Garmin G1000 - Socata TBM 850 Reference guide

Type
Reference guide

This manual is also suitable for

System Software 0719.03 or later
G1000
®
Integrated Flight Deck
Pilot’s Guide
G1000
®
Pilot’s Guide
Socata
TBM 850
190-00709-01
Revision A
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
www.garmin.com
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE & AIRFRAME SYSTEMS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A
Copyright © 2007, 2008 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0719.03 or later for the Socata TBM 850. Some differences in operation may
be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, 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
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
and G1000
®
are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH
®
, FliteCharts
®
, and SafeTaxi
®
are trademarks of
Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
NavData
®
is a registered trademark of Jeppesen, Inc.; Stormscope
®
is a registered trademark of L-3 Communications; and XM
®
is a
registered trademark of XM Satellite Radio, Inc.; Honeywell
®
and Bendix/King
®
are registered trademarks of Honeywell International,
Inc.; Becker
®
is a registered trademark of Becker Flugfunkwerk GmbH.
July, 2008 Printed in the U.S.A
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
i
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 Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. Aii
WARNINGS, CAUTIONS, AND 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 Garmin G1000 has a very high degree of functional integrity. However, the pilot must
recognize that providing monitoring and/or self-test capability for all conceivable system failures is not
practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication
shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: The 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:
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 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.
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
iii
WARNINGS, CAUTIONS, AND NOTES
CAUTION: 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.
CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the
G1000 Pilot’s Guide documentation. 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.
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.
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.
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: 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. Avoid the clusters to avoid the thunderstorms. In the cell display mode, even a single discharge
point may represent thunderstorm activity and should therefore be avoided.
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 Socata TBM 850
190-00709-01 Rev. Aiv
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00709-00
190-00709-01
A
A
11/2/07
7/7/08
All
All
Initial Release
Added Synthetic Vision System and other GDU 9.02 parameters
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
v
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 7
PFD Controls ................................................................ 7
Controls Associated With the MFD ................................. 9
AFCS Controls ............................................................ 10
Audio Panel Controls .................................................. 12
1.4 Secure Digital Cards.............................................. 14
1.5 System Power-up ................................................... 15
1.6 System Operation .................................................. 16
Normal Operation ....................................................... 16
Reversionary Mode ..................................................... 16
G1000 System Annunciations ...................................... 19
Softkey Function ......................................................... 20
GPS Receiver Operation .............................................. 25
1.7 Accessing G1000 Functionality............................ 30
Menus ....................................................................... 30
MFD Page Groups ....................................................... 30
MFD System Pages...................................................... 34
1.8 Display Backlighting ............................................. 42
Automatic Adjustment ................................................ 42
Manual Adjustment .................................................... 43
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 48
Airspeed Indicator ...................................................... 48
Attitude Indicator ....................................................... 50
Altimeter ................................................................... 51
Vertical Speed Indicator (VSI) ....................................... 55
Vertical Deviation ....................................................... 55
Horizontal Situation Indicator (HSI) .............................. 56
Course Deviation Indicator (CDI) .................................. 61
2.2 Supplemental Flight Data .................................... 69
Temperature Displays .................................................. 69
Wind Data ................................................................. 71
Vertical Navigation (VNV) Indications ........................... 72
2.3 PFD Annunciations and Alerting Functions ........ 73
System Alerting .......................................................... 73
Marker Beacon Annunciations...................................... 74
Traffic Annunciation .................................................... 74
TAWS Annunciations ................................................... 75
Altitude Alerting ......................................................... 76
Low Altitude Annunciation .......................................... 76
Minimum Descent Altitude/Decision Height Alerting ...... 77
Radar Altimeter .......................................................... 78
2.4 Abnormal Operations ........................................... 80
Abnormal GPS Conditions ........................................... 80
Unusual Attitudes ....................................................... 81
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Indication System (EIS) ............................ 85
Engine Parameters ...................................................... 86
Cabin Pressurization ................................................... 88
Fuel Information ......................................................... 88
Electrical Information .................................................. 89
Trim and Flap Indicators .............................................. 89
3.2 Synoptics ................................................................ 90
Electrical System ......................................................... 91
Fuel System ................................................................ 94
General Systems ......................................................... 96
3.3 Crew Alerting System (CAS) ................................. 97
CAS Display Inhibits .................................................... 98
CAS Messages and Prioritization .................................. 99
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 101
Audio Panel Volume Control ...................................... 101
PFD Controls and Frequency Display ........................... 102
Audio Panel Controls ................................................ 104
4.2 COM Operation .................................................... 106
COM Transceiver Selection and Activation ................... 106
COM Transceiver Manual Tuning ................................ 107
Quick-Tuning and Activating 121.500 MHz .................. 108
Auto-Tuning the COM Frequency ................................ 109
Frequency Spacing .................................................... 114
Automatic Squelch .................................................... 115
Volume .................................................................... 115
4.3 NAV Operation ..................................................... 116
NAV Radio Selection and Activation ........................... 116
NAV Receiver Manual Tuning ..................................... 117
Auto-Tuning a NAV Frequency from the MFD............... 119
Marker Beacon Receiver ............................................ 124
ADF/DME Tuning ...................................................... 125
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. Avi
TABLE OF CONTENTS
4.4 GTX 33/33D Mode S Transponders .................... 129
Transponder Controls ................................................ 130
Transponder Mode Selection ...................................... 131
Entering a Transponder Code ..................................... 133
IDENT Function ........................................................ 134
Flight ID Reporting.................................................... 135
4.5 Additional Audio Panel Functions ..................... 136
Power-Up ................................................................. 136
Mono/Stereo Headsets .............................................. 136
Speaker ................................................................... 136
Intercom .................................................................. 137
Passenger Address (PA) System .................................. 138
Simultaneous COM Operation .................................... 138
Clearance Recorder and Player ................................... 139
Entertainment Inputs ................................................ 140
4.6 Audio Panels Preflight Procedure ...................... 141
4.7 Abnormal Operation ........................................... 143
Stuck Microphone ..................................................... 143
COM Tuning Failure ................................................... 143
PFD Failure ............................................................... 144
Audio Panel Fail-Safe Operation ................................. 145
Reversionary Mode ................................................... 145
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 147
Navigation Status Box ............................................... 149
5.2 Using Map Displays ............................................. 150
Map Orientation ....................................................... 150
Map Range .............................................................. 152
Map Panning ............................................................ 155
Measuring Bearing and Distance ................................ 160
Topography .............................................................. 161
Map Symbols ........................................................... 164
Airways ................................................................... 170
Track Vector ............................................................. 172
Wind Vector ............................................................. 173
Nav Range Ring........................................................ 174
Fuel Range Ring ....................................................... 175
Field of View (SVS) .................................................... 176
5.3 Waypoints ............................................................. 177
Airports ................................................................... 178
Intersections ............................................................ 184
NDBs ....................................................................... 186
VORs ....................................................................... 188
User Waypoints ........................................................ 190
5.4 Airspaces .............................................................. 195
5.5 Direct-to-Navigation .......................................... 200
5.6 Flight Planning ..................................................... 206
Flight Plan Creation .................................................. 207
Adding Waypoints to an Existing Flight Plan ................ 210
Adding Airways to a Flight Plan ................................. 212
Adding Procedures to a Stored Flight Plan .................. 215
Flight Plan Storage ................................................... 222
Flight Plan Editing .................................................... 224
Along Track Offsets ................................................... 227
Parallel Track ............................................................ 229
Activating a Flight Plan Leg ....................................... 232
Inverting a Flight Plan ............................................... 233
Flight Plan Views ...................................................... 234
Closest Point of FPL .................................................. 236
5.7 Vertical Navigation ............................................. 237
Altitude Constraints .................................................. 239
5.8 Procedures ........................................................... 243
Departures ............................................................... 243
Arrivals ................................................................... 246
Approaches ............................................................. 248
5.9 Trip Planning ........................................................ 254
Trip Planning ............................................................ 254
Weight Planning ....................................................... 258
Weight Caution And Warning Conditions .................... 260
5.10 RAIM Prediction................................................... 261
5.11 Navigating a Flight Plan ..................................... 265
5.12 Abnormal Operation ........................................... 293
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 295
Using XM SATELLITE Weather Products ....................... 297
Weather Softkeys on the Weather Data Link Page ........ 300
6.2 Airborne Color Weather Radar .......................... 323
System Description ................................................... 323
Principles of Pulsed Airborne Weather Radar ............... 323
Safe Operating Distance ............................................ 328
Basic Antenna Tilt Setup ............................................ 328
Weather Mapping and Interpretation ......................... 330
Ground Mapping and Interpretation ........................... 343
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
vii
TABLE OF CONTENTS
6.3 Stormscope.............................................................. 344
Setting Up Stormscope on the Navigation Map ........... 344
Selecting the Stormscope Page .................................. 348
6.4 Terrain Proximity ................................................. 351
Displaying Terrain Proximity Data ............................... 352
Terrain Proximity Page ............................................... 354
6.5 Terrain-SVS ........................................................... 356
Displaying TERRAIN-SVS Data .................................... 357
TERRAIN-SVS Page ................................................... 359
TERRAIN-SVS Alerts .................................................. 361
System Status ........................................................... 365
6.6 Terrain Awareness & Warning System (TAWS) . 366
Displaying TAWS Data ............................................... 367
TAWS Page .............................................................. 369
TAWS Alerts ............................................................. 371
System Status ........................................................... 378
6.7 Traffic Information Service (TIS) ........................ 380
Displaying TRAFFIC Data ........................................... 381
Traffic Map Page ....................................................... 383
TIS Alerts ................................................................. 384
System Status ........................................................... 386
6.8 Traffic Advisory System (TAS)............................. 389
TAS Symbology ......................................................... 389
Operation ................................................................ 390
Altitude Display ........................................................ 392
Traffic Map Page Display Range ................................. 393
TAS Alerts ................................................................ 395
System Status ........................................................... 395
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 398
7.2 Flight Director Operation ................................... 400
Activating the Flight Director ..................................... 400
AFCS Status Box ....................................................... 401
Flight Director Modes ................................................ 402
Switching Flight Directors .......................................... 402
Command Bars ......................................................... 403
7.3 Vertical Modes ..................................................... 404
Pitch Hold Mode (PIT) ............................................... 405
Selected Altitude Capture Mode (ALTS) ....................... 406
Altitude Hold Mode (ALT) .......................................... 407
Vertical Speed Mode (VS) .......................................... 408
Flight Level Change Mode (FLC) ................................. 409
Vertical Navigation Modes (VPTH, ALTV) ..................... 411
Glidepath Mode (GP) ................................................ 416
Glideslope Mode (GS) ............................................... 418
Takeoff (TO) and Go Around (GA) Modes .................... 419
7.4 Lateral Modes ...................................................... 420
Roll Hold Mode (ROL) ............................................... 421
Low Bank Mode ....................................................... 421
Heading Select Mode (HDG) ...................................... 422
Navigation Modes (GPS, VOR, LOC) ............................ 423
Approach Modes (GPS, VAPP, LOC) ............................. 425
Backcourse Mode (BC) .............................................. 427
7.5 Autopilot and Yaw Damper Operation ............. 428
Flight Control ........................................................... 428
Engagement ............................................................. 429
Control Wheel Steering ............................................. 429
Disengagement ........................................................ 430
7.6 Example Flight Plan ............................................ 431
Departure ................................................................ 432
Intercepting a VOR Radial .......................................... 434
Flying a Flight Plan/GPS Course ................................. 435
Descent ................................................................... 436
Approach ................................................................. 440
Go Around/Missed Approach ..................................... 442
7.6 AFCS Annunciations and Alerts ......................... 444
AFCS Status Alerts .................................................... 444
Overspeed Protection ................................................ 445
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 448
SVS Operation .......................................................... 449
SVS Features ............................................................ 451
Field of View ............................................................ 460
8.2 SafeTaxi ................................................................ 462
SafeTaxi Cycle Number and Revision .......................... 465
8.3 ChartView ............................................................. 468
ChartView Softkeys ................................................... 468
Terminal Procedures Charts ....................................... 469
Chart Options ........................................................... 478
Day/Night View ........................................................ 484
ChartView Cycle Number and Expiration Date ............. 486
8.4 FliteCharts ............................................................ 490
FliteCharts Softkeys .................................................. 490
Terminal Procedures Charts ....................................... 491
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. Aviii
TABLE OF CONTENTS
Chart Options ........................................................... 499
Day/Night View ........................................................ 503
FliteCharts Cycle Number and Expiration Date ............. 505
8.5 XM Radio Entertainment .................................... 509
Activating XM Satellite Radio Services ........................ 509
Using XM Radio ....................................................... 511
8.6 Scheduler .............................................................. 515
8.7 Electronic Checklists ........................................... 517
8.8 Abnormal Operation ........................................... 522
SVS Troubleshooting ................................................. 522
Reversionary Mode ................................................... 522
Unusual Attitudes ..................................................... 523
APPENDICES
Annunciations and Alerts ............................................. 527
CAS Messages .......................................................... 527
Comparator Annunciations ........................................ 529
Reversionary Sensor Annunciations ............................ 530
G1000 System Annunciations .................................... 530
G1000 System Message Advisories ............................. 533
AFCS Alerts .............................................................. 545
Terrain-SVS Alerts ..................................................... 546
TAWS ALERTS ........................................................... 547
Other G1000 Aural Alerts .......................................... 548
SD Card Use ................................................................... 549
Jeppesen Databases .................................................. 549
Garmin Databases .................................................... 550
Glossary .......................................................................... 553
Frequently Asked Questions ........................................ 559
Map Symbols ................................................................. 565
INDEX
Index ................................................................................I-1
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section is designed to provide an overview of the G1000 Integrated Flight Deck. 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 1040A
Primary Flight Display (PFD)
•
GDU 1500
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit
•
GDC 74B
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 1347D Cabin
Dual Audio System with
Integrated Marker Beacon Receiver
•
GTX 33/33D
Mode S Transponder
•
GDL 69A
Data Link
•
GWX 68
Weather Radar
•
GCU 475
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GA 36
and
GA 37
GPS/WAAS Antennas
•
GSA 81
AFCS Servos
•
GSM 85
Servo Gearboxes
•
GTA 82
Trim Adapter
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, or GSM
85).
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the aircraft, the GFC 700 Automated Flight Control System (AFCS) provides the Flight Director (FD),
Autopilot (AP), and Yaw Damper (YD) functions of the G1000 system.
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.2 LINE REPLACEABLE UNITS (LRU)
•
GDU 1040A
Each unit is configured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution.
The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side
is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W
Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.
•
GDU 1500
Features a 15-inch LCD with 1024 x 768 resolution and is configured as an MFD. This unit is
linked to both PFDs via HSDB connection.
•
GIA 63W
– Functions as the main communication hub, linking all LRUs with the on-side PFD. Each GIA 63W
contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration
microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA 63Ws are not
paired together and do not communicate with each other directly.
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GDC 74B
Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure
altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with the on-
side GIA 63W, on-side GDU 1040A and on-side GRS 77, using an ARINC 429 digital interface (it also interfaces
directly with the OAT). The GDC 74B is designed to operate in Reduced Vertical Separation Minimum (RVSM)
airspace.
•
GEA 71
Receives and processes signals from the engine and airframe sensors. This unit communicates with
both GIA 63Ws using an RS-485 digital interface.
•
GRS 77
Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU 1040A
and the on-side GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors)
and interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74B to obtain air
data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this
document.
•
GMU 44
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.
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GMA 1347D Cabin
Integrates NAV/COM digital audio, intercom system and marker beacon controls, and
is installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual
control of the display reversionary mode (red
DISPLAY BACKUP
button) and communicates with the on-side
GIA 63W, using an RS-232 digital interface.
•
GTX 33 and GTX 33D
Solid-state transponders that provide Modes A, C and S capability. The GTX 33D
includes Mode S with diversity and is indicated as ‘XPDR1’. The GTX 33 is indicated as ‘XPDR2’. Both
transponders can be controlled from either PFD, and only one transponder can be active at a time. Each
transponder communicates with the on-side GIA 63W through an RS-232 digital interface.
•
GDL 69A
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.
•
GWX 68
Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A, via
HSDB connection.
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GCU 475
Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
•
GMC 710
Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing
communication with both PFDs.
•
GSA 81
, and
GSM 85
The GSA 81 servos are used for the automatic control of roll, yaw, pitch, and pitch trim.
These units interface with each GIA 63W.
The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the
mechanical flight-control surface linkage.
•
GTA 82
– The GTA 82 Trim Adapter is a remote mounted device that is used to allow the GFC 700 to drive the
yaw trim actuator.
•
GA 36
and
GA 37
– The GA 36 is a through-mount GPS/WAAS antenna. The GA 37 is a through-mount GPS/
WAAS antenna with XM/Datalink.
GA 36 GA 37
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A6
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
GDU 1040A
(PFD #1)
GDU 1040A
(PFD #2)
GDU 1500
(MFD)
GIA 63W #2
GSA 81
(Yaw)
GSA 81
(Roll)
GSA 81
(Pitch)
GSA 81
(Pitch Trim)
GRS 77 #1
GIA 63W #1
GMC 710
GMU 44 #1
GEA 71 #2
GEA 71 #1
GDC 74B #1
OAT Probe
GMA
1347D Cabin
#2
GMA
1347D Cabin
#1
GTX 33D GTX 33
GCU 475GWX 68
GDL 69A
GRS 77 #2
GMU 44 #2
GDC 74B #2
OAT Probe
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
GTA 82
(Trim Adapter)
Figure 1-1 Example G1000 System (LRU Configuration)
190-00709-01 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
7
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 1347D Cabin) and AFCS controls (GMC 710) are described in the CNS & Audio
Panel and AFCS sections respectively.
The G1000 system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and
audio panel. The controls for the PFD and MFD are discussed within the following pages of this section.
PFD CONTROLS
Figure 1-2 PFD Controls
21 5
4
6
8
7
3
11
12
10
9
15
14
13
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A8
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
The following list provides an overview of the controls located on the PFD bezel (see Figure 1-2).
1
NAV VOL/ID Knob
Controls NAV audio volume level. Press to switch the Morse code identifier audio
ON and OFF. Volume level is shown in the NAV frequency field as a percentage.
2
NAV Frequency Transfer Key
– Switches the standby and active NAV frequencies.
3
Dual
NAV Knob
Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for
kHz). Press to switch the tuning box (light blue box) between NAV1 and NAV2.
4
Joystick
– Changes the map range when rotated. Activates the map pointer when pressed.
5
BARO Knob
Sets the altimeter barometric pressure. Press to enter standard pressure (29.92in/1013 Hpa).
6
Dual COM Knob
Tunes the standby frequencies for the COM transceiver (large knob for MHz; small
knob for kHz). Press to switch the tuning box (light blue box) between COM1 and COM2.
7
COM Frequency Transfer Key
Switches the standby and active COM frequencies. Press and hold this
key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency
field.
8
COM
VOL/SQ Knob
Controls COM audio volume level. Volume level is shown in the COM frequency
field as a percentage. Press to turn the COM automatic squelch ON and OFF.
9
Direct-to Key ( )
Allows the user to enter a destination waypoint and establish a direct course to the
selected destination (the destination is either specified by the identifier, chosen from the active route, or
taken from the map pointer position).
10
FPL Key
– Displays the active Flight Plan Page for creating and editing the active flight plan.
11
CLR
Key
– Erases information, cancels entries, or removes page menus.
12
Dual FMS Knob
Flight Management System Knob. Press the
FMS
Knob to turn the selection cursor
ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small
and large
knobs. The large
knob moves the cursor on the page, while the small
knob selects individual
characters for the highlighted cursor location.
13
MENU Key
Displays a context-sensitive list of options. This list allows the user to access additional
features or make setting changes that relate to particular pages.
14
PROC Key
Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach
procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or
arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan.
If a flight plan is not used, both the desired airport and the desired procedure may be selected.
15
ENT Key
– Validates or confirms a menu selection or data entry.
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Garmin G1000 - Socata TBM 850 Reference guide

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