Vayudoot Aviation

1. What causes a DU to display a black screen with a white diagonal line?

No power.

DMC failure.

The circuit breaker for that particular DU has popped.

2. What information is supplied by the Air Data Modules (ADMs) and displayed on the PFD‟s?

Airspeed, altitude, and backup vertical speed.

Airspeed, vertical speed, and altitude.

Heading, attitude, and vertical speed.

Airspeed, attitude, altitude, and vertical speed.

3. A/THR in white means that A/THR is:

Disconnected

Armed.

Active

4. Can the aircraft be controlled with a loss of all electrics?

Yes

No

5. While in-flight, operating in Normal law, in the Alpha prot range:

The flight controls revert to direct law.

The flight controls remain in the load factor demand law.

The sidestick controller and flight controls revert to the AOA mode, and side stick deflection is proportional to AOA.

6. Which protection is not available below 100 feet AGL?

Alpha floor.

Pitch attitude.

Vls.

ALPHA SPD (alpha speed)

7. How can the present position of the aircraft be initialized?

Present position can be entered through the ADIRS CDU.

Present position can be entered on the INIT page of the MCDU.

Both are correct.

8. What is the function of the FACs?

Rudder and Yaw damping inputs and windshear protection

Rudder and Yaw damping inputs, Flight envelope and speed computations, and windshear protection

Rudder and Yaw damping inputs

Rudder and Yaw damping inputs, Flight envelope and speed computations

9. An amber flashing IR FAULT light indicates that:

Attitude and heading information may be recovered in ATT mode.

A complete failure of the respective IR has occurred.

Present position needs to be reentered.

10. The thrust delivered by A/THR is already at MAX CLB thrust. Is it possible to obtain some additional thrust?

Yes, by setting a higher speed target.

Yes, by moving the thrust levers forward from the CL detent.

No, because the A/THR already delivers the maximum available thrust.

11. In normal law all protections are active, which of the following lists is the most complete list?

Protections, Load Factor, Pitch attitude, High AOA, Vls, Alpha floor, and High speed.

Protections, Load Factor, Pitch attitude, High AOA, Alpha floor, angle of bank, and High speed.

Protections, Load Factor, Pitch attitude, High AOA, and High speed.

Protections, Load Factor and Pitch attitude.

12. When in alternate law, all protections except _______ protection will be lost.

Load factor.

Bank angle.

Pitch attitude.

Roll attitude.

13. If the LOWER ECAM DU fails, is there a way to retrieve that information?

Pressing and holding the related systems page pb on the ECAM control panel; the page will be displayed on the UPPER ECAM.

Rotating the ECAM/ND XFER switch, the LOWER ECAM page will be transferred to either the Captain or First Officer’s BND.

Both are correct.

14. If both ELACs fail, what controls the elevator and stabilizer?

SECs

FACs.

Elevator and stabilizer revert to mechanical backup.

Backup mode of ELAC’s

15. Which of the following statements is always true when operating in alternate law?

Extending the landing gear will place the aircraft in Mechanical backup law.

Extending the landing gear will place the aircraft in Direct law.

16. The white IR ALIGN light is flashing. What does this mean?

Attitude and heading information have been lost. An alignment fault may exist.

No present position has been entered and ten minutes has elapsed since the IR was selected ON. An alignment fault may exist.

No present position has been entered and ten minutes has elapsed since the IR was selected ON.

17. While in flight operating in Normal law, movement of the sidestick and subsequent return to neutral will command:

Control surface movements proportional to stick deflection, then return the aircraft to straight and level flight.

A load factor proportional to stick deflection, then maintain one G flight corrected for pitch attitude.

Control surface movements proportional to stick deflection, disconnect auto trim, and maintain its current attitude.

18. The IR ALIGN light is extinguished. What does this mean?

The respective IR is operating normally.

Alignment has been completed.

Air data output has been disconnected.

19. Placing one of the ADR push buttons OFF will accomplish what?

The respective ADIRU will become deenergized.

Both AD and IR information will be disconnected.

The OFF light will illuminate and air data output will disconnect.

All of the above.

20. What message is displayed if the database effective date does not match the clock date?

Check Effective Date.

Check Data Base Date.

Check Data Base Cycle.

Check the changeover date.

21. If the IR mode rotary selector is selected OFF:

IR information will be disconnected.

AD and IR information will be disconnected.

AD information will be disconnected.

The ADIRU is not energized: AD and IR information is lost.

22. What does the LOW ACCURACY message mean?

FMGC position & actual radio position difference exceeds limits.

FMCG position & IR position difference exceeds limits.

FMGC 1 & 2 position difference exceeds limits.

23. Where is the information displayed by DMC #1 and DMC #2?

DMC #1 supplies data to PFD #1, ND #1 and LOWER ECAM. DMC #2 supplies data for PFD #2, ND #2, and LOWER ECAM.

ADMC #1 supplies data to PFD #1, ND #1 and LOWER ECAM. DMC #2 supplies data for PFD #2, ND #2, and UPPER ECAM.

DMC #1 supplies data to PFD #1, ND #1, and UPPER ECAM. DMC #2 supplies data for PFD #2, ND #2, and LOWER ECAM.

DMC #1 supplies data to PFD #2, ND #2 and LOWER ECAM. DMC #2 supplies data for PFD #1, ND #1, and UPPER ECAM.

24. High and low speed stabilities may be available in alternate law, stabilities:

Will not allow the pilot to stall the aircraft.

Can be overridden by the pilot, and it is possible to exceed Vmo, Mmo and stall the aircraft.

Prohibit steep bank angles.

Prohibit steep climb angles and bank angles.

25. Can the autopilot be used for a single engine approach and autoland?

No

Yes.

26. During the takeoff phase

SRS mode is available up to 1500 ft.

SRS mode will provide guidance to maintain V2+10 kts (minimum) as a speed reference

SRS mode will not engage if TOGA is selected.

27. If LOW ACCURACY message is displayed, are there any approach restrictions?

No

Yes, ILS approach only.

Yes, both LNAV and VNAV approaches are forbidden.

28. How long does a normal IR alignment take?

Approximately 6 minutes.

Approximately 10 minutes.

Approximately 3 minutes.

Approximately 13 minutes.

29. What action should be taken if ADR #1 is lost?

Move the AIR DATA knob on the switching panel to CAPT 3.

Nothing.

Move the ATT HDG knob on the switching panel to CAPT 3.

30. How many Air Data/Inertial Reference Units (ADIRU‟s) are installed?

Three

Two

Four

One

31. What action should be taken if IR 2 is lost:

Move the ATT HDG rotary selector knob to CAPT 3.

Move the ATT HDG rotary selector knob to F/O 1.

Move the ATT HDG rotary selector knob to F/O 3.

Move the EIS DMC rotary selector knob to F/O 3.

32. The DDRMI provides the pilot with:

Bearing and DME information for VOR 1 and ADF 1.

Bearing only for VOR 1 and VOR 2.

Bearing and DME information for VOR 2 and ADF 2.

Bearing only for VOR 1.

33. On an autoland approach, with both autopilots on, which FMGC is master?

FMGC 1

FMGC 2

Both

34. The ON BAT light will illuminate amber:

For a few seconds at the beginning of the alignment process.

When one or more IR’s are operating on aircraft battery power.

Both are correct.

35. What does amber SPEED BRAKES mean on lower ECAM?

All of the above.

Speed brakes are extended and engines are not at idle.

Speed brakes have a fault.

Speed brakes are extended and flap handle is not at 0.

36. What information is supplied by the IR‟s and displayed on the PFD?

Airspeed, altitude, and backup vertical speed.

Heading, attitude, and vertical speed.

Heading, altitude, and vertical speed

Heading, attitude, and altitude.

37. What are the correct positions for the PFD and ND?

The PFD should be inboard and the ND should be inboard.

The PFD should be to the left of the ND for both seat positions.

The PFD should be inboard and the ND should be outboard.

The PFD should be outboard and the ND should be inboard.

38. The Flight Management part of the FMGC includes the following elements

Navigation, flight planning and A/THR commands.

Navigation, flight planning, performance optimization and flight predictions

AP and FD commands and flight envelope computation.

Performance optimization, A/THR and AP commands

39. After a single DMC failure, how could a crewmember recover the display units?

Once a DMC has failed the information is unrecoverable

Rotate the EIS DMC switch on the switching panel to replace the failed DMC with DMC #3.

No action is needed as recovery is automatic.

40. When does the sideslip indicator change to a blue Beta target?

Any EPR exceeds 1.25, and EPR‟s differ by more than 0.30

Flaps configuration 1, 2.

Heading differs from track by 20 deg or more

Flaps configuration 1.

41. The ATT HDG and AIR DATA selectors on the switching panel in the NORM position indicate that

ADIRU 1 is supplying information to PFD 1, ND 1 and the DDRMI; ADIRU 2 is supplying power to PFD 2 and ND 2.

ADIRU 1 is supplying information to PFD 1 and ND 2, and ADIRU 2 is supplying power to PFD 2 and ND 1.

42. What is the difference between -FD2 and 2FD- on the FMA?

1 off, 2 engaged. 2 engaged, 1 inop.

1 inop, 2 engaged. 2 engaged, 1 off.

Question Bank

Questions for Automatic Flight A320