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Dash 8 Q400 > Warning/Caution Panel Lights > Flashcards

Warning/Caution Panel Lights Flashcards

1
Q

CABIN PRESS

A

Cabin altitude is more than 9,800 feet

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2
Q

CHECK FIRE DET

[WARNING]

A

Engine fire, APU fire or detector loop circuit malfunction is sensed

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3
Q

SMOKE

[WARNING]

A

Smoke is sensed in the forward or aft baggage compartment

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4
Q

TOUCHED RUNWAY

[WARNING]

A

Rear outer fuselage surface has touched he runway

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5
Q 
#1 or #2 ENG OIL PRESS
[WARNING]
A

No. 1 or 2 engine oil pressure is less than 44 PSI

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6
Q 
#1 or #2 ENG FADEC FAIL
[WARNING]
A

No. 1 or 2 engine FADEC has a critical fault

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7
Q

STBY BATT HOT

[WARNING]

A

Standby battery temperature is more than 71 deg C

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8
Q

AUX BATT HOT

[WARNING]

A

Aux battery temperature is more than 71 deg C

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9
Q

MAIN BATT HOT

[WARNING]

A

Main battery temperature is more than 71 deg C

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10
Q

FUSELAGE DOORS

[WARNING]

A

One or more fuselage doors are not closed or locked

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11
Q

PITCH TRIM

A

One of the FCECU channels is not able to control its related pitch trim actuator; or
pilot and copilot pitch trim input commands are different.

Airspeed 1 and 2 mismatch (>17kts). RUD CTRL, SPLR OUTBD, and ELEVATOR FEEL caution lights will also illuminate

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12
Q

ELEVATOR FEEL

A

One of the FCECU channels is not able to control its pitch feel actuator or acceleration 1 & 2 mismatch

Airspeed 1 & 2 mismatch (>17 kts). RUD CTRL, SPLR OUTBD, and PITCH TRIM caution lights will also illuminate.

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13
Q

ELEVATOR ASYMMETRY

A

Right and left elevators have a difference in angle of:
4 deg for IAS > 185 KIAS or
6 deg for IAS < 185 KIAS

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14
Q

ELEVATOR PRESS

A

Hydraulic systems #1, 2 and 3 are supplying pressure to the elevators

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15
Q

3 STBY HYD PUMP

A

DC Motor Pump (DCMP) contactor has been energised for more than 60 sec on the ground; or

Hyd system #3 pressure is below 900 PSI

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16
Q

EMER LTS DISARMED

A

Emergency lights are not armed

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17
Q

L AC BUS

R AC BUS

A

A left or right AC variable bus fault is sensed

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18
Q

DC BUS

A

EPCU has reconfigured the main 28 VDC generation system because of a source or bus fault condition

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19
Q

L TRU

R TRU

A

Left or right TRU is outputting less than 15 Volts

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20
Q

INTERNAL DOORS

A

Internal baggage door or cockpit door not closed and locked

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21
Q

PITOT HEAT STBY

A

Standby pitot toggle switch set to OFF; or

Standby pitot/static heater malfunction

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22
Q

PITOT HEAT 1

PITOT HEAT 2

A

No 1 or 2 toggle switch set to OFF; or

No 1 or 2 pitot/static heater malfunction

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23
Q

ENG ADPT HEAT 1

ENG ADPT HEAT 2

A

Malfunction of both air intake heating elements in the respective side

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24
Q

WSHLD CTRL

A

Left or right windshield anti-ice control malfunction

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25
Q

WSHLD HOT

A

Either the left or right windshield has overheated

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26
Q

SIDE WDO HOT

A

Captain’s side window has overheated

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27
Q

ICE DETECT FAIL

A

The two ice detector probes have malfunctioned

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28
Q

PROP DEICE

A

Timer Monitor Control Unit (TMCU) has malfunctioned or it has sensed a malfunction in the prop deice system

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29
Q

DEICE TIMER

A

Timer and Monitor Unit (TMU) has malfunctioned

30
Q

DEICE PRESS

A

Airframe deice system pressure is too low (<15 PSI); and/or

There is a distributor valve malfunction

31
Q

FLT COMPT DUCT HOT

CABIN DUCT HOT

A

Flight compartment or Cabin supply duct temperature is more than 88 deg

32
Q

CABIN PACK HOT

FLT COMPT PACK HOT

A

Right or left ACM discharge temperature is hot

33
Q

L TRU HOT

R TRU HOT

A

Left or right TRU temperature is hot

34
Q

1 HYD ISOL VLV

A

No 1 Hydraulic isolation valve is closed

Loss of - normal brakes/anti skid, inboard flight spoilers

35
Q

2 HYD ISOL VLV

A

No. 2 hydraulic isolation valve is closed

Loss of outboard flight spoilers, landing gear, nose steering

36
Q

STBY BATT
MAIN BATT
AUX BATT

A

Standby, main or auxiliary battery is not connected to its main feeder bus for charging

37
Q

AVIONICS

A

An avionics no dispatch condition is sensed when the aircraft is on the ground

38
Q 
#1 PEC
#2 PEC
A

No 1 or 2 Propeller Electronic Control (PEC) malfunction

39
Q 
#1 BLEED HOT
#2 BLEED HOT
A

No 1 or 2 bleed air supply duct temperature is hot; or
duct overpressure; or
duct leak

40
Q 
#1 DC GEN HOT
#2 DC GEN HOT
A

No 1 or 2 DC generator temperature is hot

41
Q 
#1 AC GEN HOT
#2 AC GEN HOT
A

No 1 or 2 AC generator temperature is hot

42
Q 
#1 FLUID HOT
#2 FLUID HOT
A

No 1 or 2 hydraulic reservoir temperature is hot

43
Q 
#1 FUEL FLTR BYPASS
#2 FUEL FLTR BYPASS
A

No 1 or 2 fuel filter bypass impending

44
Q 
#1 ENG FUEL PRESS
#2 ENG FUEL PRESS
A

Pressure at EDP No 1 or 2 inlet is low

45
Q 
#1 ENG HYD PUMP
#2 ENG HYD PUMP
A

No 1 or 2 engine driven hydraulic pump pressure is low;
or
when the condition lever is set to the FUEL OFF position

46
Q 
#1 DC GEN
#2 DC GEN
A

No 1 or 2 DC generator is not connected to its bus because of a source fault condition;
or
the DC GEN switch is set to the OFF position;
or
external DC power is energising the left and right main buses

47
Q 
#1 AC GEN
#2 AC GEN
A

No 1 or 2 AC generator is not connected to its bus because of a source fault condition;
or
the AC Gen 1 or 2 switch is set to the OFF position;
or
external AC power is on

48
Q 
#1 ENG FADEC
#2 ENG FADEC
A

No 1 or 2 engine FADEC has a cautionary fault

49
Q 
#1 TANK FUEL LOW
#2 TANK FUEL LOW
A

No 1 or 2 fuel collector bay quantity is low (<140kg)

50
Q

ROLL SPLR INBD GND

A

FCECU is not able to control the inboard spoiler lift dump operation;
or
the inboard spoilers do not extend at touchdown;
or
the inboard spoilers extend after the TAXI mode is selected after touchdown

51
Q

1 STBY HYD PUMP HOT

A

The temperature of the electric motor windings on the No 1 standby hydraulic pump is too hot

52
Q

ROLL SPLR INBD HYD

A

Hydraulic pressure to the inboard roll spoiler actuators is low

53
Q 
# 1 RUD HYD
#2 RUD HYD
A

Hydraulics pressure to the No 1 or 2 rudder actuator is low

54
Q

RUD CTRL

A

FCECU is unable to control rudder hydraulic pressure;
or
loss of hydraulics pressure to both rudder actuators;
or
Airspeed 1 and 2 mismatch (.17kts) - ELEVATOR FEEL, SPLR OUTBD, and PITCH TRIM caution lights also illuminate

55
Q

APU

A

APU FADEC has sensed a fault and shutdown the APU

56
Q

ROLL SPLR OUTBD GND

A

FCECU is not able to control the outboard spoiler lift dump operation;
or
the outboard spoilers do not extend at touchdown;
or
the outboard spoilers extend when TAXI mode is selected after touchdown

57
Q

SPLR OUTBD

A

FCECU has failed to inhibit outboard spoiler pressure at greater than 185 KIAS;
or
has failed to re-enable outboard spoiler pressure below 150 KIAS

58
Q

ROLL SPLR OUTBD HYD

A

Hydraulic pressure to the outboard spoiler actuators is too low

59
Q

FLAP DRIVE

A

Flap system fault

60
Q

FLAP POWER

A

Flap system failure

61
Q 
#1 STALL SYST FAIL
#2 STALL SYST FAIL
A

No 1 or 2 stall warning system malfunction;
or
a loss of a valid AOA parameter

62
Q

PUSHER SYST FAIL

A

Stick pusher inhibited by SPS logic;
or
stick pusher shutoff switchlight pressed

63
Q

INBD ANTISKID

OUTBD ANTISKID

A

Inboard or outboard antiskid control unit malfunction;
or
toggle switch is set to off

64
Q

LDG GEAR INOP

A 
Landing gear sequence malfunction;
or
the landing gear inhibit switch has been set to INHIBIT;
or
there is a PSEU failure
65
Q

NOSE STEERING

A

Steering system fault with nose steering ON;
or
system remains pressurised after steering switch set to OFF

66
Q

FLT DATA RECORDER

A

Flight data recorder malfunction or it is not energised

67
Q

GPWS

A

Ground Proximity Warning System has malfunctioned;
or
there is a Radio Altimeter failure

68
Q

PARKING BRAKE

A

Emergency/parking brake is set

69
Q

WT ON WHEELS

A

PSEU has sensed a weight on wheels sensor malfunction

70
Q

FUELING ON

A

Refuel/defuel access panel is open

Dash 8 Q400 (23 decks)

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