WARNING & RECORDING Flashcards

1
Q
  1. The input to a basic stall warning system are:
A

a Angle of attack

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2
Q
  1. Where in the aircraft does JAR require the FDR to be fitted:
A

a At the back

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3
Q
  1. An FDR fitted to an aircraft of over 5700kgs after Apr 98 must record for:
A

b 25 hours

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4
Q
  1. Where is TCAS displayed?
  2. On its own screen
  3. On the EFIS
  4. Weather Radar
  5. On VSI
A

a. All 4

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5
Q
  1. The principle that TCAS uses is:
A

d. Transponders in the aircraft

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6
Q
  1. When an intruder aircraft has no Altitude Reporting facility, i.e. Mode equipped with ‘A’ transponder only, TCAS can only give:
A

c. TA only

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7
Q

What does a FDR record when combined with a CVR?

  1. Cockpit voice
  2. Radio
  3. Public addresses from the cockpit
  4. Cabin voice
A

a. 1, 2 & 3

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8
Q
  1. A GPWS system requires:
A

c Aural signals which may be supplemented by visual signals

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9
Q
  1. The Altitude Alert system alerts the pilot:
A

d When deviating from the selected altitude

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10
Q
  1. The Altitude Alert system:
A

a. May alert by visual signals when approaching the selected altitude

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11
Q
  1. TCAS II obtains information from:
    Pressure encoding from mode S transponder Radio altimeter
    Aircraft specific configurations
    Inertial reference unit (IRU)
A

c. 1, 2, & 3

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12
Q
  1. What does a CVR record?
A

d. Radio conversations

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13
Q
  1. A stall warning system fitted to a large aircraft will always include:
A

b Various inputs including landing gear micro switch, a warning module and an aural warning

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14
Q
  1. GPWS is active between what heights:
A

50ft and 2450 ft

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15
Q
  1. What is the correct response to a TCAS RA?
A

Smoothly and immediately follow the climb or descent commands

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16
Q
  1. What symbol is used to represent a RA on a TCAS PPI?
A

c. Red square

17
Q
  1. Which of the following is a preventative RA?
A

a. Monitor vertical speed

18
Q
  1. What input is there to TCAS 2?
A

d Mode ‘S’ transponder which co-ordinates avoidance manoeuvres

19
Q
  1. An aircraft registered after the 1 April 1998 requires a CVR which:
A

a. Records the last 2 hours of flight

20
Q
  1. What are the JAR OPS requirements for the CVR to start and stop recording?
A

a. From the time when the aircraft is first able to move under its own power until it is no longer able to do so.

21
Q
  1. An altitude alerting system must at least be capable of alerting the crew on:
  2. Approaching selected altitude.
  3. Excessive deviation from selected altitude.
  4. Excessive vertical speed.
  5. Excessive terrain closure.
  6. Abnormal gear/flap combination.
22
Q
  1. An aircraft that weights more than 5,700 kg and was registered after 1 April 1998, the FDR and CVR must record respectively:
A

b. 25 hr. and 2 hr.

23
Q
  1. “Other traffic” which is assessed as not being a threat will be indicated by a TCAS system as:
A

c. A hollow cyan diamond.

24
Q
  1. Which of the following are modes of the GPWS?
  2. Excessive sink rate.
  3. Altitude loss after T/O or go-around.
  4. Excessive Glideslope deviation.
  5. High climb rate.
  6. Flaps in incorrect position.
  7. High altitude descent.
  8. Stall.
A

b. 1, 2, 3, & 5

25
25. What corrective action is given by TCAS?
b. Climb or descend.
26
26. The Flight Data Recorder actually starts running:
b. Before the a/c starts moving under its own power
27
27. GPWS may indicate (list): 1. Excessive sink rate after T/O. 2. Excessive descent rate. 3. Excessive closure with terrain. 4. Ground proximity not in the landing configuration. 5. Excessive glide-slope deviation. 6. Altitude call-outs. 7. Bank Angle alerting.
All 7
28
28. TCAS 2 when fitted with mode C transponder may give:
TA and RA in vertical plane.
29
29. According to JAR OPS when must the CVR on a 50 seat turbo prop a/c begin recording?
From before the a/c is capable of moving under its own power to after the a/c is no longer capable of moving under its own power.
30
30. What is the GPWS Mode 3 audible alert?
DON’T SINK, DON’T SINK continuously.
31
31. CVR components consist of: 1. Microphone 2. Crash/Fire resistant construction 3. Independent battery 4. A Flight data recorder
a. 1& 2
32
32 If an aircraft GPWS detects an excessive rate of descent with gear and flaps up, the alert and warning will be:
SINK RATE followed by ‘WHOOP WHOOP PULL UP.
33
33 The requirement to carry a GPWS concerns aircraft which are, depending on their age, weight and passenger capacity: 1. Turbo prop. 2. Piston. 3. Jet.
b. 1, 3