更多"[单选题]During approach, flight augmen"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]DIM. BRIGHT should be on during flight preparation because:
A. It can provide lighting.
B. It is the only lighting source in the EMER ELEC configuration.
C. According to the need of crew
[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]There is predictive windshear during approach, crew should:
A. Select the most favorable runway, or delay for landing or divert
B. Use managed speed, select FLAPS 3
C. Both correct
[单选题]During final approach, the PNF calls out, if:
A. The speed becomes less than the speed target ?5 kt , or greater than the speed target +10 kt, or the descent rate becomes greater than 1 000 ft/min
B. The pitch attitude becomes less than ?2.5 °, or greater than 10 ° nose up
C. Both correct
[单选题]If flight crew select ILS approach on MCDU, ILS message will be displayed on ND when the along track distance to destination is less than _____ nm
A.180
B.200
C.250
[单选题]The function of Flight Warning Computer (FWC) is to:
A. generate alert messages, memos, aural alerts, and synthetic voice messages
B. acquire data, then generate signals, and sent the signals to the 3 DMCS (Display Management Computer), which use them to generate displays of system pages and engine parameters\
C. obtain and process data from the different sensors and computers, generate images and display on PFD, ND, E/WD and SD
[单选题]If FWC 1(Flight Warning Computer) fails,
A. manually replace FWC 1 with FWC 2
B. half of the warnings in Display Management Computer (DMC) will be lost
C. FWC2 will automatically replace FWC1
[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]Fake terrain warning alarms when approach on some airports/runways, if the visual contact does not established, the crew should_.
A.go around
B.ignores it, and continues approach because it is a fake warning.
[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]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]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
