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C5 > C5 Dash 8 Caution and Warning > Flashcards

C5 Dash 8 Caution and Warning Flashcards

1
Q

TOUCHED RUNWAY

A

Fuselage contact with runway - Series 300

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2
Q

1 ENG OIL PRESS

A

Low Oil Pressure #1 Engine

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3
Q

2 ENG OIL PRESS

A

Low Oil Pressure #2 Engine

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4
Q

SMOKE

A

Smoke Present in Baggage Area

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5
Q

CHECK FIRE DET

A

Engine Fire Detected or Detector Loop Malfunction

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6
Q

CABIN PRESS

A

Cabin Altitude Exceeds 10,000 Feet

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7
Q

PASS DOOR

A

Passenger Entry Door not Properly Secured

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8
Q

BAG DOOR

A

Baggage Door Not Properly Closed

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9
Q

SERV DOOR

A

Rear Galley Service Door not Properly Closed (-300)

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10
Q

FWD EXIT DOOR

A

Forward Exit Door not Properly Closed (-300)

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11
Q

MAIN BATT HOT

A

Main Battery Temperature Exceeds 65C

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12
Q

AUX BATT HOT

A

Auxiliary Battery Temperature Exceeds 65C

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13
Q

FLT COMPT DUCT HOT

A

Overheat Condition in Flt Compt A/C Supply Duct

  • 200: System will automatically respond by closing Flight Compartment Trim Valves
  • 300: System will automatically respond by closing #2 Fwd Pack Valves.

When duct temperature returns to its normal range the caution light will extinguish and system will resume normal operation.

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14
Q

CABIN DUCT HOT

A

Overheat Condition in Cabin A/C Supply Duct

  • 200: System will automatically respond by closing pack valves closed on the ACM.
  • 300: System will automatically respond by closing pack valves on #1 ACM.

When duct temperature returns to normal operating range the caution light extinguishes and A/C system resumes normal operation.

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15
Q

AIR COND PACK HOT

A

Overheat Condition in Air Cycle Machine (-200)

System will shut HPSOV and NSOV for both engines.

When temperature returns to normal range the caution light will extinguish and bleed airflow will be restored.

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16
Q

FLT COMPT PACK HOT

A

Overheat Condition in the #2 Forward ACM (-300)

PRSOV for Pack #2 will close.

PRSOV will open and caution light will extinguish when temperature returns to normal range.

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17
Q

CABIN PACK HOT

A

Overheat Condition in the #1 Aft ACM (-300)

PRSOV for Pack #1 will close.

PRSOV will open and caution light will extinguish when temperature returns to normal range.

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18
Q

APU

A

Fault and automatic shutdown of APU.

Reference APU Control Panel for specific APU condition.

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19
Q

PRI INV

A

Primary Inverter Inoperative

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20
Q

SEC INV

A

Secondary Inverter Inoperative

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21
Q

L TRU

A

Left TRU Inoperative

DC Logic System will close Secondary Bus Tie to power Left Secondary Bus

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22
Q

R TRU

A

Right TRU Inoperative

DC Logic System will close Secondary Bus Tie to power Right Secondary Bus

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23
Q

MAIN BATTERY

A

Main Battery is Isolated from the Main DC Bus

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24
Q

AUX BATTERY

A

Aux Battery is Isolated from the Main Bus

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25
Q

1 DC GEN

A

1 DC Generator Failed or Offline

DC Logic system has taken Gen offline via its GCU and has closed Main Bus Tie to power Left Main Bus

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26
Q

2 DC GEN

A

2 DC Generator Failed or Offline

DC Logic system has taken Gen offline via its GCU and has closed Main Bus Tie to power Right Main Bus

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27
Q

1 AC GEN

A

1 AC Generator Failed or Offline

AC Gen GCU circuits will close AC Cross Tie.

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28
Q

2 AC GEN

A

2 AC Generator Failed or Offline

AC Gen GCU circuits will close AC Cross Tie.

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29
Q

AUX INV

A

Secondary Inverter Inoperative

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30
Q

L 26 AC

A

Left 26v Transformer Inoperative

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31
Q

R 26 V

A

Right 26v Transformer Inoperative

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32
Q

L AC BUS

A

No Power on Left Variable Frequency Bus

GCU Logic circuits will isolate AC Generator from faulty bus. DC Logic Circuits will close Secondary DC Bus Tie to let Right TRU power both Secondary Buses.

All services normally supplied by faulty bus will be lost.

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33
Q

R AC BUS

A

No Power on Right Variable Frequency Bus

GCU Logic circuits will isolate AC Generator from faulty bus. DC Logic Circuits will close Secondary DC Bus Tie to let Left TRU power both Secondary Buses.

All services normally supplied by faulty bus will be lost.

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34
Q

DC BUS

A

DC Bus Fault Detected

BBPU has inhibited closing of Main and Main/Secondary Bus Ties

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35
Q

L TRU HOT

A

Left Transformer Rectifier Unit Overheated

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36
Q

R TRU HOT

A

Right Transformer Rectifier Unit Overheated

37
Q

1 DC GEN HOT

A

1 DC Generator Windings Overheated

38
Q

2 DC GEN HOT

A

2 DC Generator Windings Overheated

39
Q

1 AC GEN HOT

A

1 AC Generator Windings Overheated

40
Q

2 AC GEN HOT

A

2 AC Generator Windings Overheated

41
Q

EMER LTS DISARMED

A

Emergency Lights not Armed with DC System Energized

42
Q

RUD PRESS

A

Failure of Rudder Pressure to Decrease when IAS > 140/150

Will also illuminate with one Rudder Actuator Failed as Functioning Actuator will have full 3,000 psi.

43
Q

ROLL SPLR INBD HYD

A

Inboard Spoiler Extend Circuit Depressurized

44
Q

ROLL SPLR OUTBD HYD

A

Outboard Spoiler Extend Circuit Depressurized

45
Q

1 RUD HYD

A

1 Rudder Actuator Depressurized

Rudder Pressure Regulator will admit full hydraulic pressure (3,000 psi) to #2 Rudder Actuator

46
Q

2 RUD HYD

A

2 Rudder Actuator Depressurized

Rudder Pressure Regular will admit full hydraulic pressure (3,000 psi) to #1 Rudder Actuator

47
Q

RUD FULL PRESS

A

One Rudder Actuator has Full Hydraulic Pressure (3000 psi)

48
Q

FLAP DRIVE

A

Main Flap Drive Failed

Secondary Shaft will continue to provide normal operation

49
Q

FLAP POWER

A

Loss of pressure to Flap Power Unit (less than 1,500 psi)

50
Q

FLT DATA RECORDER

A

Recorder Failed or De-engergized

Can be malfunction or A/COL (beacon) being selected off.

51
Q

1 ENG FUEL PRESS

A

1 Boost Ejector Pump Failed

Fuel pressure of fuel being delivered to left engine driven fuel pump is low.

52
Q

2 ENG FUEL PRESS

A

2 Boost Ejector Pump Failed

Fuel pressure of fuel being delivered to right engine driven fuel pump is low.

53
Q

1 TANK FUEL LOW

A

1 Tank Quantity Less than 130 Pounds

Equals approx 12 minutes of operating time on associated engine unless fuel is transferred.

54
Q

2 TANK FUEL LOW

A

2 Tank Quantity Less than 130 Pounds

Equals approx 12 minutes of operating time on associated engine unless fuel is transferred.

55
Q

FUELING ON

A

Refuel or Defuel Selected on Fueling Control Panel

Aircraft would be unable to crossfeed in flight.

56
Q

1 FUEL FLTR BYPASS

A

1 Fuel Filter Blocked or Restricted

Fuel system will automatically reroute fuel around affected filter.

57
Q

2 FUEL FLTR BYPASS

A

2 Fuel Filter Blocked or Restricted

Fuel system will automatically reroute fuel around affected filter.

58
Q

1 HYD FLUID HOT

A

Overtemp Condition in #1 Hydraulic Reservoir

59
Q

2 HYD FLUID HOT

A

Overtemp Condition in #2 Hydraulic Reservoir

60
Q

1 STB HYD PUMP HOT

A

Overtemp Condition in #1 Standby Pump Windings

61
Q

2 STB HYD PUMP HOT

A

Overtemp Condition in #2 Standby Pump Windings

62
Q

2 SPU AUX PWR

A

2 Standby Hydraulic Pump Powered by #2 AC Generator

Switches automatically from #1 AC Bus if #1 AC Bus goes offline.

63
Q

1 ENG HYD PUMP

A

Low Pressure from the #1 Main Hydraulic Pump

The #1 Standby Hydraulic Pump can be selected on to restore hydraulic pressure to the #1 system.

64
Q

2 ENG HYD PUMP

A

2 Standby Hydraulic Pump will be activated automatically from a low pressure switch.

Low Pressure from the #2 Main Hydraulic Pump

65
Q

PITOT HEAT 1

A

1 Pitot Heater Off

66
Q

PITOT HEAT 2

A

2 Pitot Heater Off

67
Q

L ELEV HORN HEAT

A

Left Elevator Horn Heat Failure

Also illuminates during Elevator Horn Heat test.

68
Q

R ELEV HORN HEAT

A

Right Elevator Horn Heat Failure

Also illuminates during Elevator Horn Heat test.

69
Q

L WSHLD HOT

A

Left Windshield Overheated

System will de energize window until the window temperature cools.

Or loss of power to window heater element.

70
Q

R WSHLD HOT

A

Right Windshield Overheated

System will de energize window until the window temperature cools.

Or loss of power to window heater element.

71
Q

SIDE WDO HOT

A

Pilot’s Side Window Overheated

System will de energize window until the window temperature cools.

Or loss of power to window heater element.

72
Q

DEICE PRESS

A

Deice Pressure Too Low for Boot Operation

73
Q

NOSE STEERING

A

Steering ECU Malfunction

Exceeding 60 deg of travel in free castor mode.

Light will extinguish when nosewheel is back within 60 deg of center.

74
Q

PARKING BRAKE

A

Parking Brake in On

75
Q

OUTBD ANTI SKID

A

Outboard Anti-Skid Control Unit Failure

Also illuminates during self-test.

76
Q

INBD ANTI SKID

A

Inboard Anti-Skid Control Unit Failure

Also illuminates during self-test.

77
Q

LND GEAR INOP

A

Failure of Landing Gear Door Sequencing Valve

78
Q

WT ON WHEELS

A

Fault in Weight on Wheels Sensing Circuits

79
Q

1 BLEED HOT

A

Overheat Condition in #1 Bleed Air Supply Duct

HPSOV and NSOV will close on affected side until bleed system returns to normal temperature.

80
Q

2 BLEED HOT

A

Overheat Condition in #2 Bleed Air Supply Duct

HPSOV and NSOV will close on affected side until bleed system returns to normal temperature.

81
Q

1 ENG MANUAL

A

Failure of #1 Engine ECU

  1. Fuel scheduling will revert to manual via MFC
  2. Torque increase of 8-10%
  3. Loss of Np Underspeed Protection
  4. Loss of HBOV automatic operation
  5. Loss of power uptrim
82
Q

2 ENG MANUAL

A

Failure of #2 Engine ECU

Fuel scheduleing will revert to manual via MFC
 Torque increase of 8-10%
 Loss of Np Underspeed Protection
 Loss of HBOV automatic operation
 Loss of power uptrim
83
Q

L STALL WARNING

A

Left Lift Computer or Lift Transducer Inoperative (-200)

Also loss of heater element in associated transducer.

Fast-slow indicator on left EADI will be inoperative.

84
Q

R STALL WARNING

A

Right Lift Computer or Lift Transducer Inoperative (-200)

Also loss of heater element in associated transducer.

Fast-slow indicator on right EADI will be inoperative.

85
Q

1 STALL SYST FAIL

A

Fault in #1 Stall Warning / Stick Pusher Computer (-300)

Also #1 AOA heater element failure or #1 AOA vane power loss.

PUSHER SYS FAIL caution will illuminate as well.

86
Q

2 STALL SYST FAIL

A

Fault in #2 Stall Warning / Stick Pusher Computer (-300)

Also #2 AOA heater element failure or #2 AOA vane power loss.

PUSHER SYS FAIL caution will illuminate as well.

87
Q

PUSHER SYST FAIL

A

Malfunction in Stick Pusher System (-300)

Stick pusher will be offline

88
Q

GPWS

A

Failure of Ground Proximity Warning System

C5 (12 decks)

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