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发布时间:2024-05-18 18:47:48

[单选题]TAKEOFF WEIGHT is:
A. zero fuel weight + takeoff fuel
B. OEW + takeoff fuel
C. OEW + takeoff fuel + payload.

更多"[单选题]TAKEOFF WEIGHT is:"的相关试题:

[单选题]Correct the determined maximum takeoff weight on dry runway to
A. take into account QRH and bleed effects, then apply the corrections for contaminants.
B. apply the corrections for contaminants, then take into account QRH and bleed effects.
C. No need to consider the QRH effect. But the bleed effects should be considered.
[单选题]The maximum takeoff weight and associated speeds may be affected by the following conditions:
A. OAT, wind, QNH
B. OAT, wind, QNH, visibility
C. OAT, wind, QNE
[单选题]In some cases when the actual takeoff weight is lower than the maximum permissible one but no flexible takeoff possible, how to determine the speeds?
A. You can retain the speeds that have been calculated for the maximum permissible takeoff weight;
B. You can retain the speeds associated with the actual takeoff weight provided they are all lower than the speeds calculated for the maximum permissible takeoff weight.
C. You can use either of the above methods.
[单选题]If the actual takeoff weight is lower than the lowest weight value of a takeoff weight column,
A. use extrapolation
B. Do not takeoff because the speeds cannot be determined.
C. use full thrust for takeoff
[单选题]If the V1 for the actual takeoff weight on a wet runway is lower than the minimum V1:
A. the associated takeoff performance such as the maximum takeoff weight must be corrected.
B. take the minimum V1. No correction is necessary.
C. It is impossible to happen.
[单选题]Maximum takeoff weight of A320 is ____kg.
A.75900
B.75500
C.72500
[单选题]When takeoff mode engages:
A. autothrust engages automatically and be active
B. autothrust engages automatically but be inactive
C. autothrust does not engage automatically and the engine is controlled by thrust levers
[单选题]Maximum brake temperature for takeoff is:
A. 650℃
B. 450℃
C. 300℃
[单选题]SRS cannot be engaged during takeoff if there’s no _____. (A)
A. V2
B. V1
C. VR
[单选题]Takeoff charts can be presented in two different ways which are:
A. temperature entry and weight entry
B. speed entry and weight entry
C. temperature entry and speed entry
[单选题]The main purpose of using flexible takeoff thrust is to
A. save engine life.
B. provide a safer takeoff due to increased takeoff roll time and reduced difficulty in controlling during engine failure when takeoff with full thrust.
C. reduce engine noise and improve passenger comfort.
[单选题]When check hydraulic after takeoff, the green system fuel quantity less than that on ground, the reason is:
A. Hydraulic contract due to quenching
B. Green hydraulic has been used
C. Leakage of hydraulic
[单选题]If windshear is expected along the takeoff path, it is recommended to
A. use maximum thrust
B. use flexible thrust
C. maintain thrust and increase V2
[单选题]During takeoff, the final normal pitch attitude is ____ °
A.10
B.15
C.17.5
[单选题]It is possible to determine the takeoff performance for an airport without any published takeoff charts?
A. Yes, it is possible but quite conservative.
B. Yes, as long as the calculations are correct, the result is very accurate.
C. No, it is impossible.
[单选题]The aircraft is ready for takeoff on the runway centerline. If heading 233° needs to be armed:
A. pulling out heading knob to disengage navigation mode arming, adjusting to 233°and pushing to engage
B. switching heading knob, adjusting to 233°and pulling out when ATC allows to 233°
C. switching heading knob, adjusting to 233°and pulling out to engage
[单选题]HDG/TRK preset is available before takeoff and up to ____ ft.
A.30
B.40
C.50
[单选题]If the takeoff must be aborted, the autobrake system applies maximum braking as soon as the thrust levers are set to idle, if the ground speed is above ____ kt.
A.60
B.72
C.80
[单选题]NOSE sw turns the taxi and takeoff lights on and off, when landing gear is retracted:
A. Turns on both taxi and takeoff lights
B. Turns on only taxi light
C. Go off automatically

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