Garmin G1000: Cessna Citation Mustang Reference guide

Type
Reference guide

This manual is also suitable for

G1000
®
Integrated Flight Deck
Pilot’s Guide
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
Copyright © 2006-2011, 2013-2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0413.28 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.
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Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
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Garmin Corporation
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Tel: 34-93-357-2608
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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
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®
is a registered trademark of Jeppesen, Inc.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK
®
is a registered trademark of Penton Business Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK 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 AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. 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 licensee.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-05 Rev. E
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: 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
:
Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING
:
Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be older than the indicated weather product age.
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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories (if installed), ATC guidance, or
positive visual acquisition of conflicting traffic.
WARNING: For safety reasons, system operational procedures must be learned on the ground.
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.
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
WARNINGS, CAUTIONS, AND NOTES
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.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly with a
QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure
setting, as applicable.
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.
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.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-05 Rev. E
WARNINGS, CAUTIONS, AND NOTES
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.
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a
Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can
be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.
Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established
FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may
be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and
regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE
: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in
SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.
flygarmin.com by selecting ‘Database Exclusions List.
NOTE
: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact
on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting
Aviation Database Alerts.
NOTE
: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate
the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These
discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes;
or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.
com and select ‘Report An Aviation Data Error Report.’
NOTE
: If database card is inadvertently removed it should remain removed until the effective display or avionics
can be power cycled..
NOTE: Operate G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
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
190-00494-04 A December, 2011 All Added Profile View
Added Standby Navigation Database
Added new database update procedures
Updated system messages
Added other GDU 12.03 parameters
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-05 Rev. E
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00494-05 A
B
C
D
E
June, 2016
July, 2016
July, 2016
July, 2016
August, 2016
All
Page 28
Added User Defined Holds
Added Temperature Compensated Altitude
Added Auto North Up
Added Smart Airspace
Added AC-U-KWIK Airport Directory coapability
Updated CAS Messages
Added ADS-B out
Addid Visual Reporting Points
Added other GDU 15.12 parameters
Corrected various clerical errors
Corrected Print Specification
Removed GND softkey from transponder softkey table
and softkey map and updated the ALT transponder softkey
description in the System Overview section
Added the WX RADAR Softkey to the MFD Softkey
illustration and associated table
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
i
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 ............................................................ 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 ..................................................... 17
AHRS Operation ......................................................... 19
G1000 System Annunciations ...................................... 20
Softkey Function ......................................................... 21
GPS Receiver Operation .............................................. 29
1.7 Accessing G1000 Functionality............................ 34
Menus ....................................................................... 34
MFD Page Groups ....................................................... 35
MFD System Pages...................................................... 39
1.8 Display Backlighting ............................................. 49
Automatic Adjustment ................................................ 49
Manual Adjustment .................................................... 49
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 54
Airspeed Indicator ...................................................... 54
Attitude Indicator ....................................................... 56
Altimeter ................................................................... 59
Vertical Speed Indicator (VSI) ....................................... 63
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 69
GPS CDI Scaling.......................................................... 72
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 (Optional) ........................................... 85
2.4 Abnormal Operations ........................................... 87
Abnormal GPS Conditions ........................................... 87
Heading Failure Modes................................................ 88
SECTION 3 ENGINE INDICATION & CREW ALERTING
SYSTEM (EICAS)
3.1 Engine Indication System (EIS) ............................ 93
Engine Stage Rotation Speeds (N1 and N2) ................... 94
Oil Pressure and Temperature ...................................... 95
Fuel Display ............................................................... 95
Interstage Turbine Temperature .................................... 96
Electrical Display ........................................................ 96
Pressurization Display ................................................. 97
Trim and Flap Indicators .............................................. 98
3.2 Crew Alerting System (CAS) ................................. 99
CAS Messages and Prioritization ................................ 100
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 103
Audio Panel Volume Control ...................................... 103
PFD Controls and Frequency Display ........................... 104
Audio Panel Controls ................................................ 106
4.2 COM Operation .................................................... 108
COM Transceiver Selection and Activation ................... 108
COM Transceiver Manual Tuning ................................ 109
Quick-tuning and Activating 121.500 MHz .................. 110
Auto-tuning the COM Frequency ................................ 110
Frequency Spacing .................................................... 115
Automatic Squelch .................................................... 116
Volume .................................................................... 116
4.4 NAV Operation ..................................................... 117
NAV Radio Selection and Activation ........................... 117
NAV Receiver Manual Tuning ..................................... 118
Auto-tuning a NAV Frequency from the MFD ............... 120
Marker Beacon Receiver ............................................ 123
ADF/DME Tuning (Optional) ....................................... 124
4.5 GTX 33 Mode S Transponder .............................. 128
Transponder Controls ................................................ 128
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-05 Rev. Eii
TABLE OF CONTENTS
Transponder Mode Selection ...................................... 130
TCAS II Transponder Controls (optional) ...................... 132
TCAS II Transponder Mode Selection (optional) ............ 133
Entering a Transponder Code ..................................... 135
IDENT Function ........................................................ 136
Flight ID Reporting.................................................... 137
4.6 Additional Audio Panel Functions ..................... 138
Power-up ................................................................. 138
Mono/Stereo Headsets .............................................. 138
Speaker ................................................................... 138
Unmuted Inputs ....................................................... 138
Intercom .................................................................. 139
Passenger Address (PA) System .................................. 140
Simultaneous COM Operation .................................... 140
Clearance Recorder and Player ................................... 141
4.7 Audio Panels Preflight Procedure ...................... 142
4.8 Abnormal Operation ........................................... 144
Stuck Microphone ..................................................... 144
COM Tuning Failure ................................................... 144
PFD Failure, Dual System ...........................................144
Audio Panel Fail-safe Operation ................................. 145
Reversionary Mode ................................................... 145
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 147
Navigation Status Box ............................................... 148
5.2 Using Map Displays ............................................. 150
Map Orientation ....................................................... 150
Map Range .............................................................. 152
Map Panning ............................................................ 154
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 (SVT) .................................................... 176
Selected Altitude Intercept Arc ................................... 177
5.3 Waypoints ............................................................. 178
Airports ................................................................... 179
Intersections ............................................................ 186
NDBs ....................................................................... 188
VORs ....................................................................... 190
VRPs ....................................................................... 192
User Waypoints ........................................................ 194
5.4 Airspaces .............................................................. 200
5.5 Direct-to-Navigation .......................................... 205
5.6 Flight Planning ..................................................... 211
Flight Plan Creation .................................................. 212
Adding Waypoints to an Existing Flight Plan ................ 217
Adding Airways to a Flight Plan ................................. 220
Adding Procedures to a Stored Flight Plan .................. 223
Flight Plan Storage ................................................... 230
Flight Plan Editing .................................................... 232
Along Track Offsets ................................................... 236
Parallel Track ............................................................ 237
Activating a Flight Plan Leg ....................................... 240
Inverting a Flight Plan ............................................... 241
Flight Plan Views ...................................................... 242
Closest Point of FPL .................................................. 244
User-Defined Holding Patterns ................................... 245
5.7 Vertical Navigation ............................................. 250
Altitude Constraints .................................................. 252
5.8 Procedures ...........................................................257
Departures ............................................................... 258
Arrivals ................................................................... 261
Approaches ............................................................. 264
5.9 Trip Planning ........................................................ 272
Trip Planning ............................................................ 272
Weight Planning ....................................................... 276
Weight Caution And Warning Conditions .................... 278
5.10 RAIM Prediction................................................... 279
5.11 Navigating a Flight Plan ..................................... 282
5.12 Abnormal Operation ........................................... 310
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 314
Activating Services .................................................... 314
Using SiriusXM Weather Products .............................. 315
Weather Softkeys on the Weather Data Link (XM) Page 319
6.2 Airborne Color Weather Radar .......................... 350
System Description ................................................... 350
Principles of Pulsed Airborne Weather Radar ............... 350
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
iii
TABLE OF CONTENTS
Safe Operating Distance ............................................ 354
Basic Antenna Tilt Setup ............................................ 355
Weather Mapping and Interpretation ......................... 356
Ground Mapping and Interpretation ........................... 368
Weather Radar Overlay on the Navigation Map Page ... 368
System Status ........................................................... 370
6.3 TAWS-B ................................................................. 372
Displaying TAWS-B Data ............................................ 373
TAWS-B Page ........................................................... 375
TAWS-B Alerts .......................................................... 377
System Status ........................................................... 383
6.4 Profile View Terrain ............................................. 385
Profile View Display .................................................. 386
6.5 Traffic Information Service (TIS) ........................ 389
Displaying Traffic Data .............................................. 390
Traffic Map Page ....................................................... 392
TIS Alerts ................................................................. 393
System Status ........................................................... 395
6.6 Traffic Advisory System (TAS)............................. 398
TAS Symbology ......................................................... 398
Operation ................................................................ 399
Altitude Display ........................................................ 402
Traffic Map Page Display Range ................................. 402
TAS Alerts ................................................................ 404
System Status ........................................................... 405
6.7 TCAS II Traffic ....................................................... 406
TCAS II Symbology .................................................... 406
TCAS II Alerts ........................................................... 407
System Test .............................................................. 410
Operation ................................................................ 411
System Status ........................................................... 417
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 420
7.2 Flight Director Operation ................................... 422
Activating the Flight Director ..................................... 422
AFCS Status Box ....................................................... 423
Flight Director Modes ................................................ 424
Switching Flight Directors .......................................... 424
Command Bars ......................................................... 425
7.3 Vertical Modes ..................................................... 426
Pitch Hold Mode (PIT) ............................................... 427
Selected Altitude Capture Mode (ALTS) ....................... 428
Altitude Hold Mode (ALT) .......................................... 429
Vertical Speed Mode (VS) .......................................... 430
Flight Level Change Mode (FLC) ................................. 431
Vertical Navigation Modes (VPTH, ALTV) ..................... 434
Glidepath Mode (GP) ................................................ 439
Glideslope Mode (GS) ............................................... 441
Takeoff (TO) and Go Around (GA) Modes .................... 442
7.4 Lateral Modes ...................................................... 443
Roll Hold Mode (ROL) ............................................... 444
Low Bank Mode ....................................................... 444
Navigation Modes (GPS, VOR, LOC) ............................ 446
Approach Modes (GPS, VAPP, LOC) ............................. 448
Backcourse Mode (BC) .............................................. 449
7.5 Autopilot and Yaw Damper Operation ............. 451
Flight Control ........................................................... 451
Engagement ............................................................. 452
Control Wheel Steering ............................................. 452
Disengagement ........................................................ 453
7.6 Example Flight Plan ............................................ 454
Departure ................................................................ 455
Intercepting a VOR Radial .......................................... 457
Flying a Flight Plan/GPS Course ................................. 458
Descent ................................................................... 459
Approach ................................................................. 463
Go Around/Missed Approach ..................................... 466
7.7 AFCS Annunciations and Alerts ......................... 468
AFCS Status Alerts .................................................... 468
Overspeed Protection ................................................ 469
Emergency Descent Mode (EDM) ............................... 469
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 472
SVT Operation .......................................................... 473
SVT Features ............................................................ 475
Field of View ............................................................484
8.2 SafeTaxi ................................................................ 486
SafeTaxi Cycle Number and Revision .......................... 489
8.3 ChartView ............................................................. 492
ChartView Softkeys ................................................... 493
ChartView Terminal Procedures Charts ........................ 494
Chart Options ........................................................... 502
Day/Night View ........................................................ 508
ChartView Cycle Number and Expiration Date ............. 510
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-05 Rev. Eiv
TABLE OF CONTENTS
8.4 FliteCharts ............................................................ 513
FliteCharts Softkeys .................................................. 514
FliteCharts Terminal Procedures Charts ....................... 515
Chart Options ........................................................... 522
Day/Night View ........................................................ 526
FliteCharts Cycle Number and Expiration Date ............. 528
8.5 Airport Directory ................................................. 531
Airport Directory Database Cycle Number and Revision 532
8.6 SiriusXM Satellite Radio Entertainment ........... 534
Activating SiriusXM Satellite Radio Services ................ 534
Using SiriusXM Satellite Radio ................................... 535
8.7 Scheduler .............................................................. 539
8.8 Flight Data Logging ............................................ 541
8.9 Abnormal Operation ........................................... 543
SVT Troubleshooting ................................................. 543
Reversionary Mode ................................................... 543
Unusual Attitudes ..................................................... 544
APPENDICES
Annunciations and Alerts ............................................. 547
CAS Messages .......................................................... 547
Comparator Annunciations ........................................ 549
Reversionary Sensor Annunciations ............................ 550
G1000 System Annunciations .................................... 550
G1000 System Message Advisories ............................. 553
AFCS Alerts .............................................................. 564
TAWS-B ALERTS ........................................................ 565
TCAS II Alerts and Annunciations ............................... 566
Weather Radar Alerts and Annunciations .................... 567
Other G1000 Aural Alerts .......................................... 568
Flight Plan Import/Export Messages ........................... 568
Database Management ............................................. 569
Navigation Databases ............................................... 569
Garmin Databases/Jeppesen Chartview Database ........ 574
Garmin Aviation Glossary ............................................ 583
Frequently Asked Questions ........................................ 593
General TIS Information ............................................... 597
Introduction ............................................................. 597
TIS vs. TAS/TCAS ....................................................... 597
TIS Limitations.......................................................... 597
Display Symbols ............................................................ 599
INDEX
Index ................................................................................ I-1
190-00494-05 Rev. E
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 33D Optional (ES)
Mode S Transponder (not
used with optional TCAS II)
GDL 69A
Satellite Data Link Receiver
GWX 68
Color Weather Radar
GCU 475
MFD Control Unit
GMC 710
AFCS Control Unit
GSD 41
Data Concentrator (optional)
GTP 59
Outside Air Temperature (OAT) Probe
GA 36
GPS/SBAS and
GA 37
GPS/SBAS/SiriusXM
Antennas
GSA 80
and
GSA 81
AFCS Servos
GSM 85A/86
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/86).
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 Garmin AFCS.
In the Cessna Citation Mustang, the Garmin Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-00494-05 Rev. E
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 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.
190-00494-05 Rev. E
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.
190-00494-05 Rev. E
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 33D
(2)
and Optional GTX 33D ES
(1 or 2) – Solid-state transponders that provide Modes A/C/S capability,
and 1090 MHz Extended Squitter Automatic Dependent Surveillance - Broadcast (ADS-B) transmission.
Transponder #1 & #2 (XPDR1/XPDR2) is a GTX 33D, which includes Mode S with diversity. 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 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 SiriusXM 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.
190-00494-05 Rev. E
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 Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
GSD 41
(1) – This optional unit is a data concentrator used to expand the input and output capabilities of the
system when a Cockpit Voice Data Recorder is installed. 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/86
(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/86 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/SBAS antenna. The GA 37 is a through-mount
GPS/SBAS antenna with SiriusXM/Data Link.
GA 36 GA 37
190-00494-05 Rev. E
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
Optional ES
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
GTX 33D
Optional ES
Figure 1-1 G1000 System (LRU Configuration)
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
7
SYSTEM OVERVIEW
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 1347D) 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
Large (Outer) Knob
Small (Inner) Knob
11
12
10
9
15
14
13
21 5
4
6
8
7
3
The NAV, COM, and FMS knobs are concentric
dual knobs When a portion of the knob is not
specified in the text, either may be used.
190-00494-05 Rev. E
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
8
SYSTEM OVERVIEW
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 toggle 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
– Toggles 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 (cyan 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 (STD BARO).
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 (cyan box) between COM1 and COM2.
7
COM Frequency Transfer Key
– Toggles 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: Cessna Citation Mustang Reference guide

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