Garmin Beechcraft 200, Beechcraft B200 Reference Guide

®

G1000

Cockpit Reference Guide for the Beechcraft 200/B200 Series

Integrated Flight Deck

System Software 0985.00 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

Copyright © 2008 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0985.00 or later for the Beechcraft
200 and B200. Some differences in operation may be observed when comparing the information in
this manual to earlier or later software versions.

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

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

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

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

Web Site Address: www.garmin.com

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

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

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

November, 2008 190-00929-00 Rev. A Printed in the U.S.A.

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain 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 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 Beechcraft 200/B200 Series

190-00929-00 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 200/
B200 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
200 and B200 King Air Airplane Flight Manual Supplement. Thoroughly
practice basic operation prior to actual use. During flight operations, carefully
compare indications from the G1000 to all available navigation sources,
including the information from other NAVAIDs, visual sightings, charts, etc.
For safety purposes, always resolve any discrepancies before continuing
navigation.

190-00929-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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 Beechcraft 200/B200 Series

190-00929-00 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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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Warnings, Cautions & Notes

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Record of Revisions

Part Number Change Summary

190-00929-00 Initial release

Revision Date of Revision Affected Pages Description

A November, 2008 All Production release

190-00929-00 Rev. A RR-1

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Record of Revisions

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

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/Radar Altimeter Minimum Descent Altitude ......................................... 3

Testing the Radar Altimeter ................................................................................................... 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

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Table of Contents

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

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

Waypoint ................................................................................................................................... 21

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

Create a New Flight Plan ...................................................................................................... 23

Import a Flight Plan from an SD Card ................................................................................ 24

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

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

Invert An Active Flight Plan .................................................................................................. 26

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

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

Edit a Stored Flight Plan ....................................................................................................... 27

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

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

Copy a Flight Plan ................................................................................................................... 28

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

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

Export a Flight Plan to an SD Card ..................................................................................... 29

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 ........................................................................................................... 45

Synthetic Vision ....................................................................................................................... 45

Terminal Procedure Charts ...................................................................................................46

XM® Radio Entertainment..................................................................................................... 48

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Table of Contents

ANNUNCIATIONS & ALERTS ................................................................................................... 51

Advisory Annunciations......................................................................................................... 51

Comparator Annunciations ................................................................................................... 51

Reversionary Sensor Annunciations ................................................................................... 52

AFCS Alerts ............................................................................................................................... 52

TAWS Alerts .............................................................................................................................. 53

Aural Alerts .............................................................................................................................. 55

MFD & PFD Message Advisories .......................................................................................... 56

Database Message Advisories ............................................................................................. 57

GMA 1347D Message Advisories ......................................................................................... 60

GIA 63W Message Advisories ............................................................................................... 61

GEA 71 Message Advisories .................................................................................................. 64

GTX 33 Message Advisories .................................................................................................. 64

GRS 77 Message Advisories .................................................................................................. 65

GMU 44 Message Advisories ................................................................................................ 67

GDL 69A Message Advisories ............................................................................................... 67

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

GDC 74B Message Advisories ............................................................................................... 68

GCU 477 Message Advisories ............................................................................................... 69

GMC 710 Message Advisories .............................................................................................. 69

Miscellaneous Message Advisories ..................................................................................... 70

APPENDIX ....................................................................................................................................... 75

PFD Softkey Map .................................................................................................................... 75

MFD Softkey Map ................................................................................................................... 80

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

Push the BARO Knob to select standard pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

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

2)

Press the ALT UNIT Softkey.

3)

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

Or

:

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

4)

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

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

Turn the

small

FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

Turn the

190-00929-00 Rev. A 1

small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

1)

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.

2)

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.

3)

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

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)

Press the OBS Softkey to select OBS Mode.

2)

Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next

waypoint.

Flight

PlanningProcedures

3)

Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)

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

Hazard

2)

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.

3)

Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.

CONFIGURE VSPEED BUGS INDIVIDUALLY

1)

Press the TMR/REF Softkey.

2)

Turn the

3)

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

4)

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

2

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

large

FMS Knob to highlight the desired Vspeed.

190-00929-00 Rev. A

Flight Instruments

5)

Turn the

6)

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

small

FMS Knob clockwise to ON or counterclockwise to OFF.

TURN VSPEED BUGS ON OR OFF BY CATEGORY

1)

Press the TMR/REF Softkey.

2)

Press the MENU Key.

3)

Turn the FMS Knob to highlight the desired option.

4)

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

SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

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

3)

Turn the small FMS Knob clockwise to select BARO or RAD ALT.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

TESTING THE RADAR ALTIMETER

1)

Select the AUX-SYSTEM STATUS Page on the MFD.

2)

Select the RA TEST Softkey. The Radar Altitude window displays 50 feet,
indicating a properly functioning system.

3)

Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.

DISPLAYING WIND DATA

1)

Press the PFD Softkey.

2)

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

3)

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

4)

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

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Additional

Features Annun/Alerts Appendix Index

Flight Instruments

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

4

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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

1)

Press the DME Softkey.

2)

Turn the large FMS to select the DME source field.

3)

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

4)

Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

1)

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

2)

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

3)

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

4)

Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.

ACTIVATE ADS-B TRANSMIT

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

1)

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

2)

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

3)

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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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

, 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

1)

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

2)

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

NAV/COM TUNING

1)

Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.

Flight

2)

PlanningProcedures

Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.

3)

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

, 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

select or deselect the intercom.

Additional

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 Beechcraft 200/B200 Series

Nav/Com/XPDR/Audio Panel

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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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

or

APR

Key press activates flight director.

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

director.

190-00929-00 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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

GA

Switch

VPTH

GP

GS

TO

GA

10

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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

TO

GA

Switch

Disengages autopilot and

Go Around (in air)

commands a constant pitch

GA

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.

190-00929-00 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

AFCS

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

12

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

GPS NAVIGATION

GPS Navigation

Instruments

Flight

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

1)

Press the Direct-to

2)

Enter the waypoint identifier.

3)

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

4)

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

5)

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

6)

Enter the desired altitude.

7)

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

8)

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

9)

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

10)

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

11)

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

12)

Press the ENT Key to activate.

( )

Key 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

1)

Press the Direct-to Key

2)

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

3)

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

4)

Press the ENT Key.

5)

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

6)

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

190-00929-00 Rev. A 13

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

( )

on the PFD.

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude.

8)

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.

9)

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

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan

4)

Hazard

Avoidance

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

5)

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

FeaturesAnnun/AlertsAppendixIndex

Additional

press the ENT Key.

ACTIVATE A FLIGHT PLAN LEG

14

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.

2)

Select the ACT LEG Softkey.

OR

Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from

the PFD.

3)

With ‘Activate’ highlighted, press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

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

2)

Press the MENU Key to display the Page Menu Window.

3)

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

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

190-00929-00 Rev. A 15

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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.

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

16

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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.

1)

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

2)

Enter the desired aircraft empty weight.

3)

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

4)

Enter the desired weight of Pilot & Stores.

5)

Press the ENT Key.

6)

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

Entering Fuel Parameters

FMS

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

1)

Press the FMS Knob to activate the cursor.

2)

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

3)

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

4)

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

5)

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

6)

Press the FMS Knob to remove the cursor.

7)

Press the ENT Key.

TRIP PLANNING

1)

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

2)

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

3)

The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL
Softkey.

190-00929-00 Rev. A 17

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Flight Planning

4)

For Direct-to planning:

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

a)

b)

c)

d)

Or:

For point-to-point planning:

a)

b)

c)

d)

Or:

For flight plan leg planning:

a)

b)

c)

d)

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.

18

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

5)

Turn the large FMS Knob to highlight the departure time (DEP TIME) field.

NOTE: The departure time on the Trip Planning Page is used for preflight

planning. Refer to the Utility Page for the actual flight departure time.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

6)

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

7)

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

8)

The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.

9)

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

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

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

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.

b)

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

7)

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

8)

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

9)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 19

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Flight Planning

CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

WAYPOINTS

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

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

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.

b)

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

7)

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

8)

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

9)

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:

a)

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

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

20

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

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

16)

Press the FMS Knob to remove the flashing cursor.

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

ANOTHER WAYPOINT

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

190-00929-00 Rev. A 21

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Flight Planning

6)

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

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

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.

a)

b)

7)

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

8)

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

9)

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:

a)

b)

c)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.

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

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.

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.

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.

22

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

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.

15)

Press the FMS Knob to remove the flashing cursor.

DELETE A USER WAYPOINT

1)

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

2)

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

3)

Press the FMS Knob to activate the cursor.

4)

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

5)

Turn the small FMS Knob to highlight the desired waypoint.

6)

Select the DELETE Softkey.

7)

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

CREATE A NEW FLIGHT PLAN

Using the MFD

1)

Press the FPL Key on the Control Unit.

2)

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

3)

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

190-00929-00 Rev. A 23

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Flight Planning

4)

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

5)

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Enter the identifier of the departure waypoint.

6)

Press the ENT Key.

7)

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

8)

When all waypoints have been entered, press the FMS Knob to return to the
Flight Plan Catalog Page. The new flight plan is now in the list.

Using the PFD

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

using the PFD.

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

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

activated.

1)

Press the FPL Key on the PFD.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

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

5)

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

6)

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

7)

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

8)

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

IMPORT A FLIGHT PLAN FROM AN SD CARD

1)

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

2)

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

24

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

3)

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

4)

Press the FMS Knob to activate the cursor.

5)

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

6)

Press 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 press the IMPORT Softkey.

7)

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

8)

Press the ENT Key.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

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

5)

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

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 25

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Flight Planning

Or:

a)

Flight

Instruments

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

b)

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

ENTER AN AIRWAY IN A FLIGHT PLAN

1)

Press the FPL Key on the Control Unit.

2)

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

3)

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

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

point should be entered at this time.

4)

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

5)

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

altitude airways, and then high altitude airways.

6)

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

7)

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

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

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

4)

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

5)

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

26

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

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

PLAN

1)

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

Or:

a)

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

b)

Press the FMS Knob to activate the cursor.

c)

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

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.

3)

Press the CLR Key to display a confirmation window.

4)

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

STORE A FLIGHT PLAN

1)

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

2)

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

3)

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

EDIT A STORED FLIGHT PLAN

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

Select the EDIT Softkey.

5)

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

6)

Enter the changes, then press the ENT Key.

7)

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

190-00929-00 Rev. A 27

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Flight Planning

DELETE A WAYPOINT FROM THE FLIGHT PLAN

Flight

Instruments

1)

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

Or:

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

a)

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

b)

Press the FMS Knob to activate the cursor.

c)

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

d)

Select the EDIT Softkey.

2)

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

3)

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

4)

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

5)

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

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

Press the FPL Key on the Control Unit.

2)

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

3)

Press the FMS Knob to activate the cursor.

4)

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

5)

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

6)

With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.

COPY A FLIGHT PLAN

1)

Press the FPL Key on the Control Unit.

2)

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

3)

Press the FMS Knob to activate the cursor.

28

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Flight Planning

4)

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

5)

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

6)

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

DELETE A FLIGHT PLAN

1)

Press the FPL Key on the Control Unit.

2)

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

3)

Press the FMS Knob to activate the cursor.

4)

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

5)

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

6)

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

GRAPHICAL FLIGHT PLAN CREATION

1)

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

2)

Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.

3)

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

4)

Select the LD WPT Softkey. The selected waypoint will be inserted at the
selected point. The default user waypoint naming is USR000, USR001, USR002,
and so on.

5)

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

ABOVE

Instruments

XPDR/Audio AFCS GPS Nav

Planning Procedures

Avoidance

Features Annun/Alerts Appendix Index

Flight

Nav/Com/

Flight

Hazard

Additional

EXPORT A FLIGHT PLAN TO AN SD CARD

1)

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

2)

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

190-00929-00 Rev. A 29

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Flight Planning

3)

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

Flight

4)

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Press the FMS Knob to activate the cursor.

5)

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

6)

Press the EXPORT Softkey.

7)

Press the ENT Key to confirm the export.

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

30

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

PROCEDURES

Procedures

Instruments

Flight

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

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

3)

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

4)

Turn the large FMS Knob to highlight the desired departure.

5)

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

6)

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

7)

Turn the large FMS Knob to highlight the desired transition.

8)

Press the ENT Key.

9)

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

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

LOAD AN ARRIVAL PROCEDURE

1)

Press the PROC Key.

2)

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

3)

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

4)

Turn the large FMS Knob to highlight the desired arrival.

190-00929-00 Rev. A 31

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Procedures

5)

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

Flight

6)

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turn either FMS Knob to select the desired transition.

7)

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

8)

Turn the large FMS Knob to highlight the desired runway.

9)

Press the ENT Key.

10)

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

11)

The arrival will become part of the active flight plan.

ACTIVATE AN ARRIVAL LEG

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

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

Flight

PlanningProcedures

arrival.

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

32

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

1)

Press the PROC Key.

2)

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

3)

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

4)

Turn either FMS Knob to highlight the desired approach.

5)

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

6)

Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Procedures

7)

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

8)

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.

9)

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

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

4)

The final approach course becomes the active leg.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

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

3)

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

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the go-around button.

190-00929-00 Rev. A 33

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Procedures

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

34

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

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

2)

Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.

3)

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

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

1)

Press the MAP Softkey.

2)

Press the STRMSCP Softkey. Press 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

1)

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

2)

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

190-00929-00 Rev. A 35

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Hazard Avoidance

3)

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

4)

Flight

Instruments

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

5)

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

1)

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

2)

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

NOTE:

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

1)

PlanningProcedures

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

2)

Turn the small FMS Knob select the Stormscope Page.

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

1)

Select the Stormscope Page.

2)

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

Hazard

Avoidance

Press the CELL Softkey to display ‘CELL’ data or press 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˚

1)

Select the Stormscope Page.

36

2)

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

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

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

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

1)

Press the MAP Softkey.

2)

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

Display METAR and TAF information on the Airport Information Page

1)

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

2)

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

3)

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

Displaying Weather on the Weather Data Link Page

1)

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

2)

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

3)

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

4)

Select the LEGEND Softkey to view the legends for the selected products.
If necessary, turn either FMS Knob to scroll through the list. Press the small

FMS Knob or the ENT Key to return to the map.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Map Panning Information – Weather Data Link Page

1)

Push in the Joystick to display the panning arrow.

2)

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

3)

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

Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more

190-00929-00 Rev. A 37

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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, OPERATE, 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.

38

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Traffic Advisory Off Scale

190-00929-00 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

1)

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

2)

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

3)

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

4)

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

5)

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

Displaying Traffic on the Navigation Map

1)

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

2)

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Traffic Advisory System (TAS) (Optional)

System Self Test

1)

Set the range to 2/6 nm.

2)

Press the STANDBY Softkey.

3)

Press the TEST Softkey.

4)

Self test will take approximately eight seconds to complete. When
completed successfully, traffic symbols will be displayed and a voice alert
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.

Displaying Traffic on the Traffic Map Page

1)

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

2)

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Hazard Avoidance

3)

Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

displayed in the Traffic Mode field.

4)

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

5)

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

6)

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

Displaying Traffic on the Navigation Map

1)

With the Navigation Map displayed, press the MAP Softkey.

2)

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

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.

Hazard

Avoidance

Manual System Test

1)

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

FeaturesAnnun/AlertsAppendixIndex

Additional

2)

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

3)

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

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

Display Terrain on the TAWS Page

1)

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

2)

Turn the small FMS Knob to select the TAWS Page.

3)

If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.

40

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Hazard Avoidance

4)

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

1)

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

2)

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

3)

Press the ENT Key.

TAWS Inhibit

Inhibit TAWS

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

Or

:

1)

Press the MENU Key.

2)

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

3)

Press the ENT Key.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

Enable TAWS

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

Or

:

1)

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

2)

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

3)

Press the ENT Key.

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.

190-00929-00 Rev. A 41

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Hazard Avoidance

AIRBORNE COLOR WEATHER RADAR

Flight

Instruments

WARNING: Begin transmitting only when it is safe to do so. If it is desired to

transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.

Nav/Com/

XPDR/AudioAFCSGPS Nav

CAUTION: In Standby Mode, the antenna is parked at the center line. It

is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.

Displaying Weather on the Weather Radar Page

1)

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

2)

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

Flight

3)

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

Select the MODE Softkey.

4)

If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.

Or

:

If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.

5)

Turn the Joystick to select the desired range.

6)

If desired, select the VERTICAL Softkey for vertical scanning.

Adjusting Antenna Tilt

Move the

Joystick

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

tor the displayed tilt value in the TILT field.

When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt

of the antenna. If the Tilt Line is not displayed, perform the following steps:

1)

Press the MENU Key

2)

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

3)

Press the ENT Key.

42

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Hazard Avoidance

Adjusting Antenna Bearing

Move the

Joystick

right or left to adjust the azimuth position of the antenna right

or left. Monitor the displayed bearing value in the BEARING field.

When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:

1)

Press the MENU Key

2)

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

3)

Press the ENT Key.

Vertically Scan a Storm Cell

1) While in the Horizontal Scan view, move the Joystick to place the Bearing

Line on the desired storm cell, or other area, to be vertically scanned.

2)

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

3)

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

4)

Turn the Joystick to adjust the range.

5)

To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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.

1)

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

2)

Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.

3)

Press the FMS Knob to remove the cursor.

4)

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

190-00929-00 Rev. A 43

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Hazard Avoidance

Ground Mapping

Flight

1)

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Select the MODE Softkey.

2)

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

3)

Select the BACK Softkey.

Sector Scan

1)

While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.

2)

Press the FMS Knob to display the cursor.

3)

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

4)

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

5)

If desired, readjust the Bearing Line with the Joystick to change the center

Flight

PlanningProcedures

of the Sector Scan.

6)

Press the FMS Knob to remove the cursor.

Antenna Stabilization

1)

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

2)

Select the STAB ON Softkey to activate antenna stabilization or select

Hazard

Avoidance

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®)

FeaturesAnnun/AlertsAppendixIndex

To activate or deactivate the WATCH® feature, select the WATCH Softkey. This

Additional

feature is only available in the Horizontal Scan Mode.

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating

and deactivating will also enable or inhibit the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon

landing the system will automatically switch to Standby Mode.

44

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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 either the accuracy or reliability upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles,
or traffic.

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

Displaying SVS Terrain

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

Press the SYN TERR Softkey.

4)

Press the BACK Softkey to return to the previous page.

Displaying Pathways

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the PATHWAY Softkey.

5)

Press the BACK Softkey to return to the previous page.

190-00929-00 Rev. A 45

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional Features

Displaying Heading on the Horizon

Flight

1)

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the HRZN HDG Softkey.

5)

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the APTSIGNS Softkey.

5)

Press the BACK Softkey to return to the previous page.

Flight

PlanningProcedures

TERMINAL PROCEDURE CHARTS

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

Hazard

Avoidance

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,

FeaturesAnnun/AlertsAppendixIndex

Additional

control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.

Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams aid in following ground control instructions by accurately displaying
the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services. This database is updated on a 56-day cycle.

46

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Additional Features

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.

View Charts from the Navigation Map Page

1)

Press the SHW CHRT Softkey when displayed.

Or

:

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

2)

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

3)

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

View Charts from the Active Flight Plan Page

1)

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

2)

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

3)

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

4)

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

190-00929-00 Rev. A 47

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional Features

Change Day/Night View

Flight

1)

Instruments

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

2)

Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and

Nav/Com/

XPDR/AudioAFCSGPS Nav

press the ENT Key.

3)

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

4)

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

5)

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

6)

In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is

Flight

PlanningProcedures

the day/night crossover point based on backlighting intensity.

7)

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

Hazard

Avoidance

1)

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

2)

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

FeaturesAnnun/AlertsAppendixIndex

Additional

Page.

3)

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

Active Channel and Channel List

The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.

48

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Additional Features

Selecting a Category

The Category Box of the XM Radio Page displays the currently selected category

of audio.

1)

Select the CATGRY Softkey on the XM Radio Page.

2)

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

Or

:

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

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

1)

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

2)

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

Or

:

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

3)

With the desired channel highlighted, press the ENT Key.

Entering a Channel Directly

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

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

2)

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

3)

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

4)

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

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

1)

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

2)

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

190-00929-00 Rev. A 49

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Additional Features

3)

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

Flight

Instruments

active channel.

4)

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

Adjusting Volume

Nav/Com/

XPDR/AudioAFCSGPS Nav

Radio volume is controlled at each passenger station.

Flight

PlanningProcedures

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

50

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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

WOW FAULT

WOW INVALID

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

Avionics cooling fan #1 is inoperative.

Avionics cooling fan #2 is inoperative.

PFD #2 cooling fan is inoperative.

MFD cooling fan is inoperative..

Miscompare between weight on wheels inputs.

Weight on wheels inputs invalid.

Difference in altitude sensors is > 200 ft.

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

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

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

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors..

Annunciations & Alerts

Alerts Window Text

Condition

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 51

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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

52

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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.

190-00929-00 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.

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

or

or

or

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

or

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up; Ter-

rain Ahead, Pull Up”

or

“Terrain, Terrain; Pull Up,

Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

or

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 53

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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;

or

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull

“Caution, Terrain; Caution,

or

“Terrain Ahead; Terrain

“Terrain Ahead; Terrain

or

“Caution, Terrain; Caution,

“Caution, Obstacle; Cau-

or

tion, Obstacle”

“Obstacle Ahead; Obstacle

“Obstacle Ahead; Obstacle

or

“Caution, Obstacle;

Caution, Obstacle”

“Too Low, Terrain”

None None “Five-Hundred”

“Don’t Sink”

or

“Too Low, Terrain”

or

Up, Pull Up”

Terrain”

or

Ahead”

Ahead”

or

Terrain”

or

Ahead”

Ahead”

or

“Sink Rate”

or

54

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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

None “TAWS Not Available”

Aural Message

“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 Sys-

tem 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

pilot-initiated 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

190-00929-00 Rev. A 55

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Flight

Instruments

DATA LOST

Message Comments

– Pilot stored data was

lost. Recheck settings.

Nav/Com/

XPDR/AudioAFCSGPS Nav

XTALK ERROR

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

Flight

PlanningProcedures

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

– MFD1 software

mismatch, communication halted.

Hazard

PFD1 CONFIG

Avoidance

– PFD1 config error.

Config service req’d.

PFD2 CONFIG

Config service req’d.

FeaturesAnnun/AlertsAppendixIndex

Additional

MFD1 CONFIG

– PFD2 config error.

– MFD1 config

error. Config service req’d.

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

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

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

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

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

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

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

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

56

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

PFD1 COOLING

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

MFD1 COOLING

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

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

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

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

Key is stuck.

CNFG MODULE

configuration module is
inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1

– PFD1 has low

– PFD2 has low

– MFD1 has low

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

DATABASE MESSAGE ADVISORIES

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 aviation

– PFD1 aviation

– PFD2 aviation

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.

database error exists.

190-00929-00 Rev. A 57

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

Instruments

MFD1 DB ERR

Message Comments

– MFD1 basemap

database error exists.

Nav/Com/

PFD1 DB ERR

XPDR/AudioAFCSGPS Nav

database error exists.

PFD2 DB ERR

– PFD1 basemap

– 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

Flight

database error exists.

PlanningProcedures

MFD1 DB ERR

– MFD1 terrain

– PFD1 terrain

– PFD2 terrain

– MFD1 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 missing.

PFD1 DB ERR

database missing.

PFD2 DB ERR

database missing.

Hazard

Avoidance

MFD1 DB ERR

database error exists.

PFD1 DB ERR

FeaturesAnnun/AlertsAppendixIndex

Additional

database error exists.

PFD2 DB ERR

– PFD1 terrain

– PFD2 terrain

– MFD1 obstacle

– PFD1 obstacle

– PFD2 obstacle

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

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.

58

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

terrain database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport

– PFD2 airport

The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the 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

– PFD2 airport

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

terrain database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Chartview

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 59

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

Instruments

DB MISMATCH

database type mismatch. Xtalk is
off.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

– 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.

Flight

PlanningProcedures

DB MISMATCH

database mismatch.

– Obstacle

– Airport Terrain

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

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

GMA 1347D MESSAGE ADVISORIES

Hazard

Avoidance

GMA1 FAIL
GMA2 FAIL

FeaturesAnnun/AlertsAppendixIndex

Additional

GMA XTALK

Message Comments

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

– GMA crosstalk error

has occurred.

GMA1 CONFIG

– GMA1 config

error. Config service req’d.

GMA2 CONFIG

– GMA2 config

error. Config service req’d.

60

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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

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

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

190-00929-00 Rev. A

Annunciations & Alerts

GMA 1347D MESSAGE ADVISORIES (CONT.)

Message Comments

MANIFEST – GMA1 software

mismatch, communication halted.

MANIFEST – GMA2 software

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

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

– GIA1 audio config

– GIA2 audio config

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

error. Config service req’d.

GIA1 COOLING

temperature too low.

– GIA1

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

GIA2 COOLING

– GIA2

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 61

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

Instruments

HW MISMATCH

Message Comments

– GIA hardware
mismatch. GIA1 communication
halted.

Nav/Com/

XPDR/AudioAFCSGPS Nav

HW MISMATCH

– GIA hardware
mismatch. GIA2 communication
halted.

MANIFEST

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

Flight

PlanningProcedures

COM1 TEMP

– GFC software

– COM1 over temp.

Reducing transmitter power.

COM2 TEMP

– COM2 over temp.

Reducing transmitter power.

COM1 SERVICE

service. Return unit for repair.

Hazard

Avoidance

COM2 SERVICE

– COM1 needs

– COM2 needs

service. Return unit for repair.

COM1 PTT

FeaturesAnnun/AlertsAppendixIndex

Additional

key is stuck.

COM2 PTT

– COM1 push-to-talk

– COM2 push-to-talk

key is stuck.

COM1 RMT XFR

– COM1 remote

transfer key is stuck.

COM2 RMT XFR

– COM2 remote

transfer key is stuck.

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

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

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

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.
The system should be serviced when possible.

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.

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.

GPS integrity is insufficient for the current phase
of flight.

62

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

GPS NAV LOST

navigation. Insufficient satellites.

GPS NAV LOST

navigation. Position error.

GPS NAV LOST

navigation. GPS fail.

ABORT APR

navigation. Abort approach.

APR DWNGRADE

downgraded.

TRUE APR

Change HDG reference to TRUE.

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Approach

– True north approach.

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’.

GPS1 SERVICE

service. Return unit for repair.

– GPS1 needs

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

GPS2 SERVICE

– GPS2 needs

available. The system should be serviced.

service. Return unit for repair.

NAV1 SERVICE

service. Return unit for repair.

– NAV1 needs

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

NAV2 SERVICE

– NAV2 needs

available. The system should be serviced.

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 remote

– NAV2 remote

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.

G/S1 FAIL

– G/S1 is inoperative.

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

G/S2 FAIL

– G/S2 is inoperative.

be serviced.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 63

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

Instruments

G/S1 SERVICE

Message Comments

– G/S1 needs

service. Return unit for repair.

Nav/Com/

G/S2 SERVICE

XPDR/AudioAFCSGPS Nav

– G/S2 needs

service. Return unit for repair.

GEA 71 MESSAGE ADVISORIES

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

GEA2 CONFIG

Flight

PlanningProcedures

Config service req’d.

MANIFEST

– GEA2 config error.

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

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.

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

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

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

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

Hazard

Avoidance

GTX 33 MESSAGE ADVISORIES

Message Comments

XPDR1 CONFIG

FeaturesAnnun/AlertsAppendixIndex

Additional

– XPDR1 config
error. Config service req’d.

XPDR2 CONFIG

– XPDR2 config
error. Config service req’d.

MANIFEST

– GTX1 software

mismatch, communication halted.

MANIFEST

– GTX2 software

mismatch, communication halted.

64

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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

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

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

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

190-00929-00 Rev. A

Annunciations & Alerts

GTX 33 MESSAGE ADVISORIES (CONT.)

Message Comments

XPDR1 SRVC

service. Return unit for repair.

XPDR2 SRVC

service. Return unit for repair.

XPDR1 FAIL

inoperative.

XPDR2 FAIL

inoperative.

– XPDR1 needs

– XPDR2 needs

– XPDR1 is

– XPDR2 is

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.

GRS 77 MESSAGE ADVISORIES

Message Comments

AHRS1 TAS

valid airspeed.

– AHRS1 not receiving

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.

AHRS2 TAS

valid airspeed.

– AHRS2 not receiving

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 GPS

GPS source.

– 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 GPS

GPS source.

– 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 GPS

any GPS information.

– AHRS1 not receiving

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

AHRS2 GPS

any GPS information.

– AHRS2 not receiving

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

190-00929-00 Rev. A 65

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES (CONT.)

Flight

Instruments

AHRS1 GPS

Message Comments

– AHRS1 not receiving

backup GPS information.

Nav/Com/

XPDR/AudioAFCSGPS Nav

AHRS2 GPS

– AHRS2 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

AHRS2 GPS

– AHRS2 operating

exclusively in no-GPS mode.

AHRS MAG DB

– AHRS magnetic

model database version mismatch.

AHRS1 SRVC

Flight

PlanningProcedures

field model needs update.

AHRS2 SRVC

– AHRS1 Magnetic-

– AHRS2 Magnetic-

field model needs update.

GEO LIMITS

– AHRS1 too far

North/South, no magnetic compass.

GEO LIMITS

Hazard

North/South, no magnetic compass.

Avoidance

MANIFEST

– AHRS2 too far

– GRS1 software

mismatch, communication halted.

MANIFEST

FeaturesAnnun/AlertsAppendixIndex

Additional

– GRS2 software

mismatch, communication halted.

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
as invalid.

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

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

66

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

GMU 44 MESSAGE ADVISORIES

Message Comments

HDG FAULT

– AHRS1

magnetometer fault has occurred.

HDG FAULT

– AHRS2

magnetometer fault has occurred.

MANIFEST

– GMU1 software

mismatch, communication halted.

MANIFEST

– GMU2 software

mismatch, communication halted.

GDL 69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

GDL69 FAIL

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 67

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

GWX 68 ALERT MESSAGES

Flight

Instruments

GWX CONFIG

Message Comments

– GWX config error.

Config service req’d.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

weather ahead.

Flight

PlanningProcedures

– Possible severe

GDC 74B MESSAGE ADVISORIES

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.

Message Comments

ADC1 ALT EC

correction is unavailable.

Hazard

Avoidance

ADC2 ALT EC

– ADC1 altitude error

– ADC2 altitude error

correction is unavailable.

ADC1 AS EC

FeaturesAnnun/AlertsAppendixIndex

Additional

correction is unavailable.

ADC2 AS EC

– ADC1 airspeed error

– ADC2 airspeed error

correction is unavailable.

MANIFEST

– GDC1 software

mismatch, communication halted.

MANIFEST

– GDC2 software

mismatch, communication halted.

68

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

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.

190-00929-00 Rev. A

Annunciations & Alerts

GCU 477 MESSAGE ADVISORIES

Message Comments

GCU CNFG

– GCU Config error.

Config service req’d.

GCU FAIL

MANIFEST

– GCU is inoperative. A failure has been detected in the GCU 477.

– GCU software

mismatch, communication halted.

GCU KEYSTK

– GCU [key name]

Key is stuck.

GMC 710 MESSAGE ADVISORIES

Message Comments

GMC CONFIG

– GMC Config error.

Config service req’d.

GMC FAIL

MANIFEST

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

– GMC software

mismatch. Communication halted.

GMC KEYSTK

– GMC [key name]

Key is stuck.

GCU 477 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The GCU 477 is unavailable.
The GCU 477 has incorrect software installed.

The G1000 system should be serviced.
A key is stuck on the GCU 477 bezel. Attempt

to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.

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.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 69

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES

Flight

Instruments

FPL WPT LOCK

waypoint is locked.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

– 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.

Flight

PlanningProcedures

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

Hazard

Avoidance

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

FeaturesAnnun/AlertsAppendixIndex

Additional

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.

70

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

LOCKED FPL

locked flight plan.

– 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.

– 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.

ARSPC NEAR

ahead.

ARSPC NEAR

than 2 nm.

APR INACTV

active.

– Airspace near and

– Airspace near – less

– Approach is not

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

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

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

SLCT FREQ

frequency for approach.

– Select appropriate

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

SLCT NAV

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

– Parallel track

Bad parallel track geometry.

Invalid leg type for parallel offset.

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A 71

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

Instruments

PTK FAIL

past IAF.

Nav/Com/

UNABLE V WPT

XPDR/AudioAFCSGPS Nav

current vertical waypoint.

Message Comments

– Parallel track unavailable:

IAF waypoint for parallel offset has been
passed.

– Can’t reach

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

Flight

PlanningProcedures

VNV

– Unavailable. Excessive track

angle error.

VNV

– Unavailable. Excessive

crosstrack error.

VNV

– Unavailable. Parallel course

selected.

Hazard

Avoidance

NO WGS84 WPT

– Non WGS 84

waypoint for navigation -[xxxx]

waypoint.
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.

FeaturesAnnun/AlertsAppendixIndex

TRAFFIC FAIL

Additional

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.

72

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

MAG VAR WARN

variance. Verify all course angles.

– 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 [#]

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

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00929-00 Rev. A 73

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Additional

Features Annun/Alerts Appendix Index

Annunciations & Alerts

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

74

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

APPENDIX

ALERTS

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

STRMSC P

ALERTS

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)

190-00929-00 Rev. A

Inset Map Softkeys

Displays Inset Map in PFD lower left corner

Removes Inset Map

Selects desired amount of map detail; cycles
through declutter levels:

DCLTR (No Declutter): All map features

visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the

active flight plan

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

75

Additional

Features Annun/Alerts Appendix Index

Appendix

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

BACK

ADC2

ADC1

AHRS1

AHRS2

ALERTS

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

76

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

PFD Configuration Softkeys

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

ALT UNI T

METERS IN HPA

DME

ALERTS

ALERTS

ALERTS

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

190-00929-00 Rev. A

SYN VIS

PATHWAY

SYN TERR

HRZN HDG

APTSIGNS

ditional 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 Beechcraft 200/B200 Series

Displays second-level softkeys for ad-

77

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

Total direction and speed

Longitudinal and lateral components

Information not displayed

Displays the DME Information Window

Cycles the Bearing 1 Information Win­dow through NAV1 or GPS/waypoint
identifier and GPS-derived distance

information, and ADF/frequency.

Displays the HSI formatting softkeys

Displays the HSI in a 360 degree format

Displays the HSI in an arc format

Cycles the Bearing 2 Information Win­dow through NAV2 or GPS/waypoint
identifier and GPS-derived distance

information, and ADF/frequency.

Displays softkeys for setting the
altimeter and BARO settings to metric
units

When enabled, displays altimeter in
meters

78

IN

Press to display the BARO setting as
inches of mercury

HPA

Press to display the BARO setting as
hectopacals

STD BARO

Sets barometric pressure to 29.92 in Hg
(1013 hPa)

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Transponder Softkeys

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

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

ALERTS

ALERTS

ALERTS

ADS-B TX

Appendix

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

XPDR

XPDR1

XPDR2

STBY

ON

ALT

GND

Displays transponder mode selection
softkeys

Selects the #1 transponder as active

Selects the #2 transponder as active

Selects Standby Mode (transponder does
not reply to any interrogations)

Selects Mode A (transponder replies to
interrogations)

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

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

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

79

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

80

MFD Softkeys

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 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

190-00929-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

81

Appendix

Flight

Instruments

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

FeaturesAnnun/AlertsAppendixIndex

Additional

82

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A

Index

A

Activate a flight plan 14
Active Channel 48
ADF 5, 6, 78
ADS-B 80
AHRS 65, 66, 67, 69
Air Data Computer 52
Airport Signs 45, 46
Airways 81
Alert messages 68
ALT 40
Altitude mode 40
Altitude volume 40
Antenna stabilization 44
Antenna tilt 42
AP 52
Attitude & Heading Reference System

52

Audio panel controls

NAV1, NAV2 6

B

Barometric Altitude Minimums 3
Barometric pressure 78
Bearing line 43, 44

C

CDI 1, 2, 6, 71
Cell 35, 36
Cell mode 36
Channel Presets 49
ChartView 46, 47
Code selection softkeys 5
COM 5, 6

D

Database Updates 81
DCLTR Softkey 46

Declutter 75, 81
Direct-to 13
DME 5, 6

E

Edit a flight plan 27

F

FD 52
Flight Director 9
Flight path marker 45
FliteCharts® 46, 47
Frequency Transfer 6

G

Gain 43

H

HF 5, 6
Horizon heading 45
Horizontal scan 43

I

Inhibit 41
Inhibit TAWS 41
Inset Map 75, 76
IOI 54

J

Jeppesen 47

L

Lightning 35, 36, 76

M

Map panning 37
Message advisories 56 – 67, 69 – 73
MET 52

Instruments

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features Annun/Alerts Appendix Index

190-00929-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Index-1

Index

METAR 37
Minimums 55

Flight

Instruments

MISCOMP 51
Mistrim 52, 53
Mode S 79
Mode selection softkeys 5

Nav/Com/

XPDR/AudioAFCSGPS Nav

Multi Function Display (MFD)

Softkeys 80

N

NACO 47
NAV 6
NAV1 2, 6
NAV2 6
Navigation database 15, 16
NEXRAD 37, 38, 76, 81

Flight

PlanningProcedures

O

OBS 2
Obstacles 60, 62
Overspeed Protection 10

P

Hazard

Avoidance

Pathways 45
PIT 51

R

FeaturesAnnun/AlertsAppendixIndex

Additional

RADIO softkey 48
ROC 53, 54

S

SafeTaxi® 46
Sector scan 44
Sensor 52
STAB 44
Standby 42
Store Flight Plan 27
Stormscope lightning data 35, 36, 76

Strike 35
Strike mode 36
SVS 45, 73
SVS Terrain 45
Synthetic Vision System 45

T

TA 55
TAF 37
TAS 39, 40, 65
TAWS 40, 41, 53, 55
TAWS-B 40
Terrain 40, 60, 76, 81
Tilt line 42
Timer 70
Topographical data 76, 81
Traffic 35, 39, 76, 81
Traffic advisory 38
Traffic Advisory 55
Traffic map page 39, 40
Transponder 5, 79, 80

V

Vertical speed guidance 16
Vertical track 55
VNV 13, 72
Vspeed 2

W

WAAS 62
WATCH® 44
Weather Attenuated Color Highlight 44
Weather data link page 37
Weather radar 42
Wind data 78

Index-2

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

190-00929-00 Rev. A