更多"[单选题]When landing gear and flaps no"的相关试题:
[单选题]When landing gear and flaps not in landing configuration, and aircraft not on the glideslope beam, the aural alert is:
A. A. “TOO LOW FLAPS”
B. B. “DONT SINK”
C. C. “TERRAIN”“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]When failed to open the main landing gear door, and "L/G GEAR NOT DOWNLOCKED" warning alarms, which of the following operation is wrong?
A.Crew must perform a complete landing gear recycle program, i.e. choose the landing gear lever to the UP position, then wait 60 seconds, and then select the landing gear lever to the DOWN position.
B.Before executing the L/G GRAVITY EXTENSION procedure, complete execution of landing gear recycle program must be done 5 times if needed.
C.If failed after 5 cycles, need to wait for 120s before executing L/G GRAVITY EXTENSION procedure.
D.Before the next attempt to start landing gear cycle process, crew must wait for 60s after landing gear lever in DOWN position.
[单选题]Maximum speed with landing gear extended is ____kt.
A.320
B.250
C.280
[单选题]Maximum altitude at which the landing gear may be extended is ____ft.
A.15000
B.20000
C.25000
[单选题]Maximum speed at which the landing gear may be retracted is ____kt.
A.220
B.250
C.280
[单选题]Maximum flight altitude when flaps/slats extended is:
A. 15000ft
B. 18000ft
C. 20000ft
[单选题]When slats and flaps extended & slats extended and flaps retracted. the flight maneuvering load acceleration limits is:
A. 0 g to 2.5 g
B. 1 g to 2.5 g
C. 0 g to 2 g
[单选题]When landing gears are selected to extend, which system page will be displayed on ECAM？
A. WHEEL
B. CRUISE
C. F/CTL
[单选题]Which requirement below should be met when conducting a stabilized approach?
A.The rate of descent must less than 1500 ft/min above AGL 1000 ft
B.Stabilized thrust (usually above idle), glide slope established, maintain a target approach speed
C.glide slope established above AGL 500 feet
[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
[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]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]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]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
