A、An engine control box.
B、The ECU and its peripheral sensors and components.
C、A thrust control unit.
答案:B
A、An engine control box.
B、The ECU and its peripheral sensors and components.
C、A thrust control unit.
答案:B
A. 60°.
B. 55°to the Equator.
C. 45°to the Equator.
A. On ground during take-off.
B. On ground during landing.
C. On ground during take-off and landing.
A. Its consequences on other systems.
B. Its absence of consequences on other systems.
C. Associated attention getters not activated.
A. Yes.
B. No.
A. Yes.
B. No.
A. RA 2 provides data to the GPWC.
B. FMGC 1 provides data to the GPWC.
C. The GPWC no longer receivs Radio Altitude.
A. Yes,from the opposite FMGC.
B. Yes,from the opposite FMGC, but after switching.
C. No,the VOR 2 cannot be tuned.
A. Six vertical-load and four side-load rollers.
B. Four vertical-load and two side-load rollers.
C. Two vertical-load and four side-load rollers.
A. Compressor, combustion chamber, turbine.
B. Power section,load compressor, Fuel Control Unit.
C. Power section,load compressor, drive accessory gear box.
A. SDAC
B. FWC
C. DMC