ECAM WARNING A3301 ECAM WARNING A330 A330 L/H RESET PANEL ACP/AMU AEVC CIDS CMC CPC DMC EIVMU FCDC FCMC FCU FM FMGEC FWC LGCIU Pack Control PHC PSCU SDAC SDCU WHC Audio Control Panel/Audio Management Unit Avionic Equipment Ventilation Controller Cabin Intercommunication Data System Central Maintenance Computer Cabin Pressure Controller Display Management Computer Engine Interface and Vibration Monitoring Unit Flight Control Data Concentrator Fuel Control and Management Computer Flight Control Unit Flight Management Inside of Flight Management Guidance Envelope Computer Flight Warning Computer Landing Gear Control Interface Unit Pack Controller Probes Heat Computer Proximity Switch Control Unit System Data Acquisition Computer Smoke Detection Control Unit Window Heat Computer AEVC (2HQ) CIDS Director (101 RH) CMC 1 (1 TM 1 ) CPC1 (311 HL) DMC1 (1WT1) DMC3 (1WT3) EIVMU1 (1 KS1) FCDC1 (1 CE1) FCMC1 (5QM1) FCU1 (3CA1) FMGEC FMGEC 1 (1CA1) FWC1 (1WW1) LGCIU1 (5GA1) PC1 (531 HH) PHC1 (6DA1) PHC3 (6DA3) PSCU1 (5MJ1) SDAC1 (1WV1) SDCU1 (20WH2) WHC1 (2DG1) 2 A330 R/H RESET PANEL ECAM WARNING A330 ACP/AMU Audio Control Panel/Audio Management Unit CIDS Cabin Intercommunication Data System CIDS Director (102RH) CMC Central Maintenance Computer CMC2 (1TM2) CPC Cabin Pressure Controller CPC2 (312HL) DMC Display Management Computer DMC2 (1WT2) EIVMU Engine Interface and Vibration Monitoring Unit EIVMU (1 KS2) FCDC Flight Control Data Concentrator FCDC2 (1 CE2) FCMC Fuel Control and Management Computer FCMC2 (SOM2) FCU FM Flight Control Unit Flight Management Inside of FCU2 (3CA2) FMGEC FMGEC Flight Management Guidance Envelope Computer FMGEC 2 (1CA2) FWC Flight Warning Computer FWC2 (1 WW2) LGCIU Landing Gear Control Interface Unit LGCIU2 (SGA2) Pack Control Pack Controller PC2 (S32HH) PHC Probes Heat Computer PHC2 (6DA2) PSCU Proximity Switch Control Unit PSCU2 (SMJ2) SDAC System Data Acquisition Computer SDAC2 (1WV2) SDCU Smoke Detection Control Unit SDCU2 (20WH2) Vent Control WHC Zone Control Ventilation Controller Window Heat Computer Zone Controller VC (280HN) WHC2 (2DG2) ZC (630HK) 3 . ECAM WARNING A330 CAB PR A330 CAB PR AFT OFV NOT OPEN -Check forward Outflow Valve OPEN NO GO CAB PR EXCESS CAB ALT NOT APPLICABLE -Reset breakers CPC 1 and 2 on LH and RH reset panels CAB PR FWD OFV NOT OPEN -Check aft Outflow Valve OPEN NO GO CAB PR LDG ELEV FAULT MEL 21-31-05 -Reset breakers CPC 1 and 2 on LH and RH reset panels -Reset breaker DMC 3 on RH reset panel CAB PR LO DIFF PR NOT APPLICABLE -No Action CAB PR SAFETY VALVE OPEN -If safety valves are visually closed: -Reset breakers SDAC 1 and 2 on LH and RH reset panel CAB PR SYS 1 + 2 FAULT -Reset breakers CPC 1 and 2 on LH and RH reset panels CAB PR SYS 1 FAULT -Reset breaker CPC 1 on LH reset panel CAB PR SYS 2 FAULT -Reset breaker CPC 2 on RH reset panel MEL 21-31-04 MEL 21-31-01 MEL 21-31-01 MEL 21-31-01 COND A330 COMD AFT CRG ISOL FAULT -Reset breaker VENT CANT Lane 1/2 on RH reset panel COND AFT CRG VENT FAULT -Reset breaker VENT CANT Lane 1/2 on RH reset panel COND BULK CRG DUCT OVHT -Reset breaker VENT CANT Lane 1/2 on RH reset panel MEL 21-28-03-B COND BULK CRG HEAT FAULT -Reset breaker VENT CONT Lane 1/2 on RH reset panel MEL 21-43-02 COND BULK CRG ISOL FAULT -Reset breaker VENT CONT Lane 1/2 on COND BULK CRG VENT FAULT -Reset breaker VENT CONT Lane 1/2 on COND L + R CAB VENT FAULT -Reset breaker VENT CONT Lane 1/2 on COND L CAB VENT FAULT -Reset breaker VENT CONT Lane 1/2 on COND LAV+GALLEY FAN FAULT -Reset breaker VENT CONT Lane 1/2 on COND R CAB VENT FAULT -Reset breaker VENT CONT Lane 1/2 on COND VENT SYS FAULT -Reset breaker VENT CONT Lane 1/2 on COND ZONE CTLR 1 FAULT -Reset breaker ZONE CONT on RH reset MEL 21-28-04-8 MEL 21-28-03-A MEL 21-43-02 RH reset panel MEL 21 28-04-A RH reset panel MEL 21-21-01 RH reset panel MEL 21-21-01 RH reset panel MEL21-23-01 RH reset panel MEL21-21-01 RH reset panel MEL 21-26-04 RH reset panel MEL 21-63-01 panel 4 . ECAM WARNING A330 COND ZONE CTLR 2 FAULT -Reset breaker ZONE CONT on RH reset panel COND ZONE REGUL FAULT -Reset breaker ZONE CONT on RH reset panel MEL 21-63-01 MEL 21-63-01 VENT A330 MEL 21-21-01 or MEL 2126-08-A VENT BLOWING FAULT .No further action required.Reset breaker AEVC on LH reset panel VENT EXTRACT FAULT -Reset breaker AEVC on LH reset panel VENT GND COOL FAULT VENT OVBD VALVE FAULT ..Reset breaker AEVC on LH reset panel MEL 21-26-01 MEL 21-27 MEL 21-26-02 MEL 21-25 AIR A330 AIR ABNORM BLEED CONFIG -Operational message..Reset breaker AEVC on LH reset panel VENT PACK BAY VENT FAULT . AIR APU BLEED FAULT -Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AIR APU BLEED LEAK -Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AIR BLEED LO TEMP -Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AIR BMC 1 + 2 FAULT -Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AIR BMC 1 FAULT -Perform Bite Test of BMC 1 on MCDU (AT A 36) AIR BMC 2 FAULT -Perform Bite Test of BMC 2 on MCDU (ATA 36) AIR ENG 1 BLEED FAULT -Perform Bite Test of BMC 1 on MCDU (AT A 36) AIR ENG 1 BLEED LEAK -Perform Bite Test of BMC 1 on MCDU (ATA 36) AIR ENG 1 BLEED NOT CLSD -Perform Bite Test of BMC 1 on MCDU (ATA 36) AIR ENG 1 HPV NOT OPEN -Perform Bite Test of BMC 1 on MCDU (ATA 36) AIR ENG 2 BLEED FAULT -Perform Bite Test of BMC 2 on MCDU (ATA 36) AIR ENG 2 BLEED LEAK -Perform Bite Test of BMC 2 on MCDU (ATA 36) AIR ENG 2 BLEED NOT CLSD -Perform Bite Test of BMC 2 on MCDU (ATA 36) AIR ENG 2 HPV NOT OPEN -Perform Bite Test of BMC 2 on MCDU (ATA 36) AIR HOT AIR SYS 1 FAULT -Reset breaker ZONE CONT on RH reset panel MEL 36-11-01 MEL 36-12-02 MEL 36-12-01 MEL 36-11-01 MEL 36-11-01 MEL36-11-01 MEL36-11-01 MEL 36-11-01 NO GO MEL 36-11-02 MEL 36-11-07 MEL 36-11-01 NO GO MEL 36-11-02 MEL 36-11-07 MEL 21-63-03 5 . Reset breaker FMGEC1 on LH reset panel .Faulty Pack Controller 2 (532HH) AIR R WING LEAK NO GO . 2 and 3 (Flight Control Primary Computer) 6 .Reset breaker FMGEC2 on RH reset panel .Check push button packs 1 ON AIR PACK 1 OVHT MEL 21-52-01 -Perform System Test of the Temp Ctrl system on MCDU (ATA 21 ) -Faulty Pack Controller 1 (531HH) MEL 21-52 or MEL 21-53 AIR PACK 1 REGUL FAULT AIR PACK 1 RAM DOOR CLOSED or MEL 21-53.Reset breaker FMGEC2 on RH reset panel AUTO FL T AP OFF MEL 22-10-01 .Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AUTO FLT A330 AUTO FL T A/THR LIMITED Not applicable . AUTO FL T A/THR OFF MEL 22-30-01 .Recycle FCPC1.Reset breaker FMGEC1 on LH reset panel .ECAM WARNING A330 MEL 21-63-03 AIR HOT AIR SYS 2 FAULT -Reset breaker ZONE CONT on RH reset panel AIR L WING LEAK NO GO -Perform test of BMC 1 and 2 on MCDU (AT A 36) -Switch ON/OFF Engine 1 bleed AIR L WING LEAK DET FAULT NO GO -Perform test of BMC 1 and 2 on MCDU (AT A 36) AIR PACK 1 + 2 FAULT NO GO .Faulty Pack Controller 2 (532HH) AIR PACK 2 REGUL FAULT MEL 21-52 or MEL 21-53 AIR PACK 2 RAM DOOR CLOSED or MEL 21-53-04 .Perform System Test of the Temp Ctrl system on MCDU (ATA 21) .Operational message.Check push button packs 2 ON AIR PACK VALVE 1 FAULT MEL 21-51-01 or MEL 2152-01 -Faulty Pack Controller 1 (531 HH) AIR PACK VALVE 2 FAULT MEL 21-51-01 or MEL 2152-01 -Faulty Pack Controller 2 (532 HH) AIR PACK 2 OVHT MEL 21-52-01 .Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) AIR X BLEED FAULT MEL 36-12-04 . No further action required.Perform System Test of the Temp Ctrl system on MCDU (ATA 21) .Check push button packs 1 and 2 ON -Passenger doors not closed and locked? AIR PACK 1 OFF MEL 21-52-01 .Perform Bite Test of BMC 1 and 2 on MCDU (ATA 36) .Switch ON/OFF Engine 2 bleed AIR R WING LEAK DET FAULT NO GO .04 -Perform System Test of the Temp Ctrl system on MCDU (ATA 21) -Faulty Pack Controller 1 (531 HH) AIR PACK 2 OFF MEL 21-52-01 . Reset breaker FMGEC1 on LH reset panel .Perform Bite test of ACARS on MCDU (COM-Radio) COM ACARS ALERT Not applicable -If no message on PFR…NO ACTION COM ACARS CALL Not applicable .Reset breaker FMGEC2 on RH reset panel AUTO FL T REAC W/S DET FAULT MEL 22-60-02-B .Reset breaker 2RE1 on panel 721VU COM HF 2 EMMITTING . CIDS2 and DMC3 on reset panels RH and LH COM CIDS PA FAULT MEL 23-31-01 -Perform Interface and Power Up test as follow: -Open CB’s CIDS DIR2 and DIR1 ESS on panel 742VU -Open CB’s CIDS DIR2 and DIR1 NORM on panel 722VU -Close all breakers again COM HF 1 EMMITTING .If no message on PFR…NO ACTION COM CIDS 1 + 2 FAULT MEL 23-73-01 -Reset breakers CIDS1.Reset breaker 2RE2 on panel 722VU COM VHF 1 EMMITTING .Reset breaker 2RC2 on breaker panel 722VU COM_VFH3 EMMMITTING NO GO NO GO NO GO NO GO NO GO -Reset breaker 2RC3 on breaker oanel721VU ELEC A330 ELEC AC BUS 1 FAULT -Perform Bite test of the ECMU1 on MCDU (AC page) ELEC AC BUS 2 FAULT .Reset breaker FMGEC1 on LH reset panel .Perform Bite test of the ECMU2 on MCDU (AC page) NO GO NO GO 7 .Reset breaker 2RC1 on breaker panel 742VU COM VHF 2 EMMITTING .Reset breaker FCU2 on RH reset panel NO GO AUTO FLT FM 1 + 2 FAULT MEL 22-83-01 .Perform System test of Auto Flight System on MCDU (ATA 22) COM A330 COM ACARS 1 FAULT MEL 23-24-01 .Reset breaker FMGEC2 on RH reset panel AUTO FLT FM 1 FAULT MEL 22-72-01 .Reset breaker FMGEC1 on LH reset panel AUTO FLT FM 2 FAULT MEL 22-72-01 .Reset breaker FMGEC2 on RH reset panel .ECAM WARNING A330 AUTO FLT FCU FAULT . Reset breaker FCU1 on LH reset panel . Release AC ESS FEED pushbutton 3.Reset breakers ECMU 1 & 2 at panels 722VU and 742VU 8 .Close CB 41XN and 5XC on oanel721VU ELEC AC ESS BUS FAULT -Open and close -Open and close ELEC AC ESS BUS SHED -Open and close -Open and close -Open and close NO GO CB 17XH on panel 742VU CB 12XH on panel 7 42VU NO GO CB 8XH on panel 742VU CB 15XH on panel 742VU CB 17XH on panel 742VU ELEC APU BAT FAULT MEL 24-38-01-A -Switch APU battery ON/OFF ELEC APU BAT OFF MEL 24-38-01-A -Operational message.Open CB 41XN and 5XC on panel 721VU 2. No further action required ELEC DC BAT BUS FAULT NO GO . ELEC APU BCL FAULT MEL 24-38-01-B -Switch APU battery ON/OFF ELEC APU GEN FAULT MEL 24-23-01 -Perform APU GCU Bite Test on MCDU (ATA 24-AC-EPGS) ELEC APU GEN OVERLOAD MEL 24-26-01 -Perform EMCU Bite Test on MCDU (AT A 24-AC-EMCU) ELEC APU TR FAULT MEL 24-32-01 -Perform APU TR reset on APU TR or with MCDU (ATA 24 –TEST ELEC/DC –TR –APU TR –APU TR RESET) ELEC BAT 1 FAULT MEL 24-38-01-A -Switch OFF/ON the BAT 1 switch ELEC BAT 1 OFF Not applicable -Switch ON the BAT 1 switch ELEC BAT 2 FAULT MEL 24-38-01-A -Switch OFF/ON the BAT 1 switch ELEC BAT 2 OFF Not applicable -Switch ON the BAT 2 switch ELEC BCL 1 FAULT MEL 24-38-01-B -Recycle BAT 1 switch ELEC BCL 2 FAULT MEL 24-38-01-B -Recycle BAT 2 switch ELEC BUS TIE OFF Not applicable -Switch the BUS TIE ON ELEC C/B MONITOR FAULT MEL 24-53-01-A -Performed CBMU Bite Test on MCDU (ATA24-AC-CBMU) ELEC C/B TRIPPED Refer to affected system -Operation message. No further action required.Close CB 1XC on panel 715VU 4.ECAM WARNING A330 ELEC AC ESS BUS AL TN NO GO -Perform operational test of the ESS Generation Manual switching 1.Push the AC ESS FEED pushbutton -Perform operational test of the ESS Generation Automatic switching 1.Check GPCU ELEC DC BUS 1 FAULT NO GO .Open CB 1XC on panel 715VU 2.Reset breakers ECMU 1 & 2 at panels 722VU and 742VU ELEC DC BUS 1 + 2 FAULT NO GO . Perform ECMU 1 Bite test on MCDU (AT A 24-AC-ECMU 1 ) ELEC ECMU 2 FAULT MEL 24-29-01 .Check IDG 2 oil level or IDG 2 cooler ELEC IDG 2 OIL OVHT .(ATA 24 – TEST ELEC/DC – TR – ESS TR – ESS TR RESET) ELEC EXT PWR A OVERLOAD MEL 24-26-01 .Reset breaker 801PP and 805PP at panel 742VU position N63 ELEC ECMU 1 FAUL T MEL 24-29-01 . No further action required.Perform ECMU 2 Bite Test on MCDU (ATA 24-AC-ECMU) ELEC EXT PWR B OVERLOAD MEL 24-26-01 .Reset breakers ECMU 1 & 2 at panels 722VU and 742VU ELEC DC ESS BUS FAULT NO GO . ELEC ESS TR FAULT MEL 24-34-01 .Recycle Pus-button switch ELEC/GEN 1 ELEC GEN 1 OVERLOAD MEL 24-26-01 .Check Post Flight Report for IDG OIL OVHT or La OIL Pressure .Push galley and commercial P/BSW OFF and check RCCB’s ELEC IDG 1 DISCONNECTED MEL 24-22-01 .Perform ECMU 2 Bite test on MCDU (ATA 24-AC-ECMU2) ELEC EMER CONFIG NO GO .Reconnect ELEC IDG 1 MINOR FAULT MEL 24-22-02 . clogged filter or T oil temp.Reconnect ELEC IDG 2 MINOR FAULT Check Post Flight Report for high or low oil level .Check oil level . clogged filter or T oil temp. Check IDG 2 cooler.Perform ESS TR reset on ESS TR or MCDU . ELEC IDG2 OIL LO PR .Check IDG 1 oil level or IDG 1 cooler ELEC IDG 1 OIL OVHT MEL 24-22-01 .Check IDG 1 oil level or IDG 1 cooler ELEC IDG 2 DISCONNECTED MEL 24-22-01 .Perform GCU Bite Test on MCDU (ATA 24-AC-EPGS-GCU/GPCU) ELEC GEN 2 OFF Not applicable .ECAM WARNING A330 ELEC DC BUS 2 FAULT NO GO .Check ELEC/DC system for normal configuration ELECDC ESS BUS SHED NO GO .Perform GCU Bite Test on MCDU (AT A 24-AC-EPGS-GCU/GPCU) ELEC GEN 1 OFF Not applicable . Check IDG 2 oil level or IDG 2 cooler MEL 24-22-02 MEL 24-22-01 MEL 24-22-01 9 .Operational message.Perform ECMU 1 Bite Test on MCDU (ATA 24-AC-ECMU) ELEC GEN 1 FAULT MEL 24-22-01 .Check IDG 1 cooler.Check Post Flight Report for IDG OIL OVHT or La OIL Pressure . ELEC IDG1 OIL LO PR MEL 24-22-01 . Check Post Flight Report for high or low oil level .Check oil level .Recycle Pus-button switch ELEC/GEN 2 ELEC GEN 2 OVERLOAD MEL 24-26-01 .Push galley and commercial P/BSW OFF and check RCCB’s ELEC GEN2FAULT MEL 24-22-01 . Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE AFT CRG DET FAULT MEL 26-16-02 .Perform Bite Test of the APU Fire and Overheat Detection Unit ATA 26 – Fire Prot: ENG/APU – FDU APU – Test SMOKE A330 SMOKE AFT CRG BTL 1 FAULT MEL 26-23-01 .Reset breakers SDCU 1 and 2 on LH and RH reset panels .TEST) SMOKE BULK CRG DET FAULT MEL 26-16-03 .(AT A 24 – TEST ELEC/DC – TR – TR2 – TR2 RESET) APU FIRE A330 APU FIRE NO GO .Reset breakers SDCU SMOKE FWD CRG BTL 1 FAULT .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE AVNCS VENT SMOKE NO GO .Reset breakers SDCU 1 and 2 on LH and RH reset panels .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE CAB REST DET FAULT MEL 26-18-02 .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE FLT REST DET FAULT .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE DETFAULT NO GO .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE AFT/BULK CRG SMOKE NO GO .Reset breakers SDCU MEL 1 and 2 on LH and RH reset panels MEL 1 and 2 on LH and RH reset panels MEL 1 and 2 on LH and RH reset panels MEL 1 and 2 on LH and RH reset panels 26-18-01 26-23-01 26-23-01 26-16-01 10 .Perform TR 2 reset on TR 2 or with MCDU .Check breaker 6XB “STAT INV CTL” on panel 742VU position N65 ELEC TR 1 FAULT MEL 24-32-01 .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE AFT CRG BTL 2 FAULT MEL 26-23-01 .Reset breakers SDCU SMOKE FWD CRG BTL 2 FAULT .If no real smoke in bulk.Perform TR 1 reset on TR 1 or with MCDU .or oil in the Air cond system.Reset breakers CIDS 1 and 2 on LH and RH reset panels . Perform Bite Test of Smoke Detection System with MCDU (AT A 26-SMOKE.(AT A 24 – TEST ELEC/DC – TR – TR1 – TR1 RESET) ELEC TR 2 FAULT MEL 24-32-01 ..If no real smoke in avionics…or oil in the Air cond system.Reset breakers SDCU SMOKE FWD CRG DET FAULT .ECAM WARNING A330 ELEC STATIC INV FAULT NO GO . Perform Bite Test of Smoke Detection System with MCDU (AT A 26-SMOKE. .TEST) SMOKE AVIONICS DET FAULTNO GO . TEST) SMOKE LAVATORY DET FAULT MEL 26-17-01 .Reset Wing Tip Brake with MCDU (AT A 27 –FLAP/SLAT –SFCC 1 (2) –FLAP –PCU/WTB TEST/RESET) SFCC/WTB RESET –CONFIRM OF SFCC/WTB RESET) F/CTL FLAP/MCDU DISAGREE -Check Post Flight Report NO GO 11 .Reset breakers SDCU 1 and 2 on LH and RH reset panels .If no real smoke in fwd cargo…or oil in the Air cond system. Perform Bite Test of Smoke Detection System with MCDU (AT A 26-SMOKE.TEST) F/CTL A330 F/CTL ADR DISAGREE NO GO .Reset breakers SDCU 1 and 2 on LH and RH reset panels .If no real smoke in toilet…or oil in the Air cond system. Perform Bite Test of Smoke Detection System with MCDU (AT A 26-SMOKE.Check Post Flight Report F/CTL AIL SERVO FAULT MEL 27-14-01 -Recycle FCPC 2 (Flight Control Primary Computer) F/CTL ALTN LAW NO GO -Recycle FCPC 1 & 2 (Flight Control Primary Computer) -Recycle FCSC 1 & 2 (Flight Control Secondary Computer) F/CTL ECVT LAW NO GO -Check Post Flight Report F/CTL ELEV REDUND LOST NO GO -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) F/CTL ELEV SERVO FAULT MEL 27-34-01 -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) F/CTL FCFC 1 FAULT MEL 27-95-01 -Reset breaker FCDC 1 on LH reset panel F/CTL FCDC 1+2 FAULT MEL 27-95-01 -Reset breaker FCDC 1 and 2 on LH & RH reset panels F/CTL FCDC 2 FAULT MEL 27-95-01 -Reset breaker FCDC 2 on RH reset panel F/CTL FLAP SYS 1 FAULT MEL 27-51-01 -Recycle breakers SFCC 1 NORM on 721VU pas X14 -Recycle breakers SFCC 1 AVAIL on 721VU pas X13 -Recycle breakers SFCC 1 SLAT on 742VU pas L62 -Recycle breakers SFCC 1 FLAP on 742VU pas L61 F/CTL FLAPSYS2FAULT MEL 27-51-01 -Recycle breakers SFCC 2 SLAT on 722VU pas T43 -Recycle breakers SFCC 2 FLAP on 722VU pas V40 F/CTL FLAP TIP BRK FAULT NO GO .Reset breakers SDCU 1 and 2 on LH and RH reset panels SMOKE LAVATORY SMOKE .ECAM WARNING A330 SMOKE FWD CRG SMOKE NO GO . Recycle FCPC 3(Flight Control Primary Computer) F/CTL PRIM 3 PITCH FAULT F/CTL F/CTL F/CTL F/CTL MEL 27-44-01 or MEL 2793-01 MEL 27-93-01 MEL 27-44-01 or MEL 2793-01 MEL 27-93-01 MEL 27-44-01 or ME 2793-01 -Recycle FCPC 3 (Flight Control Primary Computer) R ELEV FAULT NO -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) R INR AIL FAULT NO -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) ROUTR AIL FAULT NO -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) R SIDESTICK FAULT NO -Check Post Flight Report GO GO GO GO 12 .Recycle FCPC 1 (Flight Control Primary Computer) F/CTL PRIM 2 FAULT -Recycle FCPC 2 (Flight Control Primary Computer) F/CTL PRIM 2 PITCH FAULT -Recycle FCPC 2 (Flight Control Primary Computer) F/CTL PRIM 3 FAULT . 2 and 3 F/CTL IR DISAGREE NO GO -Check Post Flight Report F/CTL L ELEV FAULT NO GO -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 -F/CTL -EFCS -EFCS1 -GND SCANNING) F/CTL L INR AIL FAULT NO GO -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 -F/CTL -EFCS -EFCS1 -GND SCANNING) F/CTL OUTRAIL FAULT H NO GO -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 -F/CTL -EFCS -EFCS1 -GND SCANNING) F/CTL L SIDESTICK FAULT NO GO -Check Post Flight Report F/CTL L+R ELEV FAULT NO GO -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 -F/CTL -EFCS -EFCS1 -GND SCANNING) F/CTL PRIM 1 FAULT MEL 27-93-01 -Recycle FCPC 1 (Flight Control Primary Computer) F/CTL PRIM 1 PITCH FAULT .ECAM WARNING A330 F/CTL FLAPS FAULT NO GO -Reset Wing Tip Brake with MCDU (AT A 27 -FLAP/SLAT -SFCC 1(2) -FLAP -PCU/WTB TEST/RESET SFCC/WTB RESET -CONFIRM OF SFCC/WTB RESET) F/CTL FLAPS LOCKED NO GO -Reset Wing Tip Brake with MCDU (AT A 27 -FLAP/SLAT -SFCC 1 (2) -FLAP -PCU/WTB TEST/RESET SFCC/WTB RESET -CONFIRM OF SFCC/WTB RESET) F/CTL GND SPLR FAULT MEL 27-92-02 or MEL 32-42-05 -Recycle Flight Control Primary Computer (FCPC) 1. 2 and 3 F/CTL RUD TRIM 2 FAULT MEL 27-22-01 -Recycle Flight Control Primary Computer (FCPC) 1. Stop. Release the LEAK MEASUREMENT VALVES/y pus-button Slowly push the right pedal until it touches the mech. 2 and 3 F/CTL RUD TRIM FAUL MEL 27-22-01 -Push rudder trim reset switch on the rudder trim control panel (115VU) F/CTL RUD TRV LIM 1 FAULT MEL 27-23-01 -Recycle Flight Control Primary Computer (FCPC) 1. 2 and 3 F/CTL RUD TRV LIM FAULT MEL 27-23-01 -Perform Bite Test of the EFCS ground scanning with MCDU (AT A 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) F/CTL RUD Y SERVO JAM -Perform the operational test of the Rudder Servo Control Pressurize the yellow Hydraulic System with the electrical pump Release the LEAK MEASUREMENT VALVES/B pus-button Release the LEAK MEASUREMENT VALVES/G pus-button Slowly push the right pedal until it touches the mech. 2 and 3 F/CTL RUD TRV LIM 2 FAULT MEL 27-23-01 -Recycle Flight Control Primary Computer (FCPC) 1. Stop Slowly push the left pedal until it touches the mech. Stop Put the pedals in the neutral position If rudder moves during test…Replace jamming detection switch If rudder does not move during Tests…replace rudder servo-control MEL 27-25-02-A F/CTL SEC 1 FAULT -Recycle Flight Control F/CTL SEC 1 PITCH FAULT -Recycle Flight Control F/CTL SEC 2 FAULT -Recycle Flight Control F/CTL SEC 2 PITCH FAULT -Recycle Flight Control F/CTL SENSOR FAULT MEL 27-94-01 Secondary Computer (FCSC) 1 and 2 MEL 27-94-01 Secondary Computer (FCSC) 1 and 2 MEL 27-94-01 Secondary Computer (FCSC) 1 and 2 MEL 27-94-01 Secondary Computer (FCSC) 1 and 2 MEL 27-92-05 or MEL 27-92-06 -Recycle Flight Control Primary Computer (FCPC) 1 and 3 13 . Stop. Stop Put the pedals in the neutral position If rudder moves during test…Replace jamming detection switch If rudder does not move during Tests …replace rudder servo-control F/CTL RUD TRIM 1 FAULT MEL 27-22-01 -Recycle Flight Control Primary Computer (FCPC) 1. Slowly push the left pedal until it touches the mech.ECAM WARNING A330 F/CTL RUD B SERVO JAM MEL 27-25-02-A -Perform the operational test of the Rudder Servo Control Pressurize the Blue Hydraulic System with the electrical pump Release the LEAK MEASUREMENT VALVES/G pus-button. Put the pedals in the neutral position If rudder moves during test…Replace jamming detection switch If rudder does not move during Tests Replace rudder servo-control F/CTL RUD G SERVO JAM MEL 27-25-02-A -Perform the operational test of the Rudder Servo Control Pressurize the green Hydraulic System with the electrical pump Release the LEAK MEASUREMENT VALVES/B pus-button Release the LEAK MEASUREMENT VALVES/y pus-button Slowly push the right pedal until it touches the mech. Stop Slowly push the left pedal until it touches the mech. ECAM WARNING A330 F/CTL SLAT SYS 1 FAULT -Recycle breakers -Recycle breakers -Recycle breakers -Recycle breakers MEL 27-81-01 SFCC SFCC SFCC SFCC 1 1 1 1 NORM on 721VU pas X14 AVAIL on 721VU pas X13 SLAT on 742VU pas L62 FLAP on 742VU pas L61 F/CTL SLAT SYS 2 FAULT -Recycle breakers SSFCC 2 SLAT on 722VU pas T 43 -Recycle breakers SFCC 2 FLAP on 722VU pas V40 F/CTL SLAT TIP BRK FAULT -Reset Wing Tip Brake with MCDU (ATA 27 -FLAP/SLAT -SFCC 1(2) -FLAP -PCU/WTB TEST/RESET SFCC/WTB RESET -CONFIRM OF SFCC/WTB RESET) MEL 27-81-01 NO GO F/CTL SLATS FAULT -Reset Wing Tip Brake with MCDU (ATA 27 -FLAP/SLAT -SFCC 1(2) -FLAP -PCU/WTB TEST/RESET SFCC/WTB RESET -CONFIRM OF SFCC/WTB RESET) NO GO F/CTL SLATS LOCKED -Reset Wing Tip Brake with MCDU (AT A 27 -FLAP/SLAT -SFCC 1(2) -FLAP -PCU/WTB TEST/RESET SFCC/WTB RESET -CONFIRM OF SFCC/WTB RESET) NO GO F/CTL SPD BRK DISAGREE -Check Post Flight Report F/CTL SPD BRK FAULT -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 -F/CTL -EFCS -EFCS1 -GND SCANNING) F/CTL SPLR FAULT -Recycle Flight Control Primary Computer (FCPC) 1 and 3 F/CTL STAB CTL FAULT -Perform Test of the EFCS ground scanning with MCDU F/CTL TURB DAMP FAULT -Recycle Flight Control Primary Computer (FCPC) 1 and 3 F/CTL YAW DAMPER 1 -Recycle Flight Control Primary Computer (FCPC) 1 -Recycle Flight Control Secondary Computer (FCSC) 1 F/CTL YAW DAMPER 2 -Recycle Flight Control Primary Computer (FCPC) 3 -Recycle Flight Control Secondary Computer (FCSC) 2 F/CTL YAW DAMPER FAULT -Perform Bite Test of the EFCS ground scanning with MCDU (ATA 27 –F/CTL –EFCS –EFCS1 –GND SCANNING) MEL 27-92-01 MEL 27-92-01 MEL 27-64-01 NO GO MEL 27-93-05 MEL 27-26-01 MEL 27-26-01 MEL 27-26-01 FUEL A330 FUEL ABNORMAL MAN FWD XFR -No action FUEL APU AFT PUMP FAULT -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL APU LP VALVE FAULT -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL ENG1 LP VALVE FAULT -Reset breakers FWC 1 and 2 on LH and RH reset panel FUEL ENG2 LP VALVE FAULT -Reset breakers FWC 1 and 2 on LH and RH reset panel Not applicable MEL 49-30-01-A MEL 49-30-03 MEL 28-24-01 MEL 28-24-01 14 . no further action is required FUEL R STBY PUMP LO PR MEL 28-21-01-B -Recycle breaker FUEL R STBY PUMP on 721VU position J05 -Check pump symbol on ECAM/FUEL page FUEL R WING PUMPS LO PR MEL 28-21-01-A and MEL 28-2101-B -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL R WING TK LO LVL NO GO or MEL 28-46-04-A -Check Post Flight Report -Operational message.ECAM WARNING A330 FUEL EXCESS AFT CG (False caution) -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL FCMC 1 FAULT -Reset breakers FCMC 1 on LH reset panel FUEL FCMC 1+2 FAULT -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL FCMC 2 FAULT MEL 28-40-13-A MEL 28-51-01-A or MEL 28-51-01B NO GO MEL 28-51-01-A or MEL 28-51-01B -Reset breakers FCMC 2 on RH reset panel FUEL FUEL LO TEMP NO GO -Reset breakers FCMC1 and 2 on LH and RH reset panel FUEL L INNER TK NI TEMP (also DELAY T. no further action is required FUEL L STBY PUMP LO PR MEL 28-21-01-B -Recycle breaker FUEL L STBY PUMP on 721VU position J05 -Check pump symbol on ECAM/FUEL page MEL 28-21-01-A FUEL L WING PUMPS LO PR and MEL 28-2101-B -Reset breakers FCMC 1 and 2 on LH and RH reset panel NO GO or MEL FUEL L WING TK LO LVL 28-46-04-A -Check Post Flight Report -Operational message.O.O.) Not applicable -Apply ECAM procedure -If MCOU shows no maintenance message. No further action needed FUEL L+R WING TK LO LVL NO GO or MEL 28-46-04-A -Check Post Flight Report -Operational message. No further action needed FUEL RIGHT PUMP 1 LO PR -Recycle breaker FUEL R PUMP 1 CTL on 722VU position Q43 MEL 28-21-01-A 15 .) Not applicable -Apply ECAM procedure -If MCDU shows no maintenance message. No further action needed FUEL LEFT PUMP 1 LO PR MEL 28-21-01-A -Recycle breaker FUEL L PUMP 1 CTL on 722VU position U46 FUEL LEFT PUMP 2 LO PR MEL 28-21-01-A -Recycle breaker FUEL L PUMP 2 CTL on 742VU position 068 FUEL OUTR TO INR FAULT MEL 28-26-01 -Perform the operational test of the FCMS controlled valves (ATA 28 –FCMC1 –FUEL VALVES TEST –CONFIRM) FUEL R INNER TK HI TEMP (also DELAY T. Check Blue Hydraulic level HYD B RSVR OVHT NO GO or MEL 29-30-03-C Check Post Flight Report -HYD G + B SYS LO PR NO DISPATCH or MEL 29-30-03-F -Check Hydraulic levels HYD G + Y SYS LO PR -Check Hydraulic levels HYD G ELEC PUMP FAULT NO GO or MEL 29-30-03-F MEL 29-21-01 or MEL 29-30-03-D -Recycle breaker HSMU B + PART G on 721VU position U10 -Recycle breaker HSMU Y + PART G on 722VU position X46 16 . Check pressure again after the ENG MODE selector is set back to NORMAL. put the ENG MODE selector switch in CRANK The APU will boost the air bleed pressure to 4 bars (58 PSI) during 30 sec. No further action needed MEL 28-21-01-A MEL 28-27 MEL 28-25-04-C or 28-27-01 or 28-27-03 or 2827-04 MEL 28-27-05 NO GO MEL 28-23-01 MEL 28-51-02 HYD A330 HYD B + Y SYS LO PR -Check Hydraulic levels HYD B ELEC PUMP FAULT -Recycle breaker HSMU B + PART G on 721VU position U10 -Recycle breaker HYD PUMP B CTL on 721VU position X12 HYD B ENG 1 PUMP LO PR -Check Blue Hydraulic level -Bleed Blue Hydraulic system HYD B RSVR LO AIR PR NO GO or MEL 29-30-03-F MEL 29-2-01 or MEL29-30-03-D NO GO NO GO or MEL 29-30-03-B -Perform the Check of the Air Pressure in the reservoir -Pressurize the hydraulic reservoir with the APU (With APU running.) HYD B RSVR LO LVL NO GO or MEL 29-30-03-A .ECAM WARNING A330 FUEL RIGHT PUMP 2 LO PR -Recycle breaker FUEL R PUMP 2 CTL on 721VU position V13 FUEL T TANK XFR FAULT -Reset breakers FCMC 1 and 2 on LH and RH reset panel FUEL TRIM LINE FAULT FUEL FUEL FUEL FUEL -Reset breakers FCMC 1 and 2 on LH and RH reset panel TRIM TK PUMP LO PR -Recycle breaker TRIM XFR PUMP CTL on 722VU position Q40 -Recycle breaker TRIM XFR PUMP SPL Yon 722VU position E40 WING TK OVERFLOW -Reset breakers FCMC 1 and 2 on LH and RH reset panel WING X FEED FAULT -Recycle Cross Feed Valve P/BSW ZFW ZFCG DISAGREE -Check Post Flight Report -Operational message. Bleed Yellow Hydraulic system 17 . Check pressure again after the ENG MODE selector is set back to NORMAL. Serv. put the ENG MODE selector switch in CRANK The APU will boost the air bleed pressure to 4 bars (58 PSI) during 30 sec.ECAM WARNING A330 HYD G ENG 1 PUMP LO PR -Check Green Hydraulic level -Bleed Green Hydraulic system HYD G ENG 1+2 PUMPS LO PR -Check Green Hydraulic level HYD G ENG 2 PUMP LO PR -Check Green Hydraulic level -Bleed Green Hydraulic system HYD G RSVR LO AIR PR HYD G HYD G HYD G HYD G NO GO or MEL 29-30-03-E NO GO or MEL 29-30-03-E NO GO or MEL 29-30-03-E NO GO or MEL 29-30-03-B -Perform the Check of the Air Pressure in the reservoir -Pressurize the hydraulic reservoir with the APU (With APU running.) RSVR LO LVL NO GO or MEL 29-30-03-A -Check Green Hydraulic level RSVR OVHT NO GO or MEL 2930-03-C -Check Post Flight Report RSVR UNDERFILLED NO GO -Check for leaks -Refill Green Hydraulic Reservoir SYS LEAK Not applicable -Cross check fluid level indication on green reservoir and ECAM hydraulic page -Check for external leakage of the hydraulic components HYD MONITORING (with HSMU racked) -Reset breakers SDAC 1 and 2 on LH and RH reset panels HYD RAT FALUT MEL 29-30-03-H NO GO or MEL 29-30-03-G -Pressurize the green hydraulic system On the yellow hydr. put the ENG MODE selector switch in CRANK The APU will boost the air bleed pressure to 4 bars (58 PSI) during 30 sec.Check Yellow Hydraulic level . pnl. set the ON/OFF switch to ON and back OFF HYD Y ELEC PUMP FAULT MEL 29-23-01-A or MEL 29-30-03D -Recycle breaker HSMU B + PART G on 721VUpositionU10 -Recycle breaker HYD PUMP Y SVCE on 722VU position N46 -Recycle breaker HYD PUMP Y CTL on 722VU position R36 -Recycle breaker HSMU Y + PART G on 722VU position X46 HYD Y RSVR LO AIR PR NO GO or MEL 29-30-03-B -Perform the Check of the Air Pressure in the reservoir -Pressurize the hydraulic reservoir with the APU (With APU running.) HYD Y ENG 2 PUMP LO PR NO GO or MEL 29-30-03-C . Check pressure again after the ENG MODE selector is set back to NORMAL. Check Hydraulic levels HYD Y RSVR OVHT NO GO or MEL 29-30-03-C .Recycle breaker FADEC A ENG 1 on panel 742VU position Q73 A.ICE CAPT PITOT HEAT MEL 30-32-02 .ICE ENG 2 VALYE OPEN .Perform operational test of the Ice detection system with MCDU ATA 30 -ICE RAIN:DETECTOR .TES A.ICE DETECT FAULT .Check thermal fuse Engine Air Intake Anti Ice Valve .Recycle breaker FADEC B ENG 1 on panel 722VU position D44 .Perform operational test of the Probe Ice protection with MCDU ATA 30 -ICE RAIN:HEATING .ICE CAPT PROBES HEAT MEL 30-31-01 .Recycle breaker ICE DET 1 on panel 721VU position B08 .ICE F/O PROBES HEAT MEL 30-31-01 18 .PHC 1 .Perform operational test of the Probe Ice protection with MCDU ATA 30 .PHC 2 .Recycle breaker ICE DET 2 on panel 722VU position F46 .PHC 1 .Check Post Flight Report A.PHC 1 .PHC 1 .ICE CAPT AOA HEAT MEL 30-31-04 .Perform visual inspection of the Anti-Ice supply duct .ICE RAIN:HEATING .Reset breaker PHC2 on RH reset panel -Perform operational test of the Probe Ice protection with MCDU (ATA 30 –ICE RAIN:HEATING – PHC 2 – TEST) A.Recycle breaker FADEC B ENG 2 on panel 722VU position K49 .ECAM WARNING A330 NO GO or MEL 29-30-03-A HYD RSVR LO L VL .Perform operational test of the Probe Ice protection with MCDU ATA 30 -ICE RAIN:HEATING .Perform operational test of the Probe Ice protection with MCDU ATA 30 -ICE RAIN:HEATING .Check Engine Air Intake Anti Ice Valve 5000DN MEL-30-81-01 A.Reset breaker PHC1 on LH reset panel .TES A.TES A.ICE A330 A.Check Engine Air Intake Anti Ice Valve 5000DN A.Perform visual inspection of the Anti-Ice supply duct .ICE F/O PITOT HEAT MEL 30-31-02 .ICE ENG 2 VALVE CLOSED .TEST A.TEST A.ICE F/O AOA HEAT MEL 30-31-04 .ICE ENG 1 VALVE CLOSED .ICE ENG 1 VALVE OPEM .Reset breaker PHC1 on LH reset panel .TEST MEL 30-31-05 A.Reset breaker PHC1 on LH reset panel .ICE CAPT TAT HEAT .Recycle breaker FADEC A ENG 2 on anel7 42VU position Q74 MEL 30-21-01 MEL 30-21-01 MEL 30-21-01 MEL 30-21-01 A.Reset breaker PHC2 on RH reset panel .Perform operational test of the Probe Ice protection with MCDU (ATA 30 –ICE RAIN:HEATING .Reset breaker PHC1 on LH reset panel .Check thermal fuse Engine Air Intake Anti Ice Valve . ICE L F/O STAT HEAT .ICE L WINDOW HEAT .ICE L CAPT STAT HEAT .ICE L WSHLD HEAT .ICE R CAPT STAT HEAT .ICE L STBY STAT HEAT MEL 30-31-03 .TES A.Perform operational test of the Probe Ice protection with MCDU ATA 30 -ICE RAIN:HEATING .ICE L OUTR WING HIGH PR .Reset breaker WHC1 on LH reset panel A.Check Wing Anti Ice Control Filter .PHC 2 .ICE F/O TAT HEAT .Check Wing Anti Ice Control Filter .Reset breakers WHC 1 and WHC 2 on LH and RH reset panel A.Fault RH inner Win Anti Ice Valve 1 ODL2 A.Perform operational test of the Probe Ice protection with MCDU (ATA 30 –ICE RAIN:HEATING .ICE L INR WING OPEN .Fault LH outer Win Anti Ice Valve 9DL 1 A.Reset breaker PHC2 on RH reset panel .Reset breaker PHC2 on RH reset panel .PHC 2 – TEST) A.ICE L OUTR WING LO PR .ICE L INR WING LP PR .ICE L INR WING HI PR -Fault LH inner Wing Anti Ice Valves (10DL1) A.ICE L + R WINDOW HEAT .Reset breaker PHC2 on RH reset panel A.Reset breaker PHC3 on LH reset panel .Reset breaker PHC2 on RH reset panel .Reset breakers WHC 1 and WHC 2 on LH and RH reset panel A.ICE R OUTR WING HI PR MEL 30-42-02 MEL 30-42-03 MEL 30-31-03 MEL 30-31-03 NO GO MEL 30-11-01 MEL 30-11-01 NO GO 19 .Perform operational test of the Probe Ice protection with MCDU (ATA 30 –ICE RAIN:HEATING .Perform operational test of the Probe Ice protection with MCDU (ATA 30 –ICE RAIN:HEATING .Faulty LH outer Wing Anti Ice Valve (9DL 1) .PHC 2 – TEST) MEL 30-31-05 MEL 30-42-02 MEL 30-42-03 MEL 30-31-03 MEL 30-31-03 A.Faulty RH inner Wing Anti Ice Valve (10DL2) .Fault LH inner Win Anti Ice Valve (10DL1) A.PHC 2 – TEST) A.Reset breaker PHC2 on RH reset panel .ICE L + R WSHLD HEAT .PHC 2 – TEST) A.Fault LH outer Win Anti Ice Valve (9DL1) A.ICE L OUTR WING OPEN MEL 30-11-01 .Check Win Anti Ice Control Filter A.Reset breaker PHC1 on LH reset panel R F/O STAT HEAT .Reset breaker WHC1 on LH reset panel A.ECAM WARNING A330 .Fault LH inner Wing Anti Ice Valve (10DL1) NO GO A.ICE R INR WING HI R Fault RH inner Win Anti Ice Valve 10DL2 A.ICE R INR WING OPEN .ICE R INR WING LO PR .Fault Bleed Valve (4001HA) NO GO MEL 30-11-01 MEL 30-11-01 MEL 30-11-01 A.Perform operational test of the Probe Ice protection with MCDU (ATA 30 – ICE RAIN: HEATING . ICE STBY PITOT HEAT .ECAM WARNING A330 .ICE WAI SYS FAULT .ICE STBY AOA HEAT .Reset breaker WHC2 on RH reset panel A.Faulty LH inner Wino Anti Ice Valve (10DL1) MEL 30-11-01 MEL 30-11-01 MEL 30-31-03 MEL 30-42-02 MEL 30-42-03 MEL 30-31-04 MEL 30-31-02 MEL 30-31-01 MEL 30-11-01 MEL 30-11-01 MEL 30-11-01 EIS A330 EIS DISPLY DISCREPANCY -Reset breaker DMC 1.ICE R STBY STAT HEAT .Faulty RH outer Wing Anti Ice Valve (9DL2) .Check Win Anti Ice Control Filter A.ICEE R OUTR WING OPEN .Fault RH outer Win Anti Ice Valve 9DL2 A.2 and 2 on LH and RH reset panel EIS ECAM DMC 1 FAULT -Reset breaker DMC 1 on LH reset panel EIS ECAM DMC 2 FAULT ME 31-62-01-B -Reset BREAKER DMC2 on RH reset panel EIS ECAM DMC 3 FAULT -Reset breaker DMC3 on LH reset panel EIS EFIS DMC 1 FAULT -Reset breaker DMC1 on LH reset panel EIS EFIS DMC 2 FAULT -Reset breaker DMC 2 on RH reset panel EIS EFIS DMC 3 FAULT -Reset breaker DMC 3 on LH reset panel NO GO MEL 31-62-01-B MEL 31-62-01-B MEL 31-62-01-B MEL 31-62-01-A MEL 31-62-01-A MEL 31-62-01-A FWS A330 FWS EPC FAULT MEL 31-56-01 20 .ICE WING OPEN ON GND .Faulty Wing Anti Ice Relay (11 DL) .Faulty Wing Anti Ice System Mode Relay (6DL) .ICE R WSHLD HEAT .Faulty RH inner Wing Anti Ice Valve (10DL2) .Reset breaker PHC3 on LH reset panel A.Fault Win Anti Ice Ground Relay (4DL) A.ICE R OUTR WING LO PR .ICE R WINDOW HEAT .Reset breaker PHC3 on LH reset panel A.Fault RH outer Win Anti Ice Valve 9DL2 A.ICE STBY PROBES HEAT .Fault Push Button Switch 3DL A.Faulty RH outer Wing Anti Ice Valve (9DL2) .Faulty Wing Anti Ice Control Relay (5DL) .Reset breaker PHC3 on LH reset panel A.Reset breaker WHC2 on RH reset panel A.Faulty LH outer Wing Anti Ice Valve (9DL1) .Reset breaker PHC3 on LH reset panel A.ICE WING VLV NOT GND . Breaking/Steering .Reset breaker SDAC 1 FAULT .Reset breaker FWC 1 and SDAC 1 on LH reset panel FWC 2 and SDAC 2 on RH reset panel MEL 31-53-01 FWC 1 on LH reset panel MEL 31-53-01 FWC 1 and 2 on LH and RH reset panel MEL 31-53-01 FWC 2 on RH reset panel MEL 31-55-01 SDAC 1 on LH reset panel MEL 31-55-01 SDAC 1 and SDAC 2 on LH and RH reset panel MEL 31-55-01 SDAC 2 on RH reset panel RECORDER A330 RECORDER DFDRFAULT .Reset breaker SDAC 1+2 FAULT .BSCU CH 1 ) .Reset breaker 2 FAULT .Perform Bite test of BSCU 2 on MCDU (AT A 32 .Recycle A/SKID & N/W STRG switch on F/O instrument panel BRAKES AUTO BRAKE FAULT NO GO MEL 32-42-02 or 32-42-04 .Breaking/Steering .Reset breaker SDAC 2 FAULT .Perform Bite test of BSCU 2 on MCDU (AT A 32 .Perform Bite test of BSCU 1 on MCDU (ATA 32 .ECAM WARNING A330 FWS FWS FWS FWS FWS FWS .Reset breaker .Perform Bite test of BSCU 1 on MCDU (AT A 32 .Recycle A/SKID & N/W STRG switch on F/O instrument panel BRAKES BSCU CH 1 FAULT MEL 32-42-03 .BSCU CH2) 21 .Perform Bite test of BSCU 1 on MCDU (AT A 32 .Reset breaker FWC1 FAULT .Cool down brakes with Brake Fan MEL 32-42-01 or BRAKES RELEASED 32-42-05 .BSCU CH2) BRAKES RESIDUAL BRAKING MEL 32-42-01 .BSCU CH2) BRAKES HOT NO GO .BSCU CH 1) BRAKES BSCU CH 2 FAUL T.BSCU CH1) .Breaking/Steering .Perform Bite test of BSCU 2 on MCDU (ATA 32 .Breaking/Steering .No action necessary (Switch A/SKID & N/W STRG is set to OFF) BRAKES ANTI SKID FAULT .Breaking/Steering .Reset breaker FWC 1+2 FAULT .Breaking/Steering .Recycle breaker FDIU/DFDR on panel 722VU position F42 RECORDER FDIU FAULT .Recycle breaker FDIU/DFDR on panel 722VU position F42 BRAKES A330 BRAKES A/SKID NWS OFF Not applicable . Reset breaker LGCIU 1 and LGCIU 2 on LH and RH reset panel WHEEL TIRE LO PR .Recycle A/SKID & N/W STRG switch on F/O instrument panel .Recycle A/SKID & N/W STRG switch on F/O instrument panel WHEEL N/W STRG FAULT .Recycle A/SKID & N/W STRG switch on FIG instrument panel .ECAM WARNING A330 L/G A330 L/G DOORS NOT CLOSED NO GO -Perform visual check of landing gear doors -Reset breaker LGCIU 1 and 2 on LH and RH reset panel L/G GEAR NOT DOWN Not applicable -No action if no Post Flight Report L/G GEAR NOT DOWNLOCKED Not applicable -Reset breaker LGCIU 1 and 2 on LH and RH reset panel L/G GEAR NOT UPLOCKED Not applicable -Reset breaker LGCIU 1 and 2 on LH and RH reset panel L/G GEAR UPLOCK FAULT FCOM 2-04-25 -Check uplock assembly of all gears L/G L LENGTHENING FAULT FCOM 2-04-25 -Check for damage to the shortening mechanism or the prox. sensor target LH L/G R LENGTHENING FAULT FCOM 2-04-25 -Check for damage to the shortening mechanism or the prox sensor target RH L/G LGCIU 1 FAULT MEL 32-31-01 -Reset breaker FWC 1 and LGCIU 1 on LH reset panel -Reset breaker FWC 2 and LGCIU 2 on RH reset panel L/G LGCIU 1+2 FAULT MEL 32-31-01 -Reset breaker FWC 1 and LGCIU 1 on LH reset panel -Reset breaker FWC 2 and LGCIU 2 on RH reset panel L/G LGCIU 2 FAULT MEL 32-31-01 -Reset breaker FWC 1 and LGCIU 1 on LH reset panel -Reset breaker FWC 2 and LGCIU 2 on RH reset panel L/G RETRACTION FAULT FCOM 2-04-25 -Check for damage to prox sensors targets or attachment brackets L/G SYS DISAGREE NO GO -Reset breaker LGCIU 1 and 2 on LH and RH reset panel -Check for damage to the down lock proximity sensors or targets WHEEL A330 WHEEL HYD SEL VALVE .Unsatisfactory tire pressure (Adjust tire pressure) NO GO MEL 32-51-01 NO GO NAV A330 NAV ADR 1 FAULT -Reset FWC1 and FWC2 on LH and R panel -Check Post Flight Report NAV ADR 1+2 FAULT -Reset FWC1 and FWC2 on LH and R panel -Check Post Flight Report NAV ADR 1+3 FAULT -Reset FWC1 and FWC2 on LH and R panel MEL 34-10-01-8 MEL 34-10-01-8 MEL 34-10-01-B 22 . No action is required if there is no Post Flight Report NAV ATT DISCREPANCY MEL 34-10-01-A -No action is required if there is no Post Flight Report NAV EXTREME LATITUDE Not applicable -No action is required if there is no Post Flight Report NAV FM/IR POS DISAGREE Not applicable -No action is required if there is no Post Flight Report NAV GPWS FAULT MEL 34-38-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV HDG DISCREPANCY MEL 34-10-01-A -No action is required if there is no Post Flight Report NAV ILS 1 FAULT MEL 34-36-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV ILS 1+2 FAULT MEL 34-36-01 -Check the Post Flight Report NAV ILS 2 FAULT MEL 34-36-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV IR 1 FAULT MEL 34-10-01-A -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV IR 1+2 FAULT MEL 34-10-01-A -Check the Post Flight Report NAV IR 1+3 FAULT MEL 34-10-01-A -Check the Post Flight Report NAV IR 2 FAULT MEL 34-10-01-A -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV IR 2+3 FAULT MEL 34-10-01-A -Check the Post Flight Report NAV IR 3 FAULT MEL 34-10-01-A -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV IR NOT ALIGNED MEL 34-10-01-A -No action is required if there is no Post Flight Report NAV RA 1 FAULT MEL 34-42-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV RA 1+2 FAULT MEL 34-42-01 -If message RA 1 and RA2 is shown only on ground. no action is necessary NAV RA 2 FAULT MEL 34-42-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel NAV TCAS FAULT MEL 34-42-01 -Reset FWC 1 and FWC 2 on LH and RH reset panel 23 .ECAM WARNING A330 -Check Post Flight Report NAV ADR 2 FAULT MEL 34-10-01-B -Reset FWC 1 and FWC2 on LH and RH reset panel -Check Post Flight Re art NAV ADR 2+3 FAULT MEL 34-10-01-B -Reset FWC 1 and FWC 2 on LH and RH reset panel -Check Post Flight Report NAV ADR 3 FAULT MEL 34-10-01-B -Reset FWC 1 and FWC 2 on LH and RH reset panel -Check Post Flight Report NAV ALTI DISCREPANCY MEL 34-10-01-8 . Faulty FDU (13WG) -Reset FWC 1 and FWC 2 on LH and RH reset panel APU FIRE LOOP 8 FAULT -If Loop B OK ….Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR AVIONIC MEL 52-71-01-B .ECAM WARNING A330 APU A330 APU FAULT -Check the Post Flight Report APU FIRE DET FAULT -Recycle breaker FDU LOOP 8 APU on panel 721VU position P08 -Recycle breaker FIRE LOOP A APU on panel 742VU position D80 APU FIRE LOOP A FAULT -If Loop A OK ….Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR BULK CARGO MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR FWD CARGO MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR L AFT CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR L EMER EXIT MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR L FWD CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR L MID CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR POS DET 1 FAULT MEL 52-71-01-A -Reset CPC 1 and CPC 2 on LH and RH reset panels -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR POS DET 1+2 FAULT MEL 52-71-01-A -Reset CPC 1 and CPC 2 on LH and RH reset panels -Recycle breaker DOORS & SLIDES CTL on panel 721VU position N09 -Recycle breaker DOORS & SLIDES CTL on panel 722VU position P41 DOOR POS DET 2 FAULT MEL 52-71-01-A -Reset CPC 1 and CPC 2 on LH and RH reset panels -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) 24 . Faulty FDU (13WG) -Reset FWC 1 and FWC 2 on LH and RH reset panel MEL 49-11-01 MEL 26-13 MEL 26-13-01 MEL 26-13-01 DOOR A330 DOOR AFT CARGO MEL 52-71-01-B . RANGE -Check Post Flight Report -If there is no message. RANGE -Check Post Flight Report -If there is no message. no action is necessary CONFIG R SIDESTICK FAULT CONFIG CONFIG CONFIG CONFIG CONFIG -Check Post Flight Report -If there is no message.O. THRUST DISAGREE -Check Post Flight Report for defective LRU(s) ENG THRUST LOSS MEL 73-30-03-B NO GO MEL 73-20-01 NO GO MEL 73-30-03-B 25 . no action is necessary SPD BRK NOT RETRACTED -Check Post Flight Report -If there is no message no action is necessary NO GO Apply ECAM procedure Apply ECAM procedure NO GO NO GO NO GO NO GO NO GO ENG A330 ENG THRUST LOSS -Reset breaker ZONE CONT on RH reset panel ENG ALL ENG FLAME OUT -Check fuel filters ENG THR LRVERS NOT SET -Operational message.O. no action is necessary SLATS NOT IN T.O. no further action required ENG T.O. RANGE -Check Post Flight Report -If there is no message. no action is necessary RUD TRIM NOT IN T. no action is necessary PARK BRK ON -Set brakes OFF PITCH TRIM NOT IN T. RANGE -Check Post Flight Report -Reset FWC 1 and FWC 2 on LH and RH reset panel CONFIG L SIDESTICK FAULT -Check Post Flight Report -If there is no message.O.ECAM WARNING A330 DOOR R AFT CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR R EMER EXIT MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR R FWD CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform system test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) DOOR R MID CABIN MEL 52-71-01-B -Check proximity sensor and target -Perform System test of PSCU on MCDU (ATA 52 -DOORS -PROXIMITY SW CTL UT) CONFIG A330 CONFIG FLAPS NOT IN T. ECAM WARNING A330 -Reset breaker ZONE CONT on RH reset panel ENG1 A330 ENG1 BLEED STATUS Apply ECAM procedure -Reset breaker EIVMU 1 on LH reset panel ENG1 CTL SYS FAULT NO GO -Recycle breaker FADEC A ENG 1 on panel 742VU position Q73 -Recycle breaker FADEC B ENG 1 on panel 722VU position D44 ENG1 EGT OVERLIMIT Not applicable -Perform visual check of engine ENG1 EIU FAULT MEL 73-25-02 -Reset breaker EIVMU 1 on LH reset panel -Reset breaker FCU 1 on LH reset panel ENG1 FADEC FAULT NO GO -Reset breaker SDAC 1 & 2 on LH and RH reset panel -Reset breaker FCU 1 on LH reset panel ENG1 FADEC OVHT NO GO -Check for excessive heat near the EEC (nacelle anti-ice duct) ENG1 FADEC SYS FAULT NO GO -Reset breaker EIVMU 1 on LH reset panel -Recycle breaker FADEC A ENG 1 on panel 742VU position Q73 -Recycle breaker FADEC B ENG 1 on panel 722VU position D44 ENG1 FIRE DET FAULT -Perform the bite test of the FDU with MCDU (ATA 26 Fire Prot -Engines -FDU -Test) ENG1 FIRE LOOP A FAULT -Perform the bite test of the FDU with MCDU (ATA 26 Fire Prot -Engines -FDU -Test) ENG1 FIRE LOOP B FAULT -Perform the bite test of the FDU with MCDU (AT A 26 Fire Prot -Engines -FDU -Test) ENG1 FUEL FILTER CLOG -Check fuel pump filter -Check fuel pump filter differential switch ENG1 HP FUEL VALVE -Perform FADEC system static test with MCDU (AT A 70-80 Engine -EEC 1 -System test) ENG1 IGN A FAULT -Reset breaker EIVMU 1 on LH reset panel ENG1 IGN B FAULT -Reset breaker EIVMU 1 on LH reset panel ENG1 IGN A+B FAULT NO GO MEL 26-12-01 MEL 26-12-01 NO GO NO GO MEL 74-31-01 or 74-31-03-A MEL 74-31-01 or 74-31-03-A MEL 74-31-01 or 74-31-03-A -Reset breaker FWC 1 & 2 on LH and RH reset panel ENG1 MINOR FAULT MEL 73-25-01-A -Recycle breaker FADEC A ENG 1 on panel 742VU position Q73 -Recycle breaker FADEC B ENG 1 on panel 722VU position D44 26 . Disagree between Throttle Control Lever Position and Position detected by EEC ENG2 A330 ENG2 BLEED STATUS Apply ECAM procedure -Reset breaker EIVMU 2 on RH reset panel ENG2 CTL SYS FAULT NO GO -Recycle breaker FADEC A ENG 2 on panel 742VU position Q73 -Recycle breaker FADEC B ENG 2 on panel 722VU position D44 ENG2 EGT OVERLIMIT Not applicable -Perform visual check of engine ENG2 EIU FAULT MEL 73-25-02 -Reset breaker EIVMU 2 on LH reset panel -Reset breaker FCU 2 on LH reset panel ENG2 FADEC FAULT NO GO -Reset breaker SDAC 1 & 2 on LH and RH reset panel -Reset breaker FCU 2 on LH reset panel ENG2 FADEC OVHT NO GO -Check for excessive heat near the EEC (nacelle anti-ice duct) ENG2 FADEC SYS FAULT NO GO -Reset breaker EIVMU 2 on LH reset panel -Recycle breaker FADEC A ENG 2 on panel 742VU position Q74 -Recycle breaker FADEC B ENG 2 on panel 722VU position D49 27 .Check engine oil level and check for leaks ENG1 REV FAULT MEL 78-30-01 .Perform visual check of engine reverse cowls ENG1 SHUT DOWN NO GO . ENG1 REV UNLOCKED MEL 78-30-01 .Reset breaker EIVMU 1 on LH reset panel ENG1 THR LEVER FAULT NO GO .Disagree between Throttle Control Lever position and position detected by EEC .ECAM WARNING A330 NO GO or MEL 79-35-02-A ENG1 OIL FILTER CLOG -Check oil filter -Check oil filter differential switch ENG1 OIL HI TEMP -Check engine oil level ENG1 OIL LO TEMP . Starter valve or starter ENG1 THR LEVER DISAGREE NO GO .Operational message .Starter valve .Starter .Reset breaker FWC 1 & 2 on LH and RH reset panel ENG1 START FAULT NO GO .No further action required ENG1 OIL LO PRESS NO GO Apply ECAM procedure NO GO or MEL 79-34-01-A .Reset breaker EIVMU 1 on LH reset panel .Ignition -etcENG1 START VALVE FAULT MEL 80-11-01 .Reset breaker EIVMU 1 on LH reset panel ENG1 REV PRESSURIZED NOT GO Heat the TRDV (directional pilot valve) using hot air source to de-ice the press switch if icing conditions are present or were present during previous descent. No further action required ENG2 OIL LO PRESS NO GO or MEL 79-34-01-A .Reset breaker EIVMU 2 on RH reset panel ENG2 THR LEVER FAULT NO GO .Starter .Reset breaker EIVMU 2 on RH reset panel 28 .Operational message .Starter valve .Reset breaker FWC 1 & 2 on LH and RH reset panel ENG2 START FAULT NO GO . Starter valve or starter ENG2 THR LEVER DISAGREE NO GO .Perform visual check of engine reverse cowls ENG2 SHUT DOWN NO GO . ENG2 REV UNLOCKED MEL 78-30-01 .Reset breaker EIVMU 2 on RH reset panel ENG2 REV PRESSURIZED NO GO Heat the TRDV (directional pilot valve) using hot air source to de-ice the press switch if icing conditions are present or were present during previous descent.Check engine oil level and check for leaks ENG2 REV FAULT MEL 78-30-01 .Disagree between Throttle Control Lever position and position detected by EEC .ECAM WARNING A330 ENG2 FIRE DET FAULT -Perform the bite test of the FDU with MCDU (ATA 26 Fire Prot -Engines -FDU -Test) ENG2 FIRE LOOP A FAULT -Perform the bite test of the FOU with MCDU (ATA 26 Fire Prot -Engines -FDU -Test) ENG2 FIRE LOOP B FAULT -Perform the bite test of the FDU with MCDU (AT A 26 Fire Prot -Engines -FDU -Test) ENG2 FUEL FILTER CLOG -Check fuel pump filter -Check fuel pump filter differential switch ENG2 HP FUEL VALVE -Perform FADEC system static test with MCDU (AT A 70-80 Engine -EEC 2 -System test) ENG2 IGN A FAULT -Reset breaker EIVMU 2 on RH reset panel ENG2 IGN B FAULT -Reset breaker EIVMU 2 on RH reset panel ENG2 IGN A+B FAULT NO GO MEL 26-12-01 MEL 26-12-01 NO GO NO GO MEL 74-31-01 or 74-31-03-A MEL 74-31-01 or 74-31-03-A MEL 74-31-01 or 74-31-03-A -Reset breaker FWC 1 & 2 on LH and RH reset panel ENG2 MINOR FAULT MEL 73-25-01-A -Recycle breaker FADEC A ENG 2 on panel 742VU position Q74 -Recycle breaker FADEC B ENG 2 on panel 722VU position D49 ENG2 OIL FILTER CLOG NO GO or MEL 79-35-02-A -Check oil filter -Check oil filter differential switch ENG2 OIL HI TEMP NO GO -Check engine oil level ENG2 OIL LO TEMP Apply ECAM procedure .Disagree between Throttle Control Lever position and position detected by EEC .Ignition -etcENG2 START VALVE FAULT MEL 80-11-01 .