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. |
APU exhaust should be directed upward. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 2. |
Avionics stands for __________ |
| A. | aviation electronics |
| B. | airfare electrons |
| C. | aviation electrical |
| D. | prop aircraft |
| Answer» B. airfare electrons | |
| 3. |
Let’s consider we need to design avionics system for general aviation aircraft. If empty weight of aircraft is 100 unit then what will be the approximate range of required avionics weight. |
| A. | 1 unit to 3 unit |
| B. | 0.3 to 0.5 units |
| C. | 0.58 units |
| D. | 4 to 5 units |
| Answer» B. 0.3 to 0.5 units | |
| 4. |
Following diagram represents _________ |
| A. | Typical APU system at tail |
| B. | Hydraulic system |
| C. | Thrust augmentation |
| D. | Fuel system |
| Answer» B. Hydraulic system | |
| 5. |
A typical electrical system may include _________ |
| A. | generators, transformers, cables, etc |
| B. | only generator |
| C. | drag polar system |
| D. | only transformers |
| Answer» B. only generator | |
| 6. |
Hydraulic system affect conceptual design based on __________ |
| A. | hydraulic pump space requirements |
| B. | space for control surface |
| C. | secondary control surface |
| D. | lift required at tail |
| Answer» B. space for control surface | |
| 7. |
Following diagram represents _____________ |
| A. | simplified hydraulic system |
| B. | wing loading diagram |
| C. | pneumatic subsystem |
| D. | fuel tank location |
| Answer» B. wing loading diagram | |
| 8. |
A pneumatic subsystem is used to ______________ |
| A. | provide compressed air for pressurization |
| B. | more pressure output |
| C. | deflect control surface |
| D. | provide electrical power |
| Answer» B. more pressure output | |
| 9. |
Which of the following is considered to be correct subsystem to deflect control surface? |
| A. | Hydraulic system |
| B. | Pneumatic subsystem |
| C. | Fuel system |
| D. | Deice system |
| Answer» B. Pneumatic subsystem | |
| 10. |
Which of the following is an example of an aircraft subsystem? |
| A. | Pneumatic |
| B. | Gear retraction |
| C. | Landing gear |
| D. | High lift device |
| Answer» B. Gear retraction | |