Garmin G1000 - Cessna Citation Mustang Reference guide

Category
Car navigation systems
Type
Reference guide

This manual is also suitable for

G1000
®
Integrated Flight Deck
Pilot’s Guide
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
Copyright © 2006-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0435.20 or later for the Cessna Citation Mustang. 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
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 per-
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
®
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.
Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc.; Becker
®
is a registered trademark of Becker
Flugfunkwerk GmbH; NavData
®
is a registered trademark of Jeppesen, Inc.; XM
®
is a registered trademark of XM Satellite Radio, Inc.
June, 2010 190-00494-03 Rev. A Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-03 Rev. AB
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.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
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: The altitude calculated by the GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based upon TCAS II Resolution Advisories (if installed), ATC guidance, or
positive visual acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 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.
WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang aircraft, has a very high degree of
functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability
for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous
operation to occur without a fault indication shown by the system. 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, system operational procedures must be learned on the ground.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-03 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system 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 Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare indications from the system
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 system to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the
Aeronautical
Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo.
WARNING:
Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING:
Because of variation in the earth’s magnetic field, operating the system within the following
areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all
longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude
75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W.
(Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia).
South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New
Zealand).
WARNING:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
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.
CAUTION: The system 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.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
iii
WARNINGS, CAUTIONS, AND NOTES
NOTE: All visual depictions contained within this document, including screen images of the panel and
displays, are subject to change and may not reflect the most current system and 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: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-03 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
Bl a n k Pa g e
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00494-00 A
B
October, 2006
November, 2006
i through I-6
4-7, 4-16,
4-34
5-108 through
5-126
7-33 through
7-45
Production release
Added ‘SQ’ and ‘RX’ annunciations.
Added transponder code entry using the FMS Knob.
Added flying an example flight plan to the GPS Navigation
section.
Udated AFCS examples to be consistent with the example
flight plan in GPS Navigation section.
190-00494-01 A
B
February, 2007
May, 2007
i through I-6
i through I-6
Added GDU 8.00 parameters and made various corrections.
Added KHF 1050 HF and KTA 870 TAS
Reformatted GPS Navigation Section
Corrected various clerical errors
190-00494-02 A
B
April, 2008
May, 2008
i through I-6
All
Production Release
Added Synthetic Vision System
Added other GDU 9.01 parameters
Corrected clerical error.
190-00494-03 A June, 2010 i through I-6 Added GDU 10.01 parameters
Added GSD 41
Added GMA -20
Added new page navigation
TCAS II
Radar Altimeter
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Corrected various clerical errors
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-03 Rev. Avi
REVISION INFORMATION
Bl a n k Pa g e
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
vii
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
AHRS Operation ......................................................... 18
G1000 System Annunciations ...................................... 19
Softkey Function ......................................................... 20
GPS Receiver Operation .............................................. 28
1.7 Accessing G1000 Functionality............................ 33
Menus ....................................................................... 33
MFD Page Groups ....................................................... 34
MFD System Pages...................................................... 38
1.8 Display Backlighting ............................................. 48
Automatic Adjustment ................................................ 48
Manual Adjustment .................................................... 48
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 54
Airspeed Indicator ...................................................... 54
Attitude Indicator ....................................................... 57
Altimeter ................................................................... 59
Vertical Speed Indicator (VSI) ....................................... 63
Vertical Deviation ....................................................... 63
Horizontal Situation Indicator (HSI) .............................. 64
Course Deviation Indicator (CDI) .................................. 69
2.2 Supplemental Flight Data .................................... 77
Temperature Displays .................................................. 77
Wind Data ................................................................. 78
Vertical Navigation (VNV) Indications ........................... 79
2.3 PFD Annunciations and Alerting Functions ........ 80
System Alerting .......................................................... 80
Marker Beacon Annunciations...................................... 81
Traffic Annunciations................................................... 81
TAWS Annunciations ................................................... 82
Minimum Descent Altitude/Decision Height Alerting ...... 82
Altitude Alerting ......................................................... 84
Low Altitude Annunciation .......................................... 84
Radar Altimeter .......................................................... 85
2.4 Abnormal Operations ........................................... 87
Abnormal GPS Conditions ........................................... 87
Unusual Attitudes ....................................................... 88
SECTION 3 ENGINE INDICATION & CREW ALERTING
SYSTEM (EICAS)
3.1 Engine Indication System (EIS) ............................ 91
Engine Stage Rotation Speeds (N1 and N2) ................... 92
Oil Pressure and Temperature ...................................... 93
Fuel Display ............................................................... 93
Interstage Turbine Temperature .................................... 94
Electrical Display ........................................................ 94
Pressurization Display ................................................. 95
Trim and Flap Indicators .............................................. 96
3.2 Crew Alerting System (CAS) ................................. 97
CAS Messages and Prioritization .................................. 98
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 Cessna Citation Mustang
190-00494-03 Rev. Aviii
TABLE OF CONTENTS
4.4 Mode S Transponder ........................................... 129
GTX 33/33D Transponder Controls .............................. 130
GTX 33/33D Transponder Mode Selection.................... 131
TCAS II Transponder Controls (optional) ...................... 133
TCAS II Transponder Mode Selection (optional) ............ 134
Entering a Transponder Code ..................................... 136
IDENT Function ........................................................ 137
Flight ID Reporting.................................................... 138
4.5 Additional Audio Panel Functions ..................... 139
Power-up ................................................................. 139
Mono/Stereo Headsets .............................................. 139
Speaker ................................................................... 139
Unmuted Inputs ....................................................... 139
Intercom .................................................................. 140
Passenger Address (PA) System .................................. 141
Simultaneous COM Operation .................................... 141
Clearance Recorder and Player ................................... 142
4.6 Audio Panels Preflight Procedure ...................... 143
4.7 Abnormal Operation ........................................... 145
Stuck Microphone ..................................................... 145
COM Tuning Failure ................................................... 145
PFD Failure, Dual System ........................................... 145
Audio Panel Fail-safe Operation ................................. 146
Reversionary Mode ................................................... 146
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 ............................................................ 185
NDBs ....................................................................... 187
VORs ....................................................................... 189
User Waypoints ........................................................ 191
5.4 Airspaces .............................................................. 197
5.5 Direct-to-Navigation .......................................... 201
5.6 Flight Planning ..................................................... 207
Flight Plan Creation .................................................. 208
Adding Waypoints to an Existing Flight Plan ................ 213
Adding Airways to a Flight Plan ................................. 215
Adding Procedures to a Stored Flight Plan .................. 218
Flight Plan Storage ................................................... 225
Flight Plan Editing .................................................... 227
Along Track Offsets ................................................... 230
Parallel Track ............................................................ 232
Activating a Flight Plan Leg ....................................... 235
Inverting a Flight Plan ............................................... 236
Flight Plan Views ...................................................... 237
Closest Point of FPL .................................................. 239
5.7 Vertical Navigation ............................................. 240
Altitude Constraints .................................................. 242
5.8 Procedures ........................................................... 245
Departures ............................................................... 245
Arrivals ................................................................... 248
Approaches ............................................................. 250
5.9 Trip Planning ........................................................ 256
Trip Planning ............................................................ 256
Weight Planning ....................................................... 260
Weight Caution And Warning Conditions .................... 262
5.10 RAIM Prediction................................................... 263
5.11 Navigating a Flight Plan ..................................... 266
5.12 Abnormal Operation ........................................... 295
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 297
Activating Services .................................................... 297
Using XM Satellite Weather Products .......................... 299
6.2 Airborne Color Weather Radar .......................... 326
System Description ................................................... 326
Principles of Pulsed Airborne Weather Radar ............... 326
Safe Operating Distance ............................................ 331
Basic Antenna Tilt Setup ............................................ 331
Weather Mapping and Interpretation ......................... 333
Ground Mapping and Interpretation ........................... 346
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
ix
TABLE OF CONTENTS
6.3 TAWS-B ................................................................. 347
Displaying TAWS-B Data ............................................ 348
TAWS-B Page ........................................................... 350
TAWS-B Alerts .......................................................... 352
System Status ........................................................... 358
6.4 Traffic Information Service (TIS) ........................ 360
Displaying TRAFFIC Data ........................................... 361
Traffic Map Page ....................................................... 363
TIS Alerts ................................................................. 364
System Status ........................................................... 366
6.5 Traffic Advisory System (TAS)............................. 369
TAS Symbology ......................................................... 369
Operation ................................................................ 370
Altitude Display ........................................................ 373
Traffic Map Page Display Range ................................. 373
TAS Alerts ................................................................ 375
System Status ........................................................... 376
6.6 TCAS II Traffic ....................................................... 377
TCAS II Symbology .................................................... 377
TCAS II Alerts ........................................................... 378
System Test .............................................................. 381
Operation ................................................................ 382
System Status ........................................................... 388
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 392
7.2 Flight Director Operation ................................... 394
Activating the Flight Director ..................................... 394
AFCS Status Box ....................................................... 395
Flight Director Modes ................................................ 396
Switching Flight Directors .......................................... 396
Command Bars ......................................................... 397
7.3 Vertical Modes ..................................................... 398
Pitch Hold Mode (PIT) ............................................... 399
Selected Altitude Capture Mode (ALTS) ....................... 400
Altitude Hold Mode (ALT) .......................................... 401
Vertical Speed Mode (VS) .......................................... 402
Flight Level Change Mode (FLC) ................................. 403
Vertical Navigation Modes (VPTH, ALTV) ..................... 406
Glidepath Mode (GP) ................................................ 411
Glideslope Mode (GS) ............................................... 413
Takeoff (TO) and Go Around (GA) Modes .................... 414
7.4 Lateral Modes ...................................................... 415
Roll Hold Mode (ROL) ............................................... 416
Low Bank Mode ....................................................... 416
Navigation Modes (GPS, VOR, LOC) ............................ 418
Approach Modes (GPS, VAPP, LOC) ............................. 420
Backcourse Mode (BC) .............................................. 421
7.5 Autopilot and Yaw Damper Operation ............. 423
Flight Control ........................................................... 423
Engagement ............................................................. 424
Control Wheel Steering ............................................. 424
Disengagement ........................................................ 425
7.6 Example Flight Plan ............................................ 426
Departure ................................................................ 427
Intercepting a VOR Radial .......................................... 429
Flying a Flight Plan/GPS Course ................................. 430
Descent ................................................................... 431
Approach ................................................................. 435
Go Around/Missed Approach ..................................... 438
7.7 AFCS Annunciations and Alerts ......................... 440
AFCS Status Alerts .................................................... 440
Overspeed Protection ................................................ 441
Emergency Descent Mode (EDM) ............................... 441
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 444
SVS Operation .......................................................... 445
SVS Features ............................................................ 447
Field of View ............................................................ 456
8.2 SafeTaxi ................................................................ 458
SafeTaxi Cycle Number and Revision .......................... 461
8.3 ChartView ............................................................. 464
ChartView Softkeys ................................................... 464
ChartView Terminal Procedures Charts ........................ 465
Chart Options ........................................................... 473
Day/Night View ........................................................ 479
ChartView Cycle Number and Expiration Date ............. 481
8.4 FliteCharts ............................................................ 484
FliteCharts Softkeys .................................................. 484
FliteCharts Terminal Procedures Charts ....................... 485
Chart Options ........................................................... 492
Day/Night View ........................................................ 496
FliteCharts Cycle Number and Expiration Date ............. 498
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-03 Rev. Ax
TABLE OF CONTENTS
8.5 AOPA Airport Directory ....................................... 501
AOPA Database Cycle Number and Revision ............... 501
8.6 XM Radio Entertainment .................................... 504
Activating XM Satellite Radio Services ........................ 504
Using XM Radio ....................................................... 506
8.7 Scheduler .............................................................. 510
8.8 Flight Data Logging ............................................ 512
8.9 Abnormal Operation ........................................... 514
SVS Troubleshooting ................................................. 514
Reversionary Mode ................................................... 514
Unusual Attitudes ..................................................... 515
APPENDICES
Annunciations and Alerts ............................................. 519
CAS Messages .......................................................... 519
Comparator Annunciations ........................................ 520
Reversionary Sensor Annunciations ............................ 521
G1000 System Annunciations .................................... 521
G1000 System Message Advisories ............................. 524
AFCS Alerts .............................................................. 536
TAWS-B ALERTS ........................................................ 537
TCAS II Alerts and Annunciations ............................... 538
Other G1000 Aural Alerts .......................................... 539
Flight Plan Import/Export Messages ........................... 539
Database Management ................................................ 541
Garmin Databases .................................................... 541
Jeppesen Databases .................................................. 542
Automatic Database Synchronization ......................... 543
Loading Updated Databases ...................................... 544
Glossary .......................................................................... 547
Frequently Asked Questions ........................................ 553
General TIS Information ............................................... 557
Introduction ............................................................. 557
TIS vs. TAS/TCAS ....................................................... 557
TIS Limitations.......................................................... 557
Display Symbols ............................................................ 559
INDEX
Index ................................................................................I-1
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna Citation
Mustang. 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
or
GMA 1347D-20
Dual Audio
System with Integrated Marker Beacon Receiver
•
GTX 33/33D
Mode S Transponder (not used with
optional TCAS II)
•
GDL 69A
Satellite Data Link Receiver
•
GWX 68
Weather Radar
•
GCU 475
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GSD 41
Data Concentrator
•
GTP 59
Outside Air Temperature (OAT) Probe
•
GA 36
GPS/WAAS and
GA 37
GPS/WAAS/XM
Antennas
•
GSA 80
and
GSA 81
AFCS Servos
•
GSM 85A
Servo Gearboxes
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, or GSM
85A).
The following equipment is also connected to the G1000 system and interfaces with the GIA 63Ws:
•
Becker RA 3502
– A remotely mounted ADF receiver that operates in the 190.0 kHz to 1799.5 kHz frequency
band with 0.5 kHz channel spacing.
•
Honeywell KN 63
A remotely mounted 200-channel, 100-watt, all-solid-state digital DME transceiver that
provides distance information to the G1000 system.
•
Honeywell KTA 870
– Traffic Advisory System
•
Honeywell KHF 1050
– HF Transceiver
•
Honeywell KRA405B
– Radar Altimeter
•
Aviation Communication & Surveillance Systems RCZ 852
– Mode S Transponder
•
L-3 FA2100
– Cockpit Voice and Flight Data Recorder
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the Cessna Citation Mustang, the GFC 700 Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
2
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
•
GDU 1040A
(2) – 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
(1) – 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
(2) 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.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
3
SYSTEM OVERVIEW
•
GDC 74B
(2) 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 on-side GTP 59). The GDC 74B is designed to operate in Reduced Vertical
Separation Minimum (RVSM) airspace.
•
GEA 71
(2) 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
(2) 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
(2) 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.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
4
SYSTEM OVERVIEW
•
GMA 1347D
or
GMA 1347D-20
(2) – 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
(1)
and GTX 33D
(1 or 2) Solid-state transponders that provide Modes A, C and S capability.
Transponder #1 (XPDR1) is a GTX 33D, which includes Mode S with diversity. Either the GTX 33 or GTX 33D
may be installed as Transponder #2 (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
(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.
•
GWX 68
(1) Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A,
via HSDB connection.
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
5
SYSTEM OVERVIEW
•
GCU 475
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
•
GMC 710
(1) Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing
communication with both PFDs.
•
GSD 41
(1) – This unit is a data concentrator used to expand the input and output capabilities of the system.
Communication is through the High Speed Data Bus.
•
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
•
GSA 80
(2),
GSA 81
(2), and
GSM 85A
(4) – The GSA 80 servos are used for the automatic control of roll and
yaw, while the GSA 81 servos are used for the automatic control of pitch and pitch trim. These units interface
with each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator
to the mechanical flight-control surface linkage.
•
GA 36
(1) and
GA 37
(1) The GA 36 is a through-mount GPS/WAAS antenna. The GA 37 is a through-mount
GPS/WAAS antenna with XM/Data Link.
GA 36 GA 37
190-00494-03 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
6
SYSTEM OVERVIEW
GDU 1040A
(PFD #1)
GDU 1040A
(PFD #2)
GDU1500
(MFD)
GIA63W #2
GSA80
(Yaw)
GSA80
(Roll)
GSA81
(Pitch)
GSA81
(Pitch Trim)
GRS77#1
GIA 63W #1
GMC710
GMU44#1
GEA71#2
GEA71#1
GDC 74B #1
GTP59#1
#2
GMA 1347D
or
GMA 1347D-20
#1
GTX 33D GTX33
GCU475
GDL 69A
GRS77#2
GMU44#2
GDC74B #2
GTP59#2
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
GMA 1347D or
GMA 1347D-20
GSD 41
GWX 68
Figure 1-1 G1000 System (LRU Configuration)
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Garmin G1000 - Cessna Citation Mustang Reference guide

Category
Car navigation systems
Type
Reference guide
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