Vayudoot Aviation

1. The ON BAT light will illuminate amber:

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

Both are correct.

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

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

Elevator and stabilizer revert to mechanical backup.

FACs.

SECs

Backup mode of ELAC’s

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

AD information will be disconnected.

AD and IR information will be disconnected.

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

IR information will be disconnected.

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

Both AD and IR information will be disconnected.

All of the above.

The respective ADIRU will become deenergized.

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

5. 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 inboard.

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

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

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

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.

Once a DMC has failed the information is unrecoverable

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

Armed.

Active

Disconnected

8. 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 3.

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

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

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

AP and FD commands and flight envelope computation.

Navigation, flight planning and A/THR commands.

Performance optimization, A/THR and AP commands

Navigation, flight planning, performance optimization and flight predictions

10. 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, and High speed.

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.

11. An amber flashing IR FAULT light indicates that:

Attitude and heading information may be recovered in ATT mode.

Present position needs to be reentered.

A complete failure of the respective IR has occurred.

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

Four

Two

Three

One

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

Heading, attitude, and vertical speed.

Heading, attitude, and altitude.

Airspeed, altitude, and backup vertical speed.

Heading, altitude, and vertical speed

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

FMGC 1

FMGC 2

Both

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

Flaps configuration 1, 2.

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

Heading differs from track by 20 deg or more

Flaps configuration 1.

16. The DDRMI provides the pilot with:

Bearing and DME information for VOR 1 and ADF 1.

Bearing and DME information for VOR 2 and ADF 2.

Bearing only for VOR 1.

Bearing only for VOR 1 and VOR 2.

17. What is the function of the FACs?

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

Rudder and Yaw damping inputs and windshear protection

18. 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.

19. 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.

20. 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.

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

Both are correct.

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.

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

Both are correct.

Present position can be entered through the ADIRS CDU.

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

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

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.

The flight controls revert to direct law.

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

Will not allow the pilot to stall the aircraft.

Prohibit steep bank angles.

Prohibit steep climb angles and bank angles.

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

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

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

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.

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

Yes.

No

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

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

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

Yes, by setting a higher speed target.

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

Load factor.

Pitch attitude.

Roll attitude.

Bank angle.

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

Speed brakes have a fault.

Speed brakes are extended and engines are not at idle.

All of the above.

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

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

Airspeed, vertical speed, and altitude.

Airspeed, attitude, altitude, and vertical speed.

Heading, attitude, and vertical speed.

Airspeed, altitude, and backup vertical speed.

31. 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.

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

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

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

Pitch attitude.

ALPHA SPD (alpha speed)

Alpha floor.

Vls.

34. What does the LOW ACCURACY message mean?

FMCG position & IR position difference exceeds limits.

FMGC 1 & 2 position difference exceeds limits.

FMGC position & actual radio position difference exceeds limits.

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

Yes

No

36. 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

37. How long does a normal IR alignment take?

Approximately 6 minutes.

Approximately 13 minutes.

Approximately 10 minutes.

Approximately 3 minutes.

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

Yes, both LNAV and VNAV approaches are forbidden.

Yes, ILS approach only.

No

39. 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.

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

Air data output has been disconnected.

The respective IR is operating normally.

Alignment has been completed.

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

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

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

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

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

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 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.

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Questions for Automatic Flight A320