Garmin G1000® for Cessna CitationJet User guide

Type
User guide
G1000
®
Integrated Flight Deck
Pilot’s Guide
Cessna CitationJet
Model 525
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
Copyright © 2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1162.00 or later for the Cessna CitationJet Model 525. 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.
May, 2010 190-01131-00 Rev. A Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
LIMITED WARRANTY
190-01131-00 Rev. A
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made
at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED
OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR
PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole
discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit
the Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
i
WARNINGS, CAUTIONS, AND NOTES
190-01131-00 Rev. A
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 CitationJet Model 525 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 CitationJet Model 525
ii
WARNINGS, CAUTIONS, AND NOTES
190-01131-00 Rev. A
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 CitationJet Model 525 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.
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
iii
WARNINGS, CAUTIONS, AND NOTES
190-01131-00 Rev. A
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 CitationJet Model 525
iv
WARNINGS, CAUTIONS, AND NOTES
190-01131-00 Rev. A
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v
REVISION INFORMATION
190-01131-00 Rev. A
Record of Revisions
Part Number Revision Date Page Range Description
190-01131-00 A May, 2010 All Initial release
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
vi
REVISION INFORMATION
190-01131-00 Rev. A
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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
vii
TABLE OF CONTENTS
190-01131-00 Rev. A
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 8
PFD Controls ................................................................ 8
MFD Control Unit ....................................................... 10
AFCS Controls ............................................................ 11
Audio Panel Controls .................................................. 13
1.4 Secure Digital Cards.............................................. 15
1.5 System Power-up ................................................... 16
1.6 System Operation .................................................. 17
Normal Operation ....................................................... 17
Reversionary Mode ..................................................... 17
AHRS Operation ......................................................... 19
G1000 System Annunciations ...................................... 20
Softkey Function ......................................................... 21
GPS Receiver Operation .............................................. 28
1.7 Accessing G1000 Functionality............................ 33
Menus ....................................................................... 33
MFD Page Groups ....................................................... 33
MFD System Pages...................................................... 37
1.8 Display Backlighting ............................................. 46
Automatic Adjustment ................................................ 46
Manual Adjustment .................................................... 46
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments .................................................52
Airspeed Indicator ...................................................... 52
Attitude Indicator ....................................................... 55
Altimeter ................................................................... 57
Vertical Speed Indicator (VSI) ....................................... 61
Vertical Deviation ....................................................... 61
Horizontal Situation Indicator (HSI) .............................. 62
Course Deviation Indicator (CDI) .................................. 67
2.2 Supplemental Flight Data .................................... 75
Temperature Displays .................................................. 75
Wind Data ................................................................. 76
Vertical Navigation (VNV) Indications ........................... 77
2.3 PFD Annunciations and Alerting Functions ........ 78
System Alerting .......................................................... 78
Marker Beacon Annunciations...................................... 79
Traffic Annunciations................................................... 79
TAWS Annunciations ................................................... 80
Minimum Descent Altitude/Decision Height Alerting ......80
Altitude Alerting ......................................................... 82
Low Altitude Annunciation .......................................... 82
Radar Altimeter .......................................................... 83
2.4 Abnormal Operations ........................................... 85
Abnormal GPS Conditions ........................................... 85
Unusual Attitudes ....................................................... 86
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Indication System (EIS) ............................ 90
Ground OAT Set Window ............................................. 91
Engine Spool Rotation Speeds (N1 and N2) ................... 92
Oil Pressure and Temperature ...................................... 94
Fuel Display ............................................................... 94
Inter-Turbine Temperature ............................................ 95
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 97
Audio Panel Volume Control ........................................ 97
PFD Controls and Frequency Display ............................. 98
Audio Panel Controls ................................................ 100
4.2 COM Operation .................................................... 102
COM Transceiver Selection and Activation ................... 102
COM Transceiver Manual Tuning ................................ 103
Quick-tuning and Activating 121.500 MHz .................. 104
Auto-tuning the COM Frequency ................................ 105
Frequency Spacing .................................................... 109
Automatic Squelch .................................................... 110
Volume .................................................................... 110
4.3 NAV Operation ..................................................... 111
NAV Radio Selection and Activation ........................... 111
NAV Receiver Manual Tuning ..................................... 112
Auto-tuning a NAV Frequency from the MFD ............... 114
Marker Beacon Receiver ............................................ 118
DME Tuning ............................................................. 119
4.4 Mode S Transponder ........................................... 120
GTX 33/33D Transponder Controls .............................. 120
GTX 33/33D Transponder Mode Selection.................... 121
Entering a Transponder Code ..................................... 123
IDENT Function ........................................................ 124
Flight ID Reporting.................................................... 125
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
viii
TABLE OF CONTENTS
190-01131-00 Rev. A
4.5 Additional Audio Panel Functions ..................... 126
Power-up ................................................................. 126
Mono/Stereo Headsets .............................................. 126
Speaker ................................................................... 126
Unmuted Inputs ....................................................... 126
Intercom .................................................................. 127
Passenger Address (PA) System .................................. 128
Simultaneous COM Operation .................................... 128
Clearance Recorder and Player ................................... 129
4.6 Audio Panels Preflight Procedure ...................... 130
4.7 Abnormal Operation ........................................... 132
Stuck Microphone ..................................................... 132
COM Tuning Failure ................................................... 132
PFD Failure, Dual System ........................................... 132
Audio Panel Fail-safe Operation ................................. 133
Reversionary Mode ................................................... 133
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 135
Navigation Status Box ............................................... 136
5.2 Using Map Displays ............................................. 138
Map Orientation ....................................................... 138
Map Range .............................................................. 140
Map Panning ............................................................ 142
Measuring Bearing and Distance ................................ 146
Topography .............................................................. 147
Map Symbols ........................................................... 150
Airways ................................................................... 156
Track Vector ............................................................. 158
Wind Vector ............................................................. 159
Nav Range Ring........................................................ 160
Fuel Range Ring ....................................................... 161
Field of View (SVS) .................................................... 162
5.3 Waypoints ............................................................. 163
Airports ................................................................... 164
Intersections ............................................................ 171
NDBs ....................................................................... 173
VORs ....................................................................... 175
User Waypoints ........................................................ 177
5.4 Airspaces .............................................................. 183
5.5 Direct-to-Navigation .......................................... 187
5.6 Flight Planning ..................................................... 192
Flight Plan Creation .................................................. 193
Adding Waypoints to an Existing Flight Plan ................ 198
Adding Airways to a Flight Plan ................................. 200
Adding Procedures to a Stored Flight Plan .................. 202
Flight Plan Storage ................................................... 209
Flight Plan Editing .................................................... 211
Along Track Offsets ................................................... 214
Parallel Track ............................................................ 216
Activating a Flight Plan Leg ....................................... 219
Inverting a Flight Plan ............................................... 220
Flight Plan Views ...................................................... 221
Closest Point of FPL .................................................. 223
5.7 Vertical Navigation ............................................. 224
Altitude Constraints .................................................. 226
5.8 Procedures ........................................................... 229
Departures ............................................................... 229
Arrivals ................................................................... 232
Approaches ............................................................. 234
5.9 Trip Planning ........................................................ 240
Trip Planning ............................................................ 240
Weight Planning ....................................................... 244
Weight Caution And Warning Conditions .................... 246
5.10 RAIM Prediction................................................... 247
5.11 Navigating a Flight Plan ..................................... 250
5.12 Abnormal Operation ........................................... 278
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 281
Activating Services .................................................... 281
Using XM Satellite Weather Products .......................... 283
6.2 WX-500 Stormscope ........................................... 310
Setting Up Stormscope on the Navigation Map ........... 310
Selecting the Stormscope Page .................................. 314
6.3 Airborne Color Weather Radar .......................... 315
System Description ................................................... 315
Principles of Pulsed Airborne Weather Radar ............... 315
Safe Operating Distance ............................................ 319
Basic Antenna Tilt Setup ............................................ 320
Weather Mapping and Interpretation ......................... 322
Ground Mapping and Interpretation ........................... 335
6.4 TAWS-B ................................................................. 336
Displaying TAWS-B Data ............................................ 337
TAWS-B Page ........................................................... 339
TAWS-B Alerts .......................................................... 341
System Status ........................................................... 347
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TABLE OF CONTENTS
190-01131-00 Rev. A
6.5 TAWS-A ................................................................. 349
TAWS-A Page ........................................................... 351
TAWS-A Alerts .......................................................... 353
System Status ........................................................... 365
TAWS-A Abnormal operations .................................... 366
6.6 Traffic Information Service (TIS) ........................ 369
Displaying TRAFFIC Data ........................................... 370
Traffic Map Page ....................................................... 372
TIS Alerts ................................................................. 373
System Status ........................................................... 375
6.7 Garmin GTS Traffic ............................................... 378
Theory of operation .................................................. 378
TAS Alerts ................................................................ 381
System Test .............................................................. 382
Operation ................................................................ 383
6.8 Honeywell KTA870 Traffic ................................... 392
TAS Symbology ......................................................... 392
Operation ................................................................ 393
Altitude Display ........................................................ 396
Traffic Map Page Display Range ................................. 396
TAS Alerts ................................................................ 398
System Status ........................................................... 399
6.9 L-3 Skywatch Traffic ............................................ 400
TAS Symbology ......................................................... 400
Operation ................................................................ 401
Altitude Display ........................................................ 404
Traffic Map Page Display Range ................................. 404
TAS Alerts ................................................................ 406
System Status ........................................................... 406
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 410
7.2 Flight Director Operation ................................... 412
Activating the Flight Director ..................................... 412
AFCS Status Box ....................................................... 413
Flight Director Modes ................................................ 414
Switching Flight Directors .......................................... 414
Command Bars ......................................................... 415
7.3 Vertical Modes ..................................................... 416
Pitch Hold Mode (PIT) ............................................... 417
Selected Altitude Capture Mode (ALTS) ....................... 418
Altitude Hold Mode (ALT) .......................................... 419
Vertical Speed Mode (VS) .......................................... 420
Flight Level Change Mode (FLC) ................................. 421
Vertical Navigation Modes (VPTH, ALTV) ..................... 424
Glidepath Mode (GP) ................................................ 429
Glideslope Mode (GS) ............................................... 431
Takeoff (TO) and Go Around (GA) Modes .................... 432
7.4 Lateral Modes ...................................................... 433
Roll Hold Mode (ROL) ............................................... 434
Low Bank Mode ....................................................... 434
Navigation Modes (GPS, VOR, LOC) ............................ 436
Approach Modes (GPS, VAPP, LOC) ............................. 438
Backcourse Mode (BC) .............................................. 439
7.5 Autopilot and Yaw Damper Operation ............. 441
Flight Control ........................................................... 441
Engagement ............................................................. 442
Control Wheel Steering ............................................. 442
Disengagement ........................................................ 443
7.6 Example Flight Plan ............................................ 444
Departure ................................................................ 445
Intercepting a VOR Radial .......................................... 447
Flying a Flight Plan/GPS Course ................................. 448
Descent ................................................................... 449
Approach ................................................................. 452
Go Around/Missed Approach ..................................... 455
7.7 AFCS Annunciations and Alerts .........................457
AFCS Status Alerts .................................................... 457
Overspeed Protection ................................................ 458
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 460
SVS Operation .......................................................... 461
SVS Features ............................................................ 463
Field of View ............................................................ 472
8.2 SafeTaxi ................................................................ 474
8.3 ChartView ............................................................. 480
ChartView Softkeys ................................................... 480
Terminal Procedures Charts ....................................... 481
Chart Options ........................................................... 489
Day/Night View ........................................................ 495
ChartView Cycle Number and Expiration Date ............. 497
8.4 FliteCharts ............................................................ 500
FliteCharts Softkeys .................................................. 500
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TABLE OF CONTENTS
190-01131-00 Rev. A
Terminal Procedures Charts ....................................... 501
Chart Options ........................................................... 508
Day/Night View ........................................................ 512
FliteCharts Cycle Number and Expiration Date ............. 514
8.5 AOPA Airport Directory ....................................... 517
AOPA Database Cycle Number and Revision ............... 518
8.6 Satellite Telephone Services .............................. 520
Registering the Iridium Satellite System ...................... 520
Telephone Communication ........................................ 520
8.7 XM Radio Entertainment .................................... 534
Activating XM Satellite Radio Services ........................ 534
Using XM Radio ....................................................... 536
8.8 Scheduler .............................................................. 539
8.9 Abnormal Operation ........................................... 541
SVS Troubleshooting ................................................. 541
Reversionary Mode ................................................... 541
Unusual Attitudes ..................................................... 542
APPENDICES
Annunciations and Alerts ............................................. 545
Comparator Annunciations ........................................ 547
Reversionary Sensor Annunciations ............................ 547
advisory AnnuNciations ............................................. 548
Message Advisory Alerts ............................................ 548
G1000 System Annunciations .................................... 548
G1000 System Message Advisories ............................. 551
AFCS Alerts .............................................................. 563
TAWS-B ALERTS ........................................................ 564
TAWS-A Alerts (Optional) .......................................... 565
TCAS I Alerts and Annunciations (Optional) ................. 567
Other G1000 Aural Alerts .......................................... 567
Flight Plan Import/Export Messages ........................... 568
Database Management ................................................ 569
Garmin Databases .................................................... 569
Jeppesen Databases .................................................. 570
Automatic Database Synchronization ......................... 571
Loading Updated Databases ...................................... 572
Glossary .......................................................................... 575
Frequently Asked Questions ........................................ 581
General TIS Information ............................................... 585
Introduction ............................................................. 585
TIS vs. TAS/TCAS ....................................................... 585
TIS Limitations.......................................................... 585
Display Symbols ............................................................ 587
INDEX
Index ................................................................................I-1
190-01131-00 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
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 CitationJet
Model 525. 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 1240A
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-20
Dual Audio System with
Integrated Marker Beacon Receiver
•
GTX 33/33D
Mode S Transponder)
•
GDL 69A
Satellite Data Link Receiver
•
GDL 59
Data Link
•
GSR 56
Iridium Transceiver
•
GWX 68
Weather Radar
•
GCU 475
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GTS 820/850
Traffic Avoidance System (optional)
•
GA 58
Directional Antenna
•
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 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
86).
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the Cessna CitationJet Model 525, the GFC 700 Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
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 1240A
(1) – Features a 12-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.
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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
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.
190-01131-00 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
4
SYSTEM OVERVIEW
•
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.
•
GDL 59
(1) – GDL 59 operation is performed with the MFD through the HSDB. Connectivity with the GSR 56
for the Iridium telephone feature is through the RS-232 bus.
190-01131-00 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
5
SYSTEM OVERVIEW
•
GSR 56
(1) The Iridium Transceiver operation for voice communication is by means of a telephone handset in
the cabin and pilot and copilot headsets in the cockpit. The tranceiver can also send and receive data provided
by the GDL 59 through the RS-232 bus.
•
GWX 68
(1) – Provides airborne weather and ground mapped radar data to the MFD, via HSDB connection.
•
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.
•
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
•
GSA 80
(3),
GSA 81
(1), and
GSM 86
(4) – The GSA 80 servos are used for the automatic control of pitch, roll
and yaw, while the GSA 81 servos are used for the automatic control of pitch trim. These units interface with
each GIA 63W.
The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to
the mechanical flight-control surface linkage.
190-01131-00 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525
6
SYSTEM OVERVIEW
•
GTS 820/850
– The GTS 820 Traffic Advisory System (TAS) and GTS 850 TCAS I use active interrogations of
Mode S and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control
system.
•
GA 58
The GA 58 is directional antenna for the Traffic Avoidance System. One top-mounted directional
antenna is required. Optional bottom mounted antenna offers better threat visibility.
•
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
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Garmin G1000® for Cessna CitationJet User guide

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User guide

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