Lights And Switches Flashcards
ON BATT LIGHT
-Self Test During full Alignment
-One or more IR are on BATT
-5 min to recover Power or two the Captain’s not using will drop off
IR 1/2/3 Fault Light/OFF
-Steady Fault Light: Fault in IR/IR Lost
-Flashing Fault Light: Attitude/Heading may be recovered
-OFF: Illuminates when inertial data output is disconnected
ADR 1/2/3 Fault Light/OFF
Fault:
-Fault in Air Data
-Pitot Static system on that side has been lost
OFF:
-Associated ADR is off
ELAC 1 (Elevator Aileron Computer)
ELAC: Normal Pitch/Roll, Alternate Pitch/LAF (if installed), Direct Pitch/Roll, Abnormal Attitude, Aileron Droop, Acquisition of Autopilot orders.
-ELAC Fault: Fault is detected/only 8 seconds during power up if it’s a good test.
SEC 1/ 2/ 3 (Spoiler Elevator Computer)
SEC: Normal Roll, Speed-brakes/GND Spoilers, Alternate/Direct Pitch (SEC 1/2 only), Direct Roll, Alternate Load Alleviation Function (LAF) if Installed, Abnormal Attitude.
-SEC Fault Light: Fault in the system
FAC 1/2 (Flight Augmentation Computer)
-FAC: Gives us Speed tape symbology; F, S, Green Dot, Low Energy Warning, Wind Shear Protection
Flying the Tail: Turn Coordination, Yaw Damping, Rudder Trim, Rudder Travel Limits.
-FAC Fault Light: Fault in the system
GEN 1 Line PB
-Off; Disconnects GEN1 from electrical system. AC Bus1 powered by GEN2 through bus tie line contactors
-Smoke Light, Smoke detected in Avionics Compartment
-Blower/Extract Fans PB will also show Fault
-PB, Isolates GEN for the #1 fuel pumps in the left/right wing tanks
RAT & EMER GEN (Fault Light)
-EMER GEN is not supplying PWR but it should be, AC Bus 1/2 not PWRD
-Lift guard and push the button for electrical power only
TERR GPWS/SYS PB (Fault Lights)
-TERR PB Fault light; Terrain Data base is lost, You will still have basics modes of the GPWS system (To Low Flaps, To Low Gear, and Terrain Recognition).
- SYS Fault; Lost all modes including GPWS
G/S MODE & FLAP MODE
-Used for Abnormal conditions to shut down the selected mode
LDG Flaps 3
-Turn on when performing a FLAP 3 Landing
-Landing memo displays Flaps 3
CVR
GND CTL PB
-Powered for 5 min on external power, Captain must turn on CVR on the ground to capture briefings/checklist test. If the CVR doesn’t test, the parking brake is off
- Comes on automatically after engine start.
-In flight
Oxygen
-Passenger PB; SYSTEM ON signal sent to the back to drop masks (Automatically at 14,000’ Cabin ALT) or Press MASK MAN ON guarded switch for manual deployment
-Crew Supply; Allows O2 bottle to connect to manifold for Cockpit Masks
CALLS
-Contact Mech, FWD/AFT FA stations (Single Chime)
-EMER; Lift Guard Pressed (Triple High/Low Chime)
Wipers
230KTS Limit
APU Master SW; ON/FAULT
-ON; ECB (Electronic Control Box) PWR-up TEST is initiated, APU Air Inlet Opens, Pressurizing Fuel pump, Fuel Isolation Valve Opens, If External PWR or Main GEN is on; APU SYS Page is displayed.
-OFF; Light extinguishes and shuts down after 2 min cooldown.
-Fault Light; Fire (on the ground only) or Shutdown was Abnormal:
- DC PWR lost, BATTs PB off on BATT PWR only
- Air inlet flap closed
- Inlet overheat
- No Acceleration
- No Speed
- Under-speed
- Slow Start
- Overspeed
- Loss of Overspeed protection
- Overcurrent
- No Flame
- Reverse flow
- Low oil Pressure
- High Oil Temperature
- Clogged oil Filter
- EGT Over-temp
- Sensor failure
- IGV failure
- ECB failure
- Loss of EGT thermocouples
ANTI ICE
-WING; Outboard 3 slats are heated; Default to closed when PWR is lost,
Fault light: Low Air Pressure/Valve Switch Disagreement/Valve intransit
-ENG; Nacelle Lip only, Defaulted to open when PWR is lost
Fault Light: Valve Switch Disagreement/Valve intransit
Probe/Window Heat
-Aircraft has PWR, Drain Mast are heated
-PB ON, All Probes/Windows heated except TAT
-PB AUTO, Probes/Windows are heated at ENG Start
-TAT, PWRD when airborne only
Cabin Pressurization/ MODE SEL Fault Light
-Switches after each landing, System failure, lost both Auto Controllers
-Selecting MAN for 10 sec, then return to AUTO will select other system
LDG ELEV AUTO Rotary Switch
-Gets Landing Elevation from FMGC
-Must take it out of Auto if destination in not in Data Base/Data Base in incorrect or ECAM or Abnormal procedure tells you to do so
-Still get auto pressurization regardless of position, Only changes the schedule to when the Outflow valve opens
Guarded “DITCHING” Switch
- SYS in Auto will close Outflow valve, Emergency Ram air inlet, Avionics Inlet/Extract valves, Pack-flow CNTRL valves.
- MODE SEL must go to Manual CNTRL, Outflow Valve now CNTRL by “MAN V/S CTL switch (Up to open, Down to Close).
ENG Fire PB 1/2
- Silence CRC/Arms Squibs
- Deactivates IDG
- Closes LP Fuel valve/De-energizes FADEC
- Closes Hydraulic Shutoff Valve
- Closes Bleed/Pack Flow Control Valves
APU Fire PB
- Silences CRC/Arms Squib
- APU Shuts Down
- Closes Low Pressure Fuel Valve/Shuts Down APU Fuel Pump
- Closes APU Bleed/Cross Bleed Valves
- Deactivates APU Generator
- APU Fire Light illuminates when warning is activated regardless of pushbutton position
ENG Test PB
Looking for:
CRC/MASTER WARN Light
ECAM
Squib Light
DISCHARGE Light
Fire Light on ENG panel
APU Test PB
Looking for:
CRC/Master Warning Light
ECAM
* APU Fire PB Light
* SQUIB Light
* DISCHARGE Light
(* If DC power only)
Hydraulic; ENG PB 1/2 Fault light
Reservoir Problem:
Low Level
Fluid Over Heat
Low Air Pressure
Pump Problem:
Low Pressure
Hydraulic; Blue/Yellow ELEC Pump PB (Fault Light)
Reservoir Problem:
Low Level
Fluid Overheat
Low Air Pressure
Pump Problem:
Low Pump Pressure
Over Heat
Hydraulic; PTU PB (Fault Light)
Reservoir Problem:
Low Level
Fluid Overheat
Low Airpressure
Fuel; LTK, RTK, CTK Pumps 1/2 (Fault Light)
Low Output Pressure
Fuel; MODE SEL (Fault Light)
CTK > 550LBS
LTK/RTK < 11000LBS
Electrical; Galley PB (Fault Light)
Any Generator Load > 100%
BAT 1/2 PB (Fault Light)
Battery Charger Current is out of limits
IDG 1/2 PB (Fault Light)
High Oil Temperature
Low Oil Pressure
GEN 1/2 PB (Fault Light)
GCU Trip
Line Contactor open
APU GEN PB (Fault Light)
GCU Trip
Line Contactor open
Inhibited at low speed
AC ESS FEED (Fault Light)
AC ESS BUS not powered
PAC 1/2 PB (Fault Light)
Compressor or PACK overheated
Valve disagreement
ENG Bleed PB (Fault Light)
-Leak
-Overheat
-Over Pressure down Stream
-Start in process & Valve opened
-APU Bleed on & Valve opened
-HP Valve failed to open on ground
-Single BTS Fail or -Disagree on the ground
-Dual BTS Fail inflight or on ground
-Fan Duct Burst detected (LEAP 1-A only)
APU Bleed PB (Fault Light)
Leak Detected
Hot Air PB (Fault Light)
Over Heat Detected, Closes:
Hot air valve
Trim Air Valve
Wing Anti-Ice PB (Fault Light)
Low Pressure
Valve Disagreement
Valve in Transit
ENG Anti-Ice PB (Fault Light)
Valve disagreement
Valve in transit
APU Master Switch PB (Fault Light)
Fire (on ground only),
Abnormal Shutdown
EMER EXIT Off Light
EMER Exit Light Selected Off
CARGO SMOKE FWD/AFT (DISCHARGE Light)
Bottle fully discharged
VENTILATION BLOWER PB (Fault Light)
Smoke
Overheat
Air Pressure Low*
Computer Power Supply Failure
*Horn sounds if on the ground
+no engines running
VENTILATION EXTRACT PB (Fault Light)
Smoke
Pressure is low*
Computer Power Supply Failure
*Horn sounds on the ground
+no engines running
Cockpit Door (Fault Light)
System Failure (Latch, Control Unit, Pressure Sensor)
ENG Control 1/2 (Fault Light)
Automatic Start Abort
HP Valve disagreement
EFIS Controls, GPWS (Fault Light)
RED Fault Light: GPWS 1-4 alert/EGPWS Alert
Amber Fault Light: GPWS 5 Alert, too far below glide slope
Minimum Battery Voltage
25.5 Volts
Batteries in Auto
Will connect Sole source of electrics, need to charge (Below 26.5V), or starting the APU
AC Bus 1/2 Lost in flight >100KTS
RAT will deploy automatically, Batteries only for 8 sec
EVAC (Guarded Switch)
ON: Activates EVAC tone/Flashes EVAC lights at FA panels
OFF: Lights out
