Lights and Switches Flashcards
IR 1/2/3 fault (flashing)
Attitude and heading may be recovered using ATT mode
IR 1/2/3 fault (steady)
Fault in IR
IR 1/2/3 White Align Light Flashing
1) No position entered after 10 minutes
2) Bad position (> 1 degree from last position)
3) Fault
ADR 1/2/3 Fault Light
Fault in air data
ELAC 1 or 2 Fault Light
Fault
SEC 1/2/3 Fault
Fault
ELAC Controls
Elevator Aileron Computer
1) Normal Pitch and Roll
2) Alternate Pitch
3) Direct Pitch and Roll
4) Abnormal Attitude
5) Aileron Droop
6) Acquisition of Autopilot Orders
SEC Controls
Spoiler Elevator Computer
1) Normal Roll (spoilers)
2) Speed Brakes & Ground Spoilers (SEC 1 & 3 only)
3) Alternate Pitch (SEC 1 & 2 only)
4) Direct Pitch (SEC 1 & 2 only)
5) Direct Roll
6) Abnormal Attitude
FAC 1/2 Fault
Fault
FAC 1/2 Controls
Flight Augmentation Computer
I. Rudder
A) Coordination & Dampening
B) Trim
C) Travel Limit
D) Yaw
II. Flight Envelope Protection
A) PFD Speed Tape-characteristic speed symbols
B) Alpha Floor Protection
III. Low Energy Warning
IV. Reactive Windshear ProtectionDitching Switch closes
1) Avionics ventilation inlet valve
2) Avionics ventilation extract valve
3) Both pack flow control valves
4) Ram air inlet valve
5) Outflow valve if under auto control
Wing anti ice valve fault
1) Low pressure
2) Either valve disagreement
3) Either valve in transit
Engine anti ice valve fault
1) Valve disagreement
2) Valve in transit
Pack 1/2 Fault
1) Overheat of compressor outlet
2) Overheat of pack outlet
3) Valve disagreement
Engine 1/2 Bleed Fault
LOOSA
1) Leak
2) Overheat
3) Overpressure
4) Start in progress and valve not closed
5) APU bleed on and valve not closed
APU bleed fault
Leak
Hot Air Fault
Overheat. Hot air and trim air valves close
Galley fault
Any generator load is greater than 109%
Battery fault
Battery charger is out of limits
IDG 1/2 Fault
1) High Oil Temperature
2) Low Oil Pressure
Generator 1/2 Fault
1) GCU Trip
2) Line contacter open
APU Gen Fault
1) GCU Trip
2) Line contactor open
AC Ess Feed Fault
AC ESS Bus not powered
GEN 1 Line
Smoke in avionics compartment
Rat & Emer Gen Fault
Emergency generator is not supply power when it should be
Fuel Mod Sel Fault
Center >550 lbs and either main <11,000 lb
Eng 1/2 Hydraulic Pumps (Green and Yellow)
I. Reservoir problem
A) Low level
B) Fluid overheat
C) Low air pressure
II. Pump problem
A) Low pump pressureElectric Hydraulic Pump Faults. (Blue & Yellow)
I. Reservoir problem
A) Low level
B) Fluid overheat
C) Low pressure
II. Pump problem
A) Low pump pressure
B) OverheatPTU Fault
I. Illuminated in conjunction with a hydraulic reservoir fault
A) Low Level
B) Fluid overheat
C) Low air pressure.
Engine 1/2 Fire Push Buttons
I. Fire Panel (2)
A) Silences CRC
B) Arms Squib
II. Hydraulic Panel (1)
A) Closes hydraulic shut off.
III. Fuel Panel (2)
A) Closes low pressure fuel valve
B) De-energizes FADEC
IV. Electric panel (1)
A) Deactivates IDG
V. Air Condition Panel (2)
A) Closes Bleed Valve
B) Closes pack flow control valve.Hot Air Valve
Duct Overheat
Ventilation Blower Fan Fault
A) Air Pressure Low
B) Computer Fault
C) Smoke
D) Overheat
Ventilation Fan Extract Fault
A) Air pressure
B) Computer fault
C) Smoke
Engine Start Switch Fault
A) Automatic Start Abort
B) HP fuel valve disagreement.
