MCQOPTIONS
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MCQOPTIONS
This section includes 12 Mcqs, each offering curated multiple-choice questions to sharpen your Avionics knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
In a typical quadruplex actuator system, how is the failure of an actuator identified? |
| A. | By comparing it with the signal of the three good ones |
| B. | By comparing it with a simulation model |
| C. | Using in-lane fault detection |
| D. | Using reflectometry |
| Answer» B. By comparing it with a simulation model | |
| 2. |
The reason for using quadruplex actuation system is _______ |
| A. | precise movement |
| B. | to counteract heavy air loads on the control surfaces |
| C. | quick reaction to the control stick movement |
| D. | as a fail safe mechanism |
| Answer» E. | |
| 3. |
Why are both electrical and hydraulic systems are used in the same aircraft? |
| A. | To generate more force |
| B. | Quick deflections |
| C. | As a fail safe |
| D. | Hydraulics for more force and electric for quick deflections |
| Answer» D. Hydraulics for more force and electric for quick deflections | |
| 4. |
Why are actuators used in FBW systems? |
| A. | Movement of control surfaces |
| B. | Reduce drag |
| C. | Increase lift |
| D. | Safety equipment |
| Answer» B. Reduce drag | |
| 5. |
What type of cable is used in ARINC 629? |
| A. | Coaxial cable |
| B. | Screened twisted pair |
| C. | Unscreened twisted pair |
| D. | Parallel lines |
| Answer» D. Parallel lines | |
| 6. |
Which one of the following is a military standard data bus? |
| A. | Mil Std 1553 |
| B. | ARINC 629 |
| C. | ARINC 429 |
| D. | COMAC C919 |
| Answer» B. ARINC 629 | |
| 7. |
How are FBW signals transmitted? |
| A. | Simplex |
| B. | Duplex |
| C. | Time division multiplexing |
| D. | Code division multiplexing |
| Answer» D. Code division multiplexing | |
| 8. |
FBW system requires an air data system for control and stability. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 9. |
Which of the following is not a component of the FBW system? |
| A. | Flight control computer |
| B. | Aircraft motion sensor |
| C. | Actuators |
| D. | Communication receivers |
| Answer» E. | |
| 10. |
Which one of the following is not true with respect to the FBW system? |
| A. | FBW is not necessary for every aircraft |
| B. | FBW makes an aircraft stealthy |
| C. | FBW provides better control and carefree flying |
| D. | FBW makes aircraft with low stability fly smoothly |
| Answer» C. FBW provides better control and carefree flying | |
| 11. |
How is fly by wire system implemented in an aircraft? |
| A. | By using control rods and linkages connecting stick to control surfaces |
| B. | By using high power radio transmitters and receivers |
| C. | By using computers and actuators to control surfaces |
| D. | Artificial intelligence |
| Answer» D. Artificial intelligence | |
| 12. |
Why is the BFW system used? |
| A. | To control aerodynamically efficient but unstable body |
| B. | For communications in aircraft |
| C. | Better navigation |
| D. | Reduced chances of enemy detection |
| Answer» B. For communications in aircraft | |