Explore topic-wise MCQs in Aircraft Performance.

This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Performance knowledge and support exam preparation. Choose a topic below to get started.

1.

The effect of TAS on airborne distance is half that of the ideal case.

A. True
B. False
Answer» B. False
Discussion
2.

The ground run distance is effected by the inverse of the density and directly proportional to square of the true airspeed.

A. True
B. False
Answer» B. False
Discussion
3.

Which of the following will not effect the ground run distance?

A. TAS
B. EAS
C. Weight
D. Thrust
Answer» E.
Discussion
4.

There is no effect of runway conditions on the airborne distance.

A. True
B. False
Answer» B. False
Discussion
5.

The headwind only effects in the kinematic energy in the case of the airborne distance.

A. True
B. False
Answer» B. False
Discussion
6.

What is the use of the headwind?

A. To change the datum height
B. To change the datum temperature
C. To change the fuel ratio
D. To change the pressure ratio
Answer» B. To change the datum temperature
Discussion
7.

The increase in aircraft weight by 10% will result in increase in aircraft ground run distance by 20%.

A. True
B. False
Answer» B. False
Discussion
8.

Which of the following is the correct formula of airborne distance with respect to aircraft weight?

A. S<sub>A</sub>= ( frac{W}{(F_N-D)_{av}} Big { frac{V_{2}^2+V_{LOF}^2}{2g}+35 Big } )
B. S<sub>A</sub>= ( frac{W}{(F_N+D)_{av}} Big { frac{V_{2}^2+V_{LOF}^2}{2g}+35 Big } )
C. S<sub>A</sub>= ( frac{W}{(F_N+D)_{av}} Big { frac{V_{2}^2-V_{LOF}^2}{2g}+35 Big } )
D. S<sub>A</sub>= ( frac{W}{(F_N-D)_{av}} Big { frac{V_{2}^2-V_{LOF}^2}{2g}+35 Big } )
Answer» E.
Discussion
9.

Which of the following is the correct formula of ground run distance with respect to aircraft weight?

A. S<sub>G</sub>= ( frac{WV_{LOF}^2}{2g[F_N+D+ mu (W-L)]_{0.7V_{LOF}^2}} )
B. S<sub>G</sub>= ( frac{WV_{LOF}^2}{2g[F_N-D+ mu (W-L)]_{0.7V_{LOF}^2}} )
C. S<sub>G</sub>= ( frac{WV_{LOF}^2}{2g[F_N+D- mu (W-L)]_{0.7V_{LOF}^2}} )
D. S<sub>G</sub>= ( frac{WV_{LOF}^2}{2g[F_N-D- mu (W-L)]_{0.7V_{LOF}^2}} )
Answer» E.
Discussion
10.

There are two atmospheric effects on the take-off distances.

A. True
B. False
Answer» B. False
Discussion