Garmin G1000: Socata TBM 700 User guide

Type
User guide

This manual is also suitable for

G1000
®
Integrated Flight Deck
Pilot’s Guide
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
www.garmin.com
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
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
Copyright © 2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0829.00 or later for the Socata TBM 700 A, B, C, and N. 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
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
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sonal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
, WATCH
®
, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin Ltd. or its subsidiaries. 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
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are registered trademarks of Honeywell International,
Inc.; Becker
®
is a registered trademark of Becker Flugfunkwerk GmbH.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
December, 2010 190-01248-00 Rev. A Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. AB
LIMITED WARRANTY
LIMITED WARRANTY
Within the warranty period, Garmin will, at its sole discretion, 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/or labor incidental to the direct repair of said product. Garmin may,
at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and
replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This
warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product
damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or
other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider
of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin
reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any
country.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS,
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 in every case.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or 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 the nearest Service Center, call
Garmin Customer Service at one of the numbers listed below.
Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction
confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original
retailer is required. Garmin will not replace missing components from any package purchased through an online auction.
Garmin International Inc.
1200 East 151st Street, Olathe, Kansas 66062
Telephone: (913)397-8200
Telephone Toll Free: (888)606-5482
Facsimile: (913)397-8282
Facsimile Toll Free: (800)801-4670
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road, Southampton, SO40
9RB, UK
Telephone: ++44 (0) 870-8501243
Telephone Toll Free: ++44 (0) 0808 238 0000
(option 5)
Facsimile: ++44 (0) 238052004
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
i
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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting
traffic.
WARNING: 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 variation in the earth’s magnetic field, operating the system within the following areas
could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes.
South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120°
W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada).
North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South
latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
CAUTION: The 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.
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.
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
iii
WARNINGS, CAUTIONS, AND NOTES
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.
NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin
accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of
the data.
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
Bl a n k Pa g e
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-01248-00 A December, 2010 All Initial release
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. Avi
REVISION INFORMATION
Bl a n k Pa g e
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
vii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 8
PFD Controls ................................................................ 8
Controls Associated With the MFD ............................... 10
AFCS Controls ............................................................ 11
Audio Panel Controls .................................................. 13
1.4 Secure Digital Cards.............................................. 15
1.5 System Power-up ................................................... 16
1.6 System Operation .................................................. 17
Normal Operation ....................................................... 17
Reversionary Mode ..................................................... 18
G1000 System Annunciations ...................................... 20
Softkey Function ......................................................... 21
GPS Receiver Operation .............................................. 27
1.7 Accessing G1000 Functionality............................ 32
Menus ....................................................................... 32
MFD Page Groups ....................................................... 33
MFD System Pages...................................................... 37
1.8 Display Backlighting ............................................. 47
Automatic Adjustment ................................................ 47
Manual Adjustment .................................................... 47
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 52
Airspeed Indicator ...................................................... 52
Attitude Indicator ....................................................... 54
Altimeter ................................................................... 55
Vertical Speed Indicator (VSI) ....................................... 59
Vertical Deviation ....................................................... 59
Horizontal Situation Indicator (HSI) .............................. 60
Course Deviation Indicator (CDI) .................................. 65
2.2 Supplemental Flight Data .................................... 73
Temperature Displays .................................................. 73
Wind Data ................................................................. 75
Vertical Navigation (VNV) Indications ........................... 76
2.3 PFD Annunciations and Alerting Functions ........ 77
System Alerting .......................................................... 77
Marker Beacon Annunciations...................................... 78
Traffic Annunciation .................................................... 78
Terrain Annunciations ................................................. 79
Altitude Alerting .........................................................80
Low Altitude Annunciation .......................................... 80
Minimum Descent Altitude/Decision Height Alerting ...... 81
Radar Altimeter .......................................................... 82
2.4 Abnormal Operations ........................................... 84
Abnormal GPS Conditions ........................................... 84
Unusual Attitudes ....................................................... 85
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Indication System (EIS) ............................ 89
Engine Parameters ...................................................... 90
Cabin Pressurization ................................................... 92
Fuel Information ......................................................... 93
Electrical Information .................................................. 93
Trim and Flap Indicators .............................................. 94
3.2 Synoptics ................................................................ 95
Electrical System ......................................................... 96
Fuel System ................................................................ 99
General Systems ....................................................... 101
3.3 Crew Alerting System (CAS) ............................... 102
CAS Messages and Prioritization ................................ 103
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 105
Audio Panel Volume Control ...................................... 105
PFD Controls and Frequency Display ........................... 106
Audio Panel Controls ................................................ 108
4.2 COM Operation .................................................... 110
COM Transceiver Selection and Activation ................... 110
COM Transceiver Manual Tuning ................................ 111
Quick-Tuning and Activating 121.500 MHz .................. 112
Auto-Tuning the COM Frequency ................................ 113
Frequency Spacing .................................................... 118
Automatic Squelch .................................................... 119
Volume .................................................................... 119
4.3 NAV Operation ..................................................... 120
NAV Radio Selection and Activation ........................... 120
NAV Receiver Manual Tuning ..................................... 121
Auto-Tuning a NAV Frequency from the MFD............... 123
Marker Beacon Receiver ............................................ 128
ADF/DME Tuning ...................................................... 129
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. Aviii
TABLE OF CONTENTS
4.4 GTX 33/33D Mode S Transponders .................... 133
Transponder Controls ................................................ 134
Transponder Mode Selection ...................................... 135
Entering a Transponder Code ..................................... 137
IDENT Function ........................................................ 138
Flight ID Reporting.................................................... 139
4.5 Additional Audio Panel Functions ..................... 140
Power-Up ................................................................. 140
Mono/Stereo Headsets .............................................. 140
Speaker ................................................................... 140
Intercom .................................................................. 141
Passenger Address (PA) System .................................. 142
Simultaneous COM Operation .................................... 142
Clearance Recorder and Player ................................... 143
Entertainment Inputs ................................................ 144
4.6 Audio Panels Preflight Procedure ...................... 145
4.7 Abnormal Operation ........................................... 147
Stuck Microphone ..................................................... 147
COM Tuning Failure ................................................... 147
PFD Failure ............................................................... 148
Audio Panel Fail-Safe Operation ................................. 149
Reversionary Mode ................................................... 149
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 151
Navigation Status Box ............................................... 152
5.2 Using Map Displays ............................................. 154
Map Orientation ....................................................... 154
Map Range .............................................................. 156
Map Panning ............................................................ 159
Measuring Bearing and Distance ................................ 164
Topography .............................................................. 165
Map Symbols ........................................................... 168
Airways ................................................................... 174
Track Vector ............................................................. 176
Wind Vector ............................................................. 177
Nav Range Ring........................................................ 178
Fuel Range Ring ....................................................... 179
Field of View (SVS) .................................................... 180
Selected Altitude Intercept Arc ................................... 181
5.3 Waypoints ............................................................. 182
Airports ................................................................... 183
Intersections ............................................................ 190
NDBs ....................................................................... 192
VORs ....................................................................... 194
User Waypoints ........................................................ 196
5.4 Airspaces .............................................................. 202
5.5 Direct-to-Navigation .......................................... 207
5.6 Flight Planning ..................................................... 213
Flight Plan Creation .................................................. 214
Adding Waypoints to an Existing Flight Plan ................ 219
Adding Airways to a Flight Plan ................................. 221
Adding Procedures to a Stored Flight Plan .................. 224
Flight Plan Storage ................................................... 231
Flight Plan Editing .................................................... 233
Along Track Offsets ................................................... 236
Parallel Track ............................................................ 238
Activating a Flight Plan Leg ....................................... 241
Inverting a Flight Plan ............................................... 242
Flight Plan Views ...................................................... 243
Closest Point of FPL .................................................. 245
5.7 Vertical Navigation ............................................. 246
Altitude Constraints .................................................. 248
5.8 Procedures ........................................................... 252
Departures ............................................................... 252
Arrivals ................................................................... 255
Approaches ............................................................. 258
5.9 Trip Planning ........................................................ 264
Trip Planning ............................................................ 264
Weight Planning ....................................................... 268
Weight Caution And Warning Conditions .................... 270
5.10 RAIM Prediction................................................... 271
5.11 Navigating a Flight Plan ..................................... 275
5.12 Abnormal Operation ........................................... 305
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 307
Activating XM Satellite Services ................................. 307
Using XM SATELLITE Weather Products ....................... 309
Weather Softkeys on the Weather Data Link (XM) Page 312
6.2 Airborne Color Weather Radar .......................... 337
System Description ................................................... 337
Principles of Pulsed Airborne Weather Radar ............... 337
Safe Operating Distance ............................................ 341
Basic Antenna Tilt Setup ............................................ 342
Weather Mapping and Interpretation ......................... 344
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
ix
TABLE OF CONTENTS
6.3 Stormscope .......................................................... 358
Setting Up Stormscope on the Navigation Map ........... 358
Selecting the Stormscope Page .................................. 362
6.4 Terrain Proximity ................................................. 365
Displaying Terrain Proximity Data ............................... 366
Terrain Proximity Page ............................................... 368
6.5 Terrain-SVS ........................................................... 370
Displaying Terrain-SVS Data ....................................... 371
Terrain-SVS Page ...................................................... 373
Terrain-SVS Alerts ..................................................... 375
System Status ........................................................... 379
6.6 TAWS-B ................................................................. 380
Displaying TAWS-B Data ............................................ 381
TAWS-B Alerts .......................................................... 385
System Status ........................................................... 393
6.7 Traffic Information Service (TIS) ........................ 395
Displaying TRAFFIC Data ........................................... 396
Traffic Map Page ....................................................... 398
TIS Alerts ................................................................. 400
System Status ........................................................... 401
6.8 GTS 820 Traffic ..................................................... 404
Theory of operation .................................................. 404
TAS Alerts ................................................................ 408
System Test .............................................................. 409
Operation ................................................................ 410
6.9 KTA 870 Traffic ..................................................... 418
TAS Symbology ......................................................... 418
Operation ................................................................ 419
Altitude Display ........................................................ 422
Traffic Map Page Display Range ................................. 422
TAS Alerts ................................................................ 424
System Status ........................................................... 424
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 428
7.2 Flight Director Operation ................................... 430
Activating the Flight Director ..................................... 430
AFCS Status Box ....................................................... 431
Flight Director Modes ................................................ 432
Switching Flight Directors .......................................... 432
Command Bars ......................................................... 433
7.3 Vertical Modes ..................................................... 434
Pitch Hold Mode (PIT) ............................................... 435
Selected Altitude Capture Mode (ALTS) ....................... 436
Altitude Hold Mode (ALT) .......................................... 437
Vertical Speed Mode (VS) .......................................... 438
Flight Level Change Mode (FLC) ................................. 439
Vertical Navigation Modes (VPTH, ALTV) ..................... 441
Glidepath Mode (GP) ................................................ 446
Glideslope Mode (GS) ............................................... 448
Takeoff (TO) and Go Around (GA) Modes .................... 449
7.4 Lateral Modes ...................................................... 450
Roll Hold Mode (ROL) ............................................... 451
Low Bank Mode ....................................................... 451
Heading Select Mode (HDG) ...................................... 452
Navigation Modes (GPS, VOR, LOC) ............................ 453
Approach Modes (GPS, VAPP, LOC) ............................. 455
Backcourse Mode (BC) .............................................. 456
7.5 Autopilot and Yaw Damper Operation ............. 458
Flight Control ........................................................... 458
Engagement ............................................................. 459
Control Wheel Steering ............................................. 459
Disengagement ........................................................ 460
7.6 Example Flight Plan ............................................ 461
Departure ................................................................ 462
Intercepting a VOR Radial .......................................... 464
Flying a Flight Plan/GPS Course ................................. 465
Descent ................................................................... 466
Approach ................................................................. 470
Go Around/Missed Approach ..................................... 473
7.7 AFCS Annunciations and Alerts ......................... 475
AFCS Status Alerts .................................................... 475
Overspeed Protection ................................................ 476
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 478
SVS Operation .......................................................... 479
SVS Features ............................................................ 481
Field of View ............................................................ 490
8.2 SafeTaxi ................................................................ 492
SafeTaxi Cycle Number and Revision .......................... 495
8.3 ChartView ............................................................. 498
ChartView Softkeys ................................................... 498
Garmin G1000 Pilot’s Guide for the Socata TBM 700
190-01248-00 Rev. Ax
TABLE OF CONTENTS
Terminal Procedures Charts ....................................... 499
Chart Options ........................................................... 507
Day/Night View ........................................................ 513
ChartView Cycle Number and Expiration Date ............. 515
8.4 FliteCharts ............................................................ 518
FliteCharts Softkeys .................................................. 518
Terminal Procedures Charts ....................................... 519
Chart Options ........................................................... 526
Day/Night View ........................................................ 530
FliteCharts Cycle Number and Expiration Date ............. 532
8.5 AOPA Airport Directory ....................................... 535
AOPA Database Cycle Number and Revision ............... 535
8.6 XM Radio Entertainment .................................... 538
Activating XM Satellite Radio Services ........................ 538
Using XM Radio ....................................................... 540
8.7 Scheduler .............................................................. 544
8.8 Electronic Checklists ........................................... 546
8.9 Flight Data Logging ............................................ 551
8.10 Abnormal Operation ........................................... 553
SVS Troubleshooting ................................................. 553
Reversionary Mode ................................................... 553
Unusual Attitudes ..................................................... 554
APPENDICES
Annunciations and Alerts ............................................. 557
CAS Messages .......................................................... 557
Comparator Annunciations ........................................ 559
Reversionary Sensor Annunciations ............................ 560
G1000 System Annunciations .................................... 560
G1000 System Message Advisories ............................. 563
AFCS Alerts .............................................................. 575
Terrain-SVS Alerts ..................................................... 576
TAWS-B ALERTS ........................................................ 577
Other G1000 Aural Alerts .......................................... 579
Flight Plan Import/Export Messages ........................... 579
Database Management ................................................ 581
Jeppesen Databases .................................................. 581
Garmin Databases .................................................... 585
Glossary .......................................................................... 589
Frequently Asked Questions ........................................ 595
Map Symbols ................................................................. 599
INDEX
Index ................................................................................I-1
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
1
SYSTEM OVERVIEW
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 (optional)
•
GWX 68
Weather Radar (optional)
•
GCU 475
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GTS 820
Traffic Avoidance System (optional)
•
GA 58
Directional Antenna
•
GA 36
and
GA 37
GPS/SBAS 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, GA 58,
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 700
190-01248-00 Rev. A2
SYSTEM OVERVIEW
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 SBAS 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.
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
3
SYSTEM OVERVIEW
•
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 700
190-01248-00 Rev. A4
SYSTEM OVERVIEW
•
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.
190-01248-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 700
5
SYSTEM OVERVIEW
•
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/SBAS antenna. The GA 37 is a through-mount GPS/
SBAS antenna with XM/Datalink.
GA 36 GA 37
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Garmin G1000: Socata TBM 700 User guide

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