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190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 3
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
• 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.
4 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
• GMA 1347D (2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with the on-side GIA 63W, using an RS-232 digital interface.
• GTX 33 (1) and GTX 33D (1 or 2) – Solid-state transponders that provide Modes A, C and S capability. Transponder #1 (XPDR1) is a GTX 33D, which includes Mode S with diversity. Either the GTX 33 or GTX 33D may be installed as Transponder #2 (XPDR2). Both transponders can be controlled from either PFD, and only one transponder can be active at a time. Each transponder communicates with the on-side GIA 63W through an RS-232 digital interface.
• GDL 69A (1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the GDL 69A capability.
• GWX 68 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A, via HSDB connection.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 5
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
• 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 (2), GSA 81 (2), and GSM 85A (4) – The GSA 80 servos are used for the automatic control of roll and yaw, while the GSA 81 servos are used for the automatic control of pitch and pitch trim. These units interface with each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to the mechanical flight-control surface linkage.
• GA 36 (1) and GA 37 (1) – The GA 36 is a through-mount GPS/WAAS antenna. The GA 37 is a through-mount GPS/WAAS antenna with XM/Data Link.
GA 36GA 37
6 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
GDU1040A(PFD#1)GDU1040A(PFD#2)GDU1500(MFD)GIA63W#2GSA80(Yaw)GSA80(Roll)GSA81(Pitch)GSA81(PitchTrim)GRS77#1GIA63W#1GMC710GMU44#1GEA71#2GEA71#1GDC74B#1GTP59#1GMA1347D#2GMA1347D #1GTX33DGTX33GCU475GWX68GDL69AGRS77#2GMU44#2GDC74B#2GTP59#2VHF COMVHF NAV/LOCGPS/WAASG/SAFCS Mode LogicFlight DirectorServo ManagementVHF COMVHF NAV/LOCGPS/WAASG/SAFCS Mode LogicFlight DirectorServo Management
　
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本文鏈接地址：Cessna Citation Mustang Pilot’Guide 1(8)