A320 T.

Question 1

1. If the CVR does not test, what should you check before you call the maintenance?A) CVR on blue light is on.
   B) Parking brake is on.
   C) Check the CB is not out.
   D) All the above.*

Answer 1

D) All the above.*

Question 2

2. What precautions should you take to disengage the IDG?A) Engine stopped.
   B) Must not press the disconnect button for more than 3 seconds.
   C) Both the above.
   D) None. As you can re-engage the IDG at any time.

Answer 2

B) Must not press the disconnect button for more than 3 seconds.

Question 3

3. Which fuel valve closes when you press and release out the Engine Fire push-button?A) LP fuel valve.
   B) HP fuel valve.
   C) Engine Fuel Return valve.
   D) A + C.

Answer 3

D) A + C.

Question 4

4. Will an APU Fire System test (i.e. pressing the APU Fire Test push-button) cause the APU to auto shutdown?A) Yes.
   B) No.

Answer 4

A) Yes.

Question 5

5. What is the function of the ELAC’s?A) ELAC 1 controls the alierons. ELAC 2 controls the elevator and stabilizer.
   B) ELAC 1 controls the alierons and spoilers. ELAC 2 controls the elevator and stabilizer.
   C) As in A). But in case of failure the other ELAC may replace the faulty one.

Answer 5

C) As in A). But in case of failure the other ELAC may replace the faulty one.

Question 6

6. When will there be no Green Dot, S Speed, or F Speed indication on the PFD’s?A) Loss of ELAC’s.
   B) Loss of SEC’s.
   C) Loss of FAC’s.
   D) Loss of flight control normal law:

Answer 6

C) Loss of FAC’s.

Question 7

7. Can the aircraft be flown with the loss of all hydraulic systems?A) No.
   B) Yes.

Answer 7

B) Yes.

Question 8

8. Can the aircraft be stalled?A) Yes. In all flight control modes.
   B) Yes. Only in direct law.
   C) Yes. In both alternate law and direct law.
   D) Yes. In alternate law without protections and in direct law.

Answer 8

D) Yes. In alternate law without protections and in direct law.

Question 9

9. Should the aircraft be disturbed by severe turbulence to an attitude of 90° bank (90 degrees), can the pilot recover and what would be the flight control laws after such a recover?A) Not relevant, as the aircraft under Normal Law, flight is limited to a bank (67 degrees).
   B) Yes. The aircraft would be in Direct Law.
   C) Yes. The Abnormal Attitude Law allows for such a recovery.
   D) Yes. In mechanical backup.

Answer 9

C) Yes. The Abnormal Attitude Law allows for such a recovery.

Question 10

10. On the A-320, in which of the following is speed brake action not inhibited?

A) SEC 1 + 3 fault.
B) Flaps Alpha Lock.
C) Flaps Full.
D) Elevator (L + R) Fault.

Answer 10

A) SEC 1 + 3 fault.

Question 11

11. Can the rudder be manually trimmed or reset with an autopilot engaged?

A) Yes.
B) Yes. But the autopilot is disconnected.
C) No.

Answer 11

C) No.

Question 12

12. Can the aircraft be refueled with battery power only?

A) Yes.
B) No.

Answer 12

A) Yes.

Question 13

13. Which of the following is not true regarding a Fault light on the PTU?

A) Reservoir Low level (either/or Green and Yellow).
B) Reservoir Low Air Pressure
C) Pump Over Temperature.
D) Green Hydraulic Pressure 2600 PSI, Yellow Hydraulic Pressure 3000 PSI PTU not running.

Answer 13

D) Green Hydraulic Pressure 2600 PSI, Yellow Hydraulic Pressure 3000 PSI PTU not running.

Question 14

14. Blue Electric Pump fails. You press the RAT MAN ON push-button. Does the Emergency Generator come on line?

A) Yes.
B) No.

Answer 14

B) No.

Question 15

15. What happens if after a Wing Anti-Ice test on Ground is performed, the Wing Anti-Ice push-button is left ON?

A) Fault Light comes on. ECM Action comes up.
B) Nothing.
C) The Wing Anti-Ice begins operating immediately after take off.

Answer 15

B) Nothing.

Question 16

16. By looking at the PFD how would you know that you are no longer in Normal Law?

A) FMA announces ALT in the fourth column.
B) Green = signs are replaced by amber X.
C) Alpha Prot Speed is replaced by Vsw Speed.
D) B + C.

Answer 16

D) B + C.

Question 17

17. Should you select the L/G Lever to the Down position at 270 Kts, will the landing gear extend?

A) No.
B) No, but when the speed decreases below 260 Kts, the Landing Gear extends.
C) Yes, but only with ADR 1 + 3 Fault.

Answer 17

B) No, but when the speed decreases below 260 Kts, the Landing Gear extends.

Question 18

18. What are the conditions necessary for autobrake activation?

A) Wheel speed above 72 Kts, spoilers armed, autobrake armed (LO MED HI).
B) Ground Speed above 72 Kts, spoilers armed, autobrake armed (LO MED HI)*
C) Spoilers extended, two SEC’s operative, and either the green or yellow hydraulic system operational, autobrake armed (LO M.BD HI).
D) Spoilers extended, speed above 72 Kts, two SEC’s operative, Green Hydraulic System Operative and autobrake armed (LO MED HI).

Answer 18

D) Spoilers extended, speed above 72 Kts, two SEC’s operative, Green Hydraulic System Operative and autobrake armed (LO MED HI).

Question 19

19. In flight, the IR Fault light is flashing. This means that:

A) IR is faulty and cannot be recovered.
B) IR alignment has to be performed.
C) IR is faulty, but may be available in ATT mode.

Answer 19

C) IR is faulty, but may be available in ATT mode.

Question 20

20. Can you still use an ADR 1 after you have selected IR 1 Mode selector OFF?

A) Yes.
B) No.

Answer 20

A) Yes.

Question 21

21. Which of the following statements is not correct regarding to what happens as the cabin altitude (CA) rises from 7 000 feet to 15 000 feet?

A) Passing 14 000 feet CA, passenger oxygen masks deploy.
B) Passing 9 500 feet CA, the cabin altitude warning sounds.
C) Passing 11 300’ feet CA, all cabin signs illuminate (Fasten Seal Belts, Return to Seat, No Smoking and Exit Signs).
D) Passing 10 500 feet CA, Cabin PA automatically broadcasts CIDS pre-recorded message to the passengers.

Answer 21

D) Passing 10 500 feet CA, Cabin PA automatically broadcasts CIDS pre-recorded message to the passengers.

Question 22

22. The external horn sounds for: IRU on battery power. APU Fire. Avionica Bay Overheat.

A) True.
B) False.f

Answer 22

A) True.

Question 23

23. Will the FADEC abort an Auto start in flight?

A) Yes.
B) No.

Answer 23

A) Yes.

Question 24

24. During a Manual Start, you see the engine is about to exceed maximum EGT. Which of the following is not correct?

A) You should do nothing as the FADEC monitors and performs auto shutdown.
B) You should shut the engine down with the Engine master switch.
C) ECAM will provide with an alert and the actions required by the crew.
D) B + C.

Answer 24

A) You should do nothing as the FADEC monitors and performs auto shutdown.