Vayudoot Aviation

1. An altitude alerting system is required to alert the crew of at least the following? 1. Abnormal flap and gear configurations. 2. Excessive closure with terrain. 3. Excessive vertical speed. 4. Excessive deviation from selected altitude. 5. Approaching selected altitude

1, 4.

1, 2.

4, 5.

3, 4.

2. What level of voice recording is required in multi-turbine engined aircraft with 9 or more passenger seate, certificated after January 1998? 1. Flight deck crew calls on intercom. 2. Flight deck crew calls on public address. 3. Internal cockpit communications. 4.External cockpit communications. 5. Cockpit environmental noises

1, 2, 3.

3, 4, 5.

2, 3, 4.

All of the above.

3. GPWS may give warnings of? 1. Excessive sink rate. 2. Excessive closure with terrain. 3. Excessive proximity with ground when not in landing configuration. 4. Excessive AOB

1, 2, 3.

2, 3, 4.

1, 3, 4.

All of the above.

4. The FDR must start running when?

Before the aircraft starts moving under its own power.

At brake release for take-off.

When lined up for take - off.

When the gear up button is pushed.

5. A combined FDR and CVR records? 1. Cockpit voice discussions. 2. Cabin voice discussions. 3. Radio discussions. 4.All Public address messages from the cockpit.

1, 2, 3.

2, 3, 4.

1, 2, 4.

1, 3, 4

6. A JAR certificated CVR must record? 1.All voce communications within the aircraft. 2.All crew voice communications within the aircraft. 3.All PA announcement. 4.All discussions between crew and ATC. 5. All signals from navigation aids

5

3, 5.

1, 3.

4.

7. A cockpit voice recorder must be capable of recording? 1. Flight deck and cabin crew intercom discussions. 2.Radio discussions. 3. Public address system announcements. 4. Flight deck noise environment. 5. Navigation aid indents

1, 3, 4, 5.

1, 2, 3, 4.

1, 2, 4, 5.

2, 3, 4, 5.

8. What type of warning must be provided by a basic GPWS?

Light

Tactile, aural and light.

Aural and light

Aural

9. In an aircraft certificated under JAR since 1 April 1998 the CVR must record for?8

30 minutes.

8 hours.

72 hours.

2 hours

10. GPWS must provide?

Aural warnings which may be supplemented by visual warnings.

Aural and visual warnings

Visual and aural warnings, which may be supplemented by tactile warnings.

Visual warnings.

11. GPWS modes include? 1. Incorrect gear position. 2. Altitude loss after lift-off or during Go-around. 3. High altitude descent. 4.Excessive glide slope deviation. 5. Excessive AOB

3, 4, 5.

2, 3, 4.

All of the above.

1, 2, 4.

12. The flight deck FDR and CVR must be capable of recording for at least?

25 hrs, 30 mins.

48 hrs, 45 mins

15 hrs, 60 mins.

24 hrs, 60 mins.

13. GPWS modes include? 1. Stalt 2.Incorrect flap positions. 3.High altitude descents. 4.High ROC. 5. Excessive glideslope deviations. 6. Loss of altitude after take-off and go-around. 7. Excessive stock rate

1, 3, 4, 5, 6, 7.

1, 2, 3, 4, 5.

4, 5, 6, 7.

2, 5, 6, 7.

14. GPWS operates between?

Zero and 500 ft.

Zero and 5000 ft.

50 ft and 2450 ft.

Zero and 1500 ft.

15. The FDR in an aircraft of mass exceeding 5700 kgs, certificated after April 1998 must be capable of recording for at least?

24 hours

60 minutes

30 minutes.

25 hours

16. A CVR records?

Radio conversations

Crew conversation on intercom.

Public address announcements and cockpit discussions.

Cabin crew conversations

17. Over what range is GPWS operative?

50 to 2450 m.

Zero to 2500 radio altitude.

50 to 2450 ft agl.

50 to 2450 ft pressure altitude.

18. The FDR in a JAR certificated aircraft must be located in?

The front.

The outer wings.

The undercarriage bay.

The back.

19. A FDR must be fitted?

At the front of an aircraft

In the cockpit

Close to the engines.

At the back of an aircraft.

20. The GPWS mode 3 audible alert is?

Continuous "don't sink, don't sink".

"Sink rate, sink rate".

Initially "don't sink, don't sink", which is followed by "Whoop, whoop, pull up", If the maximum allowable sink rate is exceeded.

"Don't sink, don't sink, whoop, whoop, pull up".

21. A CVR system includes? 1. Microphones. 2.FDR 3.Independent battery power supply. 4.Crash and fire resistant construction

1, 3.

3, 4.

2, 3.

1, 4.

22. The function of the altitude alert system is to?

Engage auto trim when the aircraft reaches its selected altitude

Upon sensing an unacceptable situation, it is to engage autopilot and fly the aircraft into a safe condition.

Disengage auto - trim when reaching selected altitude.

Illuminate a warning light as the aircraft approaches the selected altitude.

23. A basic stall warning system in a light aircraft senses?

M no

IAS.

Slat and flap positions

Alpha.

24. Which of the following are GPWS modes? 1. Approaching stall. 2. Excessive glideslope deviation. 3. Excessive ROC. 4. Excessive ROD. 5.Incorrect flap position. 6.Sinking after lift-off and during go-around. 7. High altitude descent

2, 4, 5, 6.

1, 2, 3, 5.

4, 5, 6, 7.

3, 4, 6, 7.

25. The components of a modern jet aircraft stall warning system include? 1. Angle of attack sensors. 2. Bank rate sensors. 3. Control surface position sensors. 4.Stick shaker. 5.Gear and flap sensors

All of the above.

1, 4, 5.

1, 2, 3.

2, 3, 4.

26. For certification of a heavy aircraft after 1 April 1998 the FDR and CVR must record for ........ and ....... respectively

10 hours 1 hour

25 hours 1 hour.

25 hours 2hours.

10 hours 2 hours.

27. In the altitude alerting system what lights indicate a deviation of more than 300 ft from selected altitude?

Flashing red.

Steady amber.

Steady red.

Flashing amber.

28. The FDR starts recording when?

When the leading gear squat swich detects lift-off.

Before the aircraft starts to move under its own power.

When the brakes are released.

When the undercarriage retract button is pressed.

29. JAR OPS requires that the FDR must be located at?

The back of an aircraft.

The top of an aircraft.

The bottom of an aircraft.

The front of an aircraft.

30. If sink rate is excessive the GPWS indications will be?

Too low, Toe low, Wheop, Whoop, Pull up.

Too low gear, Too low gear, Whoop, Whoop, Pull up, Pull up.

Don't sink, Whoop, Whoop, Pull up.

Sink rate, Whoop, Whoop, Pull up.

31. A JAR certificated altitude alerting system must be capable of warning of at least? 1. Deviation from selected altitude. 2. Approaching selected altitude. 3. Excessive vertical speed. 4. Excessive terrain closure rate. 5.Abnormal flap and landing gear configuration for current height

2, 3.

1, 4.

1, 2, 3, 4, 5.

2, 3, 5.

32. An altitude warning system?

Automatically disengages autotrim at 500 ft.

Automatically engages autotrim at 500 ft.

Provides visual alerts when approaching a selected altitude.

Activates a warning light and bell when approaching a selected altitude.

33. GPWS will give an altitude alert warning when?

AOB is excessive at low altitude.

The angle of attack approaches the stalling angle.

The aircraft lases glideslope signal.

Decision height is reached in a cat 2 or 3 ILS approach.

34. GPWS operates between ?

50 ft and 2500 ft.

Zero and 3450 ft.

50 ft and 2450 ft.

Zero and 2500 ft.

35. From what does the GPWS obtain its height information?

RADALT.

INS

IRS

Barometric altimeter.

36. The CVR in a 50 seat turbo-prop aircraft must record?

From lift-off to touch-down.

From first being able to move under its own power to next becoming unable to do so.

From switching on to switching off electrical power.

From commencing pre take-off taxi to turning of the runway after landing.

37. A stall warning system in a large JAR certificated aircraft must include?

Stick shaker and stick pusher.

Monitoring of landing gear squat switch and A of A, a warning module and an aural warning.

Monitoring of A of A and TAS, plus aural and visual warnings.

Monitoring of speed brake position and angle of attack, a warning module, and visual or aural warning system.

38. In an aircraft of more than 5700 kg mass certificated under JAR after April 1998, the FDR must record for?

30 minutes

60 minutes

10 hours

25 hours.

39. A basic stall warning system monitors?

Mach number

CAS

Slat and flap position.

A of A

40. GPWS may give warnings of ? 1. Deviations from selected altitude. 2. Excessive deviations from glideslope. 3.Excessive sink rate after lift-off. 4. Excessive ROD

2, 3, 4.

All of the above.

3, 4.

1, 2.

41. A flight data recorder is required in ........... aircraft weighing more than 5700 kg? 1. Turbojets. 2.Turboprops. 3. Plstonprops

All of the above.

2, 3.

1, 2.

3, 4.

42. JAR OPS requires a 50 seat turbo-prop aircraft CVR to record

From battery master switch on to off.

Whenever the aircraft is able to move under its own power.

From BRP to touch - down.

Before starting to taxi to when the parking brake is applied.

43. GPWS modes include? 1. Stall. 2.High alpha. 3.Excessive ROD. 4.Excessive terrain closure rate. 5.Incorrect flap position

3, 4, 5.

1, 2, 3.

All of the above.

2, 3, 4.

44. Between what heights is GPWS active?

50 ft and 500 ft.

zero and 2500 ft.

zero and 500 ft.

50 ft and 2450 ft.

45. The altitude alerting system?

Alerts pilot at decision height.

Alerts pilot of all changes in altitude.

Alerts pilot when approaching selected altitude.

Alerts pilot upon reaching selected altitude.

46. The GPWS mode 3 audible alert is?

Repeated "Sink rate, Sink rate, Whoop, Whoop".

Repeated "Don't sink, Don't sink".

Repeated "Whoop, Whoop, Don't sink, Don't sink".

Repeated "Pull up, Pull up".

47. JAR OPS require a CVR to start and stop recording?

From when the APU or first engine is started to when the APU or last engine is shut down.

From when the aircraft is first able to move under its own power to the time at which it is next unable to do so.

From when the aircraft is first able to move under its own power to the time of engine shut down.

From engine start up to engine shut down.

48. The inputs to a modern jet aircraft stall warning system include? 1. Alpha 2.Configuration. 3.Engine RPM. 4. Pitch attitude. 5.AOB

1, 2.

3, 4, 5.

All of the above.

2, 3, 4.

49. An altitude alert system?

Alerts the pilot if the aircraft deviates from selected altitude.

Alerts the pilot when the actual altitude is equal to the reference altitude.

Alerts the pilot when the selected height is reached.

Alert the pilot when decision height is reached.

50. GPWS can indicate? 1.Excessive bank angle. 2.Excessive terrain closure rate. 3.Excessive sink rate after lift-off. 4.Excessive glideslope deviations. 5. Too close to ground when not in landing configuration. 6. Excessive rate of descent. 7.Altitude call-outs

1, 2, 3, 5, 6, 7.

1, 4, 5, 6, 7.

2, 3, 4, 5, 6, 7.

All of the above.

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