How can a thermal discharge of the bottle be detected on a cold aircraft?

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. Engine running.

B. Engine running above 60% of N1.

C. Engine running above minimum idle.

A. Permanently.

B. When on batteries only.

C. When one engine generator fails.

A. 50 % RPM.

B. 40 % RPM.

C. 95 % RPM.

A. TLA position + Aircraft on ground.

B. TLA position + Aircraft on ground
+ Reverse indication green.

C. TLA position + Aircraft on ground
+ N2 (engine running).

A. Inhibit the windshear function.

B. Inhibit aural alerts generated by TCAS or GPWS or other FWC warnings.

C. Transmit the aural alert to the Audio Mixing Box.

A. The Glide/Slope mode is inhibited.

B. Only Glide/slope mode is valid.

C. The self test sequence is initiated.

A. When the VOR is tuned from the MCDU.

B. When the VOR is tuned from the RMP.

C. When a failure occurs.

A. Yes

B. No

A. IDG de-energized.

B. IDG disconnected.

C. IDG energized.