Vayudoot Aviation

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

Pitch attitude.

Alpha floor.

Vls.

ALPHA SPD (alpha speed)

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

Air data output has been disconnected.

Alignment has been completed.

The respective IR is operating normally.

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

Navigation, flight planning and A/THR commands.

Performance optimization, A/THR and AP commands

AP and FD commands and flight envelope computation.

Navigation, flight planning, performance optimization and flight predictions

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

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.

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

5. During the takeoff phase

SRS mode is available up to 1500 ft.

SRS mode will not engage if TOGA is selected.

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

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

Prohibit steep climb angles and bank angles.

Will not allow the pilot to stall the aircraft.

Prohibit steep bank angles.

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

7. 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.

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

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

Flaps configuration 1.

Heading differs from track by 20 deg or more

Flaps configuration 1, 2.

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

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

Yes

No

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

Check Effective Date.

Check Data Base Cycle.

Check the changeover date.

Check Data Base Date.

11. An amber flashing IR FAULT light indicates that:

Present position needs to be reentered.

A complete failure of the respective IR has occurred.

Attitude and heading information may be recovered in ATT mode.

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

Yes.

No

13. 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.

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

Airspeed, attitude, altitude, and vertical speed.

Airspeed, vertical speed, and altitude.

Heading, attitude, and vertical speed.

Airspeed, altitude, and backup vertical speed.

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

Both are correct.

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

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

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

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

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

Nothing.

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

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

The flight controls revert to direct law.

The flight controls remain in the load factor demand law.

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

Three

Two

One

Four

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

Elevator and stabilizer revert to mechanical backup.

SECs

FACs.

Backup mode of ELAC’s

20. 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, disconnect auto trim, and maintain its current attitude.

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.

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

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

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

22. 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.

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

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

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

Speed brakes are extended and engines are not at idle.

Speed brakes have a fault.

All of the above.

24. 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.

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

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

25. The DDRMI provides the pilot with:

Bearing only for VOR 1 and VOR 2.

Bearing and DME information for VOR 2 and ADF 2.

Bearing and DME information for VOR 1 and ADF 1.

Bearing only for VOR 1.

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

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

Move the ATT HDG rotary selector knob to CAPT 3.

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

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

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

Heading, altitude, and vertical speed

Heading, attitude, and vertical speed.

Heading, attitude, and altitude.

Airspeed, altitude, and backup vertical speed.

28. How long does a normal IR alignment take?

Approximately 3 minutes.

Approximately 13 minutes.

Approximately 10 minutes.

Approximately 6 minutes.

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

The circuit breaker for that particular DU has popped.

No power.

DMC failure.

30. What is the function of the FACs?

Rudder and Yaw damping inputs, Flight envelope and speed computations

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

Rudder and Yaw damping inputs

Rudder and Yaw damping inputs and windshear protection

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

Both AD and IR information will be disconnected.

All of the above.

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

The respective ADIRU will become deenergized.

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

Disconnected

Active

Armed.

33. 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.

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

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

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

No

Yes, ILS approach only.

Yes, both LNAV and VNAV approaches are forbidden.

35. The ON BAT light will illuminate amber:

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

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

Both are correct.

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

Bank angle.

Load factor.

Pitch attitude.

Roll attitude.

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

FMGC 2

FMGC 1

Both

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

IR information will be disconnected.

AD and IR information will be disconnected.

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

AD information will be disconnected.

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

Once a DMC has failed the information is unrecoverable

No action is needed as recovery is automatic.

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

40. What does the LOW ACCURACY message mean?

FMGC 1 & 2 position difference exceeds limits.

FMCG position & IR position difference exceeds limits.

FMGC position & actual radio position difference exceeds limits.

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

Protections, Load Factor and Pitch attitude.

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

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

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

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

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

Present position can be entered through the ADIRS CDU.

Both are correct.

Question Bank

Questions for Automatic Flight A320