A、By setting the leak measurement valve to OFF and operating the electric pump
B、By pressurizing the yellow system by using the PTU.
C、By setting the leak measurement valve to OFF, and manually open the LH wing spool valve.
答案：C
A、By setting the leak measurement valve to OFF and operating the electric pump
B、By pressurizing the yellow system by using the PTU.
C、By setting the leak measurement valve to OFF, and manually open the LH wing spool valve.
答案：C
A. FMGC 1
B. FMGC 2
C. Either FMGC 1 or FMGC 2, independently of AP, FD, and A/THR engagement status.
A. By visual warning on one ACP.
B. By visual warning on all the ACPS and an aural buzzer.
C. By visual warning on all the ACPS.
A. It＇s to avoid lighting.
B. It＇s to discharge static electricity.
C. It＇s to control the electricity charged on the aircraft.
A. The Thrust Lever Angle.
B. The N1 limit.
C. The N1 target.
A. Its consequences on other systems.影响其他系统
B. Its absence of consequences on other systems.它没有对其他系统造成影响
C. Associated attention getters not activated.
A. The three other door are deployed.
B. The other latches are hyd. relocked.
C. Thrust reverse is unavailable.
A. 4 inputs.
B. 2 input.
C. It depends on the selected Weather Radar Transceiver.取决于气象雷达的接收端
A. The failed WHC connects to the other.
B. Both systems are lost.
C. The heating of the related side is lost.
A. Three shock absorbers extended.三个减震器扩展
B. Three shock absorbers compressed.三个减震器压缩。
C. Only one shock absorber extended.
A. The pointer symbol and the ADF1 flag appear in RED.
B. The ground station characteristics pointer disappear and the RED ADF1 flag appears.
C. No ADF1 indications on ND.
