MCQOPTIONS
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MCQOPTIONS
This section includes 9 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. |
Specific fuel consumption effects the range of an aircraft. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 2. |
The range of the aircraft is increased if the aircraft is flown at a higher than optimum altitude. |
| A. | True |
| B. | False |
| Answer» C. | |
| 3. |
Which of the following factors are inversely proportional to the range of the aircraft? |
| A. | Altitude |
| B. | Ambient relative pressure |
| C. | Temperature |
| D. | Mach number |
| Answer» C. Temperature | |
| 4. |
The best range is obtained at 1.416 Vmd. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 5. |
The minimum drag speed in terms of equivalent airspeed is unaffected by the altitude. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 6. |
What is the relation between altitude and the aircraft range? |
| A. | Altitude increases with increase in the aircraft range |
| B. | Altitude decreases with increase in the aircraft range |
| C. | Altitude increases with decrease in the aircraft range |
| D. | Altitude is not effected by the aircraft range |
| Answer» B. Altitude decreases with increase in the aircraft range | |
| 7. |
What is the relation between air temperature and the aircraft range? |
| A. | Air temperature increases with increase in the aircraft range |
| B. | Air temperature decreases with increase in the aircraft range |
| C. | Air temperature increases with decrease in the aircraft range |
| D. | Air temperature is not effected by the aircraft range |
| Answer» B. Air temperature decreases with increase in the aircraft range | |
| 8. |
What happens if the final fuel weight increases in an aircraft? |
| A. | Fuel ratio increases |
| B. | Fuel ratio is not effected |
| C. | Range of the aircraft is increased |
| D. | Range of the aircraft is decreased |
| Answer» E. | |
| 9. |
The range factor is proportional to the square root of the initial cruising weight. |
| A. | True |
| B. | False |
| Answer» B. False | |