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d. R GEN Switch . . . . . . GEN (Check generators parallel and battery voltage 28 Volts.)
e. BATT Switch. . . . OFF (Check L AMP and R AMP decrease, battery voltage 0 Volts.)
f. BATT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . BATT (Check battery voltage 28 Volts.)
3-144 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
COCKPIT PREPARATION (Continued)
8. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMER
9. DISPLAY BACKUP Button (pilot audio panel) . . . . . . . . . . . PRESS; CHECK POWER TO
EMERGENCY BUS ITEMS; PRESS AGAIN
NOTE
When EMER is selected with the engines not running, EICAS indications for N1, N2,
and ITT will be inoperative (red “X”) because no power to the FADEC is available from
the engine-driven permanent magnet alternator (PMA).
10. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
11. STBY INST Amber Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
12. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
13. LANDING GEAR Position Lights . . . . . . . . . . . THREE GREEN LIGHTS / NO RED LIGHT
14. Cockpit Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
15. AVN PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
16. Database/Chart Currency . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
17. Rotary TEST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WARNING SYSTEMS CHECK
NOTE
The Warning Systems Rotary Test Switch must be cycled through each position to
make sure that all systems are functioning properly.
18. Oxygen System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Oxygen Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1600 to 1800 PSI
b. L and R MIC Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OXYGEN MASK
c. Pilot and Copilot Masks . . . . . . . TEST / 100% / AUDIBLE IN SPEAKER / STOWED
d. L and R MIC Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HEADSET
e. Smoke Goggles (if installed). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED
19. Fuel Quantity and Balance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
20. Pilot, Passenger, Cargo, and Fuel Weights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENTER
(MFD AUX-WEIGHT PLANNING Page)
21. ATIS/Clearance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
22. Avionics Flight Plan (if desired). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENTER
23. AVN PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (for GPU start)
OFF (for battery start)
24. Wing/Stab Deice System (if required). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. WING/STAB Deice Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HOLD in MANUAL
b. Verify WING DE-ICE FAIL and TAIL DE-ICE FAIL messages display after 6 seconds.
c. WING/STAB Deice Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d. Pitot-Static Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . RESET STALL WARN then OFF
DELAY BEFORE FLIGHT WITHOUT GPU
1. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
510FM-07 AK 3-143.1
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
BEFORE STARTING ENGINES
1. If delayed before flight without GPU:
a. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY INST
b. BATT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
2. Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
3. Wheel Chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVED
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(96)