How is the accessory gearbox driven ?

A. One main frame computer for all engines.

B. The ECU and its peripherals, per engine.

C. A signle ECU and its peripherals, for both engines.

A. Rotary selector set in IGN START or CRANK positions.

B. MASTER LEVER set in NO position.

C. Both rotary selector set in IGN START or CRANK positions and the MASTER lever set in ON position.

A. 41 736 lbs (18932 kg),

B. 45 920 lbs (20872 kg),

C. 52 174 lbs (23715 kg),

A. ENGINE REPORT ON REQUEST <05> and ENGINE RUN UP REPORT <11>.

B. ENGINE REPORT ON REQUEST <05> and LOAD REPORT <15>.

C. All.

A. SMOKE light comes on + Continuous Repetitve Chime + MASTER WARNING + ECAM Message.

B. The CIDS duplicates the cargo smoke waring to the cabin.

C. Lights come on.

A. AC ESS BUS, DC ESS BUS and AC STATIC INVERTER BUS are supplied.

B. DC ESS BUS,AC STATIC INVERTER BUS and DC BAT BUS are supplied.

C. AC ESS BUS, AC STATIC INVERTER BUS and DC BAT BUS are supplied.

A. To produce independent pneumatic and hydraulic power.

B. To produce independent pneumatic and electrical power.

C. To produce independent electrical and hydraulic power.

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. Yes, by making any new selection with the control lever.

B. Yes, by making a reverse selection with the control lever.

C. No, reset is possible on ground only.

A. Refueling busbars supplied by service bus 601PP.

B. Refueling busbars supplied by hot bus 701PP

C. Both configurations.