A: V2 has no connection with T/O flap setting, as it is a function of runway length only.
B: V2 has the same value in both cases.
C: V2 increases in proportion to the angle at which the flaps are set.
D: V2 decreases if not restricted by VMCA.
A: no pitching moment.
B: a nose-up pitching moment.
C: a nose-down pitching moment.
D: a force which reduces drag.
A: flaps and elevator.
B: ailerons and elevator.
C: flaps and speed brakes.
D: ailerons and flaps.
A: leading edge.
B: trailing edge.
C: trailing edge close to the wing root.
D: trailing edge close to the wing tip .
A: The flaps from 30(degrees) to 45(degrees).
B: The slats from the retracted to the take-off position.
C: The flaps from 0(degrees) to 15(degrees).
D: The flaps from 15(degrees) to 30(degrees).