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Q300 Notes > 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
#1 DC GEN
#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
26
#2 DC GEN
#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
27
#1 AC GEN
#1 AC Generator Failed or Offline AC Gen GCU circuits will close AC Cross Tie.
28
#2 AC GEN
#2 AC Generator Failed or Offline AC Gen GCU circuits will close AC Cross Tie.
29
AUX INV
Secondary Inverter Inoperative
30
L 26 AC
Left 26v Transformer Inoperative
31
R 26 V
Right 26v Transformer Inoperative
32
L AC BUS
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.
33
R AC BUS
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.
34
DC BUS
DC Bus Fault Detected BBPU has inhibited closing of Main and Main/Secondary Bus Ties
35
L TRU HOT
Left Transformer Rectifier Unit Overheated
36
R TRU HOT
Right Transformer Rectifier Unit Overheated
37
#1 DC GEN HOT
#1 DC Generator Windings Overheated
38
#2 DC GEN HOT
#2 DC Generator Windings Overheated
39
#1 AC GEN HOT
#1 AC Generator Windings Overheated
40
#2 AC GEN HOT
#2 AC Generator Windings Overheated
41
EMER LTS DISARMED
Emergency Lights not Armed with DC System Energized
42
RUD PRESS
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
ROLL SPLR INBD HYD
Inboard Spoiler Extend Circuit Depressurized
44
ROLL SPLR OUTBD HYD
Outboard Spoiler Extend Circuit Depressurized
45
#1 RUD HYD
#1 Rudder Actuator Depressurized Rudder Pressure Regulator will admit full hydraulic pressure (3,000 psi) to #2 Rudder Actuator
46
#2 RUD HYD
#2 Rudder Actuator Depressurized Rudder Pressure Regular will admit full hydraulic pressure (3,000 psi) to #1 Rudder Actuator
47
RUD FULL PRESS
One Rudder Actuator has Full Hydraulic Pressure (3000 psi)
48
FLAP DRIVE
Main Flap Drive Failed Secondary Shaft will continue to provide normal operation
49
FLAP POWER
Loss of pressure to Flap Power Unit (less than 1,500 psi)
50
FLT DATA RECORDER
Recorder Failed or De-engergized Can be malfunction or A/COL (beacon) being selected off.
51
#1 ENG FUEL PRESS
#1 Boost Ejector Pump Failed Fuel pressure of fuel being delivered to left engine driven fuel pump is low.
52
#2 ENG FUEL PRESS
#2 Boost Ejector Pump Failed Fuel pressure of fuel being delivered to right engine driven fuel pump is low.
53
#1 TANK FUEL LOW
#1 Tank Quantity Less than 130 Pounds Equals approx 12 minutes of operating time on associated engine unless fuel is transferred.
54
#2 TANK FUEL LOW
#2 Tank Quantity Less than 130 Pounds Equals approx 12 minutes of operating time on associated engine unless fuel is transferred.
55
FUELING ON
Refuel or Defuel Selected on Fueling Control Panel Aircraft would be unable to crossfeed in flight.
56
#1 FUEL FLTR BYPASS
#1 Fuel Filter Blocked or Restricted Fuel system will automatically reroute fuel around affected filter.
57
#2 FUEL FLTR BYPASS
#2 Fuel Filter Blocked or Restricted Fuel system will automatically reroute fuel around affected filter.
58
#1 HYD FLUID HOT
Overtemp Condition in #1 Hydraulic Reservoir
59
#2 HYD FLUID HOT
Overtemp Condition in #2 Hydraulic Reservoir
60
#1 STB HYD PUMP HOT
Overtemp Condition in #1 Standby Pump Windings
61
#2 STB HYD PUMP HOT
Overtemp Condition in #2 Standby Pump Windings
62
#2 SPU AUX PWR
#2 Standby Hydraulic Pump Powered by #2 AC Generator Switches automatically from #1 AC Bus if #1 AC Bus goes offline.
63
#1 ENG HYD PUMP
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
#2 ENG HYD PUMP
Low Pressure from the #2 Main Hydraulic Pump #2 Standby Hydraulic Pump will be activated automatically from a low pressure switch.
65
PITOT HEAT 1
#1 Pitot Heater Off
66
PITOT HEAT 2
#2 Pitot Heater Off
67
L ELEV HORN HEAT
Left Elevator Horn Heat Failure Also illuminates during Elevator Horn Heat test.
68
R ELEV HORN HEAT
Right Elevator Horn Heat Failure Also illuminates during Elevator Horn Heat test.
69
L WSHLD HOT
Left Windshield Overheated System will de energize window until the window temperature cools. Or loss of power to window heater element.
70
R WSHLD HOT
Right Windshield Overheated System will de energize window until the window temperature cools. Or loss of power to window heater element.
71
SIDE WDO HOT
Pilot's Side Window Overheated System will de energize window until the window temperature cools. Or loss of power to window heater element.
72
DEICE PRESS
Deice Pressure Too Low for Boot Operation
73
NOSE STEERING
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
PARKING BRAKE
Parking Brake in On
75
OUTBD ANTI SKID
Outboard Anti-Skid Control Unit Failure Also illuminates during self-test.
76
INBD ANTI SKID
Inboard Anti-Skid Control Unit Failure Also illuminates during self-test.
77
LND GEAR INOP
Failure of Landing Gear Door Sequencing Valve
78
WT ON WHEELS
Fault in Weight on Wheels Sensing Circuits
79
#1 BLEED HOT
Overheat Condition in #1 Bleed Air Supply Duct HPSOV and NSOV will close on affected side until bleed system returns to normal temperature.
80
#2 BLEED HOT
Overheat Condition in #2 Bleed Air Supply Duct HPSOV and NSOV will close on affected side until bleed system returns to normal temperature.
81
#1 ENG MANUAL
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
#2 ENG MANUAL
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
L STALL WARNING
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
R STALL WARNING
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
#1 STALL SYST FAIL
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
#2 STALL SYST FAIL
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
PUSHER SYST FAIL
Malfunction in Stick Pusher System (-300) Stick pusher will be offline
88
GPWS
Failure of Ground Proximity Warning System

Q300 Notes (12 decks)

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