What is displayed on the status page ?

A. THE EIU

B. The Thrust Lever Angle.

C. The engine thrust rating.

A. APU generator is de-energized.

B. APU generator is disconnected.

C. APU generator is energized.

A. The RAM Air Turbine (RAT) is extended.

B. The emergency generator comes on line.

C. The RAT is extended and the emergency gennerator comes on line.

A. Center tank pump start.

B. Center tank pump stop.

C. Center tank pump stay as they are.

A. To centralize all the audio signals and the frequencies of the communication systems.

B. To act as an interface between the users and the various radio communication and radio navigation systems.

C. To receive audio signals only.

A. When aircraft on ground, ELEC PUMP pb in AUTO position and OVRD (override) pushbutton is set to ON.

B. When G & Y system are detected in low pressure configuration.

C. As soon as one engine is running and OVRD pushbutton is set to "ON".

A. In the cutouts of the ceiling panels.

B. In the fixed partition walls.

C. In the cutouts of the ceiling panels and lateral right sidewall linings.

A. To the top line data bus.

B. To the mid line data bus.

C. To an ARINC 429 data link.

A. On the PERF page.

B. On INIT page A.

C. On INIT page B.

A. As soon as the GEN 1 LINE pushbutton is released out.

B. When any GEN 1 parameter is not correct.

C. When any GEN 1 parameter is not correct and the GEN 1 pushbutton is released out.