5.9.11

NOTE

TO CHECK YOUR PREPARATION ,PLZ WRITE DOWN YOUR SELECTED OPTIONS (A,B,C) ON ROUGH PAGE AND  AT THE END OF QUIZ , VERIFY YOUR SELECTED OPTIONS WITH THE CORRECT OPTIONS GIVEN BELOW

Question Number. 41. In an automatic flight control system, when may the yaw damper be applied?.
Option A. During manual control only.
Option B. During either manual or automatic control.
Option C. During automatic control only.


Question Number. 42. Flutter can be prevented by.
Option A. mass balance.
Option B. trim tabs.
Option C. balance panels.


Question Number. 43. In a fully fly by wire system, if the elevator loses all electrical power.
Option A. servos lock at last position.
Option B. servos remain stationary and provide damping.
Option C. servos move to neutral and lock.


Question Number. 44. In an auto trim system, for the trim system to operate.
Option A. operation of the trim controls is required.
Option B. autopilot need not be engaged.
Option C. autopilot must be engaged.



Question Number. 45. In an autopilot coordinated turn, when the turn angle is reached.
Option A. both ailerons are down.
Option B. one is up one is down.
Option C. the ailerons are faired.



Question Number. 46. How is automatic angle of attack protection provided?.
Option A. Fast/Slow indication.
Option B. Reduce flap deployment.
Option C. Autothrottle applying more power.


Question Number. 47. A single failure of fly by wire.
Option A. will reduce the operational height and speed.
Option B. will limit the flight profile.
Option C. has no effect on the aircraft's operation.



Question Number. 48. Fly-by-wire load alleviation function in turbulent weather conditions will result in.
Option A. spoiler moving symmetrically upward.
Option B. ailerons moving symmetrically upward.
Option C. ailerons and spoiler moving symmetrically upward.



Question Number. 49. Autotrim will switch to 'slow' when.
Option A. flaps are retracted.
Option B. landing gear up and locked.
Option C. flaps are extended.


Question Number. 50. How is the stabiliser automatically controlled in normal manual operation?.
Option A. Mach/Speed Trim.
Option B. Pitch Trim.
Option C. Electric Trim.

ABOVE QUESTIONS WITH ANSWERS 

Question Number. 41. In an automatic flight control system, when may the yaw damper be applied?.
Option A. During manual control only.
Option B. During either manual or automatic control.
Option C. During automatic control only.
Correct Answer is. During either manual or automatic control.
Explanation. Automatic Flight Control Pallett Page 222 - 226.

Question Number. 42. Flutter can be prevented by.
Option A. mass balance.
Option B. trim tabs.
Option C. balance panels.
Correct Answer is. mass balance.
Explanation. NIL.

Question Number. 43. In a fully fly by wire system, if the elevator loses all electrical power.
Option A. servos lock at last position.
Option B. servos remain stationary and provide damping.
Option C. servos move to neutral and lock.
Correct Answer is. servos remain stationary and provide damping.
Explanation. A319/A320/A321 Flight Crew Operating Manual.
Question Number. 44. In an auto trim system, for the trim system to operate.
Option A. operation of the trim controls is required.
Option B. autopilot need not be engaged.
Option C. autopilot must be engaged.
Correct Answer is. autopilot need not be engaged.
Explanation. Automatic Flight Control, Pallett Page 213 - 218.


Question Number. 45. In an autopilot coordinated turn, when the turn angle is reached.
Option A. both ailerons are down.
Option B. one is up one is down.
Option C. the ailerons are faired.
Correct Answer is. the ailerons are faired.
Explanation. Due to the aircraft's neutral lateral stability, the ailerons are neutralised (faired) and the aircraft will hold the turn.


Question Number. 46. How is automatic angle of attack protection provided?.
Option A. Fast/Slow indication.
Option B. Reduce flap deployment.
Option C. Autothrottle applying more power.


Question Number. 47. A single failure of fly by wire.
Option A. will reduce the operational height and speed.
Option B. will limit the flight profile.
Option C. has no effect on the aircraft's operation.



Question Number. 48. Fly-by-wire load alleviation function in turbulent weather conditions will result in.
Option A. spoiler moving symmetrically upward.
Option B. ailerons moving symmetrically upward.
Option C. ailerons and spoiler moving symmetrically upward.



Question Number. 49. Autotrim will switch to 'slow' when.
Option A. flaps are retracted.
Option B. landing gear up and locked.
Option C. flaps are extended.


Question Number. 50. How is the stabiliser automatically controlled in normal manual operation?.
Option A. Mach/Speed Trim.
Option B. Pitch Trim.
Option C. Electric Trim.