Annunciators Flashcards

1
Q
A

At or below altitude set on radio altimeter

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2
Q
A

Flashing - Spoilers deployed with 13 deg or more flaps extended (normal on landing roll)

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3
Q
A

One of 10 latch pins not fully engaged or hook motor not fully retracted

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4
Q
A
  1. Spoilers split 6 deg or more
  2. Spoiler and aileron split 6 deg or more in spoileron mode
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5
Q
A
  1. One or both pitot heaters is INOP with switches ON
  2. One or both of the pitot switches is off
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6
Q
A

Fuel is below 400-500lbs in EITHER wing tank

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7
Q
A

Steady - Spoilers not lcoked down (normal if extended)

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8
Q
A

Differential pressure is 1.25psi across one or both airframe fuel filters.

FUEL IS BYPASSING FILTER

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9
Q
A

Less than 0.25psi fuel pressure to engine (light extinguishes as 1.0psi)

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10
Q
A
  1. Switch ON - insufficient pressure to nacelle or fan spinner or failure of valve(s) open
  2. Switch OFF - nacelle or fan spinner valve(s) open
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11
Q
A
  1. Switch is OFF
  2. Computer has failed with switch ON
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12
Q
A
  1. Steady - system is off or failed (normal during pusher)
  2. Flashing - In shaker range
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13
Q
A

One motor in the vertical gyro has failed

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14
Q
A

System is INOP with speed above 0.69m and autopilot disengaged.

Overspeed warning horn sounds at 0.74m

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15
Q
A
  1. Inverter is off
  2. Inverter switch is on and output is less than 90v or less than 10 volt-amps
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16
Q
A

Inverter has failed with switch on

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17
Q
A

Oil pressure on one or both engines is below 23 +/-1psi

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18
Q
A

Stabilizer structural temp is above 215 F

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19
Q
A

Windshield heat has been turned off by temperature limit.

GND - high or low limit

AIR - high limit only

20
Q
A

Nosewheel steering is engaged

21
Q
A
  1. Overtemp of pylon or duct
  2. BOTH lights - Manifold over pressure
22
Q
A

Indicated generator is off or has failed

23
Q
A

Cabin altitude has reached 8,750 ft give or take 250ft and controller has switched to manual

24
Q
A

Wing structural temp is above 215 F

25
Q
A

Windshield anti-ice valve is open

26
Q
A

One or more battery temp is 140 F or more

land as soon as PRACTICAL

27
Q
A

One or more battery temp is 160 F or more

Land as soon as POSSIBLE

28
Q
A

The engine sync switch is on with the nose gear down and locked

29
Q
A

Airplane is on the ground and the horizontal stabilizer is not trimmed for takeoff

30
Q
A

Failure of either or both 275 amp limiters

31
Q
A

Fire extringuishing bottles are armed

32
Q
A

Fire/overheat is detected in associated engine

33
Q
A

A red light on the master warning panel is illuminated

34
Q
A

LOW HYD - hydraulic pressure 1,125psi or less

FUEL XFLO - Fuel xflow valve is open

L/R LO OIL - indicated engine oil pressure is low

35
Q
A
  1. primary pitch is running at fast rate with flaps up
  2. primary pitch has a fault (potential runaway)
  3. wheel master (MSW) switch is pressed
36
Q
A

Ferrous metal particles are detected in indicated engine oil

37
Q
A

Indicated emergency battery is powering the connected systems

38
Q
A

Indicated starter is engaged

39
Q
A

HSI heading not within 7deg

40
Q
A

Nacelle heat switches (or indicated switch) is on

41
Q
A

Ignition system is activated

42
Q
A

Indicated anti-skid generator is INOP

43
Q
A

Indicated 275 amp current limiter has failed

44
Q
A
  1. indicated pitot switch off or heat has failed
45
Q
A

Parking brake is set or brake is not fully in after release

46
Q
A
  1. illuminates momentarily when WSHLD DEFOG is set ON
  2. Overheat/underheat condition when ON
47
Q
A