A、By the 28 VDC NORM BUS.
B、By the 115 VAC NORM BUS.
C、By ±12 VDC through the ADF Receiver.
答案：C
A、By the 28 VDC NORM BUS.
B、By the 115 VAC NORM BUS.
C、By ±12 VDC through the ADF Receiver.
答案：C
A. The distance from the engine.
B. The distance from the engine, the power setting and the time exposure.
C. The distance from the engine and the power setting.
A. The funtion that integrates the routes the aircraft must follow and the constraints to construct a flight plan.
B. The function that provides the aircraft position and the follow-up the flight plan.
C. The ratio of cost of time to the cost of fuel.
A. The NAVigation mode remains active and the FPA mode engages.
B. The track and FPA mode engage.
C. There is no effect.
A. By the HP rotor.
B. By the LP rotor.
C. By the HP rotor via the transfer gearbox.
A. When the circuit operates in open circuit configuration
B. In closed circuit configuration when the skin temperature is below 11＇C(51.8＇F)(skin temp.increasing).
C. In close circuit configuration when the skin temperature is above 11＇C(51.8＇F)(skin temp.increasing).
A. ± 6 degrees.
B. ± 74 degrees.
C. ± 95 degrees.
A. Yes.
B. No.
A. RMP 1.
B. RMP 1 and RMP 2.
C. RMP 1,RMP 2 and RMP 3.
A. GEN 1 supplies AC BUS 1 and GEN 2 supplies AC BUS 2.
B. APU GEN or EXT PWR or one GEN supplies AC BUS 1 and AC BUS 2.
C. APU GEN supplies AC BUS 1 and EXT PWR supplies AC BUS 2.
A. The APU shuts down after a cooling cycle has been completed.
B. The APU shuts down immediately.
C. The APU shuts down after the closure of fuel LP shut off valve.
