MCQOPTIONS
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MCQOPTIONS
This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
A Jet transport aircraft is flying with crew load of 175kg, payload of 1400kg and fuel weight of 500kg. Find out Fuel to empty weight fraction, if design take-off gross weight of the aircraft is 5600lb. |
| A. | 1.076 |
| B. | 0.1831 |
| C. | 0.196 |
| D. | 0.1418 |
| Answer» B. 0.1831 | |
| 2. |
Cessna 172R has total gross weight of the 1110.98kg with fuel capacity of 210 kg and weight of crew and passenger is 125kg. Find out empty weight fraction. |
| A. | 775.98kg |
| B. | 69.84kg |
| C. | 0.6984 |
| D. | 0.6984lb |
| Answer» D. 0.6984lb | |
| 3. |
A jet airliner aircraft is flying with crew load of 150kg, payload of 520lb and fuel weight of 500lb. Find out the empty weight if design take-off gross weight of the aircraft is given 1525lb. |
| A. | 79kg |
| B. | 79lb |
| C. | 170lb |
| D. | 355lb |
| Answer» B. 79lb | |
| 4. |
A general aviation aircraft is flying with crew load of 115lb, payload of 220lb and fuel weight of 100lb. Find out the design take-off gross weight of the aircraft, given 95lb empty weight. |
| A. | 530lb |
| B. | 241lb |
| C. | 435lb |
| D. | 500lb |
| Answer» B. 241lb | |
| 5. |
In general, the fuel weight is represented by a fraction of total take-off weight. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 6. |
Take-off gross weight of an aircraft is summation of _____ |
| A. | empty and payload weight |
| B. | fuel, payload, crew, empty and miscellaneous weight |
| C. | fuel and crew weight |
| D. | only passenger and crew weight |
| Answer» B. fuel, payload, crew, empty and miscellaneous weight | |
| 7. |
Avionics systems are an example of ____ weight. |
| A. | empty |
| B. | crew |
| C. | passenger |
| D. | payload |
| Answer» B. crew | |
| 8. |
Design take-off gross weight includes ______ |
| A. | only fuel weight |
| B. | only crew weight |
| C. | only payload weight |
| D. | crew, payload and fuel weights |
| Answer» E. | |
| 9. |
The “Design take-off gross weight” and “maximum take-off weight” are always interchangeable. |
| A. | True |
| B. | False |
| Answer» C. | |
| 10. |
The subsequent step after the requirements in conceptual design phase is _____ |
| A. | design take-off gross weight |
| B. | control |
| C. | stability |
| D. | lofting |
| Answer» B. control | |