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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. |
At the back side of the drag curve the rate of change of drag is negative. |
A. | True |
B. | False |
Answer» B. False | |
2. |
By which of the methods the flight can be descended? |
A. | nose down pitch |
B. | nose uppitch |
C. | nose down and elevator |
D. | elevator and nose up |
Answer» C. nose down and elevator | |
3. |
The flight path gradient of descent can be increased by increasing airspeed. |
A. | True |
B. | False |
Answer» B. False | |
4. |
The flight path can be controlled by the use of __________ |
A. | elevator |
B. | rudder |
C. | flaps |
D. | slats |
Answer» B. rudder | |
5. |
The flight path is unstable during __________ |
A. | the aircraft flying at airspeed less than minimum drag speed |
B. | the aircraft flying at airspeed more than minimum drag speed |
C. | the aircraft flying at airspeed less than maximum drag speed |
D. | the aircraft flying at airspeed more than maximum drag speed |
Answer» B. the aircraft flying at airspeed more than minimum drag speed | |
6. |
At which cases does descent of flow occur? |
A. | By flying the aircraft at airspeed less than minimum drag speed |
B. | By flying the aircraft at airspeed more than minimum drag speed |
C. | By flying the aircraft at airspeed less than maximum drag speed |
D. | By flying the aircraft at airspeed more than maximum drag speed |
Answer» B. By flying the aircraft at airspeed more than minimum drag speed | |
7. |
In the case of gliders, the descent is calculated by lift-drag ratio. |
A. | True |
B. | False |
Answer» B. False | |
8. |
What are the factors for that increase the drag in an aircraft? |
A. | Varying airspeed |
B. | Constant airspeed |
C. | Varying thrust |
D. | Varying fuel ratio |
Answer» B. Constant airspeed | |
9. |
There are two ways of aircraft descend of an aircraft. |
A. | True |
B. | False |
Answer» B. False | |
10. |
In what proportion should the propulsive thrust be so that the aircraft will decelerate? |
A. | Thrust is less than airframe drag |
B. | Thrust is more than airframe drag |
C. | Greater airspeed |
D. | Less airspeed |
Answer» B. Thrust is more than airframe drag | |