MCQOPTIONS
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MCQOPTIONS
This section includes 15 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. |
During the flight of the aircraft with minimum unstick speed the tail of aircraft is in contact with the runway. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 2. |
What is meant by minimum unstick speed? |
| A. | The maximum speed at which the aircraft becomes airborne |
| B. | The minimum speed at which the aircraft does not becomes airborne |
| C. | The maximum speed at which the aircraft does not becomes airborne |
| D. | The minimum speed at which the aircraft becomes airborne |
| Answer» E. | |
| 3. |
The total take-off distance is the sum of both airborne distance and ground run distance. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 4. |
What is meant by airborne distance? |
| A. | The distance between take-off point and the point at which the screen height is cleared |
| B. | The distance between lift-off point and the point at which the screen height is not cleared |
| C. | The distance between lift-off point and the point at which the screen height is cleared |
| D. | The distance between take-off point and the point at which the screen height is not cleared |
| Answer» D. The distance between take-off point and the point at which the screen height is not cleared | |
| 5. |
Transition is known as the phase where both the safe climb gradient and directional control in the climb can be attained during the failure of an engine. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 6. |
What is meant by decision speed? |
| A. | The speed at the point where there is unequal distances on the take-off run |
| B. | The slope at the point where there is unequal distances on the take-off run |
| C. | The slope at the point where there is equal distances on the take-off run |
| D. | The speed at the point where there is equal distances on the take-off run |
| Answer» E. | |
| 7. |
What is meant by take-off safety speed? |
| A. | Airspeed at which only the safe climb gradient is attained |
| B. | Airspeed at which only the directional control is attained |
| C. | Airspeed at which only the directional control is kept constant |
| D. | Airspeed at which both the safe climb gradient and directional control is attained |
| Answer» E. | |
| 8. |
What is the use of minimum control speed airborne? |
| A. | Maintain directional control |
| B. | Maintain fuel ratio |
| C. | Maintain constant thrust |
| D. | Maintain constant power |
| Answer» B. Maintain fuel ratio | |
| 9. |
There are two parts of take-off distance. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 10. |
What is meant by ground run distance? |
| A. | The distance where the aircraft takes-off on the ground |
| B. | The vertical distance where the aircraft takes-off on the ground |
| C. | It is also known as the screen height |
| D. | It is the landing distance of the aircraft |
| Answer» B. The vertical distance where the aircraft takes-off on the ground | |
| 11. |
The rotation speed must allow the aircraft to rotate into lift-off attitude. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 12. |
What is the screen height during the take-off of an aircraft? |
| A. | 40 ft |
| B. | 14 ft |
| C. | 30 ft |
| D. | 35 ft |
| Answer» E. | |
| 13. |
Just before reaching the lift-off speed the aircraft is rotated into a nose-up altitude which is equal to the lift-off angle of attack. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 14. |
What is lift-off speed? |
| A. | The speed at which the aircraft generates enough power to become airborne |
| B. | The speed at which the aircraft generates enough speed to become airborne |
| C. | The speed at which the aircraft generates enough thrust to become airborne |
| D. | The speed at which the aircraft generates enough lift to become airborne |
| Answer» E. | |
| 15. |
What is meant by minimum control speed ground? |
| A. | The airspeed below which the rudder the will not be capable of producing a yawing moment |
| B. | The airspeed below which the rudder the will not be capable of producing a pitching moment |
| C. | The airspeed below which the rudder the will not be capable of producing a rolling moment |
| D. | The airspeed below which the rudder the will not be capable of producing a dutch moment |
| Answer» B. The airspeed below which the rudder the will not be capable of producing a pitching moment | |