AIRBUS A320 WARNINGS AND CAUTIONS

21 AIR CONDITIONING – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
PACK 1 (or 2) OVHT Pack compressor outlet temperature above 260 °C, or above 230 °C four times during one flight.	SINGLE CHIME	MASTER CAUT	BLEED	PACK FAULT lt	3, 4, 5, 7, 8
PACK 1 (or 2) FAULT Pack valve disagree with selected position, or pack valve closed.
PACK 1 + 2 FAULT Loss of ACSC 1 and ACSC 2.
PACK 1 (2) OFF Pack pb at OFF with no failure.				NIL	1, 2, 3, 4, 5, 7, 8, 9, 10
CKPT (FWD CAB OR AFT CAB) DUCT OVHT Duct temperature above 88 °C or above 80 °C four times during one flight.			COND	HOT AIR FAULT lt	3, 4, 5, 7, 8
HOT AIR FAULT Hot air pressure regulating valve disagrees with selected position.
L + R CAB FAN FAULT Both fan failure.				NIL
PACK 1 (2) REGUL FAULT Failure of the By Pass Valve, or the RAM Air Inlet, or the Compressor Outlet Temperature sensor or the Flow Control Valve.	NIL	NIL	BLEED
LAV + GALLEY FAN FAULT			NIL		3, 4, 5, 7, 8, 9
TRIM AIR SYS FAULT One trim air valve fault, or overpressure downstream hot air valve.					3, 4, 5, 7, 8
CTL 1 (2) – A (B) FAULT The lane A (B) of ACSC 1 (2) fails.					3, 4, 5, 7, 8

21 PRESSURIZATION – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
EXCESS CAB ALT Cabin altitude exceeds : ‐ In CLB and DES the higher of : 9550 ft or landing field elevation plus 1000 ft ‐ In CRZ 9550 ft	CRC	MASTER WARN	CAB PRESS	NIL	2, 3, 4, 5, 7, 8, 9, 10
SYS 1 + 2 FAULT Both pressure controllers fail.	SINGLE CHIME	MASTER CAUT	CAB PRESS	MODE SEL FAULT lt	4, 5, 7, 8
LO DIFF PR Time to reach ΔP = 0 < 1.5 min, and time to reach ΔP = 0 ≤ (time for cab alt to reach landing elevation) +30 s and aircraft is at least 3000 ft above landing field. Note: The warning is maintained, when the aircraft descends below 3000 ft above landing field.				NIL	2, 3, 4, 5, 7, 8, 9, 10
OUTFLOW VALVE NOT OPEN Valve not fully open on ground (time delay 3 min)					3, 4, 5, 6, 7, 8
SAFETY VALVE OPEN Either safety valve not fully closed on ground or not fully closed for more than 1 min in flight.					4, 5, 7, 8, 9, 10
LDG ELEV FAULT No FMGS LDG ELEV data is available.					3, 4, 5, 7, 8, 9, 10
SYS 1 (or 2) FAULT Pressure controller fault.	NIL	NIL			3, 4, 5, 7, 8

21 VENTILATION – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
BLOWER FAULT Blowing pressure low or duct overheat	SINGLE CHIME	MASTER CAUT	CAB PRESS	BLOWER(1) FAULT lt	3, 4, 5, 7, 8
EXTRACT FAULT Extract pressure low				EXTRACT (1) FAULT lt	3, 4, 5, 7, 8
SKIN VALVE FAULT 1. Extract valve fully open in phase 3 or 2. Extract valve fully open in flight or 3. Inlet valve not fully closed in flight				NIL	4, 5, 7, 8
AVNCS SYS FAULT Power up test not satisfactory or AEVC not supplied or valves position disagree				BLOWER and EXTRACT FAULT lts ([1])	3, 4, 5, 6, 7, 8, 9

(1) Associated with ground external call. 
(2) Only in case of AEVC power supply failure on ground.

21 CARGO – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
AFT (FWD) CARGO DUCT temperature OVHT Duct Temperature > 88 °C (190 °F)	SINGLE CHIME	MASTER CAUT	COND	HOT AIR FAULT lt	3, 4, 5, 7, 8
AFT (FWD) CRG HEAT FAULT Cargo heating controller fault	NIL	NIL		NIL
AFT (FWD) CRG VENT FAULT Cargo fan fault			NIL
AFT (FWD) CRG ISOL VALVE Cargo isolation valve				ISOL VALVE FAULT It

22 AUTO FLIGHT – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
FAC 1 (2) FAULT	SINGLE CHIME	MASTER CAUT	NIL	FAC FAULT lt	3, 4, 5, 7, 8
YAW DAMPER 1 (2)	NIL	NIL		NIL	3, 4, 5, 7, 8, 10
RUDDER TRIM 1 (2) FAULT					3, 4, 5, 7, 8
RUD TRV LIM 1 (2)
FCU 1 (2) FAULT
FAC 1 + 2 FAULT	SINGLE CHIME	MASTER CAUT		FAC FAULT lts	4, 5, 7, 8
YAW DAMPER SYS				NIL	4, 5, 7, 8, 10
RUD TRIM SYS			F/CTL		4, 5, 7, 8
RUD TRV LIM SYS			NIL		4, 5
A/THR OFF A/THR disconnection (Refer to FCOM).					4, 8, 10
A/THR LIMITED A/THR is active but thrust levers are set below CL detent (2 engines), or MCT detent (1 engine).	SINGLE CHIME every 5 s	MASTER CAUT every 5 s			1, 2, 3, 4, 8, 9, 10
FCU 1 + 2 FAULT	SINGLE CHIME	MASTER CAUT			3, 4, 5, 7, 8
AP OFF AP disengagement (Refer to FCOM).	CAVALRY CHARGE	MASTER WARN			–
(ILS) CAPABILITY DOWNGRADE ‐ Condition(s) required for CAT3/CAT2 are no longer fulfilled. (Refer to FCOM for Failures and Associated Actions Above 1 000 ft for CAT II or CAT III). ‐ Mode reversions (Refer to FCOM Mode Reversions)	TRIPLE CLICK	NIL			2, 3, 4, 5, 8, 9, 10
WINDSHEAR No ECAM message.	SYNTHETIC VOICE “WINDSHEAR” repeated 3 times	NIL		“WINDSHEAR” on PFDs	2, 3, 4, 8, 9
WINDSHEAR DET FAULT or REAC W/S DET FAULT (*)	SINGLE CHIME	MASTER CAUT		NIL	3, 4, 5, 8
LOW ENERGY WARNING Available between 100 and 2000 ft in CONF ≥ 2. No ECAM message.	SYNTHETIC VOICE “SPEED” 3 times every 5 s	NIL			1, 2, 3, 4, 8, 9, 10
AUTOLAND (No ECAM message) Only available below 200 ft.	NIL	AUTOLAND (red) on glareshield			2, 3, 4, 5, 8, 9, 10
When GPS primary is lost, the ″GPS PRIMARY LOST″ message is displayed on the ND and PFD.	NIL	NIL		ND/MCDU message	2, 3, 4, 5, 8, 9, 10
NAV FMS/GPS POS DISAGREE Is triggered, when FMS 1 or 2 position differs from GPS 1 or 2 position by more than: ‐ A longitude threshold that depends on the latitude: • 0.5 min for latitudes below 55 °, • 0.9 min for latitudes at or above 55 °, and below 70 °, ‐ A latitude threshold of 0.5 min , regardless of the latitude. Above 70 ° of latitude, a longitude difference does not trigger the alarm.	SINGLE CHIME	MASTER CAUT		NIL	1, 3, 4, 10
TCAS MODE FAULT TCAS flight guidance mode is operative					3, 4, 5, 7

23 COMMUNICATIONS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
CIDS 1 + 2 FAULT	SINGLE CHIME	MASTER CAUTION	NIL	NIL	3, 4, 5, 7, 8
VHF 1(2)(3) EMITTING HF 1(2) EMITTING Transmitter emitting more than 60 s
*SATCOM () FAULT**	NIL	NIL
*ACARS () FAULT**
*HF 1(2) () DATA FAULT**
*VHF 3 () DATA FAULT**
*SATCOM () DATA FAULT**

MEMO DISPLAY

This display shows “AUDIO 3 XFRD” in green, if the AUDIO SWITCHING selector is not on NORM.
ACARS (*), the display shows:
– “ACARS CALL” in green, pulsing, if ACARS has received a message from the ground requesting a voice communication.
‐ “VHF 3: VOICE” in green, if VHF 3 is operating in voice mode and ACARS communication is interrupted.
‐ “ACARS MSG” in green, pulsing, if ACARS has received a message from the ground
‐ ACARS STBY in green, if ACARS communications between the aircraft and the ground are lost.
SATCOM (*), the display shows “SATCOM ALERT” in green, when a message with a priority level below 4 is received from the ground.
HF (*) and ATSU (*), the display shows “HF VOICE”, pulsing in green for 10 s and then steady,
when all the HF radios are in voice mode.

24 ELECTRICAL – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNINGS	FLT PHASE INHIB
EMER CONFIG Loss of main generators.	CRC	MASTER WARN	NIL (1)	RAT and EMER GEN FAULT lt	4, 8
ESS BUSES ON BAT DC and AC ESS BUSES are supplied by batteries	CRC	MASTER WARN	ELEC	NIL	1, 2, 3, 4, 8, 9, 10
AC BUS 1 FAULT AC BUS 2 FAULT AC ESS BUS SHED DC BUS 1 FAULT DC BUS 2 FAULT DC BUS 1 + 2 FAULT DC ESS BUS FAULT DC ESS BUS SHED Bus(es) is (are) no longer supplied.	SINGLE CHIME	MASTER CAUTION	ELEC	NIL	4, 8
AC ESS BUS FAULT Bus is no longer supplied.				AC ESS FEED FAULT lt	4, 8
AC ESS BUS ALTN				NIL	3, 4, 5, 6, 7, 8
DC BAT BUS FAULT Bus is no longer supplied.					4, 5, 7, 8
DC EMER CONFIG DC BUS 1 and 2 and DC ESS BUS are not supplied.					4, 8
GEN 1(2) FAULT ‐ Protection trip initiated by associated GCU, or ‐ Opening of line contactor with GEN pb ON.				GEN 1(2) FAULT	1, 4, 5, 7, 8,10
GEN 1(2) OFF GEN 1(2) pb OFF with no FAULT.				NIL	1, 3, 4, 5, 7, 8, 10
APU GEN FAULT ‐ Protection trip initiated by associated GCU, or ‐ Opening of line contactor with APU GEN pb-sw ON.				APU GEN FAULT lt	4, 5, 7, 8
GEN 1(2) or APU GEN OVERLOAD Load of one generator is above 100 % of rated output				GALLEY FAULT lt	3, 4, 5, 7, 8
IDG 1(2) OIL LO PR IDG oil pressure low				IDG 1(2) FAULT lt	1, 4, 5, 7, 8, 10
IDG 1(2) OIL OVHT IDG outlet oil TEMP above 185 °C				IDG 1(2) FAULT lt	1, 4, 5, 7, 8, 10
IDG 1(2) DISCONNECTED on ground				IDG OFF It	3 to 10
BAT 1(2) FAULT Charging current increases at an abnormal rate				BAT 1(2) FAULT lt	3, 4, 5, 7, 8
ESS TR FAULT				NIL	3, 4, 5, 7, 8
C/B TRIPPED ON OVHD PNL C/B TRIPPED ON L (R) ELEC BAY C/B TRIPPED REAR PNL J-M or N-R or S-V or W-Z One C/B tripped in the designated zone.			NIL		3, 4, 5, 7, 8, 9, 10
BAT 1(2) OFF BAT pb OFF without fault.	NIL	NIL	ELEC		1, 3, 4, 5, 7, 8, 9, 10
TR 1(2) FAULT					3, 4, 5,7, 8
BCL 1(2) FAULT
STATIC INV FAULT			NIL
EMER GEN 1 LINE OFF GEN 1 LINE pb-sw in OFF position.			NIL		1, 3, 4, 5, 7, 8, 9, 10

(1) The flight crew must call up the ELEC page on the upper ECAM by pressing and holding the ELEC pushbutton on the ECAM control panel.
(*) If installed.

MEMO DISPLAY

EMER GEN is displayed in green, when the emergency generator is running.

26 ENGINE AND APU – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
ENG 1 (2) FIRE Fire detected by both loops or by one loop, the other one being faulty, or break in both loops occuring within 5 s	CRC	MASTER WARN	ENGINE	FIRE lts on ENG FIRE pb and on ENG panel	NIL
APU FIRE Fire detected by both loops or by one loop, the other one being faulty, or break in both loops occuring within 5 s	CRC	MASTER WARN	APU	FIRE lt on APU FIRE pb	NIL
ENG 1 (2) APU FIRE DET FAULT Both loops inoperative or Fire Detector Unit inoperative	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 7, 8
ENG 1 (2) APU LOOP A (B) FAULT	NIL	NIL	NIL	NIL	3, 4, 5, 7, 8

26 AVIONICS BAY – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
AVNCS SMOKE Smoke detected in ventilation extraction duct	SINGLE CHIME	MASTER CAUT	ELEC	– SMOKE lt on EMER ELEC PWR panel – FAULT lts on BLOWER and EXTRACT pb sw	4, 5, 7, 8

26 LAVATORY – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNINGS	FLT PHASE INHIB
LAVATORY SMOKE Smoke detected in one lavatory.	CRC	MASTER WARN	NIL	NIL	4, 5, 7, 8
LAVATORY DET FAULT Lavatory smoke detection fault	NIL	NIL			3, 4, 5, 7, 8
DET FAULT Both CIDS Smoke Detection functions are failed.	SINGLE CHIME	MASTER CAUT			3, 4, 5, 7, 8

26 CARGO COMPARTMENTS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
FWD (AFT) CARGO SMOKE Smoke detected	CRC	MASTER WARN	COND	SMOKE light on CARGO SMOKE panel	4, 5, 7, 8
FWD (AFT) CRG DET FAULT Smoke detection fault	NIL	NIL	NIL	NIL	3, 4, 5, 7, 8
DET FAULT Both CIDS Smoke Detection Functions are failed.	SINGLE CHIME	MASTER CAUTION			3, 4, 5, 7, 8
FWD (AFT) CARGO BTL FAULT Forward or aft bottle squib failed or bottle on low pressure.	SINGLE CHIME	MASTER CAUTION			4, 5, 7, 8

27 FLIGHT CONTROL SYSTEM – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
CONFIG SLATS/FLAPS NOT IN T.O CONFIG, or CONFIG SPD BRK NOT RETRACTED, or CONFIG PITCH TRIM NOT IN TO RANGE, or CONFIG RUD TRIM NOT IN T.O RANGE A/C not in TO configuration when thrust levers are set at TO, or Flex TO, or when pressing TO CONFIG. pb.	CRC	MASTER WARN	NIL	NIL	5, 6, 7, 8
			F/CTL
CONFIG R (L) SIDESTICK FAULT (BY TAKE OVER) L or R sidestick is inoperative (takeover pb pressed more than 30 s) when thrust levers are set at TO, or Flex TO, or when pressing TO CONFIG pb.			NIL	Red (1) SIDESTICK PRIORITY lt
L + R ELEV FAULT Loss of both elevators.			F/CTL	PFD message	NIL
L (R) SIDESTICK FAULT Transducers, on pitch or roll axis, are failed on one sidestick.	SINGLE CHIME	MASTER CAUT		NIL
ELAC 1 (2) FAULT Failure of ELAC				FAULT lt on ELAC pb	3, 4, 5, 7, 8
ELAC 1 (2) FAULT One sidestick transducer fault.				NIL
SEC 1 (2) (3) FAULT Failure of one SEC.				FAULT lt on SEC pb	3, 4, 5
FCDC 1 + 2 FAULT Failure of both FCDCs.				NIL	4, 5, 7
DIRECT LAW Direct laws are active.				PFD message	4, 5, 7, 8
ALTN LAW Alternate laws are active.			NIL	NIL
DUAL INPUT Both sidesticks are moved simultaneously.	Synthetic voice repeated every 5 s	NIL		SIDESTICK Priority light	NIL
GND SPLR FAULT Loss of ground spoiler function in SEC 1 + 3 or 1 + 2 or 2 + 3 or 1 + 2 + 3.	SINGLE CHIME	MASTER CAUTION	F/CTL	NIL	3, 4, 5
SPD BRK DISAGREE Position disagree between surfaces and lever position.
SPD BRK FAULT Speedbrake lever transducers to SEC 1 and 3 failed.
SPD BRK STILL OUT Speedbrake out with at least one engine not at idle.			NIL		1, 2, 3, 4, 5, 8, 9, 10
STABILIZER JAM Loss of the electrical control of the stabilizer (with or without jamming of the stabilizer)			F/CTL		4, 5
L (R) ELEV FAULT Loss of both servojacks on one elevator, or activation of elevator flutter protection in ELAC.
L (R) AIL FAULT Loss of both servojacks on one aileron.
SPLR FAULT Loss of one or more spoilers.					3, 4, 5, 7
ELAC 1 PITCH FAULT Failure of pitch channel in ELAC 1.	NIL	NIL			3, 4, 5, 7, 8
ELAC 2 PITCH FAULT Failure of pitch channel in ELAC 2, or loss of one or both ELAC 2 rudder pedal transducers.
GND SPLR 1 + 2 (3 + 4) Ground spoiler channel failed in SEC 3 (1).					3, 4, 5
ELEV SERVO FAULT Loss of one servojack on one elevator.
SPD BRK 2 (3 + 4) FAULT Speedbrake lever transducers to SEC 3 (1) failed.					3, 4, 5, 7, 8
AIL SERVO FAULT Loss of one servojack on one aileron, or loss of one or both ELAC 1 rudder pedal transducers.
FCDC 1 (2) FAULT			NIL
SIDESTICK PRIORITY Failure in a sidestick priority logic circuit.					3, 4, 5, 6, 7, 8, 9

(1) The red SIDESTICK PRIORITY light comes on, as soon as the sidestick becomes inoperative.

MEMO DISPLAY

The “SPEED BRK” memo display logic:
- When the speedbrakes are extended in Flight Phases 2, 3, 4, and 5, the “SPEED BRK”
  memo flashes in amber.
- When the speedbrakes are extended in Flight Phases 6 and 7, the “SPEED BRK” memo
  appears in green. It flashes in amber, after 50 s, if at least one engine is above idle.
The “GND SPLRS ARMED” message appears in green, when the ground spoilers are armed.

27 FLAPS AND SLATS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
CONFIG SLATS (FLAPS) NOT IN TO CONFIG Slats or flaps are not in takeoff configuration, when thrust levers are set at TO or FLEX TO, or when pressing the TO CONFIG pb.	CRC	MASTER WARN	NIL	NIL	5, 6⁽¹⁾, 7, 8
FLAP LVR NOT ZERO Flap lever is not in the zero position, and the aircraft is above 22000 ft.					1, 2, 3, 4, 5, 7, 8, 9, 10
SLATS (FLAPS) FAULT Failure of both slat or flap channels.	SINGLE CHIME	MASTER CAUT			4, 5, 8
SLATS (FLAPS) LOCKED Slats or flaps’ wing tip brakes applied, or non alignment detected between 2 flaps.
SLATS SYS 1(2) FAULT Failure of slat channel in one SFCC.	NIL	NIL			3, 4, 5, 7, 8
FLAP SYS 1 (2) FAULT Failure of flap channel in one SFCC.
SLAT (FLAP) TIP BRK FAULT Failure of one wing tip brake on slats or flaps, or failure of one wing tip brake solenoid on slats, or flaps.
FLAPS ATTACH SENSOR Failure of flap attachment’s failure detection sensor.

⁽¹⁾ The warning is automatically recalled by pressing the TO CONFIG pb.

28 FUEL – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
L(R) TK PUMP 1 + 2 LO PR	SINGLE CHIME	MASTER CAUT	FUEL	L(R) TK PUMP 1 + 2 FAULT lt	3, 4, 5, 7, 8⁽¹⁾
CTR TK PUMP 1(2) LO PR				CTR TK PUMP 1(2) FAULT lt
CTR TK PUMPS LO PR				CTR TK PUMP FAULT lts
CTR TK PUMPS OFF CTR TK pb at OFF with no FAULT				OFF lt on CTR TK PUMP pb	1, 3, 4, 5, 7, 8, 9, 10
AUTO FEED FAULT (CTR TK > 250 kg (550 lb) and L or R WING TK < 5000 kg (11000 lb) OR (CTR TK pumps do not stop after slat extension or CTR TK low level)				MODE SEL FAULT lts / NIL	3, 4, 5, 8
L(R) WING TK LO LVL (750 kg – 1650 lb)				NIL	3, 4, 5, 7, 8, 9
L + R WING TK LO LVL Low level detected in both wing inner cells (remaining flight time is about 30 min)					3, 4, 5, 7, 8, 9
L(R) OUTER TK HI TEMP or L(R) INNER TK HI TEMP Fuel temp above: In outer cell, above 55 °C on ground / above 60 °C in flight. In inner cell, above 45 °C on ground / above 54 °C in flight.					3, 4, 5, 7, 8
L(R) XFR VALVE CLOSED Both transfer valves fail to open after inner cell low level.					3, 4, 5, 7, 8
ENG 1(2) LP VALVE OPEN Valve disagree in open position.					4, 5, 7, 8
APU LP VALVE FAULT Valve position disagree.	NIL	NIL			3, 4, 5, 7, 8⁽²⁾
L(R) OUTER TK LO TEMP, or L(R) INNER TK LO TEMP Fuel temperature < approx. -43 °C
L(R) TK PUMP 1(2) LO PR				L(R) TK PUMP 1(2) FAULT lt
L(R) XFR VALVE OPEN Either transfer valve opens before inner tank reaches low level.				NIL
X FEED VALVE FAULT Valve position disagree.
FQI CH 1(2) FAULT

(1) Inhibited if pump selected OFF.
(2) PUMP LO PR is inhibited, if the pump is selected OFF in phases 1 and 10.

MEMO DISPLAY

OUTR TK FUEL XFRD appears in green, if at least one transfer valve is open in one wing tank.
CTR TK FEEDG appears in green, if at least one center tank pump is energized.
FUEL X FEED appears in green, if the fuel X FEED valve pushbutton is ON, and the X FEED valve is not fully closed. It appears in amber in flight phases 3, 4, or 5.
REFUELG appears in green, when the door of the refuel control panel (*) on the fuselage or on the wing is open.

29 HYDRAULIC – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE Conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
B + Y B + G SYS LO PR Y + G System pressure ≤ 1450 PSI (reset if pressure ≥ 1750 PSI)	CRC	MASTER WARN	HYD	FAULT lt	4, 5(1)
G (Y) RSVR LO AIR PR Air pressure of the reservoir ≤ 22 PSI (reset if air pressure ≥ 25 PSI)	SINGLE CHIME	MASTER CAUT		FAULT lt on associated pump(s) pb and on PTU pb-sw if Y or G SYS affected	3, 4, 5, 7, 8
B RSVR LO AIR PR Reservoir air pressure ≤ 30 PSI (detected in flight but only displayed on ground after landing)					1, 2, 3, 4, 5, 6, 7
B RSVR LO AIR PR Reservoir air pressure ≤ 22 PSI reset if pressure ≥ 25 PSI					3, 4, 5, 7, 8
G (Y)(B) RSVR OVHT Fluid temperature ≥ 93 °C (reset if TEMP ≤ 88 °C)					3, 4, 5, 7, 8
G (Y)(B) RSVR LO LVL Fluid quantity: < 3.5 l (0.92 US Gal) (green-yellow) < 2.4 l (0.63 US Gal) (blue)					4, 5 (2), 7, 8
G (Y) ENG 1(2) PUMP LO PR Pump outlet pressure ≤ 1750 PSI (reset if pressure ≥ 2200 PSI)				FAULT lt on affected pump pb	4, 5, 7, 8
Y ELEC PUMP LO PR Yellow system pressure ≤ 1450 PSI (reset if pressure ≥ 1750 PSI) with – YELLOW ELEC PUMP pb-sw at ON – Y ENG PUMP and PTU not available
B ELEC PUMP LO PR Pump outlet pressure ≤ 1450 PSI (reset if pressure ≥ 1750 PSI)
B ELEC PUMP OVHT Y ELEC PUMP OVHT					3, 4, 5, 7, 8
G (Y) SYS LO PR System pressure ≤ 1450 PSI (reset if pressure ≥ 1750 PSI)					4, 5, 7, 8 (1)
B SYS LO PR System pressure ≤ 1450 PSI (reset if pressure ≥ 1750 PSI)				NIL	1, 4, 5, 7, 8, 10
PTU FAULT PTU not running on ground in case the differential pressure is above 650 PSI, between G and Y system, or in flight PTU still at AUTO position in case of G or Y reservoir low level and G or Y system low pressure.				FAULT lt only in case of G or Y RSVR LO LVL or RSVR LO AIR PR or RSVR OVHT	3, 4, 5, 8, 9, 10
RAT FAULT RAT not fully stowed or pressure present in RAT stowing actuator or RAT pump not available				NIL	3, 4, 5, 6, 7, 8, 9

(1) Inhibited on the ground (flight phases 1, 2, 9, 10) when corresponding engine is shut down.
 
(2) The HYD G(Y) RSVR LO LVL alert is inhibited for the first 15 s of flight phase 5.
 
The HYD B RSVR LO LVL alert is inhibited for the entire flight phase 5.

MEMO DISPLAY

“RAT OUT” appears in green, if the ram air turbine is not fully stowed. The color changes to amber during flight phases 1 and 2.
“HYD PTU” appears in green, when the power transfer unit is running.

30 WING ANTI-ICE – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
WING A. ICE OPEN ON GND On ground, valves remain open more than 35 s after wing anti-ice is selected ON.	SINGLE CHIME	MASTER CAUT	BLEED	NIL	3, 4, 5, 6, 7, 8
SYS FAULT Valve not open when wing anti-ice selected ON.				ANTI ICE WING FAULT lt	3, 4, 5, 7, 8
L (R) VALVE OPEN Valve not closed when wing anti-ice selected off				ANTI ICE WING FAULT lt	4, 5, 7, 8
HI PR High pressure detected when the wing anti-ice is selected ON.	NIL	NIL		NIL	3, 4, 5, 7, 8

MEMO DISPLAY
The “WING A. ICE” message is displayed in green, if the WING ANTI ICE pb-sw is ON.

30 ENGINE ANTI-ICE – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLTPHASE INHIB
ENG 1(2) VALVE OPEN Valve disagree in the open position.	SINGLE CHIME	MASTER CAUT	NIL	ENG 1 (2) ANTI ICE FAULT lt	3, 4, 5, 7, 8
ENG 1(2) VALVE CLSD Valve disagree in the closed position.

MEMO DISPLAY
This display shows “ENG A. ICE” in green, if one or both ENG ANTI ICE pb-sw are ON.

30 WINDOW HEAT – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNINGS	FLT PHASE INHIB
L(R) WINDSHIELD Failure of L or R windshield heating	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 7, 8
L+R WINDSHIELD Failure of both windshield heating
L(R) WINDOW Failure of L or R window heating	NIL	NIL

30 PROBES HEAT – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
CAPT (F/O) PITOT CAPT (F/O) L(R) STAT CAPT (F/O) AOA CAPT (F/O) TAT Failure of corresponding probe heating	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 7, 8
STBY PITOT STBY L(R) STAT STBY AOA Failure of corresponding probe heating
CAPT (F/O) (STBY) PROBES Failure of one probe heat channel/computer
CAPT + F/O PITOT CAPT+ STBY PITOT F/O + STBY PITOT Failure of the corresponding probes heating					4, 5, and 8
ALL PITOT Failure of CAPT, F/O and STBY probes heating

31 INDICATING / RECORDING SYSTEMS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNINGS	FLT PHASE INHIB
SDAC 1 + 2 FAULT	SINGLE CHIME	MASTER CAUT	NIL	NIL	4, 5, 7, 8
DMC 1 (2) FAULT					3, 4, 5(1), 7, 8
DMC 3 FAULT
SDAC 1 (2) FAULT	NIL	NIL			3, 4, 5, 7, 8
FWC 1 (2) FAULT
FWC 1 + 2 FAULT					NIL
DFDR FAULT					3, 4, 5, 7, 8
RECORDER SYS FAULT
OEB/FWC DISCREPANCY FWC 1 and FWC 2 do not have the same OEBs listed in their OEB reminder database.	SINGLE CHIME	MASTER CAUT			3 to 8

(1) Inhibited only during first 15 s of Flight Phase 5.

32 GEARS AND DOORS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
GEAR NOT DOWNLOCKED One gear not downlocked and L/G selected down	CRC	MASTER WARN	WHEEL	UNLK lt on	3, 4, 5
GEAR NOT DOWN 1. L/G not downlocked and radio height lower than 750 ft and both engines N1 lower than 75 % (or if engine shut down N1 of remaining engine lower than 97 %). or 2. L/G not downlocked and radio height lower than 750 ft and both engines not at T.O. power and flaps at 1, 2, 3 or FULL. or 3. L/G not downlocked and flaps at 3 or FULL and both radio altimeters failed. Note: In the cases 2 and 3 above, the aural warning can only be cancelled by the emergency cancel pushbutton.			NIL	DOWN ARROW lt on LDG GEAR panel
SHOCK ABSORBER FAULT One shock absorber not extended when airborne or not compressed after landing	SINGLE CHIME	MASTER CAUT		NIL	1, 3, 4
DOORS NOT CLOSED One gear door is not uplocked			WHEEL		1, 3, 4, 5, 8, 9, 10
GEAR NOT UPLOCKED One gear not uplocked and L/G not selected down				UNLK lt on LDG GEAR panel	3, 4, 7, 8, 9, 10
GEAR UPLOCK FAULT One gear uplock engaged with corresponding gear downlocked					4
LGCIU 1 (2) FAULT	NIL	NIL		NIL	4, 5, 7, 8
SYS DISAGREE Disagree between L/G positions detected by the two LGCIU’s					3, 4, 5, 6,7, 8

32 NOSE WHEEL STEERING – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
NW STRG FAULT detected by BSCU	SINGLE CHIME	MASTER CAUT	WHEEL	NIL	3, 4, 5, 8

MEMO DISPLAY
When the nose wheel steering selector is in the towing position, this display shows “NW STRG
DISC” in green. The legend is amber if one engine is running.

32 BRAKES AND ANTISKID – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE condition	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
CONFIG PARK BRK ON parking brake is on when thrust levers are set at TO or FLX TO power position	CRC	MASTER WARN	NIL	NIL	1, 2, 4 to 10
PARK BRK ON Parking brake is ON during flight.	SINGLE CHIME	MASTER CAUT	NIL	NIL	1 to 5, 8 to 10
BRAKES HOT It is triggered when one brake temperature is higher than 300 °C and off when the highest brake temperature is lower than 290 °C.			WHEEL	HOT lt on BRK FAN pb sw	4, 8 to 10
AUTO BRK FAULT failure of autobrake when armed				NIL	3 to 5
A/SKID NWS FAULT ‐ Loss of normal brake system associated with Y HYD SYS lo PRESS or ‐ Failure of both BSCU channels					4, 5
ANTI SKID/NWS OFF switch at OFF position					4, 5
HYD SEL FAULT failure of brake normal selector valve or NWS selector valve in open position			NIL		3 to 5, 7, 8
SYS 1 (2) FAULT failure of one BSCU channel	NIL	NIL	NIL		3 to 5, 7, 8
RELEASED Brake of one wheel is released. It is detected when the landing gear is downlocked and, at least one engine is running, and normal braking is active.	SINGLE CHIME	MASTER CAUT	WHEEL		4, 5
NORM BRK FAULT Normal braking function is lost.	SINGLE CHIME	MASTER CAUT			3 to 5
ALTN BRK FAULT Alternate braking function is lost.	NIL	NIL			3, 4, 5, 7, 8
ALTN L(R) RELEASED Brakes of one gear is released. It is triggered when the landing gear is downlocked, and at least one engine is running, and alternate braking is active.	SINGLE CHIME	MASTER CAUT	NIL		3, 4, 5
NORM + ALTN FAULT Normal and alternate functions are lost. Parking brake available.			WHEEL		4, 5
BRK Y ACCU LO PR The yellow accumulator is in low pressure.					3, 4, 5, 7, 8
PARK BRK LO PR The yellow accumulator and hydraulic system pressures are low with parking brake on.					3 to 8
BRAKES-NWS MINOR FAULT Single system failure, loss of redundancy.	NIL	NIL	NIL		2 to 9

MEMO DISPLAY

If the parking brake is ON, the “PARK BRK” memo appears in green, during flight phases 1, 2, 9, and 10.
If the autobrake is armed, AUTO BRK LO, AUTO BRK MED, or AUTO BRK MAX appears.
If the autobrake is faulty, “AUTO BRK OFF” appears.
“BRK FAN” appears in green, if the BRK FAN (*) pushbutton is ON.

34 ADIRS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
STALL WARNING (No ECAM message) An aural stall warning is triggered when the AOA is greater than a predetermined angle This angle depends on the: ‐ Slats/Flap position ‐ Speed/Mach ‐ F/CTL law (normal, alternate/direct)	CRICKET + STALL (SYNTHETIC VOICE)	MASTER WARN	NIL	NIL	GND
OVERSPEED ‐ VMO/MMO Aircraft speed/mach greater than VMO + 4 kt/MMO + 0.006 ‐ VLE Aircraft speed greater than VLE + 4 kt, with L/G not uplocked, or L/G doors not closed ‐ VFE Aircraft speed greater than VFE + 4 kt, with slats or/and flaps extended	CRC	MASTER WARN		NIL	2, 3, 4, 8, 9, 10
ADR 1 (2) FAULT	SINGLE CHIME	MASTER CAUT		ADR FAULT lt	1, 4, 8, 10
ADR 3 FAULT					1, 4, 5, 7, 8, 10
ADR (1+2) (1+3) (2+3) FAULT					1, 4, 8, 10
ADR 1+2+3 FAULT	CRC	MASTER WARN		NIL	1, 4, 8, 10
IR 1 (2) FAULT	SINGLE CHIME	MASTER CAUT		IR FAULT lt	4, 5, 7, 8
IR 3 FAULT					4, 5, 7, 8
IR (1+3) (2+3) FAULT					4, 8
IR 1+2 FAULT					4, 8
CAPT (F/O) (STBY) AOA FAULT	NIL	NIL		NIL	2 to 9
HDG DISCREPANCY Difference between the heading on the CAPT and F/O displays is greater than 5 °.	SINGLE CHIME	MASTER CAUT		CHECK HDG (on PFD and ND)	4, 8
ATT DISCREPANCY Difference between roll or pitch angle, displayed on the CAPT and F/O PFD greater than 5 °.				CHECK ATT (on PFD)	3, 4, 8
ALTI DISCREPANCY Difference between the altitude, displayed on the CAPT and F/O PFD, is greater than: ‐ 500 ft, if BARO ref STD is selected ‐ 250 ft, if QNH (or QFE) is selected				CHECK ALT (on PFD)
BARO REF DISCREPANCY Difference between CAPT and F/O sides				NIL
IAS DISCREPANCY Caution activated when there is a discrepancy between the speeds displayed on the PFDs.				NIL	4, 5, 7, 8
ADR DISAGREE One ADR is faulty or has been rejected by the ELAC, and there is a speed or angle-of-attack disagree between the two remaining ADRs.				FAULT lts on ELAC pbs	3, 4, 5, 7
IR DISAGREE Disagree between two IR, with the third one failed.				PFD message	3, 4, 5, 7
IR NOT ALIGNED Problem detected during IR alignment				NIL	1, 4, 5, 6, 7, 8, 10

MEMO DISPLAY

”IRS IN ALIGN X MN” memo appears during phase 1 or 2, during IRS alignment. X MN
indicates the number of minutes remaining (1 < X < 10), until NAV mode is reached.

Before any engine is started, “IRS IN ALIGN X MN” memo:
- Appears in green when at least one active IRS is being aligned,
- Pulses in green if the alignment of one IRS is faulty.
When one engine is started, “IRS IN ALIGN X MN” memo appears in amber during IRS
alignment. If the alignment of one IRS is faulty, “IRS IN ALIGN X MN”memo is replaced by the “IR NOT ALIGNED” ECAM caution.

”IR IN ATT ALIGN” appears in green during the IR alignment in Attitude mode.

34 GPS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
GPS 1 (2) FAULT	SINGLE CHIME	MASTER CAUTION	NIL	NIL	4, 5, 7, 8
FM/GPS POS DISAGREE	SINGLE CHIME	MASTER CAUTION	NIL	NIL	1, 3, 4, 10

34 RADIO ALTIMETER – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
RA 1(2) FAULT	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 8
RA DEGRADED In case a significant discrepancy occurs in flight between the two radio-altimeters.	NIL	NIL	NIL	NIL	2 to 8

34 WEATHER RADAR – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
PRED. W/S DET FAULT	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 8

MEMO DISPLAY
The “PRED W/S OFF” message appears, when windshear is set to OFF on the weather radar
panel.
The “PRED W/S OFF”, message appears in green during flight phases 2 and 6.
It appears in amber:
‐ In flight phases 3, 4, 5, 7, 8, and 9
‐ When the T.O. CONFIG pb is pressed during phase 2.

34 GPWS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
GPWS FAULT	SINGLE CHIME	MASTER CAUT	NIL	GPWS SYS FAULT lt	1, 3, 4, 5, 8, 9, 10
GPWS TERR DET FAULT The enhanced terrain detection function is inoperative. The basic GPWS mode 1 to 5 are still operative.	SINGLE CHIME	MASTER CAUT	NIL	GPWS TERR FAULT lt	1, 3, 4, 5 8,10

MEMO DISPLAY
GPWS FLAP 3 is displayed in green when GPWS LDG FLAP 3 pb-sw is ON.
GPWS FLAP MODE OFF is displayed in green when GPWS FLAP MODE pb-sw is OFF.
Airborne TERR STBY appears in green when the aircraft position accuracy (computed by the
EGPWS) is not sufficient to allow the enhanced TCF and TAD modes to operate. These modes
are not available until the TERR STBY memo disappears. If selected, the terrain data display on
ND is automatically deselected when the TERR STBY memo is triggered.”
TERR OFF is displayed when the TERR pb-sw is switched OFF:
‐ It appears in green in flight phase 2, before the Take Off Configuration test is launched, and in
flight phase 6.
‐ It appears in amber in flight phase 2, after the Take Off Configuration test, and in flight phases
3, 4, 5, 7, 8 and 9.

34 TCAS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
TCAS FAULT in case of TCAS internal failure	SINGLE CHIME	MASTER CAUT	NIL	Flag on PFD and ND	3, 4, 5, 7
TCAS STBY in the case where the flight crew sets the TCAS on STBY in flight.	SINGLE CHIME	MASTER CAUT	NIL	NIL	ALL, except 6

MEMO DISPLAY
TCAS STBY is displayed in green, when:

‐ ATC STBY is selected by the crew, or
‐ TCAS STBY is selected by the crew during flight phases other than 6, or
‐ ALT RPTG is selected at off, or
‐ both ATC or both RA are failed.
‐ In the case of a triple ADR failure.

TCAS STBY is displayed in amber, when the flight crew sets the TCAS on STBY in flight phase 6.

36 PNEUMATIC WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
ENG 1 (2) BLEED FAULT engine 1 (2) running and bleed air pressure > 57 PSI (+3/-0) or temperature: > 257 °C for more than 55 s or > 270 °C for more than 15 s or > 290 °C for more than 5 s	SINGLE CHIME	MASTER CAUT	BLEED	ENG BLEED FAULT lt	1, 3, 4, 5, 7, 8, 10
L (R) WING LEAK temperature > 124 °C detected by the loops					3, 4, 5, 7, 8
ENG 1 (2) BLEED LEAK temperature > 204 °C detected by the loop and engine 1 (2) running
ENG 1 (2) BLEED NOT CLSD bleed valve not automatically closed during engine start or with APU bleed selected
BLEED 1 (2) OFF one engine bleed switched off with no fault				ENG BLEED OFF lt	1, 3, 4, 5, 7, 8, 9, 10
APU BLEED FAULT APU available and APU bleed valve position disagrees with selected position.				NIL	3, 4, 5, 7, 8
APU BLEED LEAK temperature > 124 °C detected by the loop				APU BLEED FAULT lt	3, 4, 5, 7, 8
ENG 1 (2) BLEED ABNORM PR regulated pressure is abnormal				NIL	1, 3, 4, 5, 7, 8, 10

47 INFORMATION SYSTEMS – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
ATSU FAULT (Failure at ATSU initialization, if associated with ATSU INIT FAULT ECAM message).	SINGLE CHIME	MASTER CAUTION	NIL	NIL	3, 4, 5, 7, 8
COMPANY FAULT AOC datalink communications failure.	NIL	NIL	NIL	NIL	3, 4, 5, 7, 8

MEMO DISPLAY
‐ The COMPANY DATALINK STBY message is displayed in green, when AOC datalink
air-ground communication is temporarily unavailable, but not lost.
‐ The COMPANY CALL message is displayed in green, when the aircraft receives a message
from the ground requesting voice communication on VHF.
‐ The COMPANY MSG message is displayed in green, when the aircraft receives a message
from the ground.
‐ The COMPANY ALERT message is displayed in green, when the aircraft receives an uplink
alert message, or when an AOC special condition requires a pilot action on the MCDU (depends
on AOC programming). This message pulses green for 180 s, then remains steady. It is
associated with a buzzer for 1 s.

49 APU – WARNINGS AND CAUTIONS

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
AUTO SHUT DOWN automatic shut down of APU for a reason other than a fire.	SINGLE CHIME	MASTER CAUT	APU	APU MASTER SW FAULT lt	3, 4, 5, 7, 8
EMER SHUT DOWN use of APU shut off pushbutton on external power panel or APU FIRE pushbutton pushed. In case of APU fire on ground, the APU FIRE warning is triggered.

MEMO DISPLAY
APU AVAIL appears in green when APU N is above 95 %.

52 DOORS – WARNINGS AND CAUTIONS

E/WD : FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
L(R) FWD (AFT) AVIONICS L(R) FWD CABIN L(R) AFT CABIN L(R) FWD EMER EXIT L(R) AFT EMER EXIT FWD CARGO AFT CARGO BULK CARGO () STAIRS* (*) Affected door not closed (proximity detectors)	SINGLE CHIME	MASTER CAUT	DOOR	NIL	1, 4, 5, 7, 8, 10

70 POWER PLANT – WARNINGS AND CAUTIONS

CFM56 Engine

E/WD: FAILURE TITLE conditions	AURAL WARNING	MASTER LIGHT	SD PAGE CALLED	LOCAL WARNING	FLT PHASE INHIB
ENG DUAL FAILURE	CRC	MASTER WARN	ENG	Associated with GEN FAULT lts and PACK FAULT lt	NIL
ENG 1(2) OIL LO PR Oil low pressure triggered at 13 PSI by the oil pressure switch.	CRC		ENG	NIL	1, 10
ENG 1(2) THR LEVER ABV IDLE ‐ One thrust lever is above idle while the other thrust lever is in the reverse detent at landing. ‐ One thrust lever is above idle while the other thrust lever is at idle, at reverser deselection during landing roll.	RETARD		NIL		1, 2, 3, 4, 5, 6, 7, 10
ENG STALL	SINGLE CHIME	MASTER CAUT	ENG		3, 4, 5, 7, 8
ENG 1(2) HP FUEL VALVE HP fuel valve failed closed.				Associated FAULT lt on ENG panel on pedestal (exception case of starter time exceeded)	3, 4, 5, 7, 8
ENG 1(2) START FAULT Start fault due to: ‐ No light up, or ‐ ENG stall or over TEMP (above 725 °C), or ‐ Starter time exceeded ‐ Thrust lever not at idle ‐ Low start air PRESS					3, 4, 5, 6, 7, 8
ENG 1(2) START VALVE FAULT Position disagree.					3, 4, 5, 7, 8
ENG 1(2) OIL HI TEMP Oil TEMP between 140 and 155 °C for more than 15 min, or oil TEMP above 155 °C.				NIL	4, 5, 7, 8
ENG 1(2) FADEC FAULT Both channels failed.					4, 5, 7, 8
ENG 1(2) LOW N1 No N1 rotation during start.					4, 5, 6, 7, 8, 9, 10
ENG THRUST LOCKED Thrust levers are not moved within 5 s, following an unvoluntary disconnection of the A/THR (or disconnection through the FCU pb).	SINGLE CHIME every 5 s	MASTER CAUT every 5 s	NIL		1, 2, 3, 4, 8, 9, 10
ENG THR LEVERS NOT SET The levers position does not correspond to T.O power mode.	SINGLE CHIME	MASTER CAUT	NIL		1, 4, 5, 6, 7, 8, 10
ENG 1(2) FADEC HI TEMP	SINGLE CHIME	MASTER CAUT	NIL	NIL	3, 4, 5, 7, 8
ENG TYPE DISAGREE Rating discrepancy between the two engines.			NIL		3 to 10
ENG 1(2) THR LEVER DISAGREE Disagree between both resolvers of a thrust lever			ENG		4, 5 (⁽¹⁾)
ENG 1(2) THR LEVER FAULT Both resolvers on one thrust lever have failed.			NIL		4, 5 (⁽¹⁾)
ENG 1(2) FAIL ENG core speed below idle, with master sw ON and fire pb not pushed.					1, 10
ENG 1(2) SHUT DOWN ENG master at off in phases 3 to 8, or ENG FIRE pb pushed in phases 1, 2, 9 and 10.					1, 10
ENG 1(2) REVERSE UNLOCKED One or more reverser doors not locked in stowed position in flight, or on ground with no deploy order.					4, 8 (_⁽²⁾)
ENG 1(2) REV PRESSURIZED Reverser system is pressurized, while rev doors are stowed and locked with no deploy order.					4, 5, 8
ENG 1(2) COMPRESSOR VANE Variable bleed valve SYS or variable stator vane SYS fault.					4, 5, 7, 8
ENG 1(2) N1 or N2 or EGT OVER LIMIT N1 above 104 % N2 above 105.0 % EGT above 950 °C					4, 8
ENG 1(2) IGN A + B FAULT Both ignition circuits are failed.					3, 4, 5, 7, 8
ENG 1(2) CTL VALVE FAULT Burn stag valve failure or HPTC, or RAC system failure.					4, 5, 7, 8
ENG 1(2) FUEL CTL FAULT Fuel metering valve position disagree.
ENG 1(2) SENSOR FAULT PS3 or T25 or T3 or N1 or N2 data unavailable on both channels.
ENG 1(2) PROBES FAULT
T12 or PO PT 2 data unavailable on both channels.
ENG 1(2) N1 (N2, EGT, FF) DISCREPANCY Discrepancy between real and displayed values.					3, 4, 5, 8
ENG 1(2) BLEED STATUS FAULT Bleed, X Bleed, pack, anti-ice valve position status not received by FADEC active channel.					3, 4, 5, 7, 8
ENG 1(2) FUEL FILTER CLOG	NIL	NIL	ENG		3, 4, 5, 7, 8
ENG 1(2) OIL FILTER CLOG			ENG		3, 4, 5, 7, 8
ENG VIB SYS FAULT Failure of vibration detection system.			NIL		3, 4, 5, 6, 7, 8, 9
ENG 1(2) OVSPD PROT FAULT Loss of overspeed protection.			NIL		3, 4, 5, 7, 8
ENG 1(2) IGN A(B) FAULT Ignition circuit A or B failed.	NIL	NIL	NIL	NIL	3, 4, 5, 6, 7, 8
ENG 1(2) FADEC ALTERNATOR Loss of electrical auto supply of either FADEC channel.					3, 4, 5, 7, 8
ENG COMPRESSOR VANE Engine 1 and 2 VBV or VSV fault.
ENG 1(2) FUEL RETURN VALVE Fuel return valve is failed in the not open, or not closed position.
ENG 1(2) FADEC A(B) FAULT One FADEC channel failed.					4, 5, 7, 8
ENG 1(2) EIU FAULT Data bus between EIU and ECU failed.					1, 3, 4, 5, 7, 8, 10
ENG 1(2) REVERSER FAULT Loss of thrust reverser on one engine, due to system components or input faults.					3, 4, 5
ENG 1(2) REV ISOL FAULT	SC	CAUT			3 to 7
ENG 1(2) REV SWITCH FAULT Failure of reverser permission switch.	NIL	NIL			3, 4, 5, 6, 7, 8
ENG REV SET Reverse thrust has been selected in flight.					1 to 4 8 to 10
ENG 1(2) ONE TLA FAULT					3, 4, 5, 6, 7, 8

⁽¹⁾ Alert not inhibited in the flight phases 4 and 5, if the FADEC automatically selects IDLE thrust. 
⁽²⁾ Alert not inhibited in the flight phase 4, if the engine thrust is automatically set to idle.

MEMO DISPLAY
IGNITION appears in green, when continuous ignition is activated on either engine.

Disclaimer: This is for educational purposes only.