曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

• Dual Integrated Avionics Units with VHF Nav/Com, GPS
receivers, Flight Directors, and Aural Warning Generator -
Garmin GIA 63W
• Single Distance Measuring Equipment (DME) receiver -
Honeywell KN 63
• Dual digital Audio Control Panels - Garmin GMA 1347D
• Single Remote Flight Management System (FMS) / MFD
control keyboard - Garmin GCU 475
• Three Axis Automatic Flight Control System (AFCS) with
Integrated Pitch Trim - Garmin GFC 700 with Garmin GMC
710 Mode Controller
• Single Mode S Diversity Transponder with Enhanced
Surveillance and Traffic Information System (TIS) -
Garmin GTX 33D
• Single Mode S Non-diversity Transponder with Enhanced
Surveillance and TIS - Garmin GTX 33
• Single four-color Weather Avoidance Radar - Garmin GWX 68
• Single Satellite Data Link Weather Transceiver - Garmin
GDL 69A
• Single Electric Standby Attitude Indicator - Mid Continent
Instruments 4200
• Single electromechanical Standby Airspeed Indicator -
Aerosonic 261440
• Single electromechanical Standby Altimeter - Aerosonic 162350
• Single Emergency Locator Transmitter (ELT) - Artex C406-N
10.2 Instrument and Control Panels
A. Installed on Left-Hand Panel (pilot):
• Master Caution / Master Warning Lights
• Digital Audio Control Panel (GMA 1347)
• Primary Flight Display
• Oxygen Control Valve
B. Installed on Right-Hand Panel (copilot):
• Rotary Test Knob
• Master Caution / Master Warning Lights
• Primary Flight Display
• Digital Audio Control Panel (GMA 1347D)
• Oxygen Supply Pressure Indicator
C. Installed on Center Panel:
• Flight Director / Autopilot Mode Controller (glareshield
mounted)
• L and R Engine Fire Warning / Arm / Discharge Buttons
• Standby Airspeed Indicator
• Standby Attitude Indicator
• Standby Altimeter
• Multi-Function Display
D. Installed on Tilt Panel (Left to Right):
• Generator and Battery Switches
• Engine Start Switches
• Avionics Power Switches
• Ignition Switches
• Fuel Boost Pump Switches
• Fuel Transfer Knob
• Oxygen Mask Microphone Switch (Pilot)
• FADEC Reset Button
• Ice Protection Switches
• Gear Selector Knob
• Gear Horn Silence Button
• Anti-skid Switch
• Instrument and Exterior Lighting Controls
• Environmental Control Panel
• Oxygen Mask Microphone Switch (Copilot)
• ELT Switch
• Flight Hour Meter
• Oxygen Supply Cutoff Knob
September 2006
13
FIGURE III — CITATION MUSTANG INSTRUMENT PANEL AND PEDESTAL LAYOUT
1. Digital Audio Control Panel
2. Master Caution / Warning
Annunciators
3. Radio Call Placard
4. Left Engine Fire Warning and
Extinguisher Bottle Arm /
Discharge Button
5. Flight Director / Autopilot Mode Controller
6. Standby Electronic Airspeed Indicator
7. Standby Electronic Attitude Indicator
8. Standby Electronic Altimeter
9. Right Engine Fire Warning and Extinguisher
Bottle Arm / Discharge Button
10. Rotary Test Knob Panel
11. Primary Flight Displays (PFD) Left and Right
12. Multi-Function Display (MFD)
13. Oxygen Control Valve
14. LH Tilt Panel Including DC Power,
Avionics, Fuel, Engine Start, and Ice
Protection Switches
15. Landing Gear Panel
16. Lighting Panel
17. RH Tilt Panel Including Environmental and ELT
Switches
18. Flight Hour Meter
19. Oxygen Shutoff Knob
20. Oxygen Supply Pressure Indicator
21. Remote Flight Management System (FMS) / MFD
Control Keyboard
22. Rudder and Aileron Electric Trim Panel
10. FLIGHT COMPARTMENT, I N S T RUMENTATION AND AVIONICS
( C o n t i nued)
14
September 2006
E. Installed on Pedestal:
• Elevator Trim Control and Indicator
• Engine Power Levers with Speed Brake Controls and
Takeoff / Go-Around Buttons
• Flap Control Handle
• Engine Synchronizer Switch
• FMS / MFD Control Keyboard
• Rudder Trim Control
• Aileron Trim Control
• Emergency Gear Release and Blow-down Handle
F. Installed Beneath the Instrument Panel:
• Emergency Brake Handle
• Parking Brake Handle
10.3 Flight Compartment
Two complete crew stations are provided on the Mustang
with dual controls including panel-mounted control yokes,
rudder pedals, and toe-actuated brakes. The crew seats
are adjustable forward and aft, by height and recline, and
　
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