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Reversionary Sensor Annunciations.............................491
G1000 System Annunciations.....................................491
G1000 System Message Advisories..............................494
AFCS Alerts...............................................................506
TAWS ALERTS............................................................507
Other G1000 Aural Alerts...........................................508
SD Card Use....................................................................509
Jeppesen Databases...................................................509
Garmin Databases.....................................................510
Glossary...........................................................................513
Frequently Asked Questions.........................................519
General TIS Information................................................525
Introduction..............................................................525
TIS vs. TAS/TCAS........................................................525
TIS Limitations..........................................................525
Display Symbols.............................................................527
Index
Index .................................................................................I-1
190-00494-02 Rev. B
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
1
Systemystem Overviewverview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Section 1 Systemystem Overviewverview
1.1 Systemystem 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 Dual Audio System with Integrated Marker Beacon Receiver• GTX 33/33D Mode S Transponder• GDL 69A Satellite Data Link Receiver• GWX 68 Weather Radar• GCU 475 MFD Control Unit• GMC 710 AFCS Control Unit• 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 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.
190-00494-02 Rev. B
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
2
Systemystem Overviewverview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
1.2 Line Replaceaeplaceable 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.
　
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