FAULTS Flashcards
COCKPIT DOOR Fault Open Indicator
3
Latch Fail
Pressure Sensor Fail
Control Unit Fail
ENG 1(2) START Fault Light (3)
Start Valve Fault
Automatic Start Abort
Disagreement between the HP fuel Valve’s actual position versus its commanded position
EGPWS TERR Fault Light
2
TCF (Terrain Clearance Floor) or
TAD (Terrain Awareness Display) Fails
Terrain is not shown on ND
GPWS SYS Fault Light
Lost a basic mode of the GPWS (modes 1 - 5)
*only mode 5 is inhibited if an ILS fails
Modes 1-5
- Excessive rate of descent
- Excessive terrain closure rate
- Altitude loss after takeoff, or go around
- Unsafe terrain clearance when not in landing config
- Too far below glideslope
RAT & EMER GEN Fault Light
2
Emergency generator is not supplying power
AC BUS 1 and 2 are not powered
ELAC 1 Fault Light
2
When a failure is detected
During ELAC power-up test (8 seconds)
*test initiated when electrical is turned on
SEC 1/2/3 Fault Light
When a failure is detected
ADR 1/2/3 Fault Light
Air Data Reference part of the ADIRU has a fault
APU Fault Light
a lot
Fire (Ground only) Air inlet flap closed Over speed No Acceleration Slow Start EGT overtemp No Flame Reverse Flow HOTLOP No Speed Under Speed Loss of over speed protection Oil System shut-down Inlet overheat Clogged Oil filter Loss of EGT Thermocouples
Cabin Press MODE SEL Fault Light
Cabin pressure controllers system 1 and 2 are faulty
Wing Anti-Ice
2
Disagreement of the anti-ice control valve
Low pressure is detected
ENG 1 /2 ANTI-ICE Fault Light
Disagreement of the anti-ice control valve
PACK 1 Fault Light
3
Disagreement of the pack control valve
Compressor outlet overheat
Pack outlet overheat
ENG 1/2 BLEED Fault Light
5
Overpressure downstream of the bleed valve
Bleed air overheat
Wing or engine leak on the related side
Bleed valve is not closed during engine
Bleed valve is not closed with APU bleed ON
APU BLEED Fault Light
APU leak