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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
WSHLD HOT
Either the left or right windshield has overheated
26
SIDE WDO HOT
Captain's side window has overheated
27
ICE DETECT FAIL
The two ice detector probes have malfunctioned
28
PROP DEICE
Timer Monitor Control Unit (TMCU) has malfunctioned or it has sensed a malfunction in the prop deice system
29
DEICE TIMER
Timer and Monitor Unit (TMU) has malfunctioned
30
DEICE PRESS
Airframe deice system pressure is too low (<15 PSI); and/or There is a distributor valve malfunction
31
FLT COMPT DUCT HOT | CABIN DUCT HOT
Flight compartment or Cabin supply duct temperature is more than 88 deg
32
CABIN PACK HOT | FLT COMPT PACK HOT
Right or left ACM discharge temperature is hot
33
L TRU HOT | R TRU HOT
Left or right TRU temperature is hot
34
#1 HYD ISOL VLV
No 1 Hydraulic isolation valve is closed | Loss of - normal brakes/anti skid, inboard flight spoilers
35
#2 HYD ISOL VLV
No. 2 hydraulic isolation valve is closed | Loss of outboard flight spoilers, landing gear, nose steering
36
STBY BATT MAIN BATT AUX BATT
Standby, main or auxiliary battery is not connected to its main feeder bus for charging
37
AVIONICS
An avionics no dispatch condition is sensed when the aircraft is on the ground
38
``` #1 PEC #2 PEC ```
No 1 or 2 Propeller Electronic Control (PEC) malfunction
39
``` #1 BLEED HOT #2 BLEED HOT ```
No 1 or 2 bleed air supply duct temperature is hot; or duct overpressure; or duct leak
40
``` #1 DC GEN HOT #2 DC GEN HOT ```
No 1 or 2 DC generator temperature is hot
41
``` #1 AC GEN HOT #2 AC GEN HOT ```
No 1 or 2 AC generator temperature is hot
42
``` #1 FLUID HOT #2 FLUID HOT ```
No 1 or 2 hydraulic reservoir temperature is hot
43
``` #1 FUEL FLTR BYPASS #2 FUEL FLTR BYPASS ```
No 1 or 2 fuel filter bypass impending
44
``` #1 ENG FUEL PRESS #2 ENG FUEL PRESS ```
Pressure at EDP No 1 or 2 inlet is low
45
``` #1 ENG HYD PUMP #2 ENG HYD PUMP ```
No 1 or 2 engine driven hydraulic pump pressure is low; or when the condition lever is set to the FUEL OFF position
46
``` #1 DC GEN #2 DC GEN ```
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
``` #1 AC GEN #2 AC GEN ```
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
``` #1 ENG FADEC #2 ENG FADEC ```
No 1 or 2 engine FADEC has a cautionary fault
49
``` #1 TANK FUEL LOW #2 TANK FUEL LOW ```
No 1 or 2 fuel collector bay quantity is low (<140kg)
50
ROLL SPLR INBD GND
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
#1 STBY HYD PUMP HOT
The temperature of the electric motor windings on the No 1 standby hydraulic pump is too hot
52
ROLL SPLR INBD HYD
Hydraulic pressure to the inboard roll spoiler actuators is low
53
``` # 1 RUD HYD #2 RUD HYD ```
Hydraulics pressure to the No 1 or 2 rudder actuator is low
54
RUD CTRL
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
APU
APU FADEC has sensed a fault and shutdown the APU
56
ROLL SPLR OUTBD GND
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
SPLR OUTBD
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
ROLL SPLR OUTBD HYD
Hydraulic pressure to the outboard spoiler actuators is too low
59
FLAP DRIVE
Flap system fault
60
FLAP POWER
Flap system failure
61
``` #1 STALL SYST FAIL #2 STALL SYST FAIL ```
No 1 or 2 stall warning system malfunction; or a loss of a valid AOA parameter
62
PUSHER SYST FAIL
Stick pusher inhibited by SPS logic; or stick pusher shutoff switchlight pressed
63
INBD ANTISKID | OUTBD ANTISKID
Inboard or outboard antiskid control unit malfunction; or toggle switch is set to off
64
LDG GEAR INOP
``` Landing gear sequence malfunction; or the landing gear inhibit switch has been set to INHIBIT; or there is a PSEU failure ```
65
NOSE STEERING
Steering system fault with nose steering ON; or system remains pressurised after steering switch set to OFF
66
FLT DATA RECORDER
Flight data recorder malfunction or it is not energised
67
GPWS
Ground Proximity Warning System has malfunctioned; or there is a Radio Altimeter failure
68
PARKING BRAKE
Emergency/parking brake is set
69
WT ON WHEELS
PSEU has sensed a weight on wheels sensor malfunction
70
FUELING ON
Refuel/defuel access panel is open

Dash 8 Q400 (23 decks)

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