How is the operator warned, when there is a residual pressure in the cabin?

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. CAPT dome light and RH CENTER lighting instrument panel.

B. F/O dome light and LH CENTER lighting instrument panel.

C. F/O dome light and F/O and RH CENTER lighting instrument panel.

A. Warning are inhibited.

B. The status page is displayed.

C. The warning are recalled.

A. A blue band and number 1.

B. A blue band and number 3.

C. A blue band and number 2.

A. Armed modes.

B. Active modes

C. Engagement status.

A. The Glide/Slope mode is inhibited.

B. Only Glide/slope mode is valid.

C. The self test sequence is initiated.

A. On the torque shafts.

B. On the actuators.

C. On the PCU output shaft.

A. On the ECAM OIL page, or on a sight glass on the oil cooler,or by CFDS interrogation.

B. On the ECAM OIL page, or on a sight glass on the accessor gearbox, or by CFDS interrogation.

C. Only by CFDS interrogation and on the ECAM ENGINE/WARNING page.

A. The Glide/Slope index disappears.

B. A red "G/S" symbol appears in the middle of the scale.

C. The Glide/Slope index and the scale flash permanently.

A. The bleed temperature sensor

B. The compressor overheat sensor

C. The compressor pneumatic overheat sensor