A、EIU takes its power from the engine generator.
B、EIU fails and engine restart is not possible.
C、The ECU & Ignition powers are no longer available.
答案：B
A、EIU takes its power from the engine generator.
B、EIU fails and engine restart is not possible.
C、The ECU & Ignition powers are no longer available.
答案：B
A. Rudder trim actuator.
B. Rudder trim and yaw damper actuators.
C. Yaw damper actuators.
A. Only the LAST LEG ECAM REPORT.
B. The LAST LEG ECAM REPORT and the LAST LEG REPORT.
C. Only the LAST LEG REPORT.
A. By depressurizing the hydraulic system and using the maintenance unlocking device.
B. By pressing the SEC p/b on the flight control panel.
C. By using the maintenance unlocking device with the actuator pressurized and SEC p/b operated.
A. In flight with two IDG supply.
B. ON ground with APU supply only.
C. ON ground with EXT PWR only.
A. AC BUS 1 or AC BUS 2.
B. AC BUS 1 and AC BUS 2.
C. AC ESS BUS or EMERGENCY GENERATOR.
A. A red square.
B. A red circle.
C. A white filled diamond shape.
A. Switch over to the other channel.
B. Control goes to a fail-safe position.
C. The channel in control supplies the winding of the other channel.
A. Set AIR DATA switch to F/03 position.
B. Set ATT HDG switch to F/03 position.
C. Leave ATT HDG switch in NORM position.
A. One
B. Two
C. Three.
A. To compare the data recorded by the SSFDR with the data sent by the FDIU.
B. To compare the data recorded by the QAR with the data sent by the FDIU.
C. A & B.
