

Instruments

GCU CNFG

Message Comments

– GCU Conﬁg error.

Conﬁg service req’d.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GCU FAIL

MANIFEST

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

– GCU software

mismatch, communication halted.

GCU KEYSTK

– GCU [key name]

Key is stuck.

Flight

PlanningProcedures

GMC 710 MESSAGE ADVISORIES

Message Comments

GMC CONFIG

– GMC Conﬁg error.

Conﬁg service req’d.

GMC FAIL

Hazard

Avoidance

MANIFEST

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

– GMC software

mismatch. Communication halted.

GMC KEYSTK

FeaturesAnnun/AlertsAppendixIndex

Additional

Key is stuck.

– GMC [key name]

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. 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 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 system should be serviced if the problem persists.

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

190-00664-01 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES

Message Comments

FPL WPT LOCK

waypoint is locked.

– Flight plan

Upon power-up, the 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

– Timer has expired. The system notiﬁes the pilot that the timer has

expired.

DB CHANGE

Verify user modiﬁed procedures.

– Database changed.

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

Verify stored airways.

– Database changed.

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 73

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

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

Instruments

LOCKED FPL

locked ﬂight plan.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

– Cannot navigate

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

– Arriving at

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

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

turn.

INSIDE ARSPC ARSPC AHEAD

less than 10 minutes.

Flight

PlanningProcedures

ARSPC NEAR

ahead.

ARSPC NEAR

than 2 nm.

APR INACTV

active.

Hazard

Avoidance

SLCT FREQ

frequency for approach.

FeaturesAnnun/AlertsAppendixIndex

Additional

– Inside airspace. The aircraft is inside the airspace.

– Airspace ahead

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

– Airspace near and

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

– Airspace near – less

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

– Approach is not

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

– 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

approach.

– Select NAV on CDI for

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

PTK FAIL

unavailable: bad geometry.

PTK FAIL

unavailable: invalid leg type.

– Parallel track

Bad parallel track geometry.

Invalid leg type for parallel offset.

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

190-00664-01 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

PTK FAIL

past IAF.

UNABLE V WPT

current vertical waypoint.

– Parallel track unavailable:

– Can’t reach

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 automatically transitions 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 prevents vertical guidance to the active vertical waypoint.

VNV

– Unavailable. Excessive track

angle error.

VNV

– Unavailable. Excessive

crosstrack error.

VNV

– Unavailable. Parallel course

selected.

NO WGS84 WPT

– Non WGS 84

waypoint for navigation -[xxxx]

The current track angle error exceeds the limit, causing the vertical deviation to go invalid.

The current crosstrack exceeds the limit, causing 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.

– Trafﬁc device has

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

STRMSCP FAIL

failed.

FAILED PATH

failed.

– Stormscope has

– A data path has

Stormscope has failed. The G1000™ system should be serviced.

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A 75

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

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

Instruments

MAG VAR WARN

variance. Verify all course angles.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

– Large magnetic

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°.

SVS

– SVS DISABLED: Out of

available terrain region.

Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database.

SVS

– SVS DISABLED: Terrain DB

resolution too low.

Synthetic Vision is disabled because a terrain database of sufﬁcient resolution (9 arc-second or better) is not currently installed.

SCHEDULER [#]

Flight

PlanningProcedures

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

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

190-00664-01 Rev. A

APPENDIX

ALERTS

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

STRMSC P

ALERTS

Appendix

Instruments

Flight

PFD SOFTKEY MAP

Top Level PFD Softkeys

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

INSET

OFF

DCLTR (3)

190-00664-01 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

Additional

Features Annun/Alerts Appendix Index

Appendix

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

BACK

ADC2

ADC1

AHRS1

AHRS2

ALERTS

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

SENSOR

FeaturesAnnun/AlertsAppendixIndex

Additional

TRAFFIC

TOPO

TERRAIN

STRMSCP

NEXRAD

XM LTNG

ADC1

ADC2

AHRS1

AHRS2

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

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

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

190-00664-01 Rev. A

PFD Conﬁguration Softkeys

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

ALT UNI T

METERS IN HPA

DME

ALERTS

BACK

ALERTS

360 HSI

ARC HSI

HSI FMT

SYN V IS

SYN TERR

HRZN HDG

PAT HWAY

APTSIGNS ALERTS

Appendix

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

PFD

190-00664-01 Rev. A

SYN VIS

PATHWAY

SYN TERR

HRZN HDG

APTSIGNS

additional PFD conﬁgurations

Displays the softkeys for enabling or disabling Synthetic Vision features

Displays rectangular boxes representing the horizontal and vertical ﬂight path of the active ﬂight plan

Enables synthetic terrain depiction

Displays compass heading along the Zero-Pitch line

Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identiﬁers are displayed when the airport is within approximately 9 nm.

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

Displays second-level softkeys for

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Appendix

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

DFLTS

WIND

DME

BRG1

HSI FRMT

BRG2

ALT UNIT

OPTN 1

OPTN 2

OPTN 3

OFF

360 HSI

ARC HSI

METERS

Resets PFD to default settings, including changing units to standard

Displays softkeys to select wind data parameters

Direction arrow and numeric speed

Direction arrow with numeric direction and magnitude

Headwind/tailwind and crosswind arrows with numeric 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

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

190-00664-01 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

ADS-B TX

Appendix

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

XPDR

XPDR1

XPDR2

STBY

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.

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A

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

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

STRMSC P

VFR

Flight

Instruments

CODE

Nav/Com/

XPDR/AudioAFCSGPS Nav

IDENT

ADS-B TX

TMR/REF

Flight

PlanningProcedures

NRST

ALERT

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

Activates/deactivates transmission of the aircraft’s three-dimensional position and aircraft heading for reception by ADS-B systems.

Displays Timer/References Window

Displays Nearest Airports Window

Displays Alerts Window

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

MFD Softkeys

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

190-00664-01 Rev. A

MAP

DCLTR (3)

SHW CHRT

CHKLIST

TRAFFIC

TOPO

TERRAIN

AIRWAYS

STRMSCP

NEXRAD

XM LTNG

BACK

Appendix

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

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00664-01 Rev. A

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

Appendix

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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

190-00664-01 Rev. A

Garmin C90A-GT Reference Guide

Specifications and Main Features

Frequently Asked Questions

User Manual

Flight Instruments

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

SYNCHRONIZE CDI

CHANGE NAVIGATION SOURCES

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

GENERIC TIMER

CONFIGURE VSPEED BUGS INDIVIDUALLY

TURN VSPEED BUGS ON OR OFF BY CATEGORY

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

DISPLAYING WIND DATA

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

DME TUNING

ENTER A TRANSPONDER CODE

ACTIVATE ADS-B TRANSMIT

SELECTING A COM RADIO

SELECTING A NAV RADIO

NAV/COM TUNING

INTERCOM

PASSENGER ADDRESS (PA) SYSTEM

CLEARANCE RECORDER AND PLAYER

AUTOMATIC FLIGHT CONTROL SYSTEM

FLIGHT DIRECTOR ACTIVATION

VERTICAL MODES

LATERAL MODES

GPS NAVIGATION

DIRECT-TO NAVIGATION

ACTIVATE A STORED FLIGHT PLAN

ACTIVATE A FLIGHT PLAN LEG

STOP NAVIGATING A FLIGHT PLAN

VERTICAL NAVIGATION (VNAV)

Flight Planning

WEIGHT PLANNING

TRIP PLANNING

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

DELETE A USER WAYPOINT

CREATE A NEW FLIGHT PLAN

IMPORT A FLIGHT PLAN FROM AN SD CARD

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

ENTER AN AIRWAY IN A FLIGHT PLAN

INVERT AN ACTIVE FLIGHT PLAN

STORE A FLIGHT PLAN

EDIT A STORED FLIGHT PLAN

DELETE A WAYPOINT FROM THE FLIGHT PLAN

INVERT AND ACTIVATE A STORED FLIGHT PLAN

COPY A FLIGHT PLAN

DELETE A FLIGHT PLAN

GRAPHICAL FLIGHT PLAN CREATION

EXPORT A FLIGHT PLAN TO AN SD CARD

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

ACTIVATE A DEPARTURE LEG

LOAD AN ARRIVAL PROCEDURE

ACTIVATE AN ARRIVAL LEG

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

ACTIVATE A VECTOR TO FINAL APPROACH FIX

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Hazard Avoidance

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

STORMSCOPE® (OPTIONAL)

XM WEATHER (OPTIONAL)

TRAFFIC SYSTEMS

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

AIRBORNE COLOR WEATHER RADAR

Additional Features

SYNTHETIC VISION

TERMINAL PROCEDURE CHARTS

XM® RADIO ENTERTAINMENT

ANNUNCIATIONS & ALERTS

ADVISORY ANNUNCIATIONS

COMPARATOR ANNUNCIATIONS

REVERSIONARY SENSOR ANNUNCIATIONS