Garmin Beechcraft A36, Beechcraft G36 User Manual
®
Integrated Flight Deck
G1000
Pilot’s Guide
Beechcraft A36/G36
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
Copyright © 2007-2008 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0464.17 or later for the
0858.03 or later for the
this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax: 503/364.2138
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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
Website Address: www.garmin.com
Beechcraft A36/G36 (WAAS). Some differences in operation may be observed when comparing the information in
Beechcraft A36/G36, or System Software version
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
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and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
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trademarks may not be used without the express permission of Garmin.
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Flugfunkwerk GmbH; NavData® is a registered trademark of Jeppesen, Inc.; and XM® is a registered trademark of XM Satellite Radio, Inc.
April 2008 Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
LIMITED WARRANTY
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made
at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED
OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR
PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole
discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit
the Garmin Website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
i
WARNINGS, CAUTIONS, AND NOTES
WARNING:
Navigation and terrain separation must NOT be predicated upon the use of the terrain function.
The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use
in applications requiring a certified terrain awareness system. Terrain data is obtained from third party
sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING:
The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING:
The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING:
Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING:
Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING:
Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually
acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual
acquisition of conflicting traffic.
WARNING:
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:
GDL 69 Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 is approved only for weather avoidance, not penetration.
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.
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. Bii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
The Garmin G1000, as installed in the Hawker Beechcraft A36/G36 aircraft, has a very high
degree of functional integrity. However, the pilot must recognize that providing monitoring and/or selftest 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:
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
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 Beechcraft
A36/G36 Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight
operations, carefully compare indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any
discrepancies before continuing navigation.
WARNING
:
The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo.”
WARNING:
Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING:
Because of anomalies in the earth’s magnetic field, operating the G1000 within the following
areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south
of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An
area south of 55° South latitude between longitude 120º East and 165º East.
CAUTION:
The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
iii
WARNINGS, CAUTIONS, AND 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:
When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
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
:
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
:
This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. Biv
Record of Revisions
REVISION INFORMATION
Part Number
190-00595-00 A 10/16/06 All Initial Release
190-00595-01 A
Revision Date Page Range Description
12/21/07
B
4/08/08
All
All
Updated to GDU SW version 8.10, and added WAAS
Change System Software version, update description of two
warning messages, and other minor corrections
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
v
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 6
PFD/MFD Controls ........................................................ 6
Additional AFCS Controls .............................................. 9
Audio Panel Controls .................................................. 10
1.4 Secure Digital Cards .............................................12
1.5 System Power-up ................................................... 12
1.6 System Operation .................................................. 14
Normal Operation ....................................................... 14
Reversionary Mode ..................................................... 14
AHRS Operation .........................................................15
G1000 System Annunciations ...................................... 17
Softkey Function ......................................................... 18
GPS Receiver Operation ..............................................23
1.7 Accessing G1000 Functionality ........................... 28
Menus ....................................................................... 28
MFD Page Groups ....................................................... 28
MFD System Pages .....................................................32
1.8 Display Backlighting ............................................. 46
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 50
Airspeed Indicator ......................................................50
Attitude Indicator ....................................................... 53
Altimeter ................................................................... 54
Vertical Speed Indicator (VSI) ....................................... 55
Vertical Deviation ....................................................... 56
Horizontal Situation Indicator (HSI) ..............................57
Course Deviation Indicator (CDI) .................................. 62
2.2 Supplemental Flight Data ....................................69
Temperature Displays ..................................................69
Wind Data .................................................................70
Vertical Navigation (VNV) Indications ...........................71
2.3 PFD Annunciations and Alerting Functions ........ 72
G1000 Alerting System ................................................ 72
Marker Beacon Annunciations ..................................... 73
Traffic Annunciation ....................................................74
TAWS Annunciations (Optional) ................................... 74
Altitude Alerting .........................................................75
Low Altitude Annunciation (WAAS only) .......................75
Minimum Descent Altitude/Decision Height Alerting ...... 76
2.4 Abnormal Operations ...........................................77
Abnormal GPS Conditions ...........................................77
Unusual Attitudes .......................................................78
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Display ....................................................... 81
3.2 Lean Display ........................................................... 83
3.3 System Display ......................................................86
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 89
MFD/PFD Controls and Frequency Display ..................... 90
Audio Panel Controls .................................................. 92
4.2 COM Operation ...................................................... 94
COM Transceiver Selection and Activation ..................... 94
COM Transceiver Manual Tuning .................................. 95
Quick-Tuning and Activating 121.500 MHz .................... 96
Auto-Tuning the COM Frequency .................................. 97
Frequency Spacing .................................................... 101
Automatic Squelch .................................................... 102
Volume .................................................................... 102
4.3 NAV Operation ..................................................... 103
NAV Radio Selection and Activation ........................... 103
NAV Receiver Manual Tuning ..................................... 104
Auto-Tuning a NAV Frequency from the MFD .............. 106
Marker Beacon Receiver ............................................ 111
DME Tuning (Optional) .............................................. 112
4.4 GTX 33 Mode S Transponder .............................. 113
Transponder Controls ................................................ 113
Transponder Mode Selection ...................................... 114
Entering a Transponder Code ..................................... 117
IDENT Function ........................................................118
Flight ID Reporting ................................................... 119
4.5 Additional Audio Panel Functions .....................120
Power-Up ................................................................. 120
Mono/Stereo Headsets .............................................. 120
Speaker ................................................................... 120
Intercom .................................................................. 121
Passenger Address (PA) System .................................. 123
Clearance Recorder and Player ................................... 123
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. Bvi
TABLE OF CONTENTS
Split COM ................................................................ 124
Entertainment Inputs ................................................ 125
4.6 Audio Panel Preflight Procedure ....................... 126
4.7 Abnormal Operation ........................................... 127
Stuck Microphone ..................................................... 127
COM Tuning Failure ................................................... 127
Audio Panel Fail-Safe Operation ................................. 127
Reversionary Mode ................................................... 127
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 129
Navigation Status Box ............................................... 131
5.2 Using Map Displays ............................................. 132
Map Orientation ....................................................... 132
Map Range .............................................................. 134
Map Panning ............................................................ 136
Measuring Bearing and Distance ................................ 141
Topography .............................................................. 142
Map Symbols ........................................................... 145
Airways ................................................................... 151
Track Vector .............................................................153
Wind Vector ............................................................. 154
Nav Range Ring ....................................................... 155
Fuel Range Ring ....................................................... 156
5.3 Waypoints .............................................................157
Airports ................................................................... 158
Intersections ............................................................164
NDBs ....................................................................... 166
VORs ....................................................................... 168
User Waypoints ........................................................ 170
5.4 Airspaces .............................................................. 175
5.5 Direct-to-Navigation .......................................... 179
5.6 Flight Planning ..................................................... 185
Flight Plan Creation .................................................. 186
Adding Waypoints to an Existing Flight Plan ................ 189
Adding Airways to a Flight Plan .................................191
Adding Procedures to a Stored Flight Plan ..................194
Flight Plan Storage ...................................................201
Flight Plan Editing ....................................................203
Along Track Offsets ................................................... 206
Parallel Track ............................................................ 208
Activating a Flight Plan Leg ....................................... 211
Inverting a Flight Plan ............................................... 212
Flight Plan Views ...................................................... 213
Closest Point of FPL .................................................. 215
5.7 Vertical Navigation ............................................. 216
Altitude Constraints .................................................. 218
5.8 Procedures ...........................................................222
Departures ............................................................... 222
Arrivals ................................................................... 225
Approaches ............................................................. 227
5.9 Trip Planning ........................................................ 233
Trip Planning ............................................................ 233
5.10 RAIM Prediction .................................................. 237
5.11 Navigating a Flight Plan ..................................... 241
5.12 Abnormal Operation ........................................... 268
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 271
Activating Services .................................................... 272
Using XM Satellite Weather Products .......................... 273
6.2 WX-500 Stormscope ...........................................295
Setting Up Stormscope on the Navigation Map ...........295
Selecting the Stormscope Page .................................. 299
6.3 Terrain Awareness and Warning System .......... 300
Displaying TAWS Data ............................................... 301
TAWS Page .............................................................. 303
TAWS Alerts .............................................................305
System Status ........................................................... 311
6.4 Traffic Information Service (TIS) ........................ 312
Displaying TRAFFIC Data ........................................... 313
Traffic Map Page ....................................................... 315
TIS Alerts ................................................................. 316
System Status ........................................................... 317
6.5 L-3 Skywatch Traffic Advisory System (TAS) ..... 320
TAS Symbology ......................................................... 320
Operation ................................................................ 321
Altitude Display ........................................................ 323
Traffic Map Page Display Range ................................. 324
TAS Alerts ................................................................325
System Status ........................................................... 326
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
vii
TABLE OF CONTENTS
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 329
Additional AFCS Controls .......................................... 331
7.2 Flight Director Operation ................................... 332
Activating the Flight Director ..................................... 332
AFCS Status Box ....................................................... 333
Flight Director Modes ................................................ 334
Command Bars ......................................................... 334
7.3 Vertical Modes ..................................................... 335
Pitch Hold Mode (PIT) ............................................... 336
Selected Altitude Capture Mode (ALTS) ....................... 337
Altitude Hold Mode (ALT) .......................................... 338
Vertical Speed Mode (VS) .......................................... 339
Flight Level Change Mode (FLC) ................................. 340
Vertical Navigation Modes (VPTH, ALTV) ..................... 342
Glidepath Mode (GP) (WAAS only) ............................. 347
Glideslope Mode (GS) ............................................... 349
Go Around Mode (GA) .............................................. 350
7.4 Lateral Modes ...................................................... 351
Roll Hold Mode (ROL) ...............................................352
Navigation Modes (GPS, VOR, LOC, BC) ...................... 354
Approach Modes (GPS, VAPP, LOC) ............................. 356
7.5 Autopilot and Yaw Damper Operation .............358
Flight Control ........................................................... 358
Engagement ............................................................. 359
Control Wheel Steering ............................................. 359
Disengagement ........................................................ 360
7.6 Example Flight Plan ............................................361
Departure ................................................................362
Intercepting a VOR Radial .......................................... 364
Flying a Flight Plan/GPS Course ................................. 365
Descent ................................................................... 366
Approach ................................................................. 370
Go Around/Missed Approach ..................................... 372
7.7 AFCS Annunciations and Alerts ......................... 374
AFCS Status Alerts .................................................... 374
Overspeed Protection ................................................ 375
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ................................................................ 377
SafeTaxi Cycle Number and Revision ..........................380
8.2 ChartView ............................................................. 383
ChartView Softkeys ................................................... 383
Terminal Procedures Charts .......................................384
Chart Options ........................................................... 394
Day/Night View ........................................................400
ChartView Cycle Number and Expiration Date ............. 402
8.3 FliteCharts ............................................................ 406
FliteCharts Softkeys .................................................. 406
Terminal Procedures Charts .......................................407
Chart Options ........................................................... 415
Day/Night View ........................................................419
FliteCharts Cycle Number and Expiration Date ............. 421
8.4 XM Radio Entertainment (Optional) ................. 425
Activating XM Satellite Radio Services ........................ 425
Using XM Radio .......................................................427
8.5 Scheduler .............................................................. 431
8.6 Abnormal Operation ........................................... 433
APPENDICES
Annunciations and Alerts ............................................. 435
Alert Level Definitions ............................................... 437
Aircraft Alerts ........................................................... 437
G1000 System Annunciations .................................... 439
G1000 System Message Advisories ............................. 442
AFCS Alerts .............................................................. 453
TAWS ALERTS ........................................................... 454
SD Card Use ................................................................... 457
Jeppesen Databases .................................................. 457
Garmin Databases .................................................... 458
Glossary .......................................................................... 461
Frequently Asked Questions ........................................ 469
Map Symbols ................................................................. 475
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. Bviii
SECTION 1 SYSTEM OVERVIEW
SYSTEM OVERVIEW
OVERVIEW
SYSTEM
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Beechcraft A36/G36
Bonanza. The G1000 system is an integrated flight control system that presents flight instrumentation, position,
navigation, communication, and identification information to the pilot through large-format displays. The system
consists of the following Line Replaceable Units (LRUs):
•
•
GDU 1040
•
GDU 1043/1045
•
GIA 63/63W
•
GDC 74A
•
GEA 71
•
GRS 77
Primary Flight Display (PFD)
Integrated Avionics Unit
Air Data Computer (ADC)
Engine/Airframe Unit
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
Multi Function Display (MFD)
GMA 1347
Beacon Receiver
•
GTX 33
•
GDL 69A
•
GTP 59
•
GSA 81
•
GSM 85
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A).
Audio System with Integrated Marker
Mode S Transponder
Satellite Data Link Receiver
Outside Air Temperature (OAT) Probe
AFCS Servos
Servo Gearboxes
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
NOTE:
Refer to the AFCS section for details on the GFC 700 AFCS.
In the Beechcraft A36/G36 Bonanza, the GFC 700 Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
1
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
SYSTEM
OVERVIEW
• GDU 1040 (1) – The GDU 1040 is configured as a Primary Flight Displays (PFD) that features a 10.4-inch LCD
with 1024 x 768 resolution. The display communicates with the MFD and with the #1 GIA 63/63W Integrated
Avionics Unit through a High-Speed Data Bus (HSDB) Ethernet connection.
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
•
GDU 1043/1045
with 1024 x 768 resolution. The display communicates with the PFD and with the #2 GIA 63/63W Integrated
Avionics Unit through a High-Speed Data Bus (HSDB) Ethernet connection. The GDU 1045 has a VNV Button,
which is needed to enable optional coupled Baro-VNAV AFCS mode.
(1) – The GDU 1043 or GDU 1045 is configured as an MFD that features a 10.4-inch LCD
HAZARD
AVOIDANCE
AFCS
•
FEATURES
ADDITIONAL
APPENDICESINDEX
GIA 63 or GIA 63W
(2) – Functions as the main communication hub, linking all LRUs with the PFD and
MFD. Each GIA 63 contains a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system
integration microprocessors. Each GIA 63W contains a GPS WAAS receiver. Each GIA 63/63W is paired with
a display via HSDB connection. The GIA 63/63Ws are not paired together and do not communicate with each
other directly.
2
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
SYSTEM OVERVIEW
•
GDC 74A
pressure altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with
the GIA 63(W)s, the displays, and the GRS 77, using an ARINC 429 digital interface (it also interfaces directly
with the GTP 59). The GDC 74A is designed to operate in Reduced Vertical Separation Minimum (RVSM)
airspace.
•
GEA 71
with both GIA 63(W)s using an RS-485 digital interface.
(1) – Processes data from the pitot/static system as well as the OAT probe. This unit provides
(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
•
GRS 77
(1) – Provides aircraft attitude and heading information via ARINC 429 to both displays and both
GIA 63Ws. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces
with the GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and with both
GIA 63/63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document.
•
GMU 44
(1) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft
magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77
using an RS-485 digital interface.
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
3
SYSTEM OVERVIEW
•
GMA 1347
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
unit also enables the manual control of the display reversionary mode (red
communicates with the #1 GIA 63(W), using an RS-232 digital interface.
•
GTX 33
(1) – Solid-state transponder that provides Modes A, C and S capability. The transponder can be
controlled from the PFD. The transponder communicates with the GIA 63/63Ws through an RS-232 digital
interface.
(1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls. This
DISPLAY BACKUP
button) and
FLIGHT
HAZARD
AFCS
•
MANAGEMENT
AVOIDANCE
•
FEATURES
ADDITIONAL
•
The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the
APPENDICESINDEX
GDL 69A
(1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and,
indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates
with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the
GDL 69A capability.
GTP 59
GSA 81
(2) – Provides Outside Air Temperature (OAT) data to the GDC 74A.
(4), and
GSM 85
(4) – The GSA 81 servos are used for the automatic control of roll, pitch, yaw, and
pitch trim. These units interface with each GIA 63/63W.
mechanical flight-control surface linkage.
4
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
SYSTEM OVERVIEW
GTX 33
Transponder
Reversionary
Control
GEA 71
Engine/Airframe
Unit
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Ve
rtical Speed
GMU 44
Magnetometer
Heading
Reversionary
Control
GMA 1347
Audio Panel
No. 2 GIA 63/63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
GPS Output
No. 1 GIA 63/63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
GPS Output
GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid
GDU 1040
Primary Flight Display
GDU 1043/1045
Multi Function Display
L-3 Skywatch
SKY497
Traffic
Advisory System
(optional)
Honeywell
KN 63
DME
(optional)
L-3 WX-500
Stormscope
Lightning Sensor
(optional)
GSA 81 (4)
Servos
GDL 69A
Data Link Weather
and Digital Audio
Entertainment
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
190-00595-01 Rev. B
Figure 1-1 G1000 System Block Diagram
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
5
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SYSTEM OVERVIEW
1.3 G1000 CONTROLS
SYSTEM
OVERVIEW
FLIGHT
PFD and MFD are discussed within the following pages of this section.
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
NOTE:
The Audio Panel (GMA 1347) and AFCS controls are also described in the CNS & Audio Panel and
AFCS sections respectively.
The G1000 system controls are located on the PFD and MFD bezels, and the audio panel. The controls for the
PFD/MFD CONTROLS
1
2
3
4
5
6
7
9
8
HAZARD
AVOIDANCE
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
17
18
19
20
21
22
23
MFD Only
24
25
26
27
28
29
Figure 1-2 PFD/MFD Controls
10
11
12
16
13
14
15
6
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
1
NAV VOL/ID Knob
2
NAV Frequency Transfer Key
3
NAV Knob
4
Heading Knob
5
Joystick
6
CRS/BARO Knob
7
COM Knob
8
COM Frequency Transfer Key (EMERG)
9
COM VOL/SQ Knob
SYSTEM OVERVIEW
Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage)
Press to toggle Morse code identifier audio ON/OFF
Transfers the standby and active NAV frequencies
Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)
Press to toggle light blue tuning box between NAV1 and NAV2
Turn to manually select a heading. When operating in Heading Select mode, this knob provides the heading reference to the flight director.
Press to display a digital heading momentarily to the left of the HSI and synchronize the
Selected Heading to the current heading
Turn to change map range
Press to activate Map Pointer for map panning
Turn large knob for altimeter barometric pressure setting
Turn the small knob to set the pilot-selected course on the HSI when the VOR1, VOR2, or
OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected
VOR. The pilot-selected course provides course reference to the pilot-side flight director
when operating in Navigation and Approach modes.
Press to re-center the CDI and return course pointer directly TO bearing of active waypoint/
station
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz)
Press to toggle light blue tuning box between COM1 and COM2
The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
Transfers the standby and active COM frequencies
Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically into
the active frequency field
Turn to control COM audio volume level (shown as a percentage in the COM Frequency
Box)
Press to turn the COM automatic squelch ON/OFF
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
AFCS
10
Direct-to Key ( )
11
FPL Key
12
CLR Key
(DFLT MAP)
13
MENU Key
14
PROC Key
15
ENT Key
190-00595-01 Rev. B
Activates the direct-to function and allows the user to enter a destination waypoint and es
tablish a direct course to the selected destination (specified by identifier, chosen from the
active route)
Displays flight plan information
Erases information, cancels entries, or removes menus
Press and hold to display the MFD Navigation Map Page (MFD only).
Displays a context-sensitive list of options for accessing additional features or making setting
changes
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and approach
procedures (IAPs) for a flight plan or selected airport
Validates/confirms menu selection or data entry
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
-
ADDITIONAL
FEATURES
APPENDICES INDEX
7
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
16
FMS Knob
(Flight Management
System Knob)
Press to turn the selection cursor ON/OFF.
Data Entry: With cursor ON, turn to enter data in the highlighted field (large knob moves
cursor location; small knob selects character for highlighted cursor location)
Scrolling: When a list of information is too long for the window/box, a scroll bar appears,
indicating more items to view. With cursor ON, turn large knob to scroll through the list.
Page Selection: Turn knob on MFD to select the page to view (large knob selects a page
group; small knob selects a specific page from the group)
17
ALT Knob
Sets the selected altitude in the Selected Altitude Box (the large knob selects the thousands,
the small knob selects the hundreds). In addition to providing the standard G1000 altitude
alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold
mode of the AFCS.
18
AP Key
Engages/disengages the Autopilot and Flight Director in the default vertical and lateral
modes.
19
FD Key Activates/deactivates the Flight Director only. Pressing the FD key turns on the Flight Direc-
tor in the default vertical and lateral modes. Pressing the FD key again deactivates the Flight
Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot
is engaged, the FD key is disabled.
20
21
22
23
NAV Key
ALT Key
VS Key
FLC Key
Selects/deselects the Navigation mode.
Selects/deselects the Altitude Hold mode.
Selects/deselects the Vertical Speed mode.
Selects/deselects the Flight Level Change mode.
HAZARD
AVOIDANCE
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
24
YD Key
25
HDG Key
26
APR Key
27
VNV Key
(if equipped)
28
NOSE UP Key
29
NOSE DN Key
Engages/disengages the Yaw Damper.
Selects/deselects the Heading Select mode.
Selects/deselects the Approach mode.
Selects/deselects Vertical Navigation mode.
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
8
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
SYSTEM OVERVIEW
The NAV, CRS/BARO, COM, FMS, and ALT knobs are concentric dual knobs, each having small (inner)
and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used.
OVERVIEW
SYSTEM
Large (Outer)
Knob
Small (Inner)
Knob
Figure 1-3 Dual Concentric Knob
The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions
depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide
documentation.
ADDITIONAL AFCS CONTROLS
The
AP DISC
Switch, and
separately from the AFCS Control Unit. These are discussed in detail in the AFCS section.
(Autopilot Disconnect) Switch,
CWS
(Control Wheel Steering) Button,
MEPT (Manual Electric Pitch Trim) Switch are additional AFCS
GO AROUND
controls and are located in the cockpit,
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
9
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SYSTEM OVERVIEW
AUDIO PANEL CONTROLS
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
11
13
15
17
18
20
22
1
3
5
7
9
2
4
6
8
10
12
14
16
19
21
23
HAZARD
AVOIDANCE
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
24
Figure 1-4 Audio Panel Controls (GMA 1347)
NOTE:
1
COM1 MIC
When a key is selected, a triangular annunciator above the key is illuminated.
– Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when
this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be
added by pressing the COM2 Key.
2
COM1
3
COM2 MIC
– When selected, audio from the #1 COM receiver can be heard.
– Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when
this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be
added by pressing the COM1 Key.
4
COM2
5
COM3 MIC
– When selected, audio from the #2 COM receiver can be heard.
– Not used in Beechcraft A36/G36 aircraft.
10
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
6
COM3
7
COM 1/2
SYSTEM OVERVIEW
– Not used in Beechcraft A36/G36 aircraft.
–
Split COM Key. Allows simultaneous transmission on COM1 and COM2 by the pilot and copilot.
OVERVIEW
SYSTEM
8
TEL
– Not used in Beechcraft A36/G36 aircraft.
9
PA
10
SPKR
– Not used in Beechcraft A36/G36 aircraft
– Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the
.
speaker.
11
MKR/MUTE
– Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver
audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded
COM audio.
12
HI SENS
13
DME
14
NAV1
15
ADF
16
NAV2
17
AUX
18
MAN SQ
– Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity.
– Pressing turns optional DME audio on or off.
– When selected, audio from the #1 NAV receiver can be heard.
– Not used in Beechcraft A36/G36 aircraft.
– When selected, audio from the #2 NAV receiver can be heard.
– Not used in Beechcraft A36/G36 aircraft.
– Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob
to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch.
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
19
PLAY
– Press once to play the last recorded COM audio. Press again while audio is playing and the
previous block of recorded audio is played. Each subsequent press plays each previously recorded block.
Pressing the
20
PILOT
21
COPLT
22
PILOT Knob
MKR/MUTE
Key during play of a memory block stops play.
– Selects and deselects the pilot intercom isolation.
– Selects and deselects the copilot intercom isolation.
– Press to switch between volume and squelch control as indicated by illumination of VOL
or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch
adjustment.
23
PASS Knob
– Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be
selected to allow squelch adjustment.
24
DISPLAY BACKUP Button
– Manually selects Reversionary Mode.
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
11
SYSTEM OVERVIEW
1.4 SECURE DIGITAL CARDS
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
right portion of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for
EIS
AUDIO PANEL
FLIGHT
aviation database and system software updates as well as terrain database storage.
& CNS
MANAGEMENT
NOTE:
NOTE:
Refer to the Appendices for instructions on updating the aviation database.
Ensure that the G1000 system is powered off before inserting the SD card.
The GDU 1040 and GDU 1043/1045 data card slots use Secure Digital (SD) cards and are located on the top
Install an SD card
Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card
should remain flush with the face of the display bezel.
Remove an SD card
Gently press on the SD card to release the spring latch and eject the card.
HAZARD
AVOIDANCE
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
1.5 SYSTEM POWER-UP
NOTE:
NOTE:
SD Card Slots
Figure 1-6 Display Bezel SD Card Slots
Refer to the Appendices for AHRS initialization bank angle limitations.
See the Appendices for additional information regarding system-specific annunciations and alerts.
12
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
SYSTEM OVERVIEW
OVERVIEW
SYSTEM
NOTE:
See the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (AFM/POH) for specific
procedures concerning avionics power application and emergency power supply operation.
The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical
busses. The G1000 PFDs, MFD and supporting sub-systems include both power-on and continuous built-in test
features that exercise the processor, RAM, ROM, external inputs and outputs to provide safe operation.
During system initialization, test annunciations are displayed, as shown in Figure 1-7. All system annunciations
should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become
momentarily illuminated on the audio panels, the control units and the display bezels.
On the PFD, the AHRS begins to initialize and displays ‘AHRS ALIGN: Keep Wings Level’. The AHRS should
display valid attitude and heading fields typically within one minute of power-up. The AHRS can align itself both
while taxiing and during level flight.
When the MFD powers up (Figure 1-8), the MFD Power-up Page displays the following information:
• System version
• Copyright
• Land database name and version
• Terrain database name and version
• Obstacle database name and version
• Aviation database name, version, and effective dates
• ChartView or FliteCharts database information
• Safe Taxi database information
INSTRUMENTS
FLIGHT
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
• Airport Terrain database name and version
Current database information includes the valid operating dates, cycle number and database type. When this
information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to
continue. Pressing the
ENT
Key acknowledges this information and displays the Navigation Map Page.
Figure 1-8 MFD Power-up PageFigure 1-7 PFD Initialization
AVOIDANCE
HAZARD
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
13
SYSTEM OVERVIEW
Audio Panel
Primary Flight Display
Multi Function Display
1.6 SYSTEM OPERATION
SYSTEM
OVERVIEW
The displays are connected together via multiple data busses, thus allowing for high-speed communication.
As shown in Figure 1-1, each GIA 63/63W is connected to one display. This section discusses the normal and
reversionary modes of operation as well as the various AHRS modes of the G1000 system.
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
NORMAL OPERATION
PFD
In normal mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude
and vertical speed), thereby replacing the traditional flight instrument cluster. The PFD also offers control for
COM and NAV frequency selection.
MFD
In normal mode, the right portion of the MFD displays a full-color moving map with navigation information,
while the left portion of the MFD is dedicated to the Engine Indication System (EIS).
Figure 1-9 gives an example of the G1000 displays in normal mode.
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
14
Figure 1-9 Normal Operation
REVERSIONARY MODE
NOTE:
In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In
reversionary mode, all important flight information is presented on the remaining display in the same format
as in normal operating mode.
If a display fails, the appropriate IAU Ethernet interface to the display is cut off. Thus, the IAU can no longer
communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to
the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup
paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is
completely automated for all LRUs and no pilot action is required.
The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A
for further information regarding system-specific alerts.
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
Figure 1-10 Reversionary Mode Operation
Audio Panel
Primary Flight Display Failed
Multi Function Display
SYSTEM OVERVIEW
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
EIS
If the system fails to detect a display problem, reversionary mode may be manually activated by pressing the
Audio Panel’s red
DISPLAY BACKUP
button (refer to the Audio Panel section for further details). Pressing this
button again deactivates reversionary mode.
Pressing the DISPLAY BACKUP
button activates/deactivates
reversionary mode for both the
PFD and the MFD.
Figure 1-11 DISPLAY BACKUP Button
Should the connection between a PFD and the on-side GIA 63/63W become inoperative, the on-side GIA
63/63W can no longer communicate with the remaining PFD (refer to Figure 1-1). As a result, the NAV and
COM functions provided to the failed PFD by the on-side GIA 63/63W are flagged as invalid (red “X”) on the
remaining PFD (see Figure 1-12).
Figure 1-12 Inoperative Input (NAV1 Shown)
AHRS OPERATION
NOTE:
Refer to the Appendices for specific AHRS alert information.
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
AFCS
ADDITIONAL
FEATURES
NOTE:
Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.
In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic field data and air
data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic
field measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air
data information for attitude determination. Four AHRS modes of operation are available (see Figure 1-13)
and depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor
inputs is communicated to the pilot by message advisory alerts.
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
APPENDICES INDEX
15
SYSTEM OVERVIEW
Attitude/Heading Invalid
AHRS
no-GP
S
Mode
AHRS Normal
Operation
AHRS no-
Mag Mode
AHRS no-Mag/
no-Air Mode
Heading Invalid
available
available
unavailable
una
vailab
le
available
unavailable
unavailable
available
Air Data
Magnetometer Data
unavailable
available
GPS Data
Magnetometer Data
Air Data
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
GPS INPUT FAILURE
NOTE:
AFCS
FEATURES
ADDITIONAL
APPENDICESINDEX
information provided from one of the GPS receivers is unreliable, the AHRS seamlessly transitions to using the
other GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both GPS inputs
fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer
inputs are available and valid.
AIR DATA INPUT FAILURE
failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid
attitude and heading information on the PFD (as indicated by red “X” flags).
In-flight initialization of AHRS, when operating without any valid source of GPS data and at true
air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it
is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an
extended period of time where valid AHRS outputs are unavailable.
The G1000 system provides two sources of GPS information. If a single GPS receiver fails, or if the
A failure of the air data input has no effect on AHRS output while AHRS is operating in normal mode. A
Figure 1-13 AHRS Operation
16
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
SYSTEM OVERVIEW
MAGNETOMETER FAILURE
If the magnetometer input fails, the AHRS transitions to one of the reversionary No-Magnetometer modes
and continues to output valid attitude information. However, if the aircraft is airborne, the heading output
on the PFD does become invalid (as indicated by a red “X”).
G1000 SYSTEM ANNUNCIATIONS
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
NOTE:
For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the (AFM/
POH) for additional information regarding pilot responses to these annunciations.
When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with
the failed data (Figure 1-14 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain
windows remain invalid as equipment begins to initialize. All windows should be operational within one
minute of power-up. If any window remains flagged, the G1000 system should be serviced by a Garminauthorized repair facility.
GIA 63/63W
Integrated
Avionics Units
GEA 71 Engine
Airframe Unit
Or
GIA 63/63W
Integrated Avionics
Unit
GIA 63/63W
Integrated Avionics
Units
GDC 74A Air
Data Computer
GRS 77 AHRS
Or
GMU 44
Magnetometer
EIS
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
AFCS
190-00595-01 Rev. B
GDC 74A Air
Data Computer
Figure 14 G1000 System Failure Annunciations
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
GIA 63/63W
Integrated Avionics
Units
GTX 33 Transponder
Or
GIA 63/63W
Integrated Avionics
Units
17
ADDITIONAL
FEATURES
APPENDICES INDEX
SYSTEM OVERVIEW
SOFTKEY FUNCTION
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
& CNS
AUDIO PANEL
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level
or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When
a softkey is selected, its color changes to black text on gray background and remains this way until it is turned
off, at which time it reverts to white text on black background.
Softkey On
Softkey Names (displayed)
Bezel-Mounted Softkeys (press)
Figure 1-15 Softkeys (Second-Level PFD Configuration)
PFD SOFTKEYS
The
CDI, IDENT, TMR/REF, NRST,
on gray background and automatically switch back to white text on black background when selected. If
messages remain after acknowledgement, the ALERTS
The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic,
and lightning. Each softkey sublevel has a
level. The ALERTS Softkey is visible in all softkey levels. For the top level softkeys and the transponder
(XPDR) levels, the IDENT Softkey remains visible.
INSET
OFF
DCLTR (3)
TRAFFIC
TOPO
and
ALERTS
Softkeys undergo a momentary change to black text
Softkey is black on white.
BACK Softkey which can be pressed to return to the previous
Displays Inset Map in PFD lower left corner
Removes Inset Map
Selects desired amount of map detail; cycles through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except for the active flight plan
Displays traffic information on Inset Map
Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale
on Inset Map
FEATURES
ADDITIONAL
APPENDICESINDEX
18
TERRAIN
STRMSCP
NEXRAD
XM LTNG
PFD
DFLTS
WIND
OPTN 1
OPTN 2
OPTN 3
OFF
Displays terrain information on Inset Map
Displays Stormscope information on Inset Map (optional)
Displays NEXRAD weather and coverage on Inset Map (optional)
Displays XM lightning information on Inset Map (optional)
Displays second-level softkeys for additional PFD configurations
Resets PFD to default settings, including changing units to standard
Displays softkeys to select wind data parameters
Longitudinal and lateral components
Total direction and speed
Total direction with head and crosswind speed components
Information not displayed
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
DME
BRG1
HSI FRMT
360 HSI
ARC HSI
BRG2
ALT UNIT
SYSTEM OVERVIEW
Displays/removes the DME Information Window (optional)
Cycles the Bearing 1 Information Window between NAV1, and GPS/ waypoint
identifier and GPS-derived distance information
Displays the softkeys for selecting the two HSI formats
Displays HSI as a 360° compass rose
Displays HSI as a 140° viewable arc
Cycles the Bearing 1 Information Window between NAV2, and GPS/ waypoint
identifier and GPS-derived distance information
Displays softkeys for setting the altimeter and BARO settings to metric units
OVERVIEW
SYSTEM
INSTRUMENTS
FLIGHT
EIS
METERS
IN
HPA
STD BARO
OBS
CDI
DME
XPDR
STBY
ON
ALT
GND
VFR
CODE
0 — 7
BKSP
IDENT
TMR/REF
NRST
ALERTS
When enabled, displays altimeter in meters
Press to display the BARO setting as inches of mercury
Press to display the BARO setting as hectopacals
Sets barometric pressure to 29.92 in Hg (1013 hPa if metric units are selected)
Selects OBS mode on the CDI when navigating by GPS (only available with active
leg)
Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI
Displays the DME Tuning Window, allowing tuning and selection of the DME
(optional)
Displays transponder mode selection softkeys
Selects standby mode (transponder does not reply to any interrogations)
Selects Mode A (transponder replies to interrogations)
Selects Mode C – altitude reporting mode (transponder replies to identification and
altitude interrogations)
Manually selects Ground Mode, the transponder does not allow Mode A and
Mode C replies, but it does permit acquisition squitter and replies to discretely
addressed Mode S interrogations
Automatically enters the VFR code (1200 in the U.S.A. only)
Displays transponder code selection softkeys 0-7
Use numbers to enter code
Removes numbers entered, one at a time
Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying
the transponder return on the ATC screen
Displays Timer/References Window
Displays Nearest Airports Window
Displays Alerts Window
AUDIO PANEL
& cNS
MANAGEMENT
FLIGHT
AVOIDANCE
HAZARD
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
19
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