A: CL(squared) and AR (aspect ratio).

B: CL and CD.

C: CL and b (wing span).

D: CL(squared)and S (wing surface).

Answer: A

A: CL(squared) and AR (aspect ratio).

B: CL and CD.

C: CL and b (wing span).

D: CL(squared)and S (wing surface).

Answer: A

A: decreases when the altitude increases.

B: increases when the altitude increases.

C: is constant whatever the altitude.

D: is 100%.

Answer: B

A: jet pipe pressure to combustion chamber pressure.

B: jet pipe pressure to compressor inlet pressure.

C: combustion chamber pressure to compressor inlet pressure.

D: compressor outlet pressure to compressor inlet pressure.

Answer: B

A: Flaps from 30(degrees) to 45(degrees).

B: The slats.

C: Flaps from 0(degrees) to 15(degrees).

D: Flaps from 15(degrees) to 30(degrees).

Answer: A

A: is the point where Drag coefficient is a minimum.

B: is the point where the Lift to Drag ratio is a maximum.

C: is the point where the Lift to Drag ratio is a minimum.

D: is the maximum drag speed.

Answer: B

A: 110

B: 11

C: 1100

D: 11000

Answer: C

A: A tailwind component increases the ground distance.

B: A headwind component increases the ground distance.

C: A tailwind component increases fuel and time to descent.

D: A tailwind component increases the time in the descent

Answer: A