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This section includes 11 Mcqs, each offering curated multiple-choice questions to sharpen your Avionics knowledge and support exam preparation. Choose a topic below to get started.
1. |
Why is FBW essential in stealth aircraft? |
A. | FBW system damps radar energy |
B. | Improves control |
C. | Reduces engine noise |
D. | Disturbs tracking techniques used by missiles |
Answer» C. Reduces engine noise | |
2. |
What is the relation between autopilot and FBW? |
A. | FBW provides autopilot commands for roll, pitch, and yaw |
B. | Autopilot provides FBW commands of roll, pitch, and yaw |
C. | Autopilot is a part of FBW system |
D. | Autopilot is not related to FBW |
Answer» C. Autopilot is a part of FBW system | |
3. |
FBW has the power to reject pilot inputs in extreme situations. |
A. | True |
B. | False |
Answer» B. False | |
4. |
Why are dampers an essential element in FBW inceptors? |
A. | Control aircraft stability by damping forces |
B. | Acts as a low pass filter on the stick movement |
C. | Provides accurate deflections |
D. | To prevent aircraft to carry out critical maneuvers |
Answer» C. Provides accurate deflections | |
5. |
A FBW control stick is referred as _______ |
A. | FBW joystick |
B. | FBW control pad |
C. | FBW inceptor |
D. | FBW analog stick |
Answer» D. FBW analog stick | |
6. |
A highly stable aircraft is not easily maneuverable. |
A. | True |
B. | False |
Answer» B. False | |
7. |
An aircraft is negatively stable when ______ |
A. | its tailplane produces negative lift (downwards) |
B. | its tailplane produces positive lift (upwards) |
C. | its tailplane does not produce lift |
D. | it is flying inverted |
Answer» C. its tailplane does not produce lift | |
8. |
Why does an FBW system use a smaller tail area? |
A. | Bigger tails are harder to move as they produce larger wing loads |
B. | Actively controls the tail thus making up for the reduced stability due to lesser area |
C. | Tail does not contribute much to stability and its area can thus be reduced effectively |
D. | To reduce weight and drag but at a cost of natural stability |
Answer» E. | |
9. |
What is the incidence angle in the yaw plane called? |
A. | Side slip angle |
B. | Yaw angle |
C. | Crossflow angle |
D. | Angle of crosswind |
Answer» B. Yaw angle | |
10. |
What does FBW use to scale the control surface deflection according to the aircraft s airspeed and height? |
A. | Air Data Computer |
B. | Flight Management System |
C. | Flight Control Computer |
D. | Autopilot system |
Answer» B. Flight Management System | |
11. |
What type of system is classified as Direct electric link system ? |
A. | Systems with parallel wire connection |
B. | System with serial wire connection |
C. | System with motion sensor feedback |
D. | System without motion sensor feedback |
Answer» E. | |