Garmin SA01535Wi_D Cockpit Reference Guide

G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Beechcraft 200/B200 Series
FLIGHT INSTRUMENTS
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2011 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.04 or later for the
Beechcraft 200 and B200. Some differences in operation may be observed when comparing
the information in this manual to earlier or later software versions.
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Tel: 913/397.8200Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411Fax 503/364.2138
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Southampton, SO40 9RB, U.K.
Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
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® , G1000®, WATCH®, FliteCharts®, and SafeTaxi® are registered trademarks of Garmin
Ltd. or its subsidiaries. ESP™ is a trademark 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.; SiriusXM™ is a trademark of SiriusXM™
Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
August, 2011
190-00929-03 Rev. A
Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: 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.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Warnings, Cautions & Notes
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: Do not use datalink weather products (e.g., XM WX Satellite
Weather, GFDS World Wide Weather, or FIS-B) for hazardous weather
penetration. Weather information provided by these products is aged by
up to several minutes and may not depict actual weather conditions as they
currently appear.
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: 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Warnings, Cautions & Notes
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
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 variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
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.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Warnings, Cautions & Notes
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Record of Revisions
Part Number
190-00929-00
190-00929-01
190-00929-02
190-00929-03
Change Summary
Initial release
Added Synthetic Vision System
Added TAWS-A
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Added other GDU 10.00 parameters
Added GDU 11.12 changes
Added GTS 820/850
Added Electronic Stabilization & Protection
Iridium Telephone and Data Link
Added Worldwide Weather
Added other GDU 12.01 parameters
Added METAR and WX LGND softkeys
Updated XM weather product symbols
Updated Iridium registration procedure
Updated SiriusXM product references
Revision Date of Revision Affected Pages
A
August, 2011
All
190-00929-03 Rev. A
Description
Production release
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 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 User Waypoint Defined by Latitude & Longitude............................................ 19
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
i
Table of Contents
Create a User Waypoint Defined by Radials from Other Waypoints............................ 20
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 22
Delete a User Waypoint.......................................................................................................... 23
Create a Flight Plan................................................................................................................. 24
Import a Flight Plan from an SD Card................................................................................. 25
Insert a Waypoint in the Active Flight Plan....................................................................... 25
Enter an Airway in a Flight Plan........................................................................................... 26
Invert An Active Flight Plan................................................................................................... 27
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 27
Store a Flight Plan................................................................................................................... 27
Edit a Stored Flight Plan........................................................................................................ 28
Delete a Waypoint from the Flight Plan............................................................................. 28
Invert and Activate a Stored Flight Plan............................................................................ 28
Copy a Flight Plan.................................................................................................................... 29
Delete a Flight Plan................................................................................................................. 29
Graphical Flight Plan Creation.............................................................................................. 29
Export a Flight Plan to an SD Card...................................................................................... 30
PROCEDURES.................................................................................................................................. 31
Load and Activate a Departure Procedure........................................................................ 31
Activate A Departure Leg...................................................................................................... 31
Load An Arrival Procedure..................................................................................................... 31
Activate An Arrival Leg.......................................................................................................... 32
Load and/or Activate an Approach Procedure.................................................................. 32
Activate An Approach in the Active Flight Plan................................................................ 33
Activate a Vector to Final Approach Fix............................................................................. 33
Activate A Missed Approach in the Active Flight Plan.................................................... 33
HAZARD AVOIDANCE................................................................................................................. 35
Customizing the Hazard Displays on the Navigation Map............................................. 35
STORMSCOPE® (Optional)...................................................................................................... 35
XM WX Satellite Weather (Optional)................................................................................... 37
Worldwide Weather................................................................................................................. 39
Traffic Avoidance Systems..................................................................................................... 50
Terrain Awareness & Warning System................................................................................ 53
Airborne Color Weather Radar............................................................................................. 56
ADDITIONAL FEATURES............................................................................................................ 61
Synthetic Vision........................................................................................................................ 61
Terminal Procedure Charts.................................................................................................... 62
AOPA Airport Directory.......................................................................................................... 64
Satellite Telephone and Data Link Services...................................................................... 65
WI-FI Connections.................................................................................................................... 78
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Table of Contents
System Data Logging.............................................................................................................. 81
SiriusXM™ Radio Entertainment........................................................................................... 83
Electronic Stability & Protection (ESP™)............................................................................. 85
ANNUNCIATIONS & ALERTS.................................................................................................... 87
WARNING Annunciation......................................................................................................... 87
Advisory Annunciations......................................................................................................... 87
Message Advisory Alerts........................................................................................................ 87
Comparator Annunciations.................................................................................................... 88
Reversionary Sensor Annunciations.................................................................................... 88
AFCS Alerts................................................................................................................................ 89
TAWS-A Alerts........................................................................................................................... 90
TAWS-B Alerts........................................................................................................................... 93
Additional Aural Alerts........................................................................................................... 96
MFD & PFD Message Advisories........................................................................................... 97
Database Message Advisories.............................................................................................. 98
GMA 1347D Message Advisories........................................................................................ 102
GIA 63W Message Advisories.............................................................................................. 103
GEA 71 Message Advisories................................................................................................. 106
GTX 33 Message Advisories................................................................................................. 106
GRS 77 Message Advisories................................................................................................. 107
GMU 44 Message Advisories............................................................................................... 108
GDL 59 Message Advisories................................................................................................. 109
GSR 56 Message Advisories................................................................................................. 109
GDL 69A Message Advisories.............................................................................................. 110
GWX 68 Alert Messages........................................................................................................ 110
GDC 74B Message Advisories.............................................................................................. 110
GCU 477 Message Advisories.............................................................................................. 111
GMC 710 Message Advisories............................................................................................. 112
Miscellaneous Message Advisories.................................................................................... 112
Flight Plan Import/Export Messages................................................................................. 116
APPENDIX...................................................................................................................................... 119
PFD Softkey Map................................................................................................................... 119
MFD Navigation Page Softkey Map.................................................................................. 125
Loading Updated Databases............................................................................................... 127
INDEX..........................................................................................................................................Index-1
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iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Nav/Com/
XPDR/Audio
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
Push the BARO Knob to select standard pressure.
AFCS
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
GPS Nav
1) Press the PFD Softkey to display the second-level softkeys.
2) Press the ALT UNIT Softkey.
Flight
Planning
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.
Procedures
4) Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
1) Select the AUX-SYSTEM SETUP Page on the MFD.
Additional
Features
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION
Window.
Annun/Alerts
4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
SYNCHRONIZE CDI
Appendix
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.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
1
CHANGE NAVIGATION SOURCES
1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes
the NAV1 standby frequency in the upper left corner of the PFD to light
blue, indicating this is the frequency selected for tuning.
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or
LOC2. This changes the NAV2 standby frequency in the upper left corner of
the PFD to light blue, indicating this is the frequency selected for tuning.
AFCS
3) Press the CDI Softkey a third time to return to GPS.
GPS Nav
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1) Press the OBS Softkey to select OBS Mode.
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
Avoidance
Procedures
Flight
Planning
2) Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3) Press the 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 large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Appendix
Annun/Alerts
Additional
Features
2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
Index
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
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Instruments
Flight
Instruments
5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6) To remove the window, press the CLR Key or the TMR/REF Softkey.
Nav/Com/
XPDR/Audio
TURN VSPEED BUGS ON OR OFF BY CATEGORY
1) Press the TMR/REF Softkey.
2) Press the MENU Key.
AFCS
3) Turn the FMS Knob to highlight the desired option.
4) Press the ENT Key. Press the TMR/REF Softkey to remove the window.
GPS Nav
SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE
1) Press the TMR/REF Softkey.
Flight
Planning
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.
Procedures
4) Press the ENT Key.
5) Use the small FMS Knob to enter the desired altitude.
6) Press the ENT Key.
Hazard
Avoidance
7) To remove the window, press the CLR Key or the TMR/REF Softkey.
TESTING THE RADAR ALTIMETER
Additional
Features
1) Select the AUX-SYSTEM STATUS Page on the MFD.
Annun/Alerts
2) Select the RA TEST Softkey. ‘RA TEST’ is displayed to the left of the Radar
Altitude window. The Radar Altitude window displays 50 feet, indicating a
properly functioning system.
3) Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.
Appendix
DISPLAYING WIND DATA
1) Press the PFD Softkey.
2) Press the WIND Softkey to display wind data below the Selected Heading.
Index
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.
190-00929-03 Rev. A
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3
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
Nav/Com/
XPDR/Audio
ADF TUNING (OPTIONAL)
Tune the ADF using the remote ADF control head.
DME TUNING
AFCS
1) Press the DME Softkey.
2) Turn the large FMS to select the DME source field.
GPS Nav
3) Turn the small FMS Knob to select the desired Nav radio.
4) Press the ENT Key to complete the selection.
1) Press the XPDR Softkey to display the transponder mode selection softkeys.
Procedures
2) Press the XPDR1 or XPDR2 Softkey to select the active transponder.
Flight
Planning
ENTER A TRANSPONDER CODE
3) Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
Hazard
Avoidance
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.
Additional
Features
ACTIVATE ADS-B TRANSMIT
1) Press the XPDR Softkey to display the transponder mode selection softkeys.
Annun/Alerts
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.
Appendix
SELECTING A COM RADIO
Transmit/Receive
Index
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
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5
Nav/Com/XPDR/Audio Panel
1) To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
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
Planning
GPS Nav
2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
2) Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
SELECTING A NAV RADIO
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Receive Only
3) Press the Frequency Transfer Key to place the frequency into the active
frequency field.
INTERCOM
Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.
The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.
The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.
During manual squelch operation, pressing the ICS Knob switches between volume
and squelch adjustment, lighting the associated annunciator beneath the knob. When
the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When
the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
PA Key is enabled on both audio panels. PA messages are one way from the flight deck
to the passengers.
Flight
Instruments
PASSENGER ADDRESS (PA) SYSTEM
CLEARANCE RECORDER AND PLAYER
AFCS
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
of recording time have been reached, the recorder begins recording over the stored
memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicate when play is in progress. The PLAY annunciator extinguishes after playback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
block, play is halted.
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
GPS Nav
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
Annun/Alerts
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
7
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
AFCS
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
AFCS
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.
Nav/Com/
XPDR/Audio
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT DIRECTOR ACTIVATION
Modes Selected
Lateral
Vertical
AP Key
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
CWS Button
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
GA Switch
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on ground)
Go Around (in air)
TO
GA
ALT Key
Roll Hold (default)
ROL
Altitude Hold
ALT
VS Key
Roll Hold (default)
ROL
Vertical Speed
VS
VNV Key
Roll Hold (default)
ROL
Vertical Path Tracking*
VPTH
NAV Key
Navigation**
GPS
VOR
LOC
Pitch Hold (default)
PIT
BC Key
Backcourse***
BC
Pitch Hold (default)
PIT
APR Key
Approach**
GPS
VAPP
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT
GP
GS
HDG Key
Heading Select
HDG
Pitch Hold (default)
PIT
Appendix
PIT
Annun/Alerts
Pitch Hold (default)
Additional
Features
ROL
Hazard
Avoidance
Roll Hold (default)
Procedures
FD Key
Flight
Planning
Control Pressed
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
Index
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV or APR Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
190-00929-03 Rev. A
GPS Nav
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
9
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
AFCS
VERTICAL MODES
Vertical Mode
Description
Control
Annunciation
Pitch Hold
Holds the current aircraft pitch attitude; may
be used to climb/descend to the Selected
Altitude
(default)
PIT
Selected Altitude
Armed
AFCS armed to capture the altitude displayed in
the Selected Altitude window
*
ALTS
Altitude Hold
Holds the current Altitude Reference
ALT Key
ALT
nnnnn ft
Vertical Speed
Maintains the current aircraft vertical speed;
may be used to climb/descend to the Selected
Altitude
VS Key
VS
nnnn fpm
FLC
nnn kt
FLC
M .nnn
Flight Level Change, Maintains the current aircraft airspeed (in
IAS or Mach) while the aircraft is climbing/
IAS Hold
descending to the Selected Altitude. Press
Flight Level Change, the SPD Key to switch between IAS and
Mach Hold
MACH.
FLC Key
VNAV
Captures and tracks the VNAV flight path
VNV Key
VPTH
VNAV Target
Altitude Armed
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window
**
ALTV
Glidepath
Captures and tracks the SBAS glidepath on
approach
Glideslope
Captures and tracks the ILS glideslope on
approach
Takeoff (on ground)
Disengages the autopilot and commands a
constant pitch angle and wings level in the
air on the ground in preparation for takeoff
Go Around (in air)
Level
Disengages the autopilot and commands a
constant pitch attitude and wings level in
the air
Commands 0° pitch attitude
GP
APR Key
GS
TO
GA
Switch
GA
Activated
only by
the ESP
function
LVL
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be
captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude
10
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
AFCS
Lateral Mode
Description
Control
Annunciation
(default)
ROL
Low Bank
Limits maximum commanded roll
angle
BANK
Key
*
Heading Select
Captures and tracks Selected
Heading
HDG Key
HDG
Navigation, GPS Arm/
Capture/Track
NAV Key
LOC
Captures and tracks a localizer
signal for backcourse approaches
BC Key
Approach, GPS Arm/Capture/
Track
LOC
Commands wings level attitude
GA
Switch
GA
LVL
Index
Activated
only by
the ESP
function
Appendix
Disengages autopilot and
commands a constant pitch angle
and wings level in the air
TO
Annun/Alerts
Disengages autopilot and commands
a constant pitch angle and wings
level in preparation for takeoff
Additional
Features
Level
Hazard
Avoidance
VAPP
APR Key
Track
(Glideslope Mode
automatically armed)
Go Around (in air)
BC
GPS
Approach, VOR Arm/Capture/
Track
Captures and tracks selected
Approach, ILS Arm/Capture/ navigation source (GPS, VOR, LOC)
Takeoff (on ground)
VOR
Procedures
Backcourse Arm/Capture/
Track
Captures and tracks selected
navigation source (GPS, VOR, LOC)
Flight
Planning
Navigation, LOC Arm/
Capture/Track
(No Glideslope)
GPS
GPS Nav
Navigation, VOR Enroute
Arm/Capture/Track
AFCS
Holds current aircraft roll attitude
or rolls wings level, depending on
commanded bank angle
Nav/Com/
XPDR/Audio
Roll Hold
Flight
Instruments
LATERAL MODES
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
11
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
AFCS
Blank Page
12
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
1) Press the Direct-to (
3)
5)
7)
9)
11)
Direct-to Navigation from the PFD
2)
3)
5)
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
13
Index
6)
Appendix
4)
) on the PFD.
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Annun/Alerts
1) Press the Direct-to Key (
Additional
Features
12)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
6)
GPS Nav
4)
AFCS
2)
) Key on the Control Unit.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) or after (+) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
Nav/Com/
XPDR/Audio
Direct-to Navigation from the MFD
GPS Navigation
Flight
Instruments
7) Turn the small FMS Knob to enter the desired altitude.
Nav/Com/
XPDR/Audio
8) Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance field.
AFCS
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
13) Turn the small FMS Knob to enter the desired course to the waypoint.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display
the Flight Plan Catalog Page.
Procedures
Flight
Planning
GPS Nav
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
2) Press the FMS Knob to activate the cursor.
Hazard
Avoidance
3) Turn the large FMS Knob to highlight the desired flight plan
4) Select the ACTIVE Softkey. The confirmation window is now displayed.
Additional
Features
5) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
Annun/Alerts
ACTIVATE A FLIGHT PLAN LEG
1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
Index
Appendix
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.
14
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
GPS Navigation
1) Press the FPL Key on the Control Unit to display the Active Flight Plan Page.
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2) Press the MENU Key to display the Page Menu Window.
AFCS
VERTICAL NAVIGATION (VNAV)
Nav/Com/
XPDR/Audio
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.
GPS Nav
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Flight
Planning
Procedures
Large White
Text
Large Light
Blue Text
Hazard
Avoidance
Small Light
Blue Text
Additional
Features
Small Light
Blue Subdued
Text
Small White Text
with Altitude
Restriction Bar
Annun/Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Cross AT or BELOW 3,000 ft
15
Altitudes associated with arrival and approach procedures are “auto-designated”.
This means the system will automatically use the altitudes loaded with the arrival
or approach for giving vertical flight path guidance outside the FAF. Note that these
altitudes will be displayed as small light blue text.
Altitudes that have been designated for use in vertical navigation may also be made
“non-designated” by placing the cursor over the desired altitude and pressing the CLR
Key. The altitude is now displayed only as a reference. It will not be used to give flight
path vertical guidance. Other displayed altitudes may change due to re-calculations
or rendered invalid as a result of manually changing an altitude to a non-designated
altitude.
White Text
Light Blue Text
Light Blue
Subdued Text
Large Text Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.
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.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text Altitude is not
designated to be used
in determining vertical
flight path guidance. 
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.
Altitude is designated
for use in giving vertical
flight path guidance. 
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
GPS Navigation
16
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT PLANNING
Nav/Com/
XPDR/Audio
All procedures apply to the MFD and the Control Unit unless otherwise stated.
Entering Weight Parameters
GPS Nav
Flight
Planning
Procedures
Entering Fuel Parameters
AFCS
The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the
small FMS Knob to select the Weight Planning 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.
1) Press the FMS Knob to activate the cursor.
3) Turn the small FMS Knob to enter the desired fuel quantity.
Additional
Features
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.
Annun/Alerts
7) Press the ENT Key.
TRIP PLANNING
2) Turn the small FMS Knob to select the Trip Planning Page.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
17
Index
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.
Appendix
1) Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page
group.
190-00929-03 Rev. A
Hazard
Avoidance
2) Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.
Flight Planning
Flight
Instruments
4) For Direct-to planning:
a) Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
Nav/Com/
XPDR/Audio
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
GPS Nav
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Flight
Planning
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
Procedures
d) Press the ENT Key to accept the waypoint.
Or:
For flight plan leg planning:
Hazard
Avoidance
a) Select the FPL Softkey (at the bottom of the display).
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
Additional
Features
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
Appendix
Annun/Alerts
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ will display the active flight plan. If an active flight
plan is selected, ‘REM’ will be an available option to display planning
data for the remainder of the flight plan.
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
5) Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Index
18
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
190-00929-03 Rev. A
Flight Planning
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
Hazard
Avoidance
Additional
Features
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
Procedures
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
Flight
Planning
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
GPS Nav
9) The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.
AFCS
8) The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
Nav/Com/
XPDR/Audio
7) The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Flight
Instruments
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.
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
2) Turn the small FMS Knob to select the User WPT Information Page.
Appendix
3) Select the NEW Softkey. A waypoint is created at the current aircraft
position.
Annun/Alerts
1) Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
4) Enter the desired waypoint name.
5) Press the ENT Key.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
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.
19
Flight Planning
Flight
Instruments
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Nav/Com/
XPDR/Audio
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8) Turn the small FMS Knob to select LAT/LON (latitude and longitude).
AFCS
9) Press the ENT Key.
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
GPS Nav
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.
Flight
Planning
3) Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4) Enter the desired waypoint name.
Procedures
5) Press the ENT Key.
6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Hazard
Avoidance
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Additional
Features
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Annun/Alerts
8) Turn the small FMS Knob to select RAD/RAD (radial/radial).
9) Press the ENT Key.
Appendix
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
Index
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
20
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Planning
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Flight
Instruments
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Hazard
Avoidance
c) Turn the large FMS Knob to select the desired waypoint.
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
12) Press the ENT Key.
Additional
Features
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
Appendix
16) Press the FMS Knob to remove the flashing cursor.
Annun/Alerts
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
21
CREATE A 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.
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
2) Turn the small FMS Knob to select the User WPT Information Page.
AFCS
3) Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4) Enter the desired waypoint name.
5) Press the ENT Key.
GPS Nav
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.
Flight
Planning
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Procedures
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Hazard
Avoidance
8) Turn the small FMS Knob to select RAD/DIS (radial/distance).
9) Press the ENT Key.
Additional
Features
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
Annun/Alerts
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
22
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Planning
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Instruments
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Procedures
12) Press the ENT Key.
Flight
Planning
d) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Hazard
Avoidance
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
Additional
Features
DELETE A USER WAYPOINT
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.
4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
Appendix
5) Turn the small FMS Knob to highlight the desired waypoint.
6) Select the DELETE Softkey.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
23
Index
7) The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
190-00929-03 Rev. A
Annun/Alerts
3) Press the FMS Knob to activate the cursor.
CREATE A FLIGHT PLAN
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
Procedures
Flight
Planning
GPS Nav
AFCS
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
4) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
24
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Planning
1) Insert the SD card containing the flight plan in the top card slot on the
MFD.
Nav/Com/
XPDR/Audio
2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
Flight
Instruments
IMPORT A FLIGHT PLAN FROM AN SD CARD
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
AFCS
4) Press the FMS Knob to activate the cursor.
5) Turn either FMS Knob to highlight an empty or existing flight plan.
6) Select the IMPORT Softkey.
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
GPS Nav
Or:
8) Press the ENT Key.
Hazard
Avoidance
7) Turn the small FMS Knob to highlight the desired flight plan for importing.
Procedures
If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK
or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite
the selected flight plan and see a list of the available flight plans on the SD
card. If overwriting the existing flight plan is not desired, select ‘CANCEL’
using the FMS Knob, press the ENT Key, select another existing or empty
flight plan, and again select the IMPORT Softkey.
Flight
Planning
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Additional
Features
1) Press the FPL Key on the Control Unit to display the active flight plan.
2) Press the FMS Knob to activate the cursor.
Appendix
4) Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
Annun/Alerts
3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint will be inserted before the highlighted waypoint.
5) Enter the new flight plan waypoint by one of the following:
a) Enter the user waypoint identifier, facility, or city.
Index
b) Press the ENT Key.
Or:
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
25
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
AFCS
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
ENTER AN AIRWAY IN A FLIGHT PLAN
1) Press the FPL Key on the Control Unit.
Procedures
Flight
Planning
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
Hazard
Avoidance
3) Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
Annun/Alerts
Additional
Features
4) Turn the small FMS Knob one click clockwise and select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”(required on
the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey
or the “Load Airway” menu item is available only when an acceptable
airway entry waypoint has been chosen (the waypoint ahead of the cursor
position).
Appendix
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.
Index
7) Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
26
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Flight Planning
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
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.
AFCS
5) With ‘OK’ highlighted, press the ENT Key to invert the 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:
Flight
Planning
GPS Nav
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
a) Turn the small FMS Knob to select the Flight Plan Catalog Page.
b) Press the FMS Knob to activate the cursor.
Procedures
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Select the EDIT Softkey.
Hazard
Avoidance
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.
1) After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
3) With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Appendix
2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
Annun/Alerts
STORE A FLIGHT PLAN
Additional
Features
4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
27
EDIT A STORED FLIGHT PLAN
1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display
the Flight Plan Catalog Page.
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
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.
AFCS
5) Turn the large FMS Knob to place the cursor in the desired location.
7) Press the FMS Knob to return to the Flight Plan Catalog Page.
DELETE A WAYPOINT FROM THE FLIGHT PLAN
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Flight
Planning
GPS Nav
6) Enter the changes, then press the ENT Key.
Procedures
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.
Hazard
Avoidance
d) Select the EDIT Softkey.
2) Turn the large FMS Knob to highlight the waypoint to be deleted.
Additional
Features
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.
Annun/Alerts
Appendix
Or:
5) Once all changes have been made, press the FMS Knob to remove the
cursor.
INVERT AND ACTIVATE A STORED FLIGHT PLAN
1) Press the FPL Key on the Control Unit.
Index
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
190-00929-03 Rev. A
Flight Planning
5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be
displayed.
AFCS
COPY A FLIGHT PLAN
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
4) Turn the large FMS Knob to highlight the desired flight plan.
1) Press the FPL Key on the Control Unit.
GPS Nav
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor.
4) Turn the large FMS Knob to highlight the flight plan to be copied.
DELETE A FLIGHT PLAN
Hazard
Avoidance
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.
5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
GRAPHICAL FLIGHT PLAN CREATION
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
29
Index
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.
Appendix
1) Press the FPL Key on the Control Unit to display the Active Flight Plan Page.
Annun/Alerts
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.
Additional
Features
4) Turn the large FMS Knob to highlight the flight plan to be deleted.
190-00929-03 Rev. A
Procedures
6) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Flight
Planning
5) Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
Flight Planning
Nav/Com/
XPDR/Audio
Flight
Instruments
3) The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4) Select the LD WPT Softkey. The selected waypoint will be inserted at the
selected point. The default user waypoint naming is USR000, USR001, USR002,
and so on.
AFCS
5) To change the user waypoint name, follow the procedure for modifying a user
waypoint.
GPS Nav
EXPORT A FLIGHT PLAN TO AN SD CARD
1) Insert the SD card into the top card slot on the MFD.
Flight
Planning
2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
Procedures
5) Turn the large FMS Knob to highlight the flight plan to be exported.
6) Select the EXPORT Softkey.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
7) Press the ENT Key to confirm the export.
30
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
Nav/Com/
XPDR/Audio
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
AFCS
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.
6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
GPS Nav
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.
Flight
Planning
7) Turn the large FMS Knob to highlight the desired transition.
8) Press the ENT Key.
Procedures
9) With ‘LOAD?’ highlighted, press the ENT Key. The departure will be active
when the flight plan is active.
ACTIVATE A DEPARTURE LEG
Hazard
Avoidance
1) Press the FPL Key to display the active flight plan.
2) Press the FMS Knob to activate the cursor.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
Annun/Alerts
4) Select the ACT LEG Softkey. A confirmation window showing the selected
leg will be displayed.
Additional
Features
3) Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the departure.
LOAD AN ARRIVAL PROCEDURE
Appendix
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
4) Turn the large FMS Knob to highlight the desired arrival.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
31
Index
3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Procedures
Flight
Instruments
5) Press the ENT Key. A list of transitions is displayed for the selected arrival.
6) Turn either FMS Knob to select the desired transition.
7) Press the ENT Key. A list of runways is displayed for the selected arrival.
Nav/Com/
XPDR/Audio
8) Turn the large FMS Knob to highlight the desired runway.
9) Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival will become part of the active flight plan.
ACTIVATE AN ARRIVAL LEG
GPS Nav
1) Press the FPL Key on the Control Unit to display the active flight plan.
2) Press the FMS Knob to activate the cursor.
4) Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Hazard
Avoidance
Procedures
Flight
Planning
3) Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the arrival.
Additional
Features
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
Annun/Alerts
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.
Appendix
5) Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
Index
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.
32
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Procedures
Flight
Instruments
7) Press the ENT Key. The cursor moves to the MINIMUMS field.
Nav/Com/
XPDR/Audio
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 ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
AFCS
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?’.
12) Press the ENT Key.
Procedures
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
Flight
Planning
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.
GPS Nav
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
Hazard
Avoidance
3) Press the ENT Key.
ACTIVATE A VECTOR TO FINAL APPROACH FIX
Additional
Features
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3) Press the ENT Key.
Annun/Alerts
4) The final approach course becomes the active leg.
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
Appendix
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.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
33
Procedures
Flight
Instruments
4) With ‘ACTIVATE’ highlighted, press the ENT Key.
Or:
Press the go-around button.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
5) After activating the missed approach procedure, and the CDI has changed
to TERM mode sensitivity, another approach procedure may be loaded.
34
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
Nav/Com/
XPDR/Audio
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.
AFCS
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.
GPS Nav
STORMSCOPE® (OPTIONAL)
Procedures
Displaying Stormscope Lightning Data on the Navigation Map Page
1) Select the MAP Softkey.
Hazard
Avoidance
2) Select the STRMSCP Softkey. Select the STRMSCP Softkey again to
remove Stormscope Lightning Data from the Navigation Map Page.
Symbol
Additional
Features
Lightning Age
Strike is less than 6 seconds old
Flight
Planning
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.
Strike is between 6 and 60 seconds old
Annun/Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
1) Press the MENU Key (with the Navigation Map Page displayed).
2) Turn either FMS Knob to highlight ‘Map Setup’.
Index
3) Press the ENT Key.
4) Turn the small FMS Knob to highlight ‘Weather’.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
35
Hazard Avoidance
Flight
Instruments
5) Press the ENT Key.
6) Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7) Turn the small FMS Knob to display the ‘Cell/Strike’ window.
Nav/Com/
XPDR/Audio
8) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
9) Push the FMS Knob to return to the Navigation Map Page.
Clear Stormscope Lightning Data from the Navigation Map Page
AFCS
1) Press the MENU Key (with the Navigation Map Page displayed).
GPS Nav
2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
after the execution of each turn. This is to ensure that the strike and/or cell
Flight
Planning
positions are depicted accurately in relation to the nose of the aircraft.
Stormscope Page
Procedures
1) 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’
Hazard
Avoidance
1) Select the Stormscope Page.
Additional
Features
2) Select the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Select the CELL Softkey to display ‘CELL’ data or select the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.
Annun/Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Change the Viewing Mode Between 360˚ and 120˚
Appendix
1) Select the Stormscope Page.
Index
2) Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select
the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to
display a 120˚ viewing area.
36
Select the CLEAR Softkey to remove all Stormscope lightning data from the
display.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Displaying XM WX Weather on the Navigation Map Page
AFCS
1) Select the MAP Softkey.
Nav/Com/
XPDR/Audio
WARNING: Use of XM WX Satellite Weather for hazardous weather
penetration is not recommended. Weather information provided by SiriusXM™
Satellite Radio is approved only for weather avoidance, not penetration.
Flight
Instruments
XM WX SATELLITE WEATHER (OPTIONAL)
GPS Nav
2) Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.
Display METAR and TAF information on the Airport Information Page
1) Turn the large FMS Knob to select the WPT Page Group.
Flight
Planning
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).
Procedures
Displaying Weather on the Weather Data Link Page
1) Turn the large FMS Knob to select the Map Page Group.
3) Select the available softkeys to select the desired XM WX weather product.
Additional
Features
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.
Hazard
Avoidance
2) Turn the small FMS Knob to select the Weather Data Link Page.
Map Panning Information – Weather Data Link Page
2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
SIGMETs, PIREPs or AIREPs.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.
Appendix
3) Press the ENT Key to display pertinent information for the selected product.
Annun/Alerts
1) Push in the Joystick to display the panning arrow.
37
Hazard Avoidance
Flight
Instruments
Weather Products and Symbols
Nav/Com/
XPDR/Audio
Wx Product
Status Icons
Description
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
AFCS
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
GPS Nav
CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.
XM LIGHTNING - The age of the displayed data is shown at the right.
Flight
Planning
CELL MOVEMENT - The age of the displayed data is shown at the right.
Procedures
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Additional
Features
Hazard
Avoidance
SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.
FREEZING LEVEL - The age of the displayed data is shown at the right.
Annun/Alerts
WINDS ALOFT - Available for the US and Canada. The age of the displayed
data for each is shown at the right. The altitude selection is shown at the
bottom.
Appendix
COUNTY WARNING - The age of the displayed data is shown at the right.
CYCLONE WARNING - The age of the displayed data is shown at the right.
Index
AIREP - The age of the displayed data is shown at the right.
38
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
Nav/Com/
XPDR/Audio
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
AFCS
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
GPS Nav
WORLDWIDE WEATHER
NOTE: Garmin Flight Data Services Worldwide Weather provides information
for avoiding hazardous weather. Do not utilize Worldwide Weather information to penetrate hazardous weather.
Hazard
Avoidance
Accessing GFDS Worldwide Weather Products
1) Turn the large FMS Knob to select the Map Page Group.
Appendix
Index
39
Annun/Alerts
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Additional
Features
2) Turn the small FMS Knob to select the GFDS Weather Data Link Page.
When a weather product is selected for display on the GFDS Weather Data Link
Page, a box containing a symbol for the product and its age (in minutes) are shown
in the upper right. If weather data has not been requested, ‘N/A’ is shown next to the
product symbol instead of age. The age of the weather product is based on the time
difference between when the data was assembled on the ground and the current GPS
time. Weather products are updated continuously or refreshed at specific intervals
(defined in the Refresh Rate column in the following table).
If for any reason, a weather product is not refreshed within the defined Expiration
Time intervals, the data is considered expired and is removed from the display. The
age of the expired product is replaced by dashes. If more than half of the expiration
time has elapsed, the color of the product age readout changes to yellow.
190-00929-03 Rev. A
Procedures
Weather data are provided when the pilot initiates either a manual or automatic
GFDS data request on the GFDS Weather Data Link Page on the MFD. No weather
data is displayed until the first GFDS Weather Data Request is made.
Flight
Planning
The refresh rate represents the interval at which the GFDS servers make available
the most current known weather data. It does not necessarily represent the rate at
which new content is received from weather sources.
Weather Product
Symbol
Radar Precipitation
(PRECIP)
Infrared Satellite
(IR SAT)
Datalink Lightning
(DL LTNG)
SIGMETs/AIRMETs
(SIG/AIR)
Meteorological Aerodrome Report
(METARs)
Winds Aloft
(WIND)
Pilot Weather Report
(PIREPs)
Temporary Flight Restrictions
no product image
(TFRs)
Terminal Aerodrome Reports
no product image
(TAFs)
Expiration
Time
(Minutes)
Refresh Rate
(Minutes)
30
U.S./Canada: 3*
Europe: 15
60
30
30
Continuous
60
Continuous
90
Continuous
60
Continuous
90
Continuous
60
Continuous
60
Continuous
* The composite precipitation image is updated every 3 minutes, but individual radar sites may take
between 3 and 10 minutes to provide new data.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
40
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
Setting Up and Customizing the GFDS Weather Data Link Page
1) Select the GFDS Weather Data Link Page.
2) Press the MENU Key.
4) Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’,
and press the ENT Key.
AFCS
5) Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Nav/Com/
XPDR/Audio
3) With ‘Weather Setup’ highlighted, press the ENT Key.
GPS Nav
6) Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings, etc.).
7) Press the ENT Key to select an option.
GFDS Worldwide Weather
Product
Precipitation
Next-generation Radar
(NEXRAD)
(PRECIP)
Cloud Top
Infrared Satellite
(CLD TOP)
(IR SAT)
XM Lightning
GFDS Lightning
(DL LTNG)
(XM LTNG)
SIGMETs/AIRMETs
SIGMETs/AIRMETs
(SIG/AIR)
(SIG/AIR)
Meteorological Aerodrome Report Meteorological Aerodrome Report
(METARs)
(METARs)
Winds Aloft
Winds Aloft
(WIND)
(WIND)
Pilot Weather Report
Pilot Weather Report
(PIREPs)
(PIREPs)
Procedures
On aircraft equipped with both GFDS and XM WX Satellite Weather services,
customizing the display settings for the corresponding weather products shown in
following table will result in identical settings for both services.
Flight
Planning
8) Press the FMS Knob or CLR Key to return to the GFDS Weather Data Link
Page with the changed settings.
XM Weather Product
Additional
Features
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Hazard
Avoidance
190-00929-03 Rev. A
41
Hazard Avoidance
Flight
Instruments
Restoring Default GFDS Weather Data Link Page Settings
1) Select the GFDS Weather Data Link Page.
Nav/Com/
XPDR/Audio
2) Press the MENU Key.
3) With ‘Weather Setup’ highlighted, press the ENT Key.
4) Press the MENU Key.
AFCS
5) Highlight the desired default(s) to restore (all or for selection) and press
ENT Key.
Switching Between GFDS and XM WX Weather Sources
GPS Nav
1) Turn the large FMS Knob on the MFD to select the MAP page group.
2) Turn the small FMS Knob to select the GFDS (or XM) Weather Data Link
Page.
Flight
Planning
3) Press the MENU Key.
Procedures
4) Turn the large FMS Knob to select ‘Display GFDS Weather’ or ‘Display XM’
Weather’ (choice dependent on current weather source) and press the ENT
Key.
Viewing Legends for Displayed GFDS Weather Products
Hazard
Avoidance
1) Select the GFDS Weather Data Link Page.
2) Select the LEGEND Softkey to display the legends for the displayed
weather products.
Additional
Features
Or:
a) Press the MENU Key.
b) Select ‘Weather Legend’ and press the ENT Key.
Annun/Alerts
3) Turn the FMS Knob to scroll through the legends if more are available than
fit in the window.
Appendix
4) To remove the Legend Window, select the LEGEND Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Setting Up and Customizing Weather Data for the Navigation Map
Page
Index
1) Select the Navigation Map Page.
2) Press the MENU Key.
42
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT
Key.
Nav/Com/
XPDR/Audio
5) Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Flight
Instruments
3) With ‘Map Setup’ highlighted, press the ENT Key.
6) Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
AFCS
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
GPS Nav
GFDS Weather Data Requests
Procedures
Requesting GFDS Weather Data Manually
Flight
Planning
The GFDS Data Request window provides the flight crew with the options to define
the requested weather coverage area(s), choose automatic weather update intervals (if
desired), and the ability to send or cancel weather data requests. The window also
displays the status of the GFDS data request process.
1) Select the GFDS Weather Data Link Page.
Hazard
Avoidance
2) Press the MENU Key.
3) With ‘GFDS Weather Request’ highlighted, press the ENT Key.
Additional
Features
4) Turn the large FMS Knob to highlight the desired coverage option(s)
and press the ENT Key to check or uncheck one of more of the following
coverage selections:
• PRESENT POSITION – Requests data based on current location.
• DESTINATION – Requests data based on active flight plan
destination (if the flight plan contains no destination, dashes ‘------” are
displayed.)
Appendix
• FPL – Requests data based on active flight plan. Turn the small
FMS Knob to select the desired flight plan look-ahead distance
option (or choose ‘REMAINING FPL’ to request the remainder of the
flight plan).
Annun/Alerts
• WAYPOINT – Requests data based on any valid waypoint.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
43
Hazard Avoidance
Flight
Instruments
5) Turn the large FMS Knob highlight to the ‘DIAMETER / RTE WIDTH’
distance field and turn the small FMS Knob to select the desired diameter
and route width of the request, then press the ENT Key.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
6) Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted. Press
the ENT Key to initiate the request immediately or press the FMS Knob to
return to the GFDS Data Link Page without requesting data.
During a GFDS Data Request, the Request Status box initially displays “Contacting
GFDS...”. Once a connection is established, the Request Status Box displays “Receiving
Wx Data... Time Remaining:” with an estimated data transfer time (either minutes or
seconds). If desired, the GFDS Data Request window may be closed while the data request
is processing by pressing the FMS Knob; the data request will continue to process in the
background. GFDS Data Requests typically take between 1 to 4 minutes to complete
depending on the size of the selected weather coverage area and Iridium signal strength.
The system retrieves all available Worldwide Weather products within the selected
coverage area during an initial GFDS Data Request, regardless of which products (if
any) are currently enabled for display. On subsequent requests, previously retrieved
textual data (such as METARs and TAFS) is retained if it has not expired, while new
textual weather data matching the current coverage area and all graphical weather data is
downloaded during every data request.
If the system cannot complete a GFDS weather data request, one or more messages
will appear in the request status window as shown in the following table.
Weather Request
Status Message
Description
Auto requests inhibited The system has disabled automatic weather data requests
due to excessive errors. Automatic weather data requests
Send manual request
have stopped. Send a manual weather data request to
to reset.
resume automatic updates.
Auto update retry: ## The system will attempt another automatic weather data
Seconds
request after an error occurred during the previous request.
Timer counts down until the next automatic request occurs.
GFDS Comm Error [2] A communications error has occurred with the GIA. The
system should be serviced.
GFDS Comm Error [4] This occurs if multiple automatic weather data requests have
recently failed, or the GDL 59 or a GIA is off-line.
44
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Description
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
45
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
AFCS
190-00929-03 Rev. A
Nav/Com/
XPDR/Audio
The Iridium or GFDS networks are not accessible. Check
Iridium signal strength. If this error persists, the G1000H
should be serviced.
GFDS Comm Error [6] A communications error has occurred. It this error persists,
the system should be serviced.
GFDS Comm Error [7] A weather data transfer has timed out. Check Iridium signal
strength and re-send the data request.
GFDS Comm Error [8] A server error has occurred or invalid data received.
GFDS Login Invalid
There is a problem with the GFDS registration. Contact
Garmin Flight Data Services at 1-866-739-5687 in the United
States or 913-397-8200, ext. 1135 for assistance.
GFDS Server
The GFDS weather data server is temporarily out of service,
Temporarily Inop
but is expected to return to service in less than 30 minutes.
GFDS Server Inop
The GFDS weather data server will be out of service for at
least 30 minutes.
Invalid Coverage Area The weather data request coverage area does not contain
at least one of the following: a waypoint, a flight plan, or a
flight plan destination. Verify at least one of the coverage
options is enabled (checked) and contains required criteria,
then re-send the data request.
No GFDS Subscription The system is not be currently subscribed to GFDS, or the
access code is incorrect. Verify the access code. Contact
Garmin Flight Data Services at 1-866-739-5687 in the United
States or 913-397-8200, ext. 1135 for assistance.
Reduce Request Area
The GFDS weather data request area exceeds size limits.
Reduce weather coverage area and re-send data request.
Request Cancelled
The user has cancelled a GFDS weather data request.
Requested area too
The size of the GFDS weather data request has exceeded
large. Reduce coverage limits. Reduce the size of the coverage area and try the
area.
weather data request again.
Request Failed - Try
The weather data request timed-out. Re-send data request.
Again
Transfer Preempted
The datalink is busy. Retry request later.
Flight
Instruments
Weather Request
Status Message
GFDS Comm Error [5]
Hazard Avoidance
Flight
Instruments
Cancelling a GFDS Weather Data Request in Progress
1) Select the GFDS Weather Data Link Page.
Nav/Com/
XPDR/Audio
2) Press the MENU Key.
3) With ‘GFDS Data Request’ highlighted, press the ENT Key.
4) Turn the large FMS Knob to select ‘CANCEL REQ’ and press the ENT Key.
The request status box indicates ‘Request Cancelled’.
AFCS
5) Press the FMS Knob to return to the GFDS Weather Datalink Page.
Enabling Automatic GFDS Data Requests
GPS Nav
1) Select the GFDS Weather Data Link Page.
2) Press the MENU Key.
3) With ‘GFDS Weather Request’ highlighted, press the ENT Key.
Flight
Planning
4) Choose the desired weather coverage options.
Procedures
5) Turn the large FMS Knob to select the ‘UPDATE RATE’ setting. Then turn
the small FMS Knob to highlight the desired automatic update frequency
(OFF, 5 Min, 10 Min, 15 Min, 20 Min, 25 Min, 30 Min, 45 Min, or 60 Min),
then press the ENT Key.
Hazard
Avoidance
6) The ‘SEND REQ” button is highlighted and a countdown timer is displayed
in the ‘REQUEST STATUS’ based on the currently selected update rate.
Press the ENT Key to immediately send an immediate GFDS Data Request.
Or:
Additional
Features
Press the FMS Knob to return to the GFDS Weather Data Link Page.
Worldwide Weather Products
Annun/Alerts
Precipitation
Index
Appendix
NOTE: Precipitation data cannot be displayed at the same time as terrain.
Precipitation data is not real-time. The lapsed time between collection, processing,
and dissemination of radar images can be significant and may not reflect the current
radar synopsis. Due to the inherent delays and the relative age of the data, it should
be used for long-range planning purposes only.
46
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Hazard Avoidance
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
47
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Procedures
To display the Infrared Satellite legend, select the LEGEND Softkey when Infrared
Satellite data is selected for display.
190-00929-03 Rev. A
Flight
Planning
Displaying Cloud Tops information
1) Select the GFDS Weather Data Link Page.
2) Select the IR SAT Softkey.
GPS Nav
Infrared Satellite
Infrared Satellite (IR SAT) data depicts cloud top temperatures from satellite imagery.
Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes.
AFCS
Precipitation Limitations
Radar images may have certain limitations:
• Radar base reflectivity does not provide sufficient information to determine cloud
layers or precipitation characteristics (wet hail vs. rain). For example, it is not
possible to distinguish between wet snow, wet hail, and rain.
• Radar base reflectivity is sampled at the minimum antenna elevation angle. An
individual radar site cannot depict high altitude storms at close ranges. It has
no information about storms directly over the site.
• When zoomed in to a range of 30 nm, each square block on the display represents
an area of four square kilometers.
The following may cause abnormalities in displayed radar images:
• Ground clutter
• Strobes and spurious radar data
• Sun strobes (when the radar antenna points directly at the sun)
• Interference from buildings or mountains, which may cause shadows
• Metallic dust from military aircraft, which can cause alterations in radar scans
Nav/Com/
XPDR/Audio
Radar data shown represents lowest level, base reflectivity, of radar returns. The
display of the information is color-coded to indicate the weather severity level. All
weather product legends can be viewed on the GFDS Weather Data Link Page. For
the Precipitation legend, select the LEGEND Softkey when Precipitation is selected
for display.
Flight
Instruments
Displaying Precipitation Weather Information
1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
This step is not necessary on the GFDS Weather Data Link Page.
2) Select the PRECIP Softkey.
Datalink Lightning
Lightning data shows the approximate location of cloud-to-ground lightning strikes.
A strike icon represents a strike that has occurred within a two-kilometer region.
Neither cloud-to-cloud nor the exact location of the lightning strike is displayed.
If the aircraft is also equipped with the L-3 WX-500 Stormscope®, only one lightning
product may be enabled for display at a time.
Displaying Datalink Lightning information
1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
This step is not necessary on the GFDS Weather Data Link Page.
2) Select the DL LTNG Softkey.
To display the Datalink Lightning legend on the Weather Data Link Page, select the
LEGEND Softkey when Datalink Lightning is selected for display.
SIGMETs and AIRMETs
The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring
within the coverage area of the GFDS data request.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
To display the SIGMET and AIRMET legend, select the LEGEND Softkey when
SIGMETs and AIRMETs are selected for display.
METARs and TAFs
Annun/Alerts
Additional
Features
Hazard
Avoidance
Displaying SIGMETs and AIRMETs
1) Select the GFDS Weather Data Link Page.
2) Select the SIG/AIR Softkey.
3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move
the Map Pointer over the icon.
4) Press the ENT key.
NOTE: METAR information is only displayed within the installed navigation
database service area.
METAR and TAF text are displayed on the Weather Information Page. TAF
information is displayed in its raw form when it is available.
Displaying METAR and TAF text
1) On the GFDS Weather Data Link Page, select the METAR Softkey.
2) Press the RANGE Knob and pan to the desired airport.
Index
Appendix
48
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
3) Press the ENT Key. The Weather Information Page is shown with METAR
and TAF text.
Nav/Com/
XPDR/Audio
4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF
text. METAR text must be completely scrolled through before scrolling
through the TAF text.
5) Press the FMS Knob or the CLR Key to return to the GFDS Weather Data
Link Page.
AFCS
Or:
1) Select the Weather Information Page.
a) Turn the large FMS Knob to select the Waypoint Page Group.
GPS Nav
b) Select the WX Softkey to select the Weather Information Page.
2) Press the FMS Knob to display the cursor.
49
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
190-00929-03 Rev. A
Annun/Alerts
To display the Winds Aloft legend, select the LEGEND Softkey when Winds Aloft
is selected for display.
Additional
Features
Displaying Winds Aloft data
1) Select the GFDS Weather Data Link Page.
2) Select the MORE WX Softkey.
3) Select the WIND Softkey.
4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select
the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND
Softkey label changes to reflect the altitude selected.
Hazard
Avoidance
Winds Aloft
Winds Aloft data shows the forecasted wind speed and direction at the surface and
at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000
feet MSL.
Procedures
4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF
text. Note that the METAR text must be completely scrolled through before
scrolling through the TAF text.
To display the METAR legend on the GFDS Weather Data Link Page, select the
LEGEND Softkey when METARs are selected for display.
Flight
Planning
3) Use the FMS Knob to enter the desired airport and press the ENT Key.
PIREPs
Pilot Weather Reports (PIREPs) describe in-flight weather encountered by pilots.
A PIREP may contain adverse weather conditions not forecasted, such as low in-flight
visibility, icing conditions, wind shear, turbulence, and type of aircraft flown. PIREPs
are issued as either Routine (UA) or Urgent (UUA).
Displaying PIREP text
1) Select the GFDS Weather Data Link Page.
2) Select the MORE WX Softkey.
3) Select the PIREPS Softkey.
4) Press the RANGE Knob and pan to the desired weather report. A gray
circle will appear around the weather report when it is selected.
5) Press the ENT Key. The PIREP text is first displayed in a decoded fashion,
then as raw text.
6) Use the FMS Knob or the ENT Key to scroll through the PIREP text.
7) Press the FMS Knob or the CLR Key to close the PIREP text window and
return to the GFDS Weather Data Link Page.
To display the PIREP or AIREP legend, select the LEGEND Softkey when PIREPs
or AIREPs are selected for display.
The PIREP color is determined by the type (routine or urgent).
TRAFFIC AVOIDANCE SYSTEMS
• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey will be displayed.
• If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE or
NORMAL, TEST, and ALT MODE Softkey will be displayed.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
50
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Description
Flight
Instruments
Traffic Symbol
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Nav/Com/
XPDR/Audio
Proximity Advisory (PA)(TAS only, not available with TIS)
(intruder is within 5 nm and less than 1200’ vertical separation)
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
AFCS
Traffic Advisory Off Scale
GPS Nav
Traffic Symbol Description
Traffic Information Service (TIS)
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
Procedures
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Flight
Planning
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.
Additional
Features
3) Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
Annun/Alerts
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
Index
1) Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.
2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
6) Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural alert.
51
Hazard Avoidance
Flight
Instruments
Traffic Advisory System (TAS) (Optional)
System Self Test
Nav/Com/
XPDR/Audio
1) Set the range to 2/6 nm.
2) Select the STANDBY Softkey.
3) Select the TEST Softkey.
GPS Nav
AFCS
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
Flight
Planning
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.
Procedures
3) Select the OPERATE or NORMAL Softkey to begin displaying traffic.
‘OPERATING’ is displayed in the Traffic Mode field.
Hazard
Avoidance
4) Select the ALT MODE Softkey to change the altitude display volume.
Select the desired altitude volume by selecting the BELOW, NORMAL,
ABOVE, or UNREST (unrestricted) Softkey. The selection is displayed in the
Altitude Mode field.
Additional
Features
5) Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ will be displayed in the Traffic Mode field.
6) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Annun/Alerts
7) Select the FLT ID Softkey (GTS 820/850 only) to enable or disable Flight ID
displayed with the intruder information.
Displaying Traffic on the Navigation Map
Appendix
1) With the Navigation Map displayed, select the MAP Softkey.
Index
2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
52
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
TERRAIN AWARENESS & WARNING SYSTEM
TAWS-A (Optional)
NOTE: TAWS operation is only available when the system is configured for
a TAWS-A installation.
GPS Nav
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
AFCS
Nav/Com/
XPDR/Audio
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Manual System Test
Flight
Planning
1) While the TAWS-A Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Test TAWS System’.
Procedures
3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-A Page.
When all is in working order, “TAWS System Test, OK” is heard.
Hazard
Avoidance
Displaying the TAWS-A Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS-A Page.
Additional
Features
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.
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Terrain/Obstacle Location
Appendix
190-00929-03 Rev. A
Color
Annun/Alerts
4) Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.
53
Hazard Avoidance
Flight
Instruments
Enable/Disable Aviation Data
1) While the TAWS-A Page is displayed, press the MENU Key.
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3) Press the ENT Key.
Inhibiting/Enabling FLTA and PDA Alerting
AFCS
1) Select the TAWS-A Page.
2) Select the TAWS INH Softkey to inhibit or enable TAWS-A (choice
dependent on current state).
GPS Nav
Overriding Flaps-based FIT Alerting
1) Select the TAWS-A Page.
Flight
Planning
2) Select the FLAP OVR Softkey.
Inhibiting/Enabling GPWS Alerting
Procedures
1) Select the TAWS-A Page.
2) Select the GPWS INH Softkey to inhibit or enable GPWS alerts (choice
dependent on current state).
Hazard
Avoidance
Inhibiting/Enabling GSD Alerting
NOTE: Only available during a GSD alert.
Additional
Features
1) Select the TAWS-A Page.
2) Select the GS INH or GP INH Softkey to inhibit or enable GSD alerts
(softkey choice dependent on present GSD alert type).
Annun/Alerts
TAWS-B
Index
Appendix
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
54
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
NOTE: TAWS operation is only available when the system is configured for
a TAWS-B installation.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Flight
Instruments
Manual System Test
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Test TAWS System’.
Nav/Com/
XPDR/Audio
3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
When all is in working order, “TAWS System Test, OK” is heard.
AFCS
Display Terrain and Obstacles on the TAWS-B Page
1) Turn the large FMS Knob to select the Map Page Group.
GPS Nav
2) Turn the small FMS Knob to select the TAWS-B Page.
Flight
Planning
3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
4) Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Additional
Features
Red
Hazard
Avoidance
Terrain/Obstacle Location
Procedures
Color
Enable/Disable Aviation Data
Annun/Alerts
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3) Press the ENT Key.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
55
Index
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Appendix
TAWS Inhibit
Hazard Avoidance
Flight
Instruments
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Nav/Com/
XPDR/Audio
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit TAWS’.
AFCS
3) Press the ENT Key.
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
GPS Nav
Or:
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable TAWS’.
Flight
Planning
3) Press the ENT Key.
Displaying Terrain and Obstacles on the Navigation Map
2) Select the TERRAIN Softkey. Terrain and obstacles will now be displayed
on the map.
AIRBORNE COLOR WEATHER RADAR
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
1) With the Navigation Map displayed, select the MAP Softkey.
Appendix
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
Index
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Weather Radar Page.
56
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
Or:
AFCS
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.
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
3) Select the MODE Softkey.
5) Turn the Joystick to select the desired range.
GPS Nav
6) If desired, select the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
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.
Procedures
Adjusting Antenna Bearing
Flight
Planning
Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
57
Hazard Avoidance
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
2) Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.
AFCS
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.
GPS Nav
5) To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.
Adjusting Gain
Procedures
Flight
Planning
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.
Hazard
Avoidance
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.
Additional
Features
4) Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.
Annun/Alerts
Ground Mapping
1) Select the MODE Softkey.
2) Select the GROUND Softkey to place the radar in Ground Map Mode.
Index
Appendix
3) Select the BACK Softkey.
58
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Hazard Avoidance
2) Press the FMS Knob to display the cursor.
3) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
Sector Scan
4) Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.
GPS Nav
6) Press the FMS Knob to remove the cursor.
AFCS
5) If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
Antenna Stabilization
Flight
Planning
1) To activate or deactivate the antenna stabilization, select the MODE
Softkey.
Annun/Alerts
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.
Additional
Features
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.
Hazard
Avoidance
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the WATCH® feature, select the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Procedures
2) Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
59
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
Blank Page
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
Flight
Planning
Procedures
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Additional
Features
Annun/Alerts
•
•
•
•
•
•
•
GPS Nav
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:
AFCS
WARNING: Do not use SVS runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
Displaying SVS Terrain
1) Press the PFD Softkey.
Appendix
2) Press the SYN VIS Softkey.
3) Press the SYN TERR Softkey.
4) Press the BACK Softkey to return to the previous page.
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
61
Additional Features
Flight
Instruments
Displaying Pathways
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
Nav/Com/
XPDR/Audio
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.
AFCS
Displaying Heading on the Horizon
1) Press the PFD Softkey.
GPS Nav
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
4) Press the HRZN HDG Softkey.
Flight
Planning
5) Press the BACK Softkey to return to the previous page.
Displaying Airport Signs
Procedures
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
4) Press the APTSIGNS Softkey.
5) Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
62
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Additional Features
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
3) Select the GO BACK Softkey to return to the previous page.
Appendix
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.
Annun/Alerts
Additional
Features
Or:
Hazard
Avoidance
1) Select the SHW CHRT Softkey when displayed.
Procedures
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services 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.
GPS Nav
FliteCharts®
AFCS
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.
Nav/Com/
XPDR/Audio
ChartView
Flight
Instruments
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
63
Additional Features
Flight
Instruments
View Charts from the Active Flight Plan Page
1) While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
Nav/Com/
XPDR/Audio
2) Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
AFCS
3) Select the SHW CHRT Softkey. The appropriate chart will be displayed, if
available for the item selected.
4) Select the GO BACK Softkey to return to the previous page.
Change Day/Night View
GPS Nav
1) While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
Flight
Planning
2) Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3) Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
Procedures
4) Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
Hazard
Avoidance
5) Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
Additional
Features
6) In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
7) Press the FMS Knob when finished to remove the Chart Setup Menu.
AOPA Airport Directory adds enhanced airport information when viewing airports
on the WPT-Airport Information Page.
This database is updated four times per year. Check fly.garmin.com for the current
database.
View Airport Directory Information
Index
Appendix
Annun/Alerts
AOPA AIRPORT DIRECTORY
64
While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Additional Features
NOTE: Separate accounts must be established to access the Iridium satellite
network for voice/SMS and low speed data transmission, and high speed data
transmission for the maintenance reports.
Hazard
Avoidance
Additional
Features
1) With the aircraft outside and having a clear view of the sky, turn the large
FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the
System ID number in the AIRFRAME field.
5) Press the MENU Key. The Page Menu window is now displayed.
6) Select ‘Register With GFDS’ in the menu list.
65
Index
7) Press the ENT Key. The Garmin Flight Data Service Registration window is
now displayed.
Appendix
4) If necessary, select the REPORTS Softkey. The AUX-REPORT STATUS Page is
now displayed.
Annun/Alerts
3) Turn the small FMS Knob to select the AUX-REPORTS STATUS or AUX-WI-FI
SETUP Page.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Procedures
Registering the system for datalink services
190-00929-03 Rev. A
Flight
Planning
A subscriber account must be established for each Iridium transceiver prior to
using the Iridium Satellite System for telephone services. Before setting up an Iridium
account, obtain the serial number of the Iridium Transceiver (GSR1) and the System
ID by selecting the AUX- SYSTEM STATUS Page. Contact Garmin Flight Data Services
at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135.
After a subscriber account has been established, the system must be registered for
datalink features such as reporting services or GFDS Worldwide Weather. Registration
is accomplished by entering the required access code. This process is only performed
when initially setting up the system for GFDS services.
GPS Nav
Registering with Garmin Flight Data Services
AFCS
Operation of these features in the cockpit is accomplished through the AUXTELEPHONE, AUX-TEXT MESSAGING, AUX-REPORT STATUS, and AUX-WI-FI
SETUP Pages. For operation using the cabin handset, consult the instructions provided
with the handset.
Nav/Com/
XPDR/Audio
Flight
Instruments
SATELLITE TELEPHONE AND DATA LINK SERVICES
Additional Features
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
8) Enter the access code obtained from Garmin Flight Data Services in the
Access Code field.
9) Press the ENT Key. REGISTER will now be highlighted.
10) Press the ENT Key. System registration is complete when ‘REGISTERED’ is
displayed in the STATUS field.
Disable/Enable Iridium Transceiver
Iridium telephone and data communications may be turned on or off by performing
these simple steps.
Disable/Enable Telephone and Low Speed Data Services:
GPS Nav
1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select the AUX-REPORTS STATUS or AUX-WI-FI
SETUP Page.
Flight
Planning
3) If necessary, select the REPORTS Softkey. The AUX-REPORT STATUS Page is
now displayed.
5) Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list.
6) Press the ENT Key. The Iridium transceiver is now disabled.
7) To enable the Iridium transceiver, repeat steps 1 through 4, then select
‘Enable Iridium Transceiver’.
Telephone Communication
The pilot or copilot can place and answer calls on the Iridium satellite network as well
as to or from the telephone handset in the cabin. Calls can also be answered or made from
the cabin phone, however, only actions initiated from the cockpit phone will be discussed
here. See the cabin handset user guide for more information. Control and monitoring of
telephone functions are accomplished through the AUX-TELEPHONE Page.
Viewing the Telephone Page
1) Turn the large FMS Knob on the MFD to select the AUX page group.
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
4) Press the MENU Key. The Page Menu window is now displayed.
2) Turn the small FMS Knob to select the AUX - TELEPHONE or AUX - TEXT
MESSAGING Page.
Index
3) If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page.
66
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Additional Features
External
Phone
Flight
Instruments
Internal
Phone
Description
Nav/Com/
XPDR/Audio
Phone is Idle
Phone is ringing
AFCS
Phone has a dial tone (off hook) or connected to
another phone
GPS Nav
Phone dialed is busy
Flight
Planning
Phone is dialing another phone
Procedures
Phone has failed
Hazard
Avoidance
Phone status not known
Phone is disabled
Additional
Features
Phone is reserved for data transmission
Annun/Alerts
Calling other phone or incoming call from other phone
Appendix
Other phone is on hold
Index
Phones are connected
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
67
Incoming Calls
When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up
alert will be displayed. If the call is from the cabin, CABIN will be displayed. If the
incoming call is an Iridium network call, IRIDIUM will be displayed. The pop-up alert
may be inhibited at times, such as during takeoff. In addition to the pop-up alert, a
ringing phone symbol will be displayed to the right of the MFD page title. Also, the
voice alert “Incoming Call” will be heard on the selected cockpit audio.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Answer an Incoming Call in the Cockpit
1) Press the TEL Key on the appropriate audio panel.
GPS Nav
2) Select the ANSWER Softkey on the MFD.
Or:
Procedures
Flight
Planning
1) Press the TEL Key on the appropriate audio panel.
2) Press the MENU Key to display the Page Menu.
3) Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’.
4) Press the ENT Key.
Selecting the IGNORE Softkey will extinguish the pop-up window and leave the
call unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page
allowing additional call information to be viewed before answering.
Mute Incoming Call Alerts
1) With the AUX-TELEPHONE Page displayed, press the MENU Key on the
MFD to display the Page Menu.
Additional
Features
Hazard
Avoidance
While viewing the AUX-TELEPHONE Page
Annun/Alerts
2) Turn either FMS Knob to place the cursor on ‘Mute Incoming Call Alerts’.
Index
Appendix
3) Press the ENT Key. The voice and pop-up alert will not be displayed now
when an incoming call is received.
68
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Additional Features
Voice calls can be made from the cockpit to the handset in the cabin, or to an
external phone through the Iridium Satellite Network.
Flight
Instruments
Outgoing Calls
Nav/Com/
XPDR/Audio
Make a Call to the Cabin:
1) Press the TEL Key on the appropriate audio panel.
2) Select the DIAL Softkey on the MFD.
AFCS
3) Press the ENT Key. The cursor will move from ‘CABIN’ to ‘OK’.
4) Press the ENT Key again. The cabin phone will now ring.
GPS Nav
To exit the call, select the HANGUP Softkey.
Make an External Call from the Cockpit
Flight
Planning
1) Press the TEL Key on the appropriate audio panel.
2) Select the DIAL Softkey on the MFD.
3) Turn the small FMS Knob to select ‘IRIDIUM’.
Hazard
Avoidance
5) Enter the desired telephone number (country code first) by selecting the
number softkeys on the MFD or by pressing the numeric keys on the MFD
Control Unit.
6) Press the ENT Key. ‘OK’ is highlighted.
Additional
Features
7) Press the ENT Key. The system will begin calling the number.
To exit the call, select the HANGUP Softkey.
Annun/Alerts
Placing The Cockpit Phone on Hold
Procedures
4) Press the ENT Key. The cursor has now moved to the phone number entry
field.
Select the HOLD Softkey on the MFD.
Or:
Appendix
1) Press the MENU Key to display the Page Menu.
2) Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’.
3) Press the ENT Key.
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Index
Select the HOLD Softkey again to resume the call.
69
Transferring a Call from the Cockpit
From the cockpit phone, a external call can be transferred to the cabin phone,
or a call with the cabin phone can be transferred to an external phone, or (when
two Iridium Transceivers are installed) an external call can be transferred to another
external phone.
1) Select the TRANS Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’.
c) Press the ENT Key.
2) Press the ENT Key. The cursor now highlights the phone number entry
field.
3) Enter the phone number as discussed earlier for making an external call on
the Iridium satellite network.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Procedures
4) Press the ENT Key. ‘OK’ is now highlighted.
5) Press the ENT Key again to place the call.
Making a Conference Call from the Cockpit
Hazard
Avoidance
1) Select the CONF Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’.
c) Press the ENT Key.
Annun/Alerts
2) Press the ENT Key. The cursor now highlights the phone number entry
field.
Appendix
3) Enter the phone number as discussed earlier for making an external call on
the Iridium satellite network.
4) Press the ENT Key. ‘OK’ is now highlighted.
Index
5) Press the ENT Key again to place the call.
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Additional Features
Viewing the Text Messaging Page
AFCS
1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select the AUX - TELEPHONE or AUX - TEXT
MESSAGING Page.
Flight
Planning
Description
GPS Nav
3) If necessary, select the SMS Softkey to display the AUX-TEXT MESSAGING
Page.
Message Symbol
Nav/Com/
XPDR/Audio
Messages may be sent to an email address or text message capable cellular telephone.
Message length is limited to 160 characters, including the email address.
The text messaging user interface is mainly through the AUX-TEXT MESSAGING
Page.
Flight
Instruments
Text Messaging (SMS)
Received text message that has not been opened
Procedures
Received text message that has been opened
Hazard
Avoidance
Saved text message, draft not sent
Additional
Features
System is sending text message
Annun/Alerts
Text message has been sent
System failed to send text message
Appendix
Predefined text message
Index
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71
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Viewing a Text Message When Received
When viewing MFD pages other than the AUX-TEXT MESSAGING Page, a pop-up
alert will be displayed when a new text message is received.
Select the VIEW Softkey to view the message. Selecting the IGNORE Softkey will
extinguish the pop-up window and leave the text message unopened. Selecting the
IGNR ALL Softkey will extinguish the pop-window and ignore all future incoming
text messages. Selecting the SMS Softkey will display the AUX-TEXT MESSAGING
Page.
The pop-up alerts may be enabled or disabled through the Page Menu.
GPS Nav
Enable/Disable Incoming Text Message Pop-Up Alerts
1) With the AUX-TEXT MESSAGING Page displayed, press the MENU Key on
the MFD to display the Page Menu.
Flight
Planning
2) Turn either FMS Knob to place the cursor on ‘Disable New Message
Popups’ or ‘Enable New Message Popups’.
Procedures
3) Press the ENT Key. The pop-up alert will not be displayed when an
incoming text message is received.
Reply to a Text Message
Hazard
Avoidance
While viewing the text message, select the REPLY Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Reply To Message’.
c) Press the ENT Key.
Annun/Alerts
Sending a Text Message
1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey.
Or:
Appendix
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Draft New Message’.
Index
c) Press the ENT Key.
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Additional Features
Flight
Instruments
Nav/Com/
XPDR/Audio
2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the
‘TO’ field. Enter the desired telephone number or email address. Entry can
be accomplished through the alphanumeric keys on the MFD Controller,
or combination of the FMS Knob on the controller and softkeys on the
MFD. The FMS Knob is used to enter letters and numbers, or numbers
can be entered from the MFD by selecting the NUMBERS Softkey. Select
the CAP LOCK Softkey to create upper and lower case alpha characters.
Special characters can be accessed by selecting the SYMBOLS Softkey.
AFCS
3) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
GPS Nav
4) Enter the desired message using any combination of entry methods as
described in step 2.
5) Press the ENT Key.
Flight
Planning
6) Select the SEND Softkey to send the message immediately, or select the
SAVE Softkey to save the message in Outbox for sending at a later time.
Select the CANCEL Softkey to delete the message.
Predefined Text Messages
Procedures
Time and effort can be saved in typing text messages that are used repeatedly by
saving these messages as a predefined message.
Create a Predefined Text Message
Hazard
Avoidance
1) While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to
display the Page Menu.
Additional
Features
2) Turn either FMS Knob to select ‘Edit Predefined Messages’.
3) Press the ENT Key. The PREDEFINED MESSSAGES view is now displayed.
4) Select the NEW Softkey.
Annun/Alerts
Or:
a) Press the MENU Key to display the Page Menu.
Appendix
b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined
Message’.
c) Press the ENT Key. The PREDEFINED SMS TEXT MESSAGE Window is
now displayed.
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73
Index
5) The cursor is displayed in the ‘TITLE’ field. Enter the desired message title.
Entry can be accomplished through the alphanumeric keys on the MFD
Controller, or combination of the FMS Knob on the controller and softkeys
Additional Features
Nav/Com/
XPDR/Audio
Flight
Instruments
on the MFD. The FMS Knob is used to enter letters and numbers, or
numbers can be entered from the MFD by selecting the NUMBERS Softkey.
Select the CAP LOCK Softkey to create upper and lower case alpha
characters. Special characters can be accessed by selecting the SYMBOLS
Softkey.
6) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
AFCS
7) Enter the desired message using any combination of entry methods as
described in step 5.
8) Press the ENT Key.
GPS Nav
9) Select the SAVE Softkey. The new predefined message is now shown in
the displayed list. Selecting the CANCEL Softkey will delete the message
without saving.
10) Press the MENU Key to display the Page Menu.
Flight
Planning
11) Turn either FMS Knob to place the cursor on ‘Stop Editing Predefined
Message’.
Procedures
12) Press the ENT Key.
Send a Predefined Text Message
1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey.
Annun/Alerts
Additional
Features
Hazard
Avoidance
2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the
‘TO’ field. Enter the desired telephone number or email address. Entry can
be accomplished through the alphanumeric keys on the MFD Controller, or
combination of the FMS Knob on the controller and softkeys on the MFD.
The FMS Knob is used to enter letters and numbers, or numbers can be
entered from the MFD by selecting the NUMBERS Softkey. Select the CAP
LOCK Softkey to create upper and lower case alpha characters. Special
characters can be accessed by selecting the SYMBOLS Softkey.
3) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
Appendix
4) Select the PREDEFD Softkey. The PREDEFINED MESSAGE MENU Window is
displayed.
Index
6) Press the ENT Key. The predefined message text is inserted into the
message field. If desired, the message can be edited by using the FMS
Knobs.
7) Press the ENT Key.
8) Select the SEND Softkey to transmit the message.
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Additional Features
Show Inbox Messages
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the INBOX Softkey.
AFCS
Nav/Com/
XPDR/Audio
Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The
Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to
be sent later are stored as Drafts. Each text message box may be viewed separately, or
together in any combination.
Flight
Instruments
Text Message Boxes
Or:
GPS Nav
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’.
Flight
Planning
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Show Outbox Messages
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the OUTBOX Softkey.
Procedures
Or:
b) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’.
Additional
Features
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Show Draft Messages
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the DRAFTS Softkey.
Annun/Alerts
Hazard
Avoidance
a) Press the MENU Key to display the Page Menu.
Or:
Appendix
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’.
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Index
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75
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Arranging Text Messages
The viewed messages may be listed according to the date/time the message was
sent or received, the type of message (read, unread, sent, unsent, etc.), or by message
address.
View Messages Sorted by Message Date/Time:
AFCS
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the TIME Softkey.
Or:
GPS Nav
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’.
Flight
Planning
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
View Messages Sorted by Message Type
Procedures
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the TYPE Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Hazard
Avoidance
b) Turn either FMS Knob to place the cursor on ‘Sort By Type’.
Additional
Features
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
View Messages Sorted by Address:
Annun/Alerts
While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE
Softkey, then select the ADDRESS Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Appendix
b) Turn either FMS Knob to place the cursor on ‘Sort By Address’.
Index
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
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Additional Features
1) While viewing the AUX-TEXT MESSAGING Page, select the desired message box.
Flight
Instruments
Viewing The Content of a Text Message
2) Press the FMS Knob to activate the cursor.
Nav/Com/
XPDR/Audio
3) Turn either FMS Knob to select the desired message.
4) Select the VIEW Softkey.
Or:
Press the ENT Key.
AFCS
Or:
b) Turn either FMS Knob to place the cursor on ‘View Selected Message’.
GPS Nav
a) Press the MENU Key to display the Page Menu.
c) Press the ENT Key.
Flight
Planning
5) To close the text message, select the CLOSE Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Procedures
b) Turn either FMS Knob to place the cursor on ‘Close Message’.
c) Press the ENT Key.
Hazard
Avoidance
Mark Selected Message As Read
1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
Additional
Features
2) Turn either FMS Knob to select the desired message.
3) Select the MRK READ Softkey.
Or:
Annun/Alerts
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message
As Read’.
Appendix
c) Press the ENT Key.
The message symbol now indicates the message has been opened.
Index
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77
Additional Features
Flight
Instruments
Mark All Messages As Read
1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
MENU Key to display the Page Menu.
Nav/Com/
XPDR/Audio
2) Turn either FMS Knob to place the cursor on ‘Mark All New Messages As
Read’.
3) Press the ENT Key. A confirmation window is displayed.
AFCS
4) With cursor highlighting ‘YES’, press the ENT Key. The message symbols
now indicate all the message have been opened.
GPS Nav
Delete a Message
1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
Flight
Planning
2) Turn either FMS Knob to select the desired message.
3) Select the DELETE Softkey.
Or:
b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’.
c) Press the ENT Key.
WI-FI CONNECTIONS
The system can connect to a IEEE 802.11g compatible network provided the
aircraft is on the ground and located within range of the network. The system is
capable of WEP64, WEP128,WPA-PSK, and WPA2-PSK encryption formats. WPAEnterprise and WPA2-Enterprise are not supported. Connections that require web
proxies, captive portals, or other elements that require user credentials, including a
username and password or a redemption or access code; or require action such as
accepting a user agreement, are not supported.
Control and monitoring of Wi-Fi functions are accomplished through the AUXWI-FI SETUP Page.
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
a) Press the MENU Key to display the Page Menu.
View the Wi-Fi Setup Page
1) Turn the large FMS Knob on the MFD to select the AUX page group.
Index
2) Turn the small FMS Knob to select the AUX - WI-FI SETUP or AUX - REPORT
STATUS Page.
3) If necessary, select the WI-FI Softkey to display the AUX-WI-FI SETUP Page.
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Additional Features
2) If necessary, select the RESCAN Softkey to have the system scan again for
available networks.
Nav/Com/
XPDR/Audio
1) Select the AVAIL Softkey on the MFD. A list of available networks will
be displayed in the AVAILABLE NETWORKS window. Signal strength is
shown for each network, as well as security requirements and whether the
network has been saved in the system’s memory.
Flight
Instruments
Set Up a New Wi-Fi Connection
AFCS
Or:
a) Press the MENU Key to display the Page Menu.
GPS Nav
b) Turn either FMS Knob to place the cursor on ‘Rescan Available
Networks’.
c) Press the ENT Key.
Flight
Planning
3) Press the FMS Knob to place the cursor in the list of networks.
4) Turn either FMS Knob to select the desired network.
5) Select the CONNECT Softkey.
Procedures
Or:
a) Press the MENU Key to display the Page Menu.
Hazard
Avoidance
b) Turn either FMS Knob to place the cursor on ‘Connect To Selected
Network’.
c) Press the ENT Key.
8) Press the ENT Key again.
10) The selected network can be saved to system memory to make reconnection easier at a later time.
Appendix
9) The SAVE SETTINGS window is now displayed with the cursor highlighting
‘SAVE CONNECTION’.
Annun/Alerts
7) Press the ENT Key. ‘OK’ will be highlighted.
Additional
Features
6) If the network is secured, a window will be displayed in order to enter
the necessary passcode. Use the FMS Knobs to enter the desired alpha
numeric characters. Select the CAP LOCK Softkey to enter upper case
letters. If there is no security associated with the network, proceed to step
9.
Index
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79
Additional Features
Flight
Instruments
To connect the selected network without saving:
a) Turn the large FMS Knob to move the cursor to highlight ‘CONNECT’.
b) Press the ENT Key.
Nav/Com/
XPDR/Audio
To save and connect the selected network:
a) Press the ENT Key. A checkmark is placed in the checkbox and the
cursor moves to the airport field.
AFCS
b) Using the FMS Knobs, enter an airport identifier to be associated with
the saved network. This aids in identifying the network later in the
event of duplicate network names.
GPS Nav
c) Press the ENT Key. The cursor moves to ‘CONNECT’.
d) Press the ENT Key again to connect to the selected network.
Flight
Planning
Edit a Saved Network
1) While viewing list of saved networks, press the FMS Knob to activate the
cursor.
Procedures
2) Turn either FMS Knob to highlight the network to be edited.
3) Pressing the ENT Key at this point will check or uncheck the AUTO
CONNECT checkbox. When a checkmark is present, the system will
automatically connect to the network when within range.
Hazard
Avoidance
4) Select the EDIT Softkey. The cursor now appears in the CONNECTION
SETTINGS window.
5) Turn the large FMS Knob to select the network attribute to be edited.
Additional
Features
6) Turn the small FMS Knob to begin editing the field.
7) When the entry is complete, press the ENT Key.
Annun/Alerts
8) Turn the large FMS Knob or press the ENT Key until ‘SAVE’ is highlighted.
9) Press the ENT Key.
Disconnect a Wi-Fi Network
Appendix
Select the DISCNCT Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
Index
b) Turn either FMS Knob to place the cursor on ‘Disconnect From
Network’.
c) Press the ENT Key.
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Additional Features
Flight
Instruments
Delete a Saved Wi-Fi Network:
1) While viewing the list of saved networks, press the FMS Knob to activate
the cursor.
3) Select the DELETE Softkey. The selected network is removed from the list.
AFCS
SYSTEM DATA LOGGING
Nav/Com/
XPDR/Audio
2) Turn either FMS Knob to highlight the network to be deleted.
Hazard
Avoidance
Additional
Features
1) Turn the large FMS Knob on the MFD to select the AUX page group.
Procedures
View the Report Status Page
Flight
Planning
The system selects the appropriate transmission method based on communication
network availability. Data transmission is manually when the airplane is on the
ground.
If report transmission is interrupted for some reason (e.g. networks unavailable,
hardware failure, loss of power), the system will attempt to resume sending the reports
at the next opportunity. The system ensures the complete data set is transmitted.
Transmitted reports remain in the system’s memory until they are overwritten by
newer data.
Control and monitoring of report transmissions is accomplished through the AUXREPORT STATUS Page.
GPS Nav
NOTE: An account must be established with Garmin Flight Data Services to
make full use of the System Data Logging feature.
2) Turn the small FMS Knob to select AUX-WI-FI SETUP or AUX-REPORT
STATUS Page.
Annun/Alerts
3) If necessary, select the REPORT Softkey to display the AUX-REPORT STATUS
Page.
Changing Transmission Method
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
2) Turn the large FMS Knob to move the cursor to the 1st or 2nd transmit
method for the desired data report.
Appendix
1) While viewing the Report Status Page, press the FMS Knob to activate the
cursor.
81
Additional Features
Nav/Com/
XPDR/Audio
Flight
Instruments
3) Turn the small FMS Knob to select the desired option (SAT SHORT BURST,
SAT RUDICS, WI-FI, or NONE). Sat Short Burst is generally used for
transmission of data packets less than 300 bytes. Wi-Fi is used only when
the aircraft on the ground.
4) Press the ENT Key.
Send All Unsent Data
AFCS
1) While viewing the Report Status Page, press the FMS Knob to activate the
cursor.
GPS Nav
2) Turn the large FMS Knob to move the cursor to the SEND button on the
desired data report.
3) Press the ENT Key. The Send Report window is displayed.
4) Turn the large FMS Knob to highlight the ‘SELECT DATA TO SEND’ field.
Flight
Planning
5) Turn the small FMS Knob to select ‘ALL UNSENT DATA’.
6) Press the ENT Key.
Procedures
Resend Data or Send Data Recorded in a Specific Time Frame
NOTE: Transmission of data can only be performed while the aircraft is
Hazard
Avoidance
on the ground.
Additional
Features
1) While viewing the Report Status Page, press the FMS Knob to activate the
cursor.
2) Turn the large FMS Knob to move the cursor to the SEND button on the
desired data report.
Annun/Alerts
3) Press the ENT Key. The Send Report window is displayed.
4) Turn the large FMS Knob to highlight the ‘SELECT DATA TO SEND’ field.
5) Turn the small FMS Knob to select ‘DATA WITHIN TIME FRAME’.
Appendix
6) Press the ENT Key. The time frame selection fields are now displayed.
7) Turn the large FMS Knob to select the starting time or date field.
8) Turn the small FMS Knob to select the desired starting time or date.
Index
9) Press the ENT Key. The cursor will move to the next field.
10) When the last field is addressed, ‘OK’ will be highlighted. Press the ENT
Key to send the selected data.
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Additional Features
Flight
Instruments
Restore Reports Page Options to Default Settings:
1) While viewing the Report Status Page, press the MENU Key.
2) Turn the FMS Knob to select ‘Restore Defaults’ in the menu list.
Nav/Com/
XPDR/Audio
3) Press the ENT Key.
4) A confirmation window is now displayed.
5) Turn the large FMS Knob to select ‘YES’ or ‘NO’.
AFCS
6) With ‘YES’ highlighted, press the ENT Key.
SIRIUSXM™ RADIO ENTERTAINMENT
Flight
Planning
Selecting the XM Radio Page
1) Turn the large FMS Knob to select the Auxiliary Page Group.
Procedures
2) Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3) Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Selecting a Category
Index
83
Appendix
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Annun/Alerts
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the CATGRY Softkey on the XM Radio Page.
2) Select the CAT + and CAT - Softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
Additional
Features
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.
Hazard
Avoidance
Active Channel and Channel List
190-00929-03 Rev. A
GPS Nav
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM™ Satellite Radio.
Additional Features
Flight
Instruments
Select an Available Channel within the Selected Category
1) While on the XM Radio Page, select the CHNL Softkey.
Nav/Com/
XPDR/Audio
2) Select the CH + Softkey to move down through the list in the Channel Box,
or move up the list with the CH – Softkey.
Or:
AFCS
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.
GPS Nav
Entering a Channel Directly
1) While on the XM Radio Page, select the CHNL Softkey.
Flight
Planning
2) Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3) Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
Procedures
4) Press the ENT Key to activate the selected channel.
Assigning Channel Presets
Annun/Alerts
Additional
Features
Hazard
Avoidance
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).
2) Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Selecting the
MORE Softkey repeatedly cycles through the preset channels.
3) Select the SET Softkey.
4) Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
Appendix
Adjusting Volume
Index
Radio volume is controlled at each passenger station.
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Additional Features
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
4) Press the FMS Knob to activate the cursor.
Procedures
3) If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
Flight
Planning
2) Turn the small FMS Knob to select the System Setup Page.
GPS Nav
1) Turn the large FMS Knob to select the AUX Page Group.
AFCS
To enable or disable ESP:
Nav/Com/
XPDR/Audio
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo, Mmo,
and/or angle of attack) beyond the normal flight parameters. Enhanced stability for each
condition is provided by applying a force to the appropriate control surface to return the
aircraft to the desired flight envelope. This is perceived by the pilot as resistance to control
movement in the undesired direction when the aircraft approaches a steep attitude, high
airspeed, or when a stall is imminent.
As the aircraft deviates further from the desired attitude, angle of attack, or airspeed
continues to increase, the force increases (up to an established maximum) to encourage
control movement in the direction necessary to return to the desired attitude and/or
airspeed range. Except in the case of high airspeed, when maximum force is reached, force
remains constant up to the maximum engagement limit. Above the maximum engagement
limit, forces are no longer applied. There is no maximum engagement related to a high
airspeed condition.
When ESP has been engaged for more than ten seconds (cumulative; not necessarily
consecutive seconds) of a 20-second interval, the autopilot is automatically engaged with
the flight director in Level Mode in the pitch and/or roll axis, bringing the aircraft into
level flight. An aural “Engaging Autopilot” alert is played and the flight director mode
annunciation will indicate ‘LVL’ for vertical and lateral modes.
The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering
(CWS) or Autopilot Disconnect (AP/YD DISC TRIM INTRPT) switch. Upon releasing the
CWS or AP/YD DISC TRIM INTRPT switch, ESP force will again be applied, provided
aircraft attitude, angle of attack and/or airspeed are within their respective engagement
limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit.
ESP can be enabled or disabled on the AUX-SYSTEM SETUP 2 Page on the MFD.
Flight
Instruments
ELECTRONIC STABILITY & PROTECTION (ESP™)
5) Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
Index
6) Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7) Press the FMS Knob to remove the cursor.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
85
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Roll Engagement
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the onside Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing
where ESP will disengage as roll attitude decreases to within the desirable roll attitude
range.
Once engaged, ESP force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force
is intended to encourage pilot input that returns the airplane to a more normal roll
attitude. As roll attitude decreases, ESP will disengage at 30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
ESP engages at 20° nose-up and 17° nose-down. Once ESP is engaged, it will apply
opposing force between 15° and 50° nose-up and between 12° and 50° nose-down.
Maximum opposing force is applied between 25° and 50° nose-up and between 22°
and 50° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP engage and disengage limits in
these nose-up/nose-down conditions.
Angle of Attack Protection
If the Angle of Attack Proctection feature is available in the current installation,
ESP force may be applied if the compatible lift computer determines a stall warning
condition is imminent. In this condition, the Pitch Limit Indicator will be initially
displayed 4° below this computed pitch attitude. When pitch attitude equals that
indicated by the Pitch Limit Indicator, ESP will engage, applying a force in the direction
necessary to lower the nose of the aircraft.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Pitch Engagement
High Airspeed Protection
Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of
the aircraft. When the high airspeed condition is remedied, ESP force is no longer
applied.
86
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
WARNING ANNUNCIATION
Alerts Window
Text
Nav/Com/
XPDR/Audio
Aural Alert
“Airspeed” is heard once when an altitude-notUNDERSPEED critcal flight director mode is active. “Airspeed”
PROTECT ACTIVE - repeats every five seconds when an altitudecritical flight director mode is active.
AFCS
Annunciation
Window Text
UNDERSPEED
PROTECT ACTIVE
GPS Nav
ADVISORY ANNUNCIATIONS
Alerts Window Text
AVN FAN 2 FAIL
AVN FAN 2 FAIL - Avionics cooling fan #2 is inoperative.
PFD 1 FAN FAIL
PFD 2 FAN FAIL
PFD 1 FAN FAIL - PFD #1 cooling fan is inoperative.
MFD FAN FAIL
MFD FAN FAIL - MFD cooling fan is inoperative.
Procedures
AVN FAN 1 FAIL - Avionics cooling fan #1 is inoperative.
Flight
Planning
Annunciation
Window Text
AVN FAN 1 FAIL
PFD FAN FAIL - PFD #2 cooling fan is inoperative.
Hazard
Avoidance
MESSAGE ADVISORY ALERTS
Alerts Window Message
Additional
Features
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
190-00929-03 Rev. A
Annun/Alerts
*ESP DEGRADE – ESP AOA mode is inoperative.
ESP DEGRADE – ESP IAS mode is inoperative.
ESP FAIL – ESP is inoperative.
ESP OFF – ESP selected off.
ESP CONFIG – ESP config error. Config service req’d.
TAWS GEAR FAULT – Landing Gear detected in the DOWN position.
TAWS FLAP FAULT – Flaps detected in the LDG position.
WOW FAULT – Miscompare between weight on wheels inputs.
WOW INVALID – Weight on wheels inputs invalid.
YD OFF – AP engaged without Yaw Damper.
*only available when compatible lift computer is installed.
87
COMPARATOR ANNUNCIATIONS
Comparator Window
Text
ALT MISCOMP
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
If either airspeed sensor detects > 35 knots, and the difference in sensors
is > 10 kts.
Procedures
Flight
Planning
GPS Nav
AFCS
If either airspeed sensor detects > 80 knots, and the difference in
sensors is > 7 kts.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..
Condition
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
Both PFDs are displaying data from the number one GPS receiver.
Index
Appendix
Reversionary Sensor
Window Text
Additional
Features
REVERSIONARY SENSOR ANNUNCIATIONS
Annun/Alerts
Hazard
Avoidance
Condition
88
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 GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
Nav/Com/
XPDR/Audio
USING AHRS2
USING GPS1
USING GPS2
Condition
Flight
Instruments
Reversionary Sensor
Window Text
PFD1 is displaying data from the #2 GPS.
Condition
Annunciation Description
Roll Failure
Roll axis control failure.
Pitch Trim Axis
Control Failure
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
System Failure
AP and MET are unavailable. FD may still be available.
Flight
Planning
Pitch axis control failure.
GPS Nav
Pitch Failure
Procedures
YD axis control failure.
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
Hazard
Avoidance
Yaw Damper/
Ruddar Boost
Failure
Elevator Mistrim
Up
AFCS
AFCS ALERTS
A condition has developed causing the roll servo to provide
a sustained left force.
Aileron Mistrim
Right
A condition has developed causing the roll servo to provide
a sustained right force.
Rudder Mistrim
Left
A condition has developed causing the yaw servo to
provide a sustained force.
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force.
Preflight Test
Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Preflight system test has failed.
Appendix
Aileron Mistrim
Left
Annun/Alerts
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
Additional
Features
Elevator Mistrim
Down
89
TAWS-A ALERTS
Alert Type
PFD/MFD
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Reduced Required Terrain
Clearance Warning (RTC)
or
Imminent Terrain Impact
Warning (ITI)
or
Reduced Required Obstacle
Clearance Warning (ROC)
or
Imminent Obstacle Impact
Warning (IOI)
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
Excessive Closure Rate
Warning (ECR)
“<whoop><whoop>
Pull Up”
or
Annun/Alerts
“<whoop><whoop>
Pull Up”
Reduced Required Terrain
Clearance Caution (RTC)
Imminent Terrain Impact
Caution (ITI)
or
Reduced Required Obstacle
Clearance Caution (ROC)
or
Index
Additional
Features
Aural Message
Excessive Descent Rate
Warning (EDR)
Appendix
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
90
“Caution, Terrain;
Caution, Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain;
Caution, Terrain”
“Caution, Obstacle;
Caution, Obstacle”
or
“Obstacle Ahead;
Obstacle Ahead”
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
or
Aural Message
“Obstacle Ahead;
Obstacle Ahead”
or
“Caution, Obstacle;
Caution, Obstacle”
Excessive Descent Rate
Caution (EDR)
“Sink Rate”
Excessive Closure Rate
Caution (ECR)
“Terrain, Terrain”
Negative Climb Rate
Caution (NCR)
“Don’t Sink”
or
“Too Low, Terrain”
Flight Into Terrain Gear
Caution (FIT)
“Too Low, Gear”
Flight Into Terrain Flaps
Caution (FIT)
“Too Low, Flaps”
Flight Into Terrain Takeoff
Caution (FIT)
“Too Low, Terrain”
or
or
None
None
(depends on approach type)
(all are configurable, except
“Five-Hundred”)
“Five-Hundred”
“Four-Hundred”
“Three-Hundred”
“Two-Hundred”
“One-Hundred”
Annun/Alerts
Altitude Voice Callout
(VCO)
“Glide Slope”
or
“Glide Path”
Additional
Features
Glide Slope Deviation
Caution (GSD)
Hazard
Avoidance
“Too Low, Terrain”
Procedures
Flight Into Terrain High
Speed Caution (FIT)
Flight
Planning
or
GPS Nav
“Too Low, Terrain”
AFCS
Premature Descent Alert
Caution (PDA)
Nav/Com/
XPDR/Audio
Imminent Obstacle Impact
Caution (IOI)
MFD Map Page
Pop-Up Alert
Flight
Instruments
PFD/MFD
TAWS Page
Annunciation
Alert Type
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
91
Annunciations & Alerts
Flight
Instruments
TAWS-A System Status Annunciations
Nav/Com/
XPDR/Audio
Alert Type
PFD/MFD
Additional TAWS-A Page
TAWS-A Page
Annunciation
Annunciation
TAWS FAIL
“TAWS System
Failure”
System Test in progress
TAWS TEST
None
Flight
Planning
GPS Nav
AFCS
TAWS System Fail
System Test pass
None
None
“TAWS System
Test OK”
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
None
TERRAIN DATABASE FAILURE
None
GPWS System Fail,
Radar Altimeter invalid,
Altitude or Vertical
Speed unavailable
None
“GPWS System
Failure”
No GPS position,
excessively degraded
GPS signal
NO GPS
POSITION
“TAWS Not
Available”
“TAWS
Available” when
sufficient GPS
signal is received.
Out of database
coverage area
None
“TAWS Not
Available”
“TAWS
Available”
when aircraft
enters database
coverage area.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Aural
Message
92
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Flight
Instruments
TAWS-A Alert Type Availability Under Various Conditions
TAWS-A Alert Type Available
GSD VCO
No
No
No
No
No
No
No
No
No
No
No
No
No
No
No
No
Yes
Yes
Yes
Yes
*No
**Yes
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
**Yes
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
No
No
No
No
**Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
#Yes
Yes
Yes
AFCS
Flight
Planning
Hazard
Avoidance
Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is
displayed.
MFD Map Page
Pop-Up Alert
or
Imminent Terrain Impact
Warning (ITI)
or
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
93
Index
190-00929-03 Rev. A
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Appendix
Reduced Required Terrain
Clearance Warning (RTC)
Aural Message
Annun/Alerts
PFD/MFD
TAWS Page
Annunciation
Additional
Features
TAWS-B ALERTS
Alert Type
Procedures
GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being
received.
** VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available.
#
GPS Nav
*
FIT
Nav/Com/
XPDR/Audio
TAWS-A
Status
RTC ITI ROC IOI PDA EDR ECR NCR
Annunciation
Displayed
Alert Type
PFD/MFD
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Reduced Required Obstacle
Clearance Warning (ROC)
or
Imminent Obstacle Impact
Warning (IOI)
or
Aural Message
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
Excessive Descent Rate
Warning (EDR)
“Pull Up”
Reduced Required Terrain
Clearance Caution (RTC)
or
Imminent Terrain Impact
Caution (ITI)
or
Reduced Required Obstacle
Clearance Caution (ROC)
or
Imminent Obstacle Impact
Caution (IOI)
or
“Caution, Terrain;
Caution, Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain;
Caution, Terrain”
“Caution, Obstacle;
Caution, Obstacle”
or
“Obstacle Ahead;
Obstacle Ahead”
“Obstacle Ahead;
Obstacle Ahead”
or
“Caution, Obstacle;
Caution, Obstacle”
Premature Descent Alert
Caution (PDA)
“Too Low, Terrain”
Excessive Descent Rate
Caution (EDR)
“Sink Rate”
Negative Climb Rate
Caution (NCR)
or
“Don’t Sink”
or
“Too Low, Terrain”
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
94
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Aural
Message
TAWS FAIL
“TAWS System
Failure”
System Test in progress
TAWS TEST
None
AFCS
TAWS System Fail
Nav/Com/
XPDR/Audio
PFD/MFD
Additional TAWS-A Page
TAWS-A Page
Annunciation
Annunciation
Alert Type
Flight
Instruments
TAWS-B System Status Annunciations
None
None
“TAWS System
Test OK”
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
None
TERRAIN DATABASE FAILURE
None
No GPS position,
excessively degraded
GPS signal
NO GPS
POSITION
“TAWS Not
Available”
“TAWS
Available”
when sufficient
GPS signal is
received.
Out of database
coverage area
None
“TAWS Not
Available”
“TAWS
Available”
when aircraft
enters database
coverage area.
GPS Nav
System Test pass
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
95
ADDITIONAL AURAL ALERTS
Aural Alert
“Minimums”
Description
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.
Played when the traffic system passes a pilot-initiated self test.
“Traffic Advisory
- SKY 497 TAS
System Test Passed”
“SKYWATCH System
Test Passed”
- SKY 899 TAS
“TAS System Test OK”
- KTA 870 TAS
Played when the traffic system fails a pilot-initiated self test.
- SKY 497 TAS
“Traffic Advisory
System Test Failed”
“SKYWATCH System
Test Failed”
- SKY 899 TAS
“TAS System Test Fail” - KTA 870 TAS
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
96
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Flight
Instruments
MFD & PFD MESSAGE ADVISORIES
Message
Comments
DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts
lost. Recheck settings.
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
XTALK ERROR – A flight display
The MFD and PFDs are not communicating with
crosstalk error has occurred.
each other. The system should be serviced.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD2 SERVICE – PFD2 needs
The PFD and/or MFD self-test has detected a
service. Return unit for repair.
problem. The system should be serviced.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – PFD2 software
The PFD and/or MFD has incorrect software
mismatch, communication halted. installed. The system should be serviced.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 config error.
The PFD configuration settings do not match
Config service req’d.
backup configuration memory. The system
PFD2 CONFIG – PFD2 config error. should be serviced.
Config service req’d.
MFD1 CONFIG – MFD1 config
The MFD configuration settings do not match
error. Config service req’d.
backup configuration memory. The system
should be serviced.
SW MISMATCH – GDU software
The MFD and PFDs have different software
version mismatch. Xtalk is off.
versions installed. The system should be
serviced.
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
97
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
MFD & PFD MESSAGE ADVISORIES (CONT.)
Message
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is
inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Comments
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the system should
be serviced.
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if
the problem persists.
The PFD1 configuration module backup memory
has failed. The system should be serviced.
The PFD1 voltage is low. The system should be
serviced.
The PFD2 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
Index
Appendix
Annun/Alerts
DATABASE MESSAGE ADVISORIES
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
PFD2 DB ERR – PFD2 navigation
database error exists.
98
Comments
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
navigation database. If problem persists, the
system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
The MFD and/or PFD detected a failure in the
basemap database.
AFCS
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.
GPS Nav
Flight
Planning
Procedures
The terrain database is present on another LRU,
but is missing on the specified LRU.
Hazard
Avoidance
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Annun/Alerts
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.
Additional
Features
190-00929-03 Rev. A
Comments
Nav/Com/
XPDR/Audio
Message
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
PFD2 DB ERR – PFD2 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
PFD2 DB ERR – PFD2 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
PFD2 DB ERR – PFD2 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
PFD2 DB ERR – PFD2 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD2 DB ERR – PFD2 obstacle
database missing.
Flight
Instruments
DATABASE MESSAGE ADVISORIES (CONT.)
99
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
DATABASE MESSAGE ADVISORIES (CONT.)
Message
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
PFD2 DB ERR – PFD2 airport
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
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Comments
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.
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
The MFD and/or PFDs detected a failure in the
ChartView database (optional feature). Ensure that
the data card is properly inserted. Replace data card.
If problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD and/or PFDs detected a failure in the
database error exists.
FliteCharts 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 – MFD1 Airport
The MFD detected a failure in the Airport Directory
Directory database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
100
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Comments
The PFDs and MFD have different navigation
database versions or regions installed. Crossfill
is off. Check the AUX-SYSTEM STATUS Page
to determine versions or regions. Also, check
the AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Standby
The PFDs and MFD have different standby
Navigation database mismatch.
navigation database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to
determine versions or regions. Also, check the
AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
Nav/Com/
XPDR/Audio
Message
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
Flight
Instruments
DATABASE MESSAGE ADVISORIES (CONT.)
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
101
DATABASE MESSAGE ADVISORIES (CONT.)
Message
DB MISMATCH – Airport Terrain
database mismatch.
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
NAV DB UPDATED – Active
navigation database updated.
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
GMA 1347D MESSAGE ADVISORIES
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
GMA2 FAIL – GMA2 is inoperative. The audio panel is unavailable. The system
should be serviced.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data
has occurred.
between the two GMAs. The system should be
serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The system
GMA2 CONFIG – GMA2 config
should be serviced.
error. Config service req’d.
MANIFEST – GMA1 software
Appendix
mismatch, communication halted.
Index
Comments
The PFDs and MFD have different airport terrain
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
System has updated the active navigation
database from the standby navigation database.
One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD
or MFD is missing or invalid.
MANIFEST – GMA2 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
102
The audio panel has incorrect software installed. The
system should be serviced.
The audio panel self-test has detected a problem
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
system should be serviced.
Procedures
Hazard
Avoidance
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
Flight
Planning
The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be
serviced.
GPS Nav
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
AFCS
The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.
Nav/Com/
XPDR/Audio
Additional
Features
A GIA mismatch has been detected, where only
one is SBAS capable.
Appendix
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Index
Incorrect servo software is installed, or gain
settings are incorrect.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Annun/Alerts
190-00929-03 Rev. A
Flight
Instruments
GIA 63W MESSAGE ADVISORIES
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1
temperature too low.
GIA2 COOLING – GIA2
temperature too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
103
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
MANIFEST– COM1 software
mismatch, communication halted.
MANIFEST– COM2 software
mismatch, communication halted.
MANIFEST– NAV1 software
mismatch, communication halted.
MANIFEST– NAV2 software
mismatch, communication halted.
COM1 CONFIG – COM1 config
error. Config service req’d.
COM2 CONFIG– COM2 config
error. Config service req’d.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk
key is stuck.
COM2 PTT – COM2 push-to-talk
key is stuck.
Comments
COM1 and/or COM2 software mismatch. The
G1000 system should be serviced.
NAV1 and/or NAV2 software mismatch. The
G1000 system should be serviced.
COM1 and/or COM2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
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.
COM1 RMT XFR – COM1 remote The COM1 and/or COM2 transfer switch is stuck
transfer key is stuck.
in the enabled (or “pressed”) position. Press
COM2 RMT XFR – COM2 remote the transfer switch again to cycle its operation.
If the problem persists, the system should be
transfer key is stuck.
serviced.
LOI – GPS integrity lost. Crosscheck GPS integrity is insufficient for the current phase
with other NAVS.
of flight.
104
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Annunciations & Alerts
Abort approach due to loss of GPS navigation.
Vertical guidance generated by SBAS 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’.
Flight
Planning
Procedures
A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be
available. The system should be serviced.
Hazard
Avoidance
A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be
available. The system should be serviced.
Appendix
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should
be serviced.
Annun/Alerts
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.
Additional
Features
G/S2 FAIL – G/S2 is inoperative.
Loss of GPS navigation due to GPS failure.
GPS Nav
G/S1 FAIL – G/S1 is inoperative.
Loss of GPS navigation due to position error.
AFCS
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
Comments
Loss of GPS navigation due to insufficient
satellites.
Nav/Com/
XPDR/Audio
Message
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS
navigation. Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
Flight
Instruments
GIA 63W MESSAGE ADVISORIES (CONT.)
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
105
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Comments
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
GEA 71 MESSAGE ADVISORIES
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
MANIFEST – GEA1 software
The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
MANIFEST – GEA2 software
The #2 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GTX 33 MESSAGE ADVISORIES
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
MANIFEST – GTX1 software
mismatch, communication halted.
MANIFEST – GTX2 software
mismatch, communication halted.
106
Comments
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Comments
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.
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Message
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is
inoperative.
XPDR2 FAIL – XPDR2 is
inoperative.
Flight
Instruments
GTX 33 MESSAGE ADVISORIES (CONT.)
GRS 77 MESSAGE ADVISORIES
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
107
Index
190-00929-03 Rev. A
Appendix
AHRS2 GPS – AHRS2 not receiving
any GPS information.
Annun/Alerts
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Additional
Features
AHRS2 GPS – AHRS2 using backup
GPS source.
Hazard
Avoidance
AHRS1 GPS – AHRS1 using backup
GPS source.
Procedures
AHRS2 TAS – AHRS2 not receiving
valid airspeed.
Comments
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.
The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.
The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.
The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.
Flight
Planning
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
GRS 77 MESSAGE ADVISORIES (CONT.)
Message
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
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 – AHRS1 Magneticfield model needs update.
AHRS2 SRVC – AHRS2 Magneticfield model needs update.
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass.
GEO LIMITS – AHRS2 too far
North/South, no magnetic compass.
MANIFEST – GRS1 software
mismatch, communication halted.
MANIFEST – GRS2 software
mismatch, communication halted.
Comments
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.
GMU 44 MESSAGE ADVISORIES
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
Comments
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
108
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
AFCS
The GMU 44 has incorrect software installed.
The system should be serviced.
GPS Nav
MANIFEST – GMU1 software
mismatch, communication halted.
MANIFEST – GMU2 software
mismatch, communication halted.
Comments
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.
Nav/Com/
XPDR/Audio
Message
HDG FAULT – AHRS2
magnetometer fault has occurred.
Flight
Instruments
GMU 44 MESSAGE ADVISORIES (CONT.)
GDL 59 MESSAGE ADVISORIES
Appendix
Comments
A failure has been detected in the #1 GSR 56.
The system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
190-00929-03 Rev. A
Annun/Alerts
GSR 56 MESSAGE ADVISORIES
Message
GSR1 FAIL – GSR1 has failed.
Additional
Features
MANIFEST – GDL software
mismatch, communication halted.
Hazard
Avoidance
GDL59 SERVICE – GDL 59 needs
service. Return unit for repair.
GDL59 RTR FAIL – The GDL 59
router has failed.
REGISTER GFDS – Data services
are inoperative, register w/GFDS.
Procedures
GDL59 FAIL – GDL 59 has failed.
Comments
GDL 59 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GDL 59. The
receiver is unavailable. The system should be
serviced.
A failure has been detected in the GDL 59. The
system should be serviced.
A failure has been detected in the GDL 59
router. The system should be serviced.
The GDL 59 is not registered with Garmin Flight
Data Services, or it’s current registration data
has failed authentication.
The GDL 59 has incorrect software installed.
The system should be serviced.
Flight
Planning
Message
GDL59 CONFIG – GDL 59 config
error. Config service req’d.
109
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
GDL 69A MESSAGE ADVISORIES
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
GDL69 FAIL – GDL 69 has failed.
MANIFEST – GDL software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GDL 69. The
receiver is unavailable. The system should be
serviced
The GDL 69 has incorrect software installed.
The system should be serviced.
GWX 68 ALERT MESSAGES
Message
GWX CONFIG – GWX config error.
Config service req’d.
GWX FAIL – GWX is inoperative.
GWX SERVICE – GWX needs
service. Return unit for repair.
MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The system
should be serviced.
The GDU is not recieving status packet from the
GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
The GWX 68 has incorrect software installed.
The system should be serviced.
Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.
GDC 74B MESSAGE ADVISORIES
Message
Comments
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
GDC1 or GDC2 is reporting that the altitude
ADC2 ALT EC – ADC2 altitude error error correction is unavailable.
correction is unavailable.
110
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
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Annunciations & Alerts
Comments
Nav/Com/
XPDR/Audio
GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.
The GDC1 and/or GDC2 self-test has detected
a problem in the unit. The system should be
serviced
GPS Nav
Hazard
Avoidance
Additional
Features
Annun/Alerts
MANIFEST – GCU software
mismatch, communication halted.
GCU KEYSTK – GCU [key name]
Key is stuck.
Procedures
GCU FAIL – GCU is inoperative.
Comments
GCU 477 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GCU 477.
The GCU 477 is unavailable.
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.
Flight
Planning
The GDC 74B has incorrect software installed.
The system should be serviced.
GCU 477 MESSAGE ADVISORIES
Message
GCU CNFG – GCU Config error.
Config service req’d.
AFCS
Message
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC2 AS EC – ADC2 airspeed error
correction is unavailable.
ADC1 SERVICE – ADC1 needs
service. Return unit for repair
ADC2 SERVICE – ADC1 needs
service. Return unit for repair
MANIFEST – GDC1 software
mismatch, communication halted.
MANIFEST – GDC2 software
mismatch, communication halted.
Flight
Instruments
GDC 74B MESSAGE ADVISORIES (CONT.)
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
111
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
GMC 710 MESSAGE ADVISORIES
Message
GMC CONFIG – GMC Config error.
Config service req’d.
GMC FAIL – GMC is inoperative.
MANIFEST – GMC software
mismatch. Communication halted.
GMC KEYSTK – GMC [key name]
Key is stuck.
Comments
Error in the configuration of the GMC 710.
A failure has been detected in 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.
MISCELLANEOUS MESSAGE ADVISORIES
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Comments
Upon power-up, the system detects that a
stored flight plan waypoint is locked. This
occurs when a navigation database update
eliminates an obsolete waypoint. The flight
plan cannot find the specified waypoint and
flags this message. This can also occur with
user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it
no longer exists in any database,
Or
update the waypoint name/identifier to reflect
the new information.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint
waypoint moved.
coordinate has changed due to a new
navigation 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.
112
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
113
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
GPS Nav
190-00929-03 Rev. A
AFCS
Comments
This occurs when a stored flight plan contains
procedures that have been manually edited.
This alert is issued only after an navigation
database update. Verify that the user-modified
procedures in stored flight plans are correct
and up to date.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify stored airways.
an airway that is no longer consistent with the
navigation database. This alert is issued only
after an navigation database update. Verify
use of airways in stored flight plans and reload
airways as needed.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate
locked flight plan.
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint -[xxxx]
waypoint name.
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to
turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
ARSPC AHEAD – Airspace ahead
Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
APR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach
when required.
Nav/Com/
XPDR/Audio
Message
DB CHANGE – Database changed.
Verify user modified procedures.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on CDI for
approach.
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
VNV – Unavailable. Unsupported
leg type in flight plan.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
TRAFFIC FAIL – Traffic device has
failed.
114
Comments
The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
The system notifies the pilot to set the CDI to
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been
passed.
The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.
The lateral flight plan contains a procedure
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.
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 system is no longer receiving data from
the traffic system. The traffic device should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
115
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
AFCS
190-00929-03 Rev. A
Nav/Com/
XPDR/Audio
Message
Comments
NON WGS84 WPT – Do not use GPS The position of the selected waypoint [xxxx]
for navigation to [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in
error as displayed. Do not use GPS to navigate
to the selected non-WGS84 waypoint.
STRMSCP FAIL – Stormscope has
Stormscope has failed. The G1000™ system
failed.
should be serviced.
FAILED PATH – A data path has
A data path connected to the GDU or the GIA
failed.
63/W has failed.
MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine
variance. Verify all course angles.
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
Synthetic Vision is disabled because the aircraft
available terrain region.
is not within the boundaries of the installed
terrain database.
SVS – SVS DISABLED: Terrain DB
Synthetic Vision is disabled because a terrain
resolution too low.
database of sufficient resolution (9 arc-second
or better) is not currently installed.
SCHEDULER [#] – <message>.
Message criteria entered by the user.
USER MAG VAR – User magnetic
User magnetic variation mode was selected
variation is active.
during previous operation and is still active
(checked at power-up.)
CHECK CRS – Database course for Selected course for LOC1 differs from published
LOC1 / [LOC ID] is [CRS]°.
localizer course by more than 10 degrees.
CHECK CRS – Database course for Selected course for LOC2 differs from published
LOC2 / [LOC ID] is [CRS]°.
localizer course by more than 10 degrees.
[PFD1, PFD2, or MFD1] CARD
The SD card was removed from the top card
1 REM – Card 1 was removed.
slot of the specified PFD or MFD. The SD card
Reinsert card.
needs to be reinserted.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
[PFD1, PFD2, or MFD1] CARD
2 REM – Card 2 was removed.
Reinsert card.
[PFD1, PFD2, or MFD1] CARD 1
ERR – Card 1 is invalid.
[PFD1, PFD2, or MFD1] CARD 2
ERR – Card 2 is invalid.
FPL TRUNC – Flight plan has been
truncated.
Comments
The SD card was removed from the bottom card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
The SD card in the top card slot of the specified
PFD or MFD contains invalid data.
The SD card in the bottom card slot of the
specified PFD or MFD contains invalid data.
This occurs when a newly installed navigation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
‘Flight plan successfully imported.’
Description
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints only. User The file stored on the SD card did not contain a flight plan,
waypoints imported successfully. No
only user waypoints. These waypoints have been saved to the
stored flight plan data was modified.’
system user waypoints. No flight plans stored in the system
have been modified.
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported from the SD
card.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported
from the SD card, however others had errors and were not
imported. A partial stored flight plan now exists in the
system.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
116
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Annunciations & Alerts
‘File contained user waypoints only.’
Description
‘Too many points. Flight plan truncated.’ The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.
Nav/Com/
XPDR/Audio
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
Flight
Instruments
Flight Plan Import/Export
Results
AFCS
‘One or more user waypoints renamed.’
One or more imported user waypoints were renamed when
imported due to naming conflicts with waypoints already
existing in the system.
‘Flight plan successfully exported.’
The stored flight plan was successfully exported to the SD
card.
‘Flight plan export failed.’
The stored flight plan was not successfully exported to the SD
card. The SD card may not have sufficient available memory
or the card may have been removed prematurely.
Hazard
Avoidance
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD
card have been imported. Any flight plan user waypoints
that were not imported are locked in the flight plan. The
flight plan must be edited within the system before it can be
activated for use.
Procedures
‘User waypoint database full. Not all
loaded.’
Flight
Planning
The flight plan on the SD card contains one or more
waypoints that the system cannot find in the navigation
database. The flight plan has been imported, but must be
edited within the system before it can be activated for use.
GPS Nav
‘Some waypoints not loaded. Waypoints
locked.’
Additional
Features
Annun/Alerts
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
117
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Blank Page
118
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
Nav/Com/
XPDR/Audio
ALERTS
AFCS
GPS Nav
Top Level PFD Softkeys
(optional)
(optional)
(optional)
PRECIP
or
DL LTNG
(optional)
or
METAR
STRMSCP
TRFC-1
ALERTS
Select the BACK Softkey
to return to the top-level softkeys.
Hazard
Avoidance
TRFC-2
Displays Inset Map in PFD lower left corner
INSET
Removes Inset Map
DCLTR
(3)
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
119
Index
OFF
Appendix
190-00929-03 Rev. A
Description
Annun/Alerts
Level 2
Additional
Features
Inset Map Softkeys
Level 1
Procedures
(optional)
WX LGND
(optional)
Flight
Planning
ALERTS
Level 1
Level 2
Description
WX LGND Displays icon and age on the Inset Map for the
selected weather products (optional)
TRAFFIC Displays traffic information on Inset Map
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
AFCS
TOPO
TERRAIN
GPS Nav
STRMSCP
NEXRAD
Flight
Planning
or
PRECIP
Procedures
XM LTNG
or
Hazard
Avoidance
DL LTNG
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)
Displays Worldwide Weather precipitation on
Inset Map (optional)
Displays XM lightning information on Inset Map
(optional)
Displays Worldwide Weather lightning
information on Inset Map (optional)
Displays METAR flags on airport symbols shown on
the Inset Map (optional)
Additional
Features
METAR
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on Inset
Map
Displays terrain information on Inset Map
Annun/Alerts
ALERTS
ADC1
ADC2
AHRS1
BACK
AHRS2
ALERTS
Appendix
Select the BACK Softkey to
return to the top level softkeys.
Sensor Softkeys
Index
Level 1
Level 2
SENSOR
ADC1
120
Description
Displays softkeys for selecting the #1 and #2 AHRS
and Air Data Computers
Selects the #1 Air Data Computer
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
Level 2
Description
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Nav/Com/
XPDR/Audio
ADC2
Flight
Instruments
Level 1
DME
ALERTS
AFCS
SYN VIS
ALERTS
ALT UNIT
HSI FMT
GPS Nav
Select the BACK Softkey
to return to the top-level softkeys
Flight
Planning
360 HSI
IN
ALERTS
HPA
ALERTS
PATHWAY
SYN TERR HRZN HDG APTSIGNS
ALERTS
Additional
Features
PFD Configuration Softkeys
Level 1
Level 2
Level 3
Annun/Alerts
SYN VIS
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
121
Index
SYN TERR
Displays rectangular boxes representing
the horizontal and vertical flight path of
the active flight plan
Enables synthetic terrain depiction
Appendix
PATHWAY
190-00929-03 Rev. A
Description
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
PFD
Hazard
Avoidance
ALERTS
Procedures
METERS
BACK
ARC HSI
Level 1
Level 2
Level 3
Description
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
DFLTS
GPS Nav
WIND
OPTN 1
OPTN 3
Wind direction arrow with digital
direction and speed
Longitudinal and lateral components
OFF
Information not displayed
Flight
Planning
OPTN 2
Procedures
Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings, including
changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrow and speed
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information, and ADF/
Hazard
Avoidance
DME
BRG1
Additional
Features
frequency.
HSI FRMT
Annun/Alerts
360 HSI
ARC HSI
Appendix
BRG2
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.
Index
ALT UNIT
122
Displays softkeys for setting the
altimeter and BARO settings to metric
units
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
Level 2
Level 3
Description
When enabled, displays altimeter in
meters
IN
Press to display the BARO setting as
inches of mercury
HPA
Press to display the BARO setting as
hectopacals
Nav/Com/
XPDR/Audio
METERS
Flight
Instruments
Level 1
ALERTS
ALERTS
Transponder Softkeys
Hazard
Avoidance
Select the BACK Softkey to return
to the previous level softkeys.
Procedures
Select the BACK Softkey to return
to the top-level softkeys.
Flight
Planning
ADS-B TX
GPS Nav
ALERTS
AFCS
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
STD BARO
Additional
Features
Level 1
Level 2
Level 3
Description
STBY
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
ON
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index
Selects the #2 transponder as active
Appendix
XPDR2
Annun/Alerts
XPDR1
Displays transponder mode selection
softkeys
Selects the #1 transponder as active
XPDR
123
Level 1
Level 2
Level 3
0—7
BKSP
Removes numbers entered, one at a time
AFCS
GND
GPS Nav
VFR
Flight
Planning
CODE
TMR/REF
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
NRST
Displays Nearest Airports Window
ALERTS
Displays Alerts Window
Procedures
IDENT
Hazard
Avoidance
ADS-B TX
Index
Appendix
Annun/Alerts
Additional
Features
Description
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.
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
ALT
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
124
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
(optional)
DCLTR
MAP
SHW CHRT
CHKLIST
DCLTR-3
PROFILE
TOPO
AIRWAYS
(optional)
STRMSCP
(optional)
(optional)
PRECIP
or
NEXRAD
DL LTNG
or
XM LTNG
(optional)
(optional)
METAR
LEGEND
AFCS
TRAFFIC
(optional)
TERRAIN
Select the BACK Softkey
on this level to return to the
top softkey level.
Nav/Com/
XPDR/Audio
DCLTR-1
DCLTR-2
Flight
Instruments
MFD NAVIGATION PAGE SOFTKEY MAP
BACK
AIRWY ON
GPS Nav
AIRWY LO
AIRWAY HI
Flight
Planning
MFD Softkeys
Level 2
Description
Procedures
Level 1
Enables second-level Navigation Map softkeys
MAP
TRAFFIC
Displays traffic information on Navigation Map
Additional
Features
Annun/Alerts
Appendix
AIRWAYS Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed
STRMSCP Displays Stormscope weather and coverage
information on Navigation Map (optional feature)
Hazard
Avoidance
Displays topographical data (e.g., coastlines, terrain,
rivers, lakes) and elevation scale on Navigation Map
TERRAIN Displays terrain information on Navigation Map
TOPO
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
125
Flight
Instruments
Appendix
Level 1
Level 2
NEXRAD
Nav/Com/
XPDR/Audio
or
Displays Worldwide Weather precipitation on the
Navigation Map (optional)
XM LTNG Displays XM lightning information on the
Navigation Map (optional)
or
AFCS
GPS Nav
METAR
Flight
Planning
LEGEND
DCLTR (3)
Hazard
Avoidance
Procedures
BACK
Additional
Features
Displays NEXRAD weather and coverage
information on the Navigation Map (optional)
PRECIP
DL LTNG
SHW
CHRT
CHKLIST
Displays Worldwide Weather lightning information
on the Navigation Map (optional)
Displays METAR flags on airport symbols shown on
the Navigation Map (optional)
Displays the legend for the selected weather
products. Available only when NEXRAD, XM
LTNG, and/or METAR softkeys are selected.
Returns to top-level softkeys
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
Index
Appendix
Annun/Alerts
Description
126
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
Hazard
Avoidance
Additional
Features
Annun/Alerts
Index
2) Update the Garmin databases on the MFD card.
Appendix
1) With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
3) Insert the MFD database card into the bottom card slot of the MFD.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Procedures
Loading Garmin Database Updates
190-00929-03 Rev. A
Flight
Planning
Error Message
Description
Canceled
Database synchronization has been canceled by removing the
bottom SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
GPS Nav
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database
features.
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected diaplays listed after it. When an error
message is displayed, the problem must be corrected before synchronization can be
completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
AFCS
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
Nav/Com/
XPDR/Audio
CAUTION: Never disconnect power to the system when loading a database.
Power interuption during the database loading process could result in maintenance being required to reboot the system.
Flight
Instruments
LOADING UPDATED DATABASES
127
Appendix
Nav/Com/
XPDR/Audio
Flight
Instruments
4) Apply power to the system, check that the databases are initialized
and displayed on the power-up screen. When updating the terrain and
FliteCharts databases, a ‘Verifying’ message may be seen. If this message is
present, wait for the system to finish loading before proceeding to step 5.
5) Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right most softkey.
6) Turn the large FMS Knob to select the AUX Page group on the MFD.
AFCS
7) Turn the small FMS Knob to select the System Status Page.
8) Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
GPS Nav
9) Remove and reapply power to the system.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct
database cycle information is shown for each database for each display.
Loading the Jeppesen Navigation Database as the Active Navigation
Database
Hazard
Avoidance
Procedures
Flight
Planning
11) Turn the small FMS Knob to select the System Status Page.
Additional
Features
Annun/Alerts
NOTE: Loading the Jeppesen navigation database as the active database
prior to its effective date will result in the expiration date on the power-up
screen and the effective date on the AUX-System Status Page being displayed
in yellow.
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Appendix
1) With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2) Turn the system ON. A prompt is displayed in the upper left corner of the
display:
Index
3) Press the NO Softkey to proceed to loading the active database.
4) A prompt similar to the following is displayed. Press the YES Softkey to update
the active navigation database.
5) After the update completes, the display starts in normal mode.
128
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Appendix
7) Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD).
9) Turn the large FMS Knob to select the AUX Page group on the MFD.
10) Turn the small FMS Knob to select the System Status Page.
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Flight
Planning
GPS Nav
Loading the Jeppesen Navigation Database as the Standby Navigation
Database
AFCS
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify
the correct active navigation database cycle information is shown for each
display.
Nav/Com/
XPDR/Audio
8) Apply power to the system and press the ENT Key to acknowledge the startup
screen.
Flight
Instruments
6) Turn the system OFF and remove the SD card from the top card slot.
Procedures
1) With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
Hazard
Avoidance
2) Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
3) Turn the system ON. A prompt is displayed.
Appendix
8) Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
Annun/Alerts
5) After the navigation database files are copied to the bottom SD card, press
any key to continue, as instructed.
7) Again, press any key to continue as instructed on the display.
Additional
Features
4) Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
9) Press the ENT Key to acknowledge the startup screen.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Index
11) Turn the small FMS Knob to select the System Status Page.
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
129
Appendix
Nav/Com/
XPDR/Audio
Flight
Instruments
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
AFCS
NOTE: During the synchronization process, version differences between
standby navigation databases will exist. This will result in the system
displaying a ‘DB Mismatch’ alert for the standby navigation databases. This
alert will remain until the next power cycle.
13) Turn system power OFF.
14) Remove the SD card from the top card slot of the MFD.
GPS Nav
15) Turn system power ON.
16) Press the ENT Key to acknowledge the startup screen.
Flight
Planning
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
18) Turn the small FMS Knob to select the System Status Page.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
19) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Verify the correct standby navigation database cycle information is shown
for each display.
130
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Index
D
Nav/Com/
XPDR/Audio
Data reports 81, 82
DB Mismatch 127, 130
DCLTR Softkey 62
Declutter 119, 126
Direct-to 13
DME 5, 6
AFCS
E
GPS Nav
Edit a flight plan 28
ESP 85, 86
F
Flight
Planning
FD 89
Flight Director 9
Flight path marker 61
FliteCharts® 62, 63
Frequency Transfer 6
Procedures
Hazard
Avoidance
G
Gain 58
Garmin Flight Data Services 81
Additional
Features
Access code 66
Activate a flight plan 14
Active Channel 83
Active database 128
Active Navigation Database 128
ADF 5, 6, 122
ADS-B 124
Advisory alerts 87
AHRS 107, 108, 109, 111, 112
Air Data Computer 88
Airport Signs 61, 62
Airways 125
Alert messages 110
ALT 52
Altitude mode 52
Altitude volume 52
Antenna stabilization 59
Antenna tilt 57
AOPA’s Airport Directory 64
AP 89
Attitude & Heading Reference System
88
Audio panel controls
NAV1, NAV2 6
Code selection softkeys 5
COM 5, 6
Flight
Instruments
A
H
Barometric Altitude Minimums 3
Barometric pressure 123
Bearing line 57, 58, 59
HF 5, 6
Horizon heading 61
Horizontal scan 58
C
I
CDI 1, 2, 6, 114
Cell 35, 36
Cell mode 36
Channel Presets 84
ChartView 62, 63
CLD TOP Softkey 47
Inhibit 56
Inhibit TAWS 56
Inset Map 119, 120
IOI 90, 91, 94
Iridium satellite network 65, 66, 70
Index-1
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Appendix
190-00929-03 Rev. A
Annun/Alerts
B
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
J
Jeppesen 63
L
R
Level Mode 85
Lightning 35, 36, 120
Low speed data 65, 66
RADIO softkey 83
Register 66
Report transmissions 81
ROC 90, 94
M
S
Map panning 37
Message advisories 97–116
MET 89
METAR 37
Minimums 96
MISCOMP 88
Mistrim 89
Mode S 124
Mode selection softkeys 5
Multi Function Display (MFD)
Softkeys 125
NAV 6
NAV1 2, 6
NAV2 6
Navigation database 15, 16, 117
NEXRAD 37, 120, 125, 126
NEXRAD Softkey 46
SafeTaxi® 62
SBAS 10, 32, 55, 103, 105
Sector scan 59
Sensor 88
STAB 59
Standby 57
Standby Navigation Database 101, 129
Store Flight Plan 27
Stormscope lightning data 35, 36, 120
Strike 35
Strike mode 36
SVS 61, 115
SVS Terrain 61
Switching Between GFDS and XM WX
42
Synchronization 127
SYNC Status 130
Synthetic Vision System 61
System ID 65
O
T
OBS 2
Obstacles 101, 102, 103
Overspeed Protection 10
TA 96
TAF 37, 48
TAS 52, 107
TAWS 53–56, 90– 93, 95
TAWS-B 53, 54
Telephone 66
Terrain 53, 54, 90, 91, 93, 94, 101,
N
P
Index
PIT 88
Predefined message 73, 74
Pathways 61, 62
PIREP 50
Index-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Index
Flight
Instruments
120, 125
Text messaging 71, 72, 73, 75
Tilt line 57
Timer 112
Topographical data 120, 125
Traffic 35, 51, 120, 125
Traffic Advisory (TA) 51, 96
Traffic map page 51, 52
Transponder 5, 123, 124
Nav/Com/
XPDR/Audio
AFCS
V
GPS Nav
Vertical speed guidance 16
Vertical track 96
VNV 13, 114
Vspeed 2
Flight
Planning
W
Procedures
WATCH® 59
Waypoint Selection Submenu 24
Weather Attenuated Color Highlight 59
Weather data link page 37
Weather radar 56
Wi-Fi 78, 79, 80, 81, 82
Wind data 122
Winds Aloft 49
WIND Softkey 49
Hazard
Avoidance
Additional
Features
X
Annun/Alerts
XM lightning 120, 126
XM WX weather 37
XPDR Softkey 5
Appendix
Index
190-00929-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
Index-3
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-03 Rev. A
Garmin International, Inc.
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© 2011 Garmin Ltd. or its subsidiaries
190-00929-03 Rev. A