FLIGHT CONTROLS

Question 1

1. THE PITCH DIRECT LAW IS:

A. A LOAD FACTOR DEMAND WITH NO PROTECTION
B. A DIRECT SIDE STICK TO ELEVATOR RELATIONSHIP
C. A DIRECT SIDE STICK TO ELEVATOR RELATIONSHIP WITH AUTOTRIM OPERATION
D. ACHIEVED THROUGH THE THS USING MANUAL TRIM CONTROL

Answer 1

B. A DIRECT SIDE STICK TO ELEVATOR RELATIONSHIP

Question 2

2. WHEN IS THE THS NOT AVAILABLE?

A. AFTER BLUE HYDRAULIC SYSTEM FAILURE
B. AFTER YELLOW AND GREEN SYSTEM FAILURE
C. NEVER LOST, ALWAYS AVAILABLE MANUALLY
D. AFTER LOSS OF FAC 1 AND 2

Answer 2

B. AFTER YELLOW AND GREEN SYSTEM FAILURE

Question 3

3. WHICH SURFACES ARE USED FOR THE LOAD ALLEVIATION FUNCTION (LAF)?

A. SPOILERS 1 TO 5
B. AILERONS AND SPOILERS 4 AND 5
C. AILERONS AND SPOILERS 1 AND 2

Answer 3

B. AILERONS AND SPOILERS 4 AND 5

Question 4

4. WHICH SURFACES ARE USED FOR LIFT DUMPING?

A. ALL SPOILERS
B. SPOILERS 1 TO 3
C. SPOILERS 1 TO 4

Answer 4

A. ALL SPOILERS

Question 5

5. WHICH SIGNALS CAUSE RUDDER PEDAL MOVEMENT?

A. YAW DAMPING SIGNALS
B. RUDDER TRIM SIGNALS
C. TURN COORDINATION SIGNALS

Answer 5

B. RUDDER TRIM SIGNALS

Question 6

6. IF ELAC 1 AND 2 HAVE FAILED:

A. PITCH CONTROL IS PROVIDED BY THE FAC’S
B. PITCH CONTROL CAN ONLY BE ACHIEVED-FROM THE TRIM WHEEL
C. THE ELEVATOR AND PITCH TRIM ARE CONTROLLED BY SEC 1 OR 2

Answer 6

C. THE ELEVATOR AND PITCH TRIM ARE CONTROLLED BY SEC 1 OR 2

Question 7

7. IF FAC 1 AND 2 HAVE FAILED:

A. THE RUDDER CAN ALWAYS BE CONTROLLED FROM THE PEDALS
B. THE RUDDER CONTROL IS LOST
C. THE RUDDER CONTROL IS PROVIDED BY SEC 3

Answer 7

A. THE RUDDER CAN ALWAYS BE CONTROLLED FROM THE PEDALS

Question 8

8. WHEN BOTH STICKS ARE MOVED IN THE SAME OR OPPOSITE DIRECTION:

A. THE SURFACE MOVEMENT IS PROPORTIONAL TO THE ALGEBRAIC SUM OF THE DEFLECTIONS OF BOTH STICKS
B. THE SURFACE MOVEMENT IS PROPORTIONAL TO THE LAST STICK DEFLECTED
C. THE SURFACE MOVEMENT IS PROPORTIONAL TO THE FIRST STICK DEFLECTED
D. THE LEFT STICK HAS A PRIORITY

Answer 8

A. THE SURFACE MOVEMENT IS PROPORTIONAL TO THE ALGEBRAIC SUM OF THE DEFLECTIONS OF BOTH STICKS

Question 9

9. ELEVATORS, AILERONS, SPOILER ARE

A. HYDRAULICALLY ACTIVATED AND MECHANICALLY CONTROLLED
B. ELECTRICALLY ACTIVATED AND HYDRAULICALLY CONTROLLED
C. HYDRAULICALLY ACTIVATED AND ELECTRICALLY CONTROLLED

Answer 9

C. HYDRAULICALLY ACTIVATED AND ELECTRICALLY CONTROLLED

Question 10

10. RUDDER CONTROL IS ELECTRICAL FOR YAW DAMPING AND TRIM

A. YES
B. NO

Answer 10

A. YES

Question 11

11. WHAT STATEMENT IS CORRECT?

A. GROUND SPOILER FUNCTION: ALL SPOILERS DEPLOY
B. SPEED BRAKE FUNCTION: SPOILERS 1.2.3. DEPLOY
C. ROLL FUNCTION: AILERONS + SPOILERS 4 AND 5 DEPLOY

Answer 11

A. GROUND SPOILER FUNCTION: ALL SPOILERS DEPLOY

Question 12

12. HOW MANY CONTROL MODES ARE THERE ON THE ELEVATORS SERVO JACKS?

A. 2
B. 3
C. 4

Answer 12

B. 3

Question 13

13. WHAT ARE THE LIMITS FOR MANEUVER PROTECTION?

A. + 2,5 G - 1 G CLEAN
B. + 2 G - 0 FLAPS EXTENDED
C. A & B

Answer 13

C. A & B

Question 14

14. WHICH ELAC NORMALLY CONTROLS THE ELEVATORS AND THE STABILIZER?

A. ELAC 1
B. ELAC 2

Answer 14

B. ELAC 2

Question 15

15. HOW MANY HYDRAULIC MOTORS DRIVE THE SCREW JACK OF THE STABILIZER?

A. 2
B. 3

Answer 15

A. 2

Question 16

16. HOW MANY ELECTRIC MOTORS CAN CONTROL THE HYDRAULIC MOTOR OF THE STABILIZER?

A. 1
B. 2
C. 3

Answer 16

C. 3

Question 17

17. IF NEITHER ELAC 1 NOR ELAC 2 ARE AVAILABLE, PITCH CONTROL IS AUTOMATICALLY TRANSFERRED TO:

A. SEC 1 OR SEC 2
B. SEC 1 OR SEC 3
C. SEC 3

Answer 17

A. SEC 1 OR SEC 2

Question 18

18. IN NORMAL LAW, THE FLIGHT MODE CHANGES TO THE LANDING MODE WHEN PASSING:

A. 50 FT
B. 100 FT

Answer 18

A. 50 FT

Question 19

19. AT LANDING WHEN PASSING 30 FT:

A. THE ATTITUDE IS MEMORIZED
B. THE ATTITUDE -IS PROGRESSIVELY REDUCED TO 2° NOSE DOWN

Answer 19

B. THE ATTITUDE -IS PROGRESSIVELY REDUCED TO 2° NOSE DOWN

Question 20

20. HOW CAN A DEACTIVATED STICK BE REACTIVATED?

A. BY MOMENTARY ACTION ON TAKE OVER PUSH BUTTON OF THE ACTIVE STICK
B. BY SIMULTANEOUS ACTION ON BOTH TAKE OVER PUSH BUTTONS
C. BY MOMENTARY ACTION ON TAKE OVER PUSH BUTTON OF DEACTIVATED STICK

Answer 20

C. BY MOMENTARY ACTION ON TAKE OVER PUSH BUTTON OF DEACTIVATED STICK

Question 21

21. IN ROLL NORMAL LAW, THE BANK ANGLE PROTECTION IS ACTIVE WHEN BANK ANGLE IS:

A. 45°
B. 33°
C. 67°

Answer 21

B. 33°

Question 22

22. THE ROLL NORMAL LAW PROVIDES COMBINED CONTROL OF THE:

A. AILERONS + SPOILERS 2 TO 5 + RUDDER
B. AILERONS SPOILER 2 TO 5

Answer 22

A. AILERONS + SPOILERS 2 TO 5 + RUDDER

Question 23

23. IF ELAC 1 AND ELAC 2 HAVE FAILED:

A. ROLL CONTROL IS PROVIDED BY AILERONS ONLY
B. ROLL CONTROL IS PROVIDED BY AILERONS AND SPOILERS
C. ROLL CONTROL IS PROVIDED BY SPOILERS ONLY

Answer 23

C. ROLL CONTROL IS PROVIDED BY SPOILERS ONLY

Question 24

24. IN FLIGHT, IF A WTB (WING TIP BRAKE) IS ACTIVATED, CAN YOU RELEASE IT?

A. YES
B. NO

Answer 24

B. NO

Question 25

25. WHAT HAPPENS WHEN SFCC 1 FAILS? A. NOTHING B. FLAPS AND SLATS OPERATE AT HALF SPEED C. FLAPS SYSTEM LOST

Question 26

26. FLAP ONE POWER CONTROL UNIT FAILS, WHAT HAPPENS? A. NOTHING B. FLAPS AT HALF SPEED C. FLAPS ARE LOST

Question 27

27. IF CONF. 0 IS NOT SELECTED AFTER TAKE-OFF, THE FLAPS AUTOMATICALLY RETRACT AT: A. 180 KTS B. 210 KTS C. V2

Question 28

28. AFTER AN AUTOMATIC RETRACTION OF THE FLAPS WITH CONF. 1, THE FLAPS WILL AUTOMATICALLY REEXTEND WHEN SPEED DECREASES. A. YES B. NO

Question 29

29. IS IT POSSIBLE TO SELECT AN INTERMEDIATE POSITION WITH THE FLAPS AND SLATS SELECTOR? A. YES B. NO

Question 30

30. IF YOU ARE FLYING AT AN ANGLE OF ATTACK MORE THAN ALPHA PROT WHAT HAPPENS WHEN YOU RELEASE THE STICK? A. SPEED RETURNS TO VLS B. SPEED RETURNS TO ALPHA PROT

Answer 30

B. SPEED RETURNS TO ALPHA PROT

Question 31

31. WHEN ALTERNATE LAW IS ACTIVE, THE HIGH SPEED AND HIGH ANGLE OF ATTACK PROTECTIONS ARE: A. DEGRADED B. LOST

Answer 31

B. LOST

Question 32

32. WHEN ALTERNATE LAW IS ACTIVE, THE YAW DAMPING IS: A. AVAILABLE (DAMPER AUTHORITY IS LIMITED TO ± 5°) B. LOST

Answer 32

A. AVAILABLE (DAMPER AUTHORITY IS LIMITED TO ± 5°)

Question 33

33. LOAD ALLEVIATION FUNCTION IS INHIBITED WHEN: A. SPEED < 200 KTS OR SLAT/FLAP LEVER NOT AT 0 OR WTB ON OR ABOVE VMO/MMO B. SPEED < 200 KTS OR WTB ON C. S/F LEVER NOT AT 0 OR WTB ON

Answer 33

A. SPEED < 200 KTS OR SLAT/FLAP LEVER NOT AT 0 OR WTB ON OR ABOVE VMO/MMO

Question 34

34. HOW MANY HYDRAULIC SYSTEMS ACTIVATE THE RUDDER? A. 1 B. 2 C. 3

Answer 34

C. 3

Question 35

35. LIFT AUGMENTATION IS ACHIEVED ON EACH WING BY: A. 3 FLAP SURFACES + 4 SLAT SURFACES B. 2 FLAP SURFACES + 5 SLAT SURFACES

Answer 35

B. 2 FLAP SURFACES + 5 SLAT SURFACES

Question 36

36. IN THE A320, SLAT RETRACTION FROM 1 TO 0 IS INHIBITED IF ANGLE OF ATTACK EXCEEDS 8°5 OR SPEED < 148 KTS. A. YES B. NO

Answer 36

A. YES

Question 37

37. IN ALTERNATE LAW, THE CHANGE TO DIRECT LAW OCCURS WHEN: A. LANDING GEAR DOWN OR AT THE SELECTION OF FLAPS 2 (LGCIU 1 + 2 FAULT) B. LANDING GEAR DOWN C. PASSING 50 FT

Answer 37

A. LANDING GEAR DOWN OR AT THE SELECTION OF FLAPS 2 (LGCIU 1 + 2 FAULT)

Question 38

38. SLATS SYS 1 FAULT ON THE ECAM WARNING DISPLAY MEANS: A. SFCC 1 HAS FAILED B. THE SLAT CHANNEL IN ONE SFCC HAS FAILED

Answer 38

B. THE SLAT CHANNEL IN ONE SFCC HAS FAILED

Question 39

39. WITH HYDRAULIC BLUE SYSTEM REMAINING AND BEFORE LANDING GEAR EXTENSION THE FLIGHT CONTROL LAW IS: A. ALTERNATE B. NORMAL C. DIRECT

Answer 39

A. ALTERNATE

Question 40

40. IN FLIGHT CONTROL NORMAL, THE STALL WARNING IS ACTIVATED: A. IF SLATS ARE NOT EXTENDED WHEN REACHING A SPEED OF 148 KNOTS B. WHEN ALPHA MAX IS REACHED C. WHEN ALPHA PROT IS REACHED D. ANGLE OF ATTACK CORRESPONDING TO STALL WARNING CANNOT BE REACHED IN NORMAL LAW

Answer 40

D. ANGLE OF ATTACK CORRESPONDING TO STALL WARNING CANNOT BE REACHED IN NORMAL LAW

Question 41

41. THE PITCH NORMAL LAW PROVIDES A. MANEUVER PROTECTION + PITCH ATTITUDE PROTECTION + HIGH SPEED PROTECTION B. MANEUVER PROTECTION + HIGH ANGLE OF ATTACK PROTECTION + HIGH SPEED PROTECTION C. MANEUVER + HIGH ANGLE OF ATTACK + HIGH SPEED + PITCH ATTITUDE D. MANEUVER PROTECTION + PITCH ATT. PROTECTION + LOW SPEED STABILITY

Answer 41

C. MANEUVER + HIGH ANGLE OF ATTACK + HIGH SPEED + PITCH ATTITUDE