更多"[单选题]DIM. BRIGHT should be on durin"的相关试题:
[单选题]During flight, no clutter displayed on ND and no fault message, but there are obvious weather phenomenons, the possible reason is:
A. A. GAIN knob at Minimum position;
B. B. ND radar display brightness control at minimum position;
C. C. Both correct
[单选题]During flight, when CTR runs out, if the aircraft is affected by low-pressure caution on CTR Pump, how to dispose:
A. select automatic fuel mode +CTR Pump 1+2 close
B. select manual fuel mode+ CTR Pump 1+2 open
C. select manual fuel mode+ CTR Pump 1+2 close
[单选题]During flight, if CTR is with fuel, select automatic refueling mode, what will take place when slat extends?
A. CTR Pump open
B. CTR Pump close
C. CTR Pump keeps at original mode
[单选题]During normal flight, when skin temperature is lower than +35 ℃， ventilation system of avionics bay control and cool the air temperature, the method is：
A. to increase the air which is from cockpit
B. to let air pass skin heat exchanger
C. to extract air outside
[单选题]During approach, flight augmentation computer calculates the speed tendency and the minimum selectable speed (VLS). The tendency limit or VLS indicates the speed the aircraft will reach in the future 10 seconds and _____ times of VS1g under any configuration.
A.1.13
B.1.23
C.1.33
[单选题]When encounter windshear, flight crew should inform ATC ASAP, reporting information should contain.
A.the increment/reduction of height and of speed when encounter windshear
B.number of passengers
C.Aircraft weight and fuel quantity
[单选题]During the future examinations you should avoid ________ such mistakes.
A.make
B.to make
C.making
D.made
[单选题]During fast alignment, MODE sel should be change from OFF to NAV in ____.
A. A. 3s
B. B. 5s
C. C. 7s
[单选题]During the oxygen mask test, crew should first____:
A. Confirm that INT/RAD sw at RAD position
B. LOUDSPEAKERS on the glareshield at ON position
C. CREW SUPPLY pb on the OXYGEN panel white light comes on
[单选题]When should the pilot set a QNE during take-off climb phase?
A.When getting the instruction from the controller
B.Reaching the transition level
C.Reaching 10,000 feet
[单选题]Flight maneuvering load acceleration limits on clean configuration is:
A. –1 g to 2.5 g
B. - 1 g to 2 g
C. 0 g to 2.5 g
[单选题]Critical flight phases refer to:
A.cruise flight phase
B.climb & descent operation phase
C.phases including taxiing, takeoff, landing, and all flight operations carried out bellow 3000 meters (10,000 feet) except cruise flight
[单选题]When is the flight plan optimized?
A. only after flight crew revise it
B. anytime when flight crew change the altitude or engine thrust
C. it is continuously updated according to the environment and aircraft weight
[单选题]The vertical waypoint of the vertical flight path refers to :
A. the point in navigation database with fixed geographic position
B. the point imposed by ATC
C. the point without fixed geographic position but affected by atmospheric point
[单选题]The establishment of flight plan uses:
A. information from navigation database
B. information from performance database
C. information from navigation database and performance database
[单选题]In managed descent profile, the flight guidance part of FMGC gives partial priority to ____
A. thrust grade
B. target speed/mach number
C. descent track
[单选题]How can the flight crew determine DU failure besides the blank screen with an “F” letter in amber？
A. a distorted display
B. a blank screen with the“INVALID DISPLAY UNIT” message in amber
C. both of the above
[单选题]If the flight crew performs an automatic approach without autoland, the autopilot must be disengaged no later than at ____.
A. 80ft AGL
B. 100ft AGL
C. 160ft AGL
[单选题]In flight, when the autothust disconnect button is pressed for more than seconds, the autothrust function and alpha-floor protection are lost.
A.5
B.10
C.15
