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Dash 8 > Cautions & Warnings > Flashcards

Cautions & Warnings Flashcards

0
Q

CABIN PRESS

A

Cabin Altitude exceeds 10,000’

OR

Fault in the Cabin Pressurisation Computer (fault light must be illuminated)

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1
Q

BAG DOOR

A

Baggage door is not properly closed

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2
Q

FLT COMPT DUCT HOT

A

Flight compartment duct temperature exceeds 88°C

Pack control valves will drive to the full cold position until 82°C

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3
Q

CABIN DUCT HOT

A

Cabin duct temperature exceeds 88°C

Pack control valves will drive to the full cold position until 82°C

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4
Q

CABIN PACK HOT

A

ACM compressor discharge temp exceeds 207°C

Normal operation automatically interrupted. Bleed Air system shutdown until ACM cools

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5
Q

FLIGHT COMPT PACK HOT

A

ACM compressor discharge temp exceeds 207°C

Normal operation automatically interrupted. Bleed Air system shutdown until ACM cools

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6
Q

TOUCHED RUNWAY

A

Rear outer fuselage surface below pressure bulkhead has touched the RWY

Advise Maintenance

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7
Q

SERV DOOR

A

Service door not properly closed (N/A to the 200)

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8
Q

PRI INV

A

Primary Inverter is inoperative

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9
Q

DC BUS

A

DC Bus fault detected.

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10
Q

SEC INV

A

Secondary Inverter is inoperative

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11
Q

AUX INV

A

Auxiliary Inverter is inoperative

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12
Q

L 26 AC

A

Left 26V fixed frequency transformer is inoperative.

Possible loss of associated 115V fixed frequency bus

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13
Q

R 26 AC

A

Right 26V fixed frequency transformer inoperative

Possible loss of associated 115V fixed bus

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14
Q

APU

A

ESU has detected a fault has automatically shut down the APU

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15
Q

R AC BUS

A

Right AC variable frequency bus not powered

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16
Q

L AC BUS

A

Left AC variable frequency bus not powered

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17
Q

What happens with a DC BUS caution?

A 
# The BBPU inhibits buses from tying for 7 seconds.
# After 7 seconds if fault is still evident, it will isolate and shutdown the associated DC GEN and will isolate the affected  
# Battery from the faulty main bus
# All services on affected MAIN BUS will be lost.
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18
Q

L TRU

A

Left TRU is inoperative

SEC BUS will tie

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19
Q

MAIN BATTERY

A

Main Battery has been isolated from R MAIN BUS

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20
Q

AUX BATTERY

A

Auxiliary Battery is isolated from L MAIN BUS

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21
Q

1 DC GEN

A

1 DC GEN is offline or has failed

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22
Q

2 DC GEN

A

2 DC GEN is offline or has failed

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23
Q

1 AC GEN

A

1 AC GEN is offline or has failed

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24
Q

2 AC GEN

A

2 AC GEN is offline or has failed

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25
Q

MAIN BAT HOT

A

Main Battery temperature exceeds 65°C

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26
Q

AUX BAT HOT

A

Auxiliary Battery temperature exceeds 65°C

27
Q

L TRU HOT

A

Left TRU has overheated

28
Q

R TRU

A

Right TRU is inoperative

SEC BUS will tie

29
Q

1 DC GEN HOT

A

Generator windings have overheated

30
Q

How can a TRU be shutdown

A

By pulling the associated TRU CB on the 115V AC VAR FREQ panel

31
Q

1 AC HOT

A

Generator windings have overheated

32
Q

2 AC HOT

A

Generator windings have overheated

33
Q

2 DC GEN HOT

A

Windings of generator have overheated

34
Q

SMOKE

A

Smoke is detected in the baggage area

35
Q

EMER LTS DISARMED

A

Emergency lights not armed OR DC system not energised

36
Q

FWD EXIT DOOR

A

Forward exit door not properly secured

37
Q

PASS DOOR

A

Passenger entry door not properly secured

38
Q

Where are the Fire Detection loops situated

A

Loop A - maintains temperature monitoring over the complete engine nacelle

Loop B - maintains temperature monitoring near the inter- compressor case near the P2.5/P3.0 pipe only

39
Q

CHECK FIRE DET

A

Engine fire detected or detector loop circuit malfunction

40
Q

RUD PRESS

A

1/2 rudder actuator pressure failed to regulate pressure based on airspeed.

Failed to DECREASE to 900psi ABV 150KTS
Failed to INCREASE to 1500psi BLW 150KTS

Reduce airspeed to 200KTS

41
Q

FLAP POWER

A

Loss of Hydraulic pressure in Flap Power Unit (<1500psi) during extension or retraction

42
Q

ROLL SPLR OUTBD HYD

A

Hydraulic de-pressurisation of OB roll spoilers extension circuit

43
Q

ROLL SPLR INBD HYD

A

Hydraulic de-pressurisation of IB roll spoilers extension circuit

44
Q

1 RUD HYD

A

1 rudder actuated de-pressurised

Px decreasing BLW 900psi

45
Q

2 RUD HYD

A

2 rudder actuated de-pressurised

Px decreasing BLW 900psi

46
Q

FLAP DRIVE

A

Main Flap Drive failure.

Flaps will using secondary transmission shaft

47
Q

RUD FULL PRESS

A

Either rudder actuator has de-pressurised causing 3000psi to be applied to remaining actuator.

48
Q

FLT DATA RECORDER

A

FDR has failed or is de-energised (Anti-Col lights off)

49
Q

1 ENG FUEL PRESS

A

1 engine boost ejector pump has failed (output less than 5.5psi)

50
Q

2 ENG FUEL PRESS

A

2 engine boost ejector pump has failed and output Px is less than 5.5psi

51
Q

2 FUEL TANK LOW

A

2 fuel tank has less than 130LBS

52
Q

2 FUEL FLTR BYPASS

A

Fuel filter has become restricted or is blocked

53
Q

FUELLING ON

A

REFUEL or DEFUEL selection has been made on the refuelling panel

Tank to tank XSF not available

54
Q

1 FUEL FLTR BYPASS

A

Fuel filter has become restricted or is blocked

55
Q

1 FUEL TANK LOW

A

1 fuel tank has less than 130LBS

56
Q

1 HYD FLUID HOT

A

1 HYD fluid exceeds 109°C

Caution light extinguishes when fluid cools to 95°C

Operate services powered by # 1 HYD system to circulate fluid and cool fluid

57
Q

2 HYD FLUID HOT

A

2 HYD fluid has exceeded 109°C

Caution light extinguishes when fluid cools to 95°C

Operate services powered by # 2 HYD system to circulate fluid and cool fluid

58
Q

1 STBY HYD PUMP HOT

A

1 Standby Pump electric motor exceeds 170°C

59
Q

2 STBY HYD PUMP HOT

A

2 Standby HYD pump electric motor temperature exceeds 170°C

60
Q

1 ENG HYD PUMP

A

1 Engine driven hydraulic pump outlet pressure less than 2000psi

61
Q

2 ENG HYD PUMP

A

2 Engine driven hydraulic pump outlet pressure less than 2000psi

62
Q

2 SPU AUX PWR

A

Failure of one of two AC power sources to # 2 SPU

63
Q

PITOT HEAT 1/2

A

Pitot heat selected off with DC system energised

64
Q

B
Siding
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A

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65
Q

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A

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66
Q

Hello

A

Goodbye

Dash 8 (7 decks)

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