曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

5. Land as soon as practical.
PROCEDURE COMPLETED
• IF BOTH GENERATORS COME ON LINE
PROCEDURE COMPLETED
(Continued Next Page)
3-36 AL 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
 DUAL GENERATOR FAILURE
(RED GEN OFF L-R CAS MESSAGE)
6. DISPLAY BACKUP Button (pilot audio panel) . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
7. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9. Exit icing environment if required.
10. Land as soon as possible (within 30 minutes). Refer to BEFORE LANDING, this
procedure.
WARNING
With the battery switch in EMER, wing and tail deice systems will be
inoperative. Avoid entering or exit icing conditions as required. STALL
WARNING-HIGH landing data is provided and must be used in the event
any ice remains on the wings and/or tail during approach and landing.
With the battery switch in EMER position and the generators OFF, power is supplied for at
least 30 minutes to the following equipment:
(Continued Next Page)
1. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET THEN OFF
2. Generator Voltages. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
NOTE
If generator voltage is significantly below or above 28 volts, the Generator Control
Unit (GCU) will not allow that generator to remain on line.
3. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
• IF NEITHER GENERATOR COMES ON LINE
4. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
5. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RAPIDLY SELECT EMER
• PFD 1 - Reversion Mode
• COM 1
• NAV 1 including Marker Beacon
• GPS 1
• ADC 1
• AHRS 1
• Transponder 1 (XPDR 1)
• Pilot’s and Copilot’s Audio Panels
• L and R N1, N2, and ITT Indications
• L Oil Temperature
• L Fuel Flow
• Fuel Temperature
• Battery Voltage Indication
• Autopilot Control Panel (HDG, CRS, ALT
knobs only)
• Cabin Altitude and Differential Pressure
Indications
• Cabin Dump System
• Cockpit Flood Light
• Pilot’s Pitot-Static Heat
• Landing Gear Indicator Lights
• Avionics Audio Warnings
• Standby Instruments (Airspeed, Altitude,
Attitude)
• Magnetic Compass Lighting
• ELT GPS Position Interface
510FM-07 AM 3-35.1
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
 DUAL GENERATOR FAILURE
(RED GEN OFF L-R CAS MESSAGE) (Continued)
NOTE
• With no generator online and the BATT switch in EMER, the battery will supply DC
power to the emergency bus equipment for approximately 30 minutes, provided
EMER is selected within 1 minute after failure of the second generator.
• The battery switch must be moved from BATT to EMER within 1 second to
maintain adequate avionics power. If the switch is moved slowly, the PFD, AHRS,
ADC, and other devices may need to re-initialize.
• ENG CTRL SYS L-R message will display due to loss of normal aircraft DC power
to the FADEC’s. Engine operation will not be degraded and no pilot action is
required.
• Flap system will be inoperative. Plan to land with the flap position set when EMER
selected.
• Normal gear extend will be inoperative. Plan to use emergency extension and
blow-down.
• Power brakes and antiskid will be inoperative. Plan to use emergency brake
system for landing.
• Exterior lighting will be inoperative.
• Windshield anti-ice and defog will be inoperative.
• Master Warning and Master Caution lights will be inoperative. However, the pressto-
reset function will still work to acknowledge flashing EICAS messages.
• Avionics audio warnings including Altitude Alert, Decision Height (BARO only),
Marker Beacon, TAWS, and Vertical Track will be functional. Aircraft generated
tones including Overspeed, Landing Gear, and Stall Warning will be inoperative.
• The AP button on the autopilot control panel may be pressed two times to cancel
the autopilot disconnect tone if required.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 1(42)