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CPL Test Series
Question Bank
Questions for Kw inst Warning and recording
Answer the following questions
Test Mode
Training Mode
1. In an aircraft of more than 5700 kg mass certificated under JAR after April 1998, the FDR must record for?
10 hours
60 minutes
30 minutes
25 hours.
2. 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
1, 2, 3.
1, 4, 5.
All of the above.
2, 3, 4.
3. 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
2, 3, 4, 5.
1, 3, 4, 5.
1, 2, 3, 4.
1, 2, 4, 5.
4. JAR OPS requires that the FDR must be located at?
The top of an aircraft.
The bottom of an aircraft.
The front of an aircraft.
The back of an aircraft.
5. 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, 2, 3, 4, 5.
1, 3, 4, 5, 6, 7.
2, 5, 6, 7.
4, 5, 6, 7.
6. What type of warning must be provided by a basic GPWS?
Aural
Tactile, aural and light.
Light
Aural and light
7. The GPWS mode 3 audible alert is?
Repeated "Sink rate, Sink rate, Whoop, Whoop".
Repeated "Whoop, Whoop, Don't sink, Don't sink".
Repeated "Don't sink, Don't sink".
Repeated "Pull up, Pull up".
8. 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
1, 2.
All of the above.
3, 4.
2, 3, 4.
9. An altitude alert system?
Alert the pilot when decision height is reached.
Alerts the pilot if the aircraft deviates from selected altitude.
Alerts the pilot when the selected height is reached.
Alerts the pilot when the actual altitude is equal to the reference altitude.
10. 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.
2, 3, 5.
1, 2, 3, 4, 5.
11. JAR OPS requires a 50 seat turbo-prop aircraft CVR to record
Before starting to taxi to when the parking brake is applied.
From BRP to touch - down.
From battery master switch on to off.
Whenever the aircraft is able to move under its own power.
12. The function of the altitude alert system is to?
Disengage auto - trim when reaching selected altitude.
Upon sensing an unacceptable situation, it is to engage autopilot and fly the aircraft into a safe condition.
Illuminate a warning light as the aircraft approaches the selected altitude.
Engage auto trim when the aircraft reaches its selected altitude
13. 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
2, 3, 4.
All of the above.
3, 4, 5.
1, 2, 4.
14. 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
4, 5.
1, 4.
3, 4.
1, 2.
15. GPWS operates between ?
Zero and 3450 ft.
50 ft and 2450 ft.
50 ft and 2500 ft.
Zero and 2500 ft.
16. The altitude alerting system?
Alerts pilot when approaching selected altitude.
Alerts pilot upon reaching selected altitude.
Alerts pilot at decision height.
Alerts pilot of all changes in altitude.
17. A FDR must be fitted?
In the cockpit
Close to the engines.
At the back of an aircraft.
At the front of an aircraft
18. The inputs to a modern jet aircraft stall warning system include? 1. Alpha 2.Configuration. 3.Engine RPM. 4. Pitch attitude. 5.AOB
3, 4, 5.
All of the above.
1, 2.
2, 3, 4.
19. A basic stall warning system monitors?
Slat and flap position.
CAS
Mach number
A of A
20. In the altitude alerting system what lights indicate a deviation of more than 300 ft from selected altitude?
Steady amber.
Flashing red.
Flashing amber.
Steady red.
21. 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
1, 2, 3, 5.
4, 5, 6, 7.
3, 4, 6, 7.
2, 4, 5, 6.
22. Between what heights is GPWS active?
zero and 2500 ft.
zero and 500 ft.
50 ft and 500 ft.
50 ft and 2450 ft.
23. 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
All of the above.
3, 4, 5.
2, 3, 4.
1, 2, 3.
24. 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, 4, 5, 6, 7.
2, 3, 4, 5, 6, 7.
All of the above.
1, 2, 3, 5, 6, 7.
25. The CVR in a 50 seat turbo-prop aircraft must record?
From commencing pre take-off taxi to turning of the runway after landing.
From switching on to switching off electrical power.
From first being able to move under its own power to next becoming unable to do so.
From lift-off to touch-down.
26. The flight deck FDR and CVR must be capable of recording for at least?
48 hrs, 45 mins
25 hrs, 30 mins.
15 hrs, 60 mins.
24 hrs, 60 mins.
27. The FDR starts recording when?
When the leading gear squat swich detects lift-off.
When the undercarriage retract button is pressed.
When the brakes are released.
Before the aircraft starts to move under its own power.
28. An altitude warning system?
Automatically disengages autotrim at 500 ft.
Activates a warning light and bell when approaching a selected altitude.
Provides visual alerts when approaching a selected altitude.
Automatically engages autotrim at 500 ft.
29. A flight data recorder is required in ........... aircraft weighing more than 5700 kg? 1. Turbojets. 2.Turboprops. 3. Plstonprops
1, 2.
2, 3.
3, 4.
All of the above.
30. A CVR system includes? 1. Microphones. 2.FDR 3.Independent battery power supply. 4.Crash and fire resistant construction
1, 3.
1, 4.
3, 4.
2, 3.
31. A stall warning system in a large JAR certificated aircraft must include?
Monitoring of speed brake position and angle of attack, a warning module, and visual or aural warning system.
Monitoring of A of A and TAS, plus aural and visual warnings.
Monitoring of landing gear squat switch and A of A, a warning module and an aural warning.
Stick shaker and stick pusher.
32. 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, 3, 4.
All of the above.
1, 2, 3.
2, 3, 4.
33. GPWS modes include? 1. Stall. 2.High alpha. 3.Excessive ROD. 4.Excessive terrain closure rate. 5.Incorrect flap position
3, 4, 5.
All of the above.
2, 3, 4.
1, 2, 3.
34. GPWS must provide?
Visual and aural warnings, which may be supplemented by tactile warnings.
Visual warnings.
Aural and visual warnings
Aural warnings which may be supplemented by visual warnings.
35. 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
36. The FDR must start running when?
When the gear up button is pushed.
At brake release for take-off.
When lined up for take - off.
Before the aircraft starts moving under its own power.
37. The FDR in a JAR certificated aircraft must be located in?
The outer wings.
The front.
The undercarriage bay.
The back.
38. In an aircraft certificated under JAR since 1 April 1998 the CVR must record for?8
8 hours.
2 hours
72 hours.
30 minutes.
39. GPWS will give an altitude alert warning when?
Decision height is reached in a cat 2 or 3 ILS approach.
The aircraft lases glideslope signal.
AOB is excessive at low altitude.
The angle of attack approaches the stalling angle.
40. For certification of a heavy aircraft after 1 April 1998 the FDR and CVR must record for ........ and ....... respectively
25 hours 2hours.
25 hours 1 hour.
10 hours 2 hours.
10 hours 1 hour
41. 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
4.
5
3, 5.
1, 3.
42. A CVR records?
Cabin crew conversations
Crew conversation on intercom.
Public address announcements and cockpit discussions.
Radio conversations
43. GPWS operates between?
Zero and 1500 ft.
50 ft and 2450 ft.
Zero and 5000 ft.
Zero and 500 ft.
44. The GPWS mode 3 audible alert is?
Initially "don't sink, don't sink", which is followed by "Whoop, whoop, pull up", If the maximum allowable sink rate is exceeded.
Continuous "don't sink, don't sink".
"Don't sink, don't sink, whoop, whoop, pull up".
"Sink rate, sink rate".
45. From what does the GPWS obtain its height information?
Barometric altimeter.
RADALT.
IRS
INS
46. Over what range is GPWS operative?
50 to 2450 ft pressure altitude.
Zero to 2500 radio altitude.
50 to 2450 m.
50 to 2450 ft agl.
47. A basic stall warning system in a light aircraft senses?
Slat and flap positions
M no
IAS.
Alpha.
48. If sink rate is excessive the GPWS indications will be?
Don't sink, Whoop, Whoop, Pull up.
Too low, Toe low, Wheop, Whoop, Pull up.
Too low gear, Too low gear, Whoop, Whoop, Pull up, Pull up.
Sink rate, Whoop, Whoop, Pull up.
49. JAR OPS require a CVR to start and stop recording?
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 engine start up to engine shut down.
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 of engine shut down.
50. The FDR in an aircraft of mass exceeding 5700 kgs, certificated after April 1998 must be capable of recording for at least?
60 minutes
30 minutes.
24 hours
25 hours
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