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发布时间:2023-12-25 22:49:21

[单选题]LANDING WEIGHT is equal to:
A. takeoff weight minus trip fuel
B. takeoff fuel minus trip fuel and holding fuel
C. zero fuel weight

更多"[单选题]LANDING WEIGHT is equal to:"的相关试题:

[单选题]Maximum landing weight of A320 is ____kg.
A.66000
B.64000
C.62500
[单选题]When landing gear and flaps not in landing configuration, with the excessive fall rates, the aural alert is:
A. A. “TERRAIN”
B. B. “DONT SINK”
C. C. “PULL UP”
[单选题]Landing gear down, and flaps not in landing configuration or, landing gear up, and flaps in landing configuration, the aural alert is:
A. A. “TOO LOW—TERRAIN”
B. B. “TOO LOW—GEAR”or“TOO LOW—FLAPS”
C. C. Both correct
[单选题]The actual landing distance is calculated based on the assumptions that:
A. the approach speed is VLS for a manual landing and VLS + 5 for an automatic landing.
B. Maximum manual braking is applied and antiskid and all ground spoilers operative.
C. Both of the above.
[单选题]In case of aircraft failure affecting landing distance occurs in the air, the required landing distance can be calculated by reference to
A. the FCOM or the MEL
B. the FCOM and the QRH
C. the MEL only
[单选题]After landing, will pressurization system automatically transfer?
A. No, another system must be chosen
B. Yes, it will immediately transfer at touchdown
C. Yes, after touching ground 70 seconds
[单选题]If the calculated RLD for automatic landing is longer than the RLD for manual landing, )
A. take this distance for automatic landing.
B. take the RLD for manual landing.
C. no automatic landing should be made.
[单选题]For damp runway, the required landing distance is how many times of that of a dry runway?
A.115%
B.135%
C. It depends on the specific runway.
[单选题]After landing on a contaminated runway, which stage is more probably to have the problem of directional control?
A. Low speeds
B. High speeds
C. Lift off or touchdown
[单选题]During landing and taxiing , air-conditioning unit inlet valve will be open when the speed is lower than:
A.77kt(after 30s delay)
B.70kt(after 3 minutes)
C.70kt(after 20s delay)
[单选题]The wind correction on landing distance for manual landing is
A. + 14% per 10 kt of tailwind, no correction for headwind.
B. that no correction is necessary due to automatic ground speed protection
C. + 10% per 10 kt of tailwind, - 5% for headwind
[单选题]Maximum speed with landing gear extended is ____kt.
A.320
B.250
C.280
[单选题]Any increase in landing distance, resulting from an emergency or abnormality, must be based on :
A. the Actual Landing Distance without Autobrake - CONF 2
B. the Actual Landing Distance without Autobrake - CONF 3
C. the Actual Landing Distance without Autobrake - CONF FULL
[单选题]Which hydraulic system is used for landing gear?
A. Green system
B. Blue system
C. Yellow system
[单选题]Maximum altitude at which the landing gear may be extended is ____ft.
A.15000
B.20000
C.25000
[单选题]The actual landing distance is the distance between
A. the point at 50 ft above runway threshold and the point where the aircraft come to a full stop
B. the touchdown point and the point where the aircraft come to a full stop
C. the decision altitude and the point where the aircraft come to a full stop
[单选题]If the difference between FMS landing strip centerline and actual landing strip centerline is ____, the managed approach speed shall not be used.
A. 30 degree
B. 50 degree
C. 70 degree

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