A 320 Ffs 5 Simulated Malfunctions List

8/11/2019 A 320 Ffs 5 Simulated Malfunctions List

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A320-200 FFS5

LISTE DES MALFONCTIONS CLASSEES PAR ATA

Updated on May 20th, 2014

ATA 21 'AIR CONDITIONING & PRESS'

TITLE OUTFLOW VALVE STUCKOutflow valve flap mechanical is stuck in current position.

TITLE LDG ELEVATION FAULTLanding elevation data from FMGC not valid.

TITLE EXCESS CAB ALT WINDOW BLOWOUTExplosive decompression (window blow-out).

TITLE EXCESS CAB ALT - CABIN LEAKCabin leak causes according effects on pressurization system.

TITLE NEGATIVE LO DIFFERENTIAL PRESSURE

False warning. Controller does not command sufficient descent rate.

TITLE 'PACK 1(2) OVHT - CLOGGED HEAT EXCHANGER'Compressor overheat due to partially clogged heat exchanger.

TITLE 'PACK 1(2) REGUL FAULT - CONTROLLER FAILURE'Pack 1(2) Controller primary and secondary channel fault detected.

TITLE 'PACK 1(2) FAULT (FCV DRIVES FULLY CLOSED)'PACK FLOW CONTROL VALVE drives fully closed.

TITLE '(NO ECAM) - PACK AUTO SHUTDOWN FOR STARTING INOP'Failure of close relay 12 HB of the flow control valve. FCV remain open.

TITLE 'ZONE REGUL FAULT - PRIMARY CHANNEL FAILURE'Zone controller primary channel fails.

TITLE CABIN DUCT OVERHEATDrive failure commanding trim air valve to fully open.

TITLE 'BLOWER(EXTRACT) FAULT - FAN FAILURE'Blower (extract) fan failure.

TITLE 'CABIN PRESSSYS 1(2) FAULT - LOSS OF 28 VDC'Loss of 28 V DC.

TITLE '(NO ECAM) - LDG ELEV FAULT - ROTRACTOR FAILURE'LDG ELEVATION rotractor failure


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ATA 22 'AUTOFLIGHT/FMGEC'

TITLE FMGC FAULTLoss of 28V power supply to FMGC 1(2).

TITLE FCU FAULTChannel 1(2) is declared invalid (internal power supply fails).

TITLE AP DISENGAGEDFailure of FMGC AP function; FD not affected.

TITLE ATHR FAULTInterruption of A/THR Bus information between FMGC 1(2) and EIU.

TITLE FD FAULTFlight director data to the EFIS is faulty.

TITLE MCDU FAULTLoss of 115 VAC power supply to MCDU 1(2).

TITLE '(NO ECAM) - AUTOLAND FAILURE - LOCALIZER DRIFT'LOC deviation sent by ILS1 and ILS2 to FMGC1 and FMGC2 has a drift of20 microA/sec.

TITLE '(NO ECAM) - NO FLARE - NO IDLE SIGNAL'Error in the radio altitude transmitted by the radio altimeter 1 and2 to FMGC1 and FMGC2 (RA1 = RA2 = RATRUE + 15 ft).

TITLE LONG FLAREError in the radio altitude transmitted by the radio altimeter 1 and 2 toFMGC1 and FMGC2 (RA1 = RA2 = RATRUE - 25).

TITLE 'LAND CAPABILITY DOWNGRADED'Land capability is downgraded during approch.

TITLE LAND CAPABILITY CHANGE'Land capability is downgraded during approach.

TITLE NO LAND MODERadio altitude of radio altimeter 1 and 2 received by FMGC 1 and 2 alwaysabove 400 ft (only values transmitted to FMGC 1 and 2 are altered)

TITLE NO G/S MODEGlide deviation received by FMGC 1 and 2 is fixed to a value of 80uA (onlyvalues transmitted to FMGC 1 and 2 and EGPWS are altered)

TITLE FAC FAULT'

FAC fails internally (FAC not healthy).

TITLE MAP SHIFTIncorrect internal FM position computation due to IRS drift. Slow(Fast)map shift on both NDs.

TITLE YAW DAMPER FAULT'Electrical power failure of actuator 1. Loss of CAT 3 DUAL capability.

TITLE RUDDER TRV LIM FAULTElectrical power failure of side 1 motor.

TITLE '(NO ECAM) - A/P 1(2) LOC CAPTURE FAIL'

Localizer beam capture is inhibited.

TITLE '(NO ECAM) - A/P 1(2) GS CAPTURE FAIL'Glideslope beam capture is inhibited.


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TITLE '(NO ECAM) GS FAULT - RECEIVER FAILURE'There is no output signal due to receiver failure.

TITLE '(NO ECAM) - LOC FAULT - SIGNAL LOSS'Bad coupling of the LOC antenna on the LOC receiver part of the ILS1(2) receiver. Reception of LOC signal is not possible.

TITLE '(NO ECAM) - RADIO ALT DISAGREE - RA#2 15 FT HIGH'

Undetected fault of one radio altimeter.(RA2 delivers a wrong value = RA1 value + 15 ft).

TITLE RUDDER TRIM FAULTElectrical power failure of side 1 motor

TITLE RUDDER TRIMS RESET FAULTCut of the two normally open signals from the reset switch to FAC1 andFAC2.

TITLE RUDDER TRIM RUNAWAYThe connector of the rudder trim control selector is stuck in the leftposition.

ATA 23'COMMUNICATIONS'

TITLE ACP FAULTInternal power failure.- No transmission or reception possible on Capt,F/O or OBS ACP

TITLE 'CIDS 1(2) FAULT - CIDS FAILURE'Respective CIDS failure.

TITLE '(NO ECAM) - VHF TRANSCEIVER FAILURE'Receiver/transmitter failure.

TITLE '(NO ECAM) RMP FAIL'Respective RMP becomes inoperative.

TITLE ACARS FAULTATSU power supply fails. ATSU prompt disappears from all MCDU menus

TITLE VHF 1(2)(3) EMITTINGRespective VHF becomes permanent emitting.


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ATA 24A 'ELECTRICAL AC'

TITLE GEN FAULT (EXCITATION) - 1(2)Generator excitation circuit fails.

TITLE GEN FAULT (EXCITATION) APU

Generator excitation circuit fails.

TITLE GEN FAULT (EXCITATION) EMERGEmergency generator excitation circuit fails

TITLE 'EMER CONFIG - DUAL GEN FAILURE'Simultaneous failure of generators 1 and 2 excitation circuits.

TITLE GEN VOLTAGE INC/DECGenerator excitation fails (voltage increases/decreases to 180 V/60 V at arate of 3V/s).

TITLE GEN FREQUENCY INC/DECSpeed regulation of the constant speed drive fails (frequencyincreases/decreases to 500 Hz/300 Hz at a rate of 4 Hz/s).

TITLE GEN TRANSFER FAULTContactor GLC1 (GLC2) fails open.

TITLE IDG OIL OVERHEATAbnormal friction in the IDG constant speed drive

TITLE IDG OIL LO PRESSOil low pressure switch fails.

TITLE 'AC 1(2) BUS FAULT - UNPOWER DUE TO DIFF PROTECTION'AC BUS 1(2) unpowers due to differential protection.

TITLE 'AC ESS BUS FAULT - SHORT CIRCUIT'AC ESS BUS short circuit.

TITLE 'AC ESS BUS SHED - RELAY FAILS OPEN'Relay 8XH fails in open position.

TITLE 'AC ESS BUS FAULT - FEED CONTACTOR FAILS OPEN'Contactor 3XC side 1 and 2 fail open.

TITLE 'AC ESS BUS FAULT - AC BUS TIE CONTACTOR 1 OPEN'(XU1 (GLC1) contactor coil failure and BTC1 11XU1 contactor coil failure.

TITLE 'ESS BUSES ON BAT - EMER GEN FAULT IN EMER CONFIG'Emergency generator trips due to GCU fault detection.

TITLE '(NO ECAM) - EMER GEN TEST FAIL'Relay 16XE fails in open circuit. Failure of emergency generator testwhen activated via test pb on EMER ELEC PWR Panel.

TITLE '(NO ECAM) - RAT AUTO EXT FAIL'Total electrical failure, but RAT automatic extension fails.


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ATA 24D'ELECTRICAL DC'

TITLE 'DC BUS 1(2)(BAT) FAULT - BUS UNPOWERS'DC BUS becomes unpowered and unpowers supplying TR due to minimumcurrent protection.

TITLE 'DC ESS BUS FAULT - BUS UNPOWERS'

DC essential bus unpowers.

TITLE 'DC ESS BUS SHED - RELAY OPENS'Relay 8PH fails in open position shedding bus 801PP.

TITLE BAT FAULTFaulty BAT 1(2) overheat detection

TITLE 'TR 1(2)(ESS) FAULT - FALSE OVHT DETECTION'TR fault due to false OVHT detection.

TITLE EMERG GEN FAULTConstant Speed Motor/Generator fails. EMER GEN not available with theelectrical system in emergency configuration.

TITLE STATIC INV FAULTStatic inverter internal failure.

ATA 26'FIRE PROTECTION'

TITLE EXTINGUISHABLE FIRE BY FIRST AGENTOverheat detected in engine core element. Fire indications will extinguish10s after one agent

TITLE EXTINGUISHABLE FIRE BY SECOND AGENTOverheat detected in engine core element. Fire indications extinguish 10safter both agents

TITLE UNEXTINGUISHABLE FIREOverheat detected in engine core element. Fire is not extinguishable.

TITLE 'APU FIRE LOOP A(B) FAULT - LOW PRESSURE'Low pressure in the loop detector.

TITLE 'ENG 1 FIRE LOOP A(B) FAULT 'Low pressure in the loop detector.

TITLE 'ENG 2 FIRE LOOP A(B) FAULT 'Fire loop fault.

TITLE AVIONIC SMOKEElectrical fire in avionics bay. Perceptible smoke emanates from foot area

TITLE CARGO SMOKEFire in cargo compartment, detected by SDCU.

TITLE 'LAVATORY SMOKE 'Fire in lavatory A.

TITLE '(NO ECAM) AIR CONDITIONING SMOKE

'Pack smoke.

TITLE '(NO ECAM) AFT CB PANEL SMOKE'Smoke in Aft CB panel caused by faulty bus 101XP.


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ATA 27'FLIGHT CONTROLS'

TITLE ELAC FAULTELAC 1(2) power supply fails.

TITLE SEC FAULTSEC power supply fails.

TITLE FCDC FAULTFCDC power supply fails.

TITLE SLAT SYS FAULTPower supply fails on the slats channel in SFCC 1(2).

TITLE SLATS LOCKED (WTB)Asymmetric slats movement detected by SFCC after control handle selection.

TITLE FLAP SYS FAULTPower supply fails on the flaps channel in SFCC\n1(2).

TITLE FLAPS LOCKED (WTB)Asymmetric flaps movement detected by SFCC after control handle selection.

TITLE SLATS/FLAP HANDLE INOPFlaps/slats do not respond to inputs from FLAP lever.Flap lever position disappears 10s after insertion of malfunction (even ifFlap lever is moved)

TITLE SIDE STICK FAULTCapt(F/O) side stick electronically fails (pitch and roll).

TITLE SIDE STICK PITCH FAULT CAPTCaptain pitch side stick transducer unit mechanically fails. The sidestick pitch order is blocked to up (neutral) (down) deflection

TITLE SIDE STICK PITCH FAULT - F/OF/O pitch side stick transducer unit mechanically fails. The side stickpitch order is blocked to up (neutral) (down) deflection.

TITLE SIDE STICK ROLL FAULT CAPTCaptain roll side stick transducer unit mechanically fails. The side stickroll order is blocked to left (neutral) (right) deflection.

TITLE SIDE STICK ROLL FAULT - F/OF/O roll side stick transducer unit mechanically fails. The side stickroll order is blocked to left (neutral) (right) deflection.

TITLE STABILIZER JAMTHS screw jack is blocked. THS remains blocked.

TITLE PITCH TRIM RUNAWAY UPTHS runaway up. THS and control wheel runaway up to a speed of 0.225 deg/s

TITLE ELEVATOR FAULTJamming of the left(right) elevator.

TITLE '(NO ECAM) - ELEVATOR JAM'Mechanical jam in surface driving mechanism.

TITLE '(NO ECAM) - THS MOTOR FAIL'

Failure of the motor electrical control. Control of hydraulicactuators is switched from motor 1 to 2 (2 to 3) (3 to 2). Autotrimstill operative with at least one motor healthy.


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TITLE 'SPLR FAULT - SPOILER RUNAWAY'Spoiler runaway.

TITLE SPOILER RETRACTION FAULTJamming of the left spoiler #3 servo when out.

TITLE SPEED BRAKE FAULTSpeed brake control transducer unit fails.

TITLE GROUND SPOILERS FAULTErroneous tachowheel signal to SEC.

TITLE '(NO ECAM) - RUDDER PEDALS JAMMED'Jamming of the rudder control channel.

TITLE '(NO ECAM) ERRONEOUS PITCH UP ORDER'Erroneous potentiometers order in pitch to ELACs and SECs.

TITLE '(NO ECAM) ERRONEOUS PITCH DOWN ORDER'Erroneous potentiometers order in pitch to ELACs and SECs.

TITLE '(NO ECAM) ERRONEOUS ROLL LEFT ORDER'

Erroneous potentiometers order in roll to ELACs and SECs.

TITLE '(NO ECAM) ERRONEOUS ROLL RIGHT ORDER'Erroneous potentiometers order in roll to ELACs and SECs.

TITLE 'ELAC 1 ROLL FAULT'Left Blue Aileron and Right green Aileron jam

ATA 28'FUEL'

TITLE MAIN PUMP FAULTFor the Left system malfunctions: Pump 21QA(25QA) mechanically failed. Forthe Right system malfunctions: Pump 22QA(26QA) mechanically failed.

TITLE 'CTR TK PUMP 1(2) LO PR - MECHANICAL FAILURE'Boost pump mechanical failure.

TITLE TANK FUEL LEAK OUTERBreak in the L(R) outer tank (200 kg/min (441 lb/min))

TITLE TANK FUEL LEAK INNER

Leak in the L(R) inner tank (200 kg/min (441 lb/min)).

TITLE TANK FUEL LEAK CENTERLeak in the center tank (200 kg/min (441 lb/min)).

TITLE FQI FAULTFQI fails internally.

TITLE WING QTY PROBE FAILEDLoss of accuracy of the inner and outer probes.

TITLE X FEED VALVE FAILValve stuck in position.

TITLE OUTR TO INR FAULTL(R) Intercell valve is closed.


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TITLE FUEL TEMP INC/DECLeft (Right) inner fuel temperature sensors are defective.

TITLE FUEL QTY INC/DECIncorrect operation of fuel quantity computer. Displayed left(right) innercell fuel quantity varies from 0kg to 6000kg (13,227 lb) at a rate of20kg/s (44 lb/s)

ATA 29'HYDRAULIC SYSTEM'

TITLE 'G(Y) ENG 1(2) PUMP LO PR - SHAFT BROKEN'EDP 1(2) PUMP shaft broken.

TITLE 'B(Y) ELEC PUMP LO PR - PUMP FAILURE'B(Y) HYD ELEC PUMP fails. B(Y) system pressure drops to reservoirpressure.

TITLE 'HYD PRESS TRANSMITTER INC/DEC'Faulty pressure switch and pressure transmitter (pressure varies to aselected pressure (from 0 to 3600 psi) at a rate of 200 psi/s).

TITLE 'RSVR FLUID QTY INC/DEC'Reservoir quantity change. Quantity varies to selected value at arate of .25 gal/s (1 l/s).G system: 0 to 4.76 gal (18 l)Y system: 0 to 4.76 gal (18 l)B system: 0 to 2.11 gal (8 l)

TITLE 'G(Y)(B) RSVR LO LVL - INSTANTANEOUSReservoir will empty in approximatively 2 sec

TITLE RSVR OVERHEATTemperature of the reservoir is greater than 93 degrees C.

TITLE RSVR LO AIR PRESSAir pressure in the affected reservoir is lower than 22 psi.

TITLE ELEC PUMP FAULTThe three phase AC bus control unit fails and de-energizes the affectedELEC Pump actuator relay.

TITLE 'PTU FAULT 'PTU mechanical failure.

TITLE 'RAT FAULT - MECHANICAL FAILURE'RAT mechanical failure (partially extended).

TITLE RAT NO AUTOMATIC EXTENSIONRAT deployment solenoid failure.

TITLE 'BRAKES ACCUMULATOR LOW PRESSURE'Nitrogen leak in the brakes accumulator.


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ATA 30'ICE PROTECTION'

TITLE 'ENG 1(2) VALVE CLSD(OPEN) - FAILS IN POSITION'Engine anti ice valve fails in position, effects accordingly.

TITLE 'WING A.ICE SYS FAULT - VALVE FAULT'

Wing anti-ice valve fault.

TITLE PITOT HEAT FAULTPITOT power supply input of PHC 1(2)(3) fails.

TITLE TAT HEAT FAULTTAT power supply input of PHC 1(2) fails.

TITLE PROBES HEAT FAULTHeating availability output of PHC 1(2) in open circuit.

TITLE CAPT STAT HEAT FAULTL(R) static probes power supply of PHC 1 fails (open circuit).

TITLE F/O STAT HEAT FAULTL(R) static probes power supply of PHC 2 fails (open circuit).

TITLE WING A.ICE FAULTWing anti-ice valve is stuck in the closed position.

TITLE ENG A.ICE VALVE FAULTEngine anti ice valve stuck in current position, effects accordingly.

TITLE WING A.ICE OPEN ON GROUNDTime delay relay fails.

TITLE 'WING A.ICE L(R) VALVE OPEN - VALVE STUCK OPEN'Wing anti-ice valve stuck open when wing anti-ice selected off.

TITLE 'L(R) WINDSHEILD(WINDOW) - INTERNAL FAILURE OF WHC'Internal failure of WHC. Fault signal for the affected windows aresent to the ECAM. Phase B of the AC power supply to the windshieldand windows is lost on the left or right.


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ATA 31 'FLIGHT INSTRUMENTS'

TITLE DMC FAULTEIS DMC 1(2)(3) power supply fails.

TITLE FWC FAULTFWC fails internally.

TITLE SDAC FAULTSDAC 1(2) fails internally.

TITLE DISPLAY FAULT PFDCapt(F/O) PFD display unit power supply failure.

TITLE DISPLAY FAULT NDCapt(F/O) ND display unit power supply fails.

TITLE DISPLAY FAULT - ECAMUpper or lower ECAM display unit power supply fails.

TITLE ECP FAULTECP fails internally.

ATA 32'LANDING GEAR'

TITLE LGCIU FAULTLGCIU 1(2) internally fails.

TITLE AUTO BRK FAULTServo valve norm brake is jammed closed.

TITLE AUTO BRK CONDITION FAULTThe auto-brake conditions for arming flag are not setAUTO/BRK pb inoperative

TITLE ANTISKID FAULTA/SKID & N/W STRG switch fails.

TITLE '(NO ECAM) - YELLOW ACCUM PRESS INDICATOR FAILURE'Failure of ACCU PRESS indicator circuit.

TITLE NOSE WHEEL STEERING FAULT - BSCU SIGNAL FAILUREFailure coming from the signal in the BSCU.

TITLE NOSE WHEEL STEERING FAULTServo valve fails. Loss of tiller control on nosewheel steering. Rudderpedal steering also not available

TITLE BSCU FAULTInternal failure of the BSCU SYS 1(2).

TITLE BRAKE HOTBrake dragging on affected wheel.

TITLE LOSS OF BRAKINGDisagreement between the two BSCU channels. Normal braking and Autobrakeon all wheels are lost.


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TITLE '(NO ECAM) - BRAKES FAN INOP'BRK FAN pb sw is inoperative.This malfunction is available only if the brakes fan is installed.

TITLE '(NO ECAM) - BRAKE FAILURE'Brake is inoperative on selected wheels.

TITLE L/G LEVER LOCKEDLever latch fails. The baulk solenoid fails to release the mechanism when

the shock absorbers are extended.

TITLE '(NO ECAM) - L/G PANEL INDICATOR FAILS'Circuit breaker 1GA (49VU/C9) trips.

TITLE L/G - DOORS NOT CLOSEDSelected L/G door not closed.

TITLE L/G NOT DOWN LOCKEDSelected uplock actuator fails.

TITLE L/G - GEAR UPLOCK FAULTUplock mechanism fails (affected gear uplock in locked position when the

L/G is downlocked).

TITLE 'GEAR NOT DOWN(UP)LOCKED - IN TRANSIT(GRAV NOT POS)'Selected gear fails in transit.

TITLE 'RETRACTION FAULT'Selected gear remains in transit and does not uplock.

TITLE '(NO ECAM) GEAR COLLAPSE'There is a mechanical failure on the gear.

TITLE 'TYRE LO PR - DUAL TYRE BURST'Selected landing gear tires burst when on ground.

TITLE 'TYRE LO PR - SINGLE TYRE BURST'MLG tire blows when on ground.

TITLE 'TYRE LO PR - NLG TYRE BURST'NLG tire blows.


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ATA 34 'NAVIGATION'

TITLE IR FAULTInternal failure detected.

TITLE ATT DISCREPANCY - ROLL INCREASE TO 5 DEG IN 1 SEC

IR internal drift. Displayed roll increases by 5.1 Deg in 1s.

TITLE ATT DISCREPANCY - PITCH INCREASE +5 DEG IN 1 SECIR internal drift. Displayed pitch increases by 5.1 Deg in 1s.

TITLE HDG DISCREPANCY - DRIFT 1 DEG/SEC TO 15 DEGIR 1(2)(3) heading computation drift.

TITLE ADR FAULTInternal ADR fault.

TITLE AIRSPEED CHANNEL ADR FAULTOctal label 206 computed airspeed: Bad transmission.

TITLE 'ADR 1(2)(3) AND IR 1(2)(3) FAULT - POWER LOSS'AC and DC power supplies of ADIRU fail.

TITLE 'STBY IAS FAULT - STBY AIRSPEED INDICATOR FAULT'Standby airspeed indicator fault : indicates 0 knot.

TITLE BLOCKED PITOTObstruction of the hole of the CAPT (F/O)(STBY) pitot.

TITLE ILS RECEIVER FAILILS 1(2) receiver power supply fails.

TITLE '(NO ECAM) - ADF RECEIVER FAIL'ADF receiver failure.

TITLE '(NO ECAM) - VOR RECEIVER FAIL'VOR receiver failure.

TITLE '(NO ECAM) - DME RECEIVER FAIL'DME interrogator failure.

TITLE '(NO ECAM) - DDRMI FAIL'VOR/DME/ADF RMI power supply failure.

TITLE RMP FAULTRespective RMP power supply fails.

TITLE '(NO ECAM) - WR R/T FAULT'Radar transceiver internal failure.

TITLE R/A RECEIVER FAULTAssociated R/A receiver power supply failure.

TITLE ERRONEOUS RADIO ALTITUDE (-6 FT)Erroneous Radio Altitude Height Indication to RF Leak betweenTransmitter and Receiver Antennas leading to a frozen negative value( - 6 ft).

TITLE RADIO ALTITUDE (PARAMETER FROZEN)

Erroneous Radio Altitude Height Indication, due to a software issue insideRA Transmitter (Frozen Parameter).


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TITLE UNTIMELY STALL WARNINGNo existing cause: Synthetic failure setting Alarm STALLOnly active in Flight Phases 5, 6 and 7.

TITLE 'SPEED INDICATION INC/DEC FROM DMC 1(2)(3)'DMC 1, 2 AND 3 speed indication increase or decreaseto the selected value at a rate of 2 knots/sec.

TITLE 'TCAS FAULT - ADR ALTITUDE FAULT'Octal labels 203, 204 and 220 (Altitude, Baro Cor Alt 1 & 2): Badtransmission.

TITLE '(NO ECAM) - TCAS COMPUTER FAIL'Internal power supply failure resulting in complete shutdown of theTCAS Computer Unit.

TITLE '(NO ECAM) - TCAS VOICE ADVISORY FAIL'TCAS synthesized voice advisories fail.

TITLE 'GPS1(2) FAULT - RECEIVER FAILURE'Single GPS receiver failure due to an internal hardware fault.

TITLE 'GPS PRIMARY LOST'Loss of GPS navigation mode.

TITLE GPS PRIMARY LOST CAPT OR F/OLoss of GPS Primary Navigation on CAPT or F/O side

TITLE FM/GPS POS DISAGREEDifference of more or equal than 0.5mn (0.5Nm)between FMGC and GPS1(2) position (lat/long)

TITLE 'GPWS FAULT - POWER FAILURE'Total failure of the GPWS power supply.

TITLE '(NO ECAM) - GPWS FALSE WARNING'Radio Altitude processing failure.

TITLE '(NO ECAM) - GPWS TERRAIN TERRAIN PULLUP WARNING'Warning TERRAIN_TERRAIN_PULLUP is generated.

TITLE '(NO ECAM) - WR STAB FAULT'Loss of antenna stabilization.

TITLE 'SPEED INC/DEC CAUSE BY RAPID MODIFICATION OF PRES/TEMP'As a result of rapid modification of external pressure,

speed of aircraft inc/dec suddenly.


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ATA 35'OXYGEN'

TITLE '(NO ECAM) - CREW OXYGEN LEAK - RUPTURED BOTTLE'Ruptured crew oxygen bottle leaks at 1000 psi/min. OXY pressure

TITLE '(NO ECAM)-PASS OXY AUTO DEPLOY FAIL-PRESS SW FAIL'

Altitude pressure switch failure.

ATA 36 'PNEUMATICS'

TITLE 'ENG 1(2) BLEED FAULT - HP VALVE STUCK OPEN'HP VALVE ENG 1(2) stuck open or going to open position (4000HA1(2)).

TITLE BLEED FAULT (PR VALVE)

Pressure regulating valve stuck in its current position.

TITLE BLEED LEAKPylon duct leak.

TITLE WING BLEED LEAKLeak upstream of WING A/I VALVE.

TITLE 'APU BLEED LEAK - APU DUCT LEAK'APU duct leak.

TITLE 'X BLEED FAULT'X feed stuck closed (auto control motor failure).

TITLE BLEED NOT CLOSEDPressure Regulating Valve 1(2) stuck in open position.

TITLE 'AIR BLEED MONITORING 1+2 FAULT'Loss of bleed information on SD.


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ATA 49 'APU'

TITLE APU FIRE (EXTING)Fire in APU compartment. Fire indications extinguish 10s after dischargeof agent.

TITLE APU FIRE (UNEXTING)

Severe APU fire.

TITLE APU FAULTAPIC: CPU operative faultGARRETT: Fuel solenoid driver fails closedECB's protective circuit will operate to cause an automatic APU shutdownif the APU is running. If the APU is not running and normal startingprocedure is carried out, starting of the APU is impossible.

TITLE 'AUTO SHUT DOWN - INLET FLAP LOCKED IN POSITION'The inlet flap stays locked in position. ECB's protective circuitwill operate to cause an automatic shutdown if a normal startingprocedure is carried out. If the APU is running, a normal shutdowncan be attempted.

TITLE 'AUTO SHUT DOWN - STARTER CONTACTOR STUCK OPEN'Main start contactor stuck open. If the APU is not running and normalstarting procedure is carried out, a slow start will be detected bythe ECB after approximately 30 seconds and will cause a shut-down.

TITLE 'AUTO SHUT DOWN - OIL QUANTITY VARIABLE'Oil quantity is set by the instructor. A shut-down from the ECB mayoccur in the following conditions: a low oil pressure signal has beendetected or a high oil temperature signal has been detected (i.e., anoil level equal to 0.5 L). The low oil pressure signal is set whenoil pressure decreases below 27.5 psi (for GARRETT) P > 35 psi (forAPIC). The high oil temperature signal is set if the oil temperaturereaches 305C (for GARRETT), T > 185C for 2s (for APIC).

TITLE 'APU OVERSPEED'APU auto shutdown due to an overspeed fault.

ATA 52 'DOOR'

TITLE 'L FWD(AFT) CABIN - DOOR UNLOCKED'

Selected cabin door unlocked.

TITLE FWD(AFT) CARGO DOOR OPEN (SWITCH)Selected cargo door switch false open.

TITLE 'L FWD(AFT) CABIN - DOOR OPEN'Selected cabin door open.

TITLE 'FWD(AFT) CARGO - DOOR OPEN'Selected cargo door open.

TITLE REAR LEFT/RIGHT SLIDE NOT ARMEDSlide detected not armed (faulty switch).


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ATA 71C 'CFM ENGINE FAILURES'

TITLE FLAME OUT (NO DAMAGE)Engine combustion stopped.

TITLE FLAME OUT (WITH DAMAGE)

LP compressor damage due to the absorption of foreign matter.

TITLE SERIOUS DAMAGE WITH UNEXTINGUISHABLE FIRECompressor stall with engine core fire.

TITLE SERIOUS DAMAGE WITH ABRUPT POWER LOSSForeign object ingestion and engine seizure.

TITLE N2 ACCESSORY DRIVE LOSTRadial drive shaft rupture.

TITLE 'COMPRESSOR STALL'Compressor stalls.

TITLE EIU FAULTEIU power supply fails.

TITLE FADEC FAULTFADEC internally fails.

TITLE REVERSER FAULTThrust Reverser Direction Control Unit stuck in position.

TITLE REVERSER UNLOCKEDReverser doors unlocked (door position remains below 5% of maximum doordeployment).

TITLE THR LEVER DISAGREEMisrigging of one resolver: the intended position is higher than the realthrust lever position.

TITLE THR LEVER FAULTBoth throttle resolvers fail.

TITLE HIDDEN FUEL LEAKEngine fuel pump assembly seal is broken.

TITLE OIL PRESS INC/DECOil pump failure or oil jet clogging.

TITLE OIL TEMP INC/DECOil temperature adjusts at a rate of 20 degrees C/s to the selected value.

TITLE OIL QTY INC/DECOil quantity adjusts to the selected value at a rate of 0.5 qts/s.

TITLE N1 INC/DECMalfunctioning of the fuel metering valve.

TITLE N2 INC/DECMalfunctioning of the fuel metering valve.

TITLE EGT INC/DEC

A value is entered, an offset is created which remains until themalfunction is removed or is set differently.

TITLE VIBRATION N1 INC/DEC


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Unbalanced engine. When the engine is running, N1 vibration adjusts to theselected value at a rate of 2 cockpit units/s.

TITLE VIBRATION N2 INC/DECIncorrect engine operation. When the engine running, the N2 vibrationadjusts to the selected value at a rate of 2 cockpit units/s.

TITLE VOLCANIC ASHVolcanic dust cloud above FL190.

TITLE ENGINE BIRDSTRIKE - ENGINE STALLBird strike leading to non-recoverable engine stall.

TITLE ENGINE BIRDSTRIKE - HIGH VIBRATIONSA bird strike causes a fan blade to be out of balance.

TITLE ENGINE BIRDSTRIKE - HIGH VIBRATIONS - NO N1 DROPA bird strike causes a fan blade to be out of balance.

TITLE FLAME OUT (NO DAMAGE) RESTARTABLEEngine combustion is stopped.

TITLE FLAME OUT (NO DAMAGE) NON-RESTARTABLEEngine combustion is stopped.

TITLE N1 LIMITED TO 60 PERCENTN1 rise normally until 60 percent and then is blocked.


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ATA 77C 'CFM ENGINE INDICATIONS'

TITLE '(NO ECAM) - N1 INDICATION FAULT'Analog and digital signals of N1 lost by ECAM.

TITLE '(NO ECAM) - N2 INDICATION FAULT'Digital signal of N2 lost by ECAM.

TITLE '(NO ECAM) - OIL QUANTITY VARIABLE'Leak in oil circuit.

TITLE OIL LO PRESS - SENSOR FAILOil sensor failure.

TITLE '1(2) OIL LO PR - OIL PRESS VARIABLE'Oil pump failure or oiljet clogging.

TITLE '1(2) OIL HI TEMP - OIL TEMP VARIABLE'Incorrect engine operation.

TITLE '(NO ECAM) - VIBRATION N1 VARIABLE'Fan imbalance.

TITLE '(NO ECAM) - VIBRATION N2 VARIABLE'High pressure compressor imbalance.

TITLE 'FUEL FILTER CLOGGING'Clogging of fuel filter.

TITLE 'OIL FILTER CLOGGED'Clogging of oil filter.

TITLE '(NO ECAM) - N1, FF & EGT DIFFER BETWEEN ENG1 AND ENG2'Values of N1, FF and EGT of ENG1 are 5% lower versus thesame parameter of ENG2


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ATA 71I 'IAE ENGINE FAILURES'

TITLE '1(2) FAIL - FLAMEOUT - RESTARTABLE'Engine flames out with a restart possible.

TITLE '1(2) FAIL - FLAMEOUT - NON-RESTARTABLE'Engine flames out due to HP Fuel Pump being sheared.

TITLE '(NO ECAM) - COMPRESSOR STALL'Compressor stalls.

TITLE '(NO ECAM) - SERIOUS DAMAGE WITH PARTIAL POWER LOSS'Compressor stall and fan damage.

TITLE '1(2) FADEC FAULT - FADEC POWER SUPPLY LOST'Internal FADEC power supply lost.

TITLE '1(2) FAIL - N2 ACCESSORY DRIVE LOST'Engine N2 accessory drive is lost.

TITLE '1(2) REVERSER UNLOCKED - FAULTY SWITCH OPERATION'Faulty switch operation.

ATA 77I 'IAE ENGINE INDICATIONS'

TITLE '(NO ECAM) - N1 INDICATION FAULT'Analog and digital signals of N1 lost by ECAM.

TITLE '(NO ECAM) - N2 INDICATION FAULT'Digital signal of N2 lost by ECAM.

TITLE '(NO ECAM) - OIL QUANTITY VARIABLE'Leak in oil circuit.

TITLE '1(2) OIL LO PR - OIL PRESS VARIABLE'Oil pump failure or oiljet clogging.

TITLE '1(2) OIL HI TEMP - OIL TEMP VARIABLE'Engine oil temperature rises slowly above 165C.

TITLE '(NO ECAM) - VIBRATION N1 VARIABLE'Fan imbalance.

TITLE '(NO ECAM) - VIBRATION N2 VARIABLE'High pressure compressor imbalance.

TITLE '1(2) FUEL FILTER CLOG - FILTER CLOGGED'Clogging of fuel filter.

TITLE '1(2) OIL FILTER CLOG - FILTER CLOGGED'Clogging of oil filter.


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ATA 80C 'CFM ENG. START/IGN FAULTS'

TITLE ENG HOT STARTIncorrect engine operation. N2 acceleration is slower than normal. EGTincreases towards an abnormal value.

TITLE 'START FAULT - HUNG START (LOW FUEL FLOW)'

Offset in the fuel metering valve position causing a fuel flow lowerthan normal during start.

TITLE '1(2) HP FUEL VALVE - FAILS IN POSITION'HP valve fails in position.

TITLE 'START VALVE FAULT - VALVE STUCK IN POSITION'Start valve stuck in position.

TITLE IGNITION FAULTIgnition plugs fail. Start attempt takes place normally. FADEC detects nolight up.

TITLE '1(2) HP FUEL VALVE FAULT - MAN START FAULT'Master Switch position and HPSOV position disagree (HPSOV is stuckclosed).

TITLE '1(2) LOW N1 - N1 ROTOR SEIZED'N1 rotor seized during start up (N1 L.E. 5%).

ATA 80I 'IAE ENG. START/IGN FAULTS'

TITLE '1(2) START FAULT - HOT START (HIGH FUEL FLOW)'Offset in the fuel metering valve position causing a fuel flow higherthan normal during start.

TITLE '1(2) START FAULT - HUNG START (LOW FUEL FLOW)'Offset in the fuel metering valve position causing a fuel flow lowerthan normal during start.

TITLE '1(2) FUEL VALVE FAULT - FAILS IN CLOSED POSITION'HP fuel valve fails in closed position.

TITLE 'START VALVE FAULT - VALVE STUCK IN POSITION'Start valve stuck in position.

TITLE '1(2) START FAULT - BOTH IGNITORS FAIL'Loss of electrical supply for system ignitor plugs.

TITLE '1(2) FUEL VALVE FAULT - MAN START FAULT'Disagreement between Master Switch position and HPSOV position.

TITLE '1(2) START FAULT - N1 ROTOR SEIZED'N1 rotor seized during start up (N1 L.E. 5%).

A 320 Ffs 5 Simulated Malfunctions List

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