N4048J

Part: SENSOR — FAILED (ZONE 200) · airframe 16,569 hrs · 2,460 cycles

FLT 2163, LHR-JFK. (ETOPS) TEMP CTL 2 CLASS 2 MSG ON ECAM ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 4) FAULT(S) INDICATED BY TEMP CTL 1 (2) . REF MDDR 602750 AND LP 4430437(PER TSM 21-61-00-810-831-A REPLACED PACK 2 OUTLET TEMP SENSOR (34HH) REF AMM 21-61-15. TEST OK. MX-4 UPDATED, PLACARD RMEOVED). FAULT CLEARED. MX-4 UPDATED, PLACARD REMOVED.

Part: SENSOR — FAULTED (ZONE 100) · airframe 16,582 hrs · 2,462 cycles

FLT#34, CDG-BOS. (ETOPS) PACK 2 REGULATOR FAULT ( ECAM INDICATION ON BLEED PAGE PACK COMPRESSOR OUTLET TEMPERATURE ); PER TSM 21-61-00-810-831-A REPLACED PACK 2 OUTLET TEMP SENSOR (34HH) REF AMM 21-61-15. TEST OK. MX-4 UPDATED, PLACARD REMOVED.

Part: IGNITER — FAULTED (NR 2 ENGINE) · airframe 16,555 hrs · 2,458 cycles

FLT 2220, LHR-JFK. (ETOPS) ENG 2 ING B FAULT ON TOUCHDOWN, REMOVED AND REPLACED ENG NR 2 IGNITER PLUG B (LOWER) IAW AMM 74-21-01. OPS TESTED GOOD.

Part: RADAR — INOPERATIVE (NR2 WX) · airframe 15,670 hrs · 2,324 cycles

FLT#2288, JFK-AMS. (ETOPS) NR 2 WX RADAR INOPERATIVE. OPEN

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 15,485 hrs · 2,297 cycles

FLT# 834, SFO-BOS. (ETOPS) "WXR R/T ON BOTH NDS FOR FIRST 4 HRS ON FLIGHT BEFORE CLEARING; REMOVED AND REPLACED #1 WX RADAR TRANSCEIVER PER AMM 34-41-33 OPS CK NORMAL CANNOT DUPLICATE PROBLEM AT THIS TIME A/C OK FOR SVC."

Part: IGNITER — FAULTED (APU) · airframe 15,460 hrs · 2,293 cycles

FLT#1621, LHR-BOS. (ETOPS), APU AUTO SHUTDOWN ON TAXI IN; REPLACED THE IGNITER PLUG IAW AMM 49-41-41. OPS TEST WAS PERFORMED IAW AMM 49-00-00.A/C IS OK FOR SVC.

Part: FIRE LOOP — DEFECTIVE (ZONE 400) · airframe 15,109 hrs · 2,241 cycles

FLT#20, LHR-JFK. (ETOPS) ENG 2 PYLON LOOP B 4WD2 DEFECTIVE; REPLACED ENG 2 PYLON LOOP B 4WD2 IAW AMM 26-12-16 OPS CHKS REQD REF LP 3504569-1 FOR OPS CHKS.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR SYS) · airframe 15,109 hrs · 2,241 cycles

FLT$20, LHR-JFK. (ETOPS) "AIR BLEED CLASS 2 MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY AIR BLEED ); (RESOLVED ON W/O: 1433886 TASKCARD: NR-00003) PERFORMED FIM TASK 36-11-0-810-993-A. TEST PASSED AT THIS TIME AND WAS SPURIOUS. MX-4 UPDATED PLACARD REMOVED. THIS CLEARS MEL 36-00-00 MDDR.

Part: WIRE HARNESS — SHORTED (ZONE 400) · airframe 15,109 hrs · 2,241 cycles

FLT#20, LHR-JFK. (ETOPS) ENG 2 PYLON LOOP B STUD A HARNESS 41WD2 DEFECTIVE SHORT TO GND; REPLACED ENG 2 PYLON LOOP B HARNESS 41WD2 IAW AMM 26-12-63. OPS CHKS REQD REF LP 3504569-1 FOR OPS CHKS.

Part: FIRE DETECTOR — FAULTED (ZONE 400) · airframe 15,031 hrs · 2,228 cycles

FLT#32, AMS-BOS. (ETOPS) "ENG FIRE LOOP FAULT LOOP B ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); REF LPS 3504565-1/2 (REPLACED ENG 2 PYLON LOOP B HARNESS 41WD2 IAW AMM 26-12-63. OPS CHKS REQD REF LP 3504569-1 FOR OPS CHKS) AND 3504566-1/2(REPLACED ENG 2 PYLON LOOP B 4WD2 IAW AMM 26-12-16 OPS CHKS REQD REF LP 3504569-1 FOR OPS CHKS) (REPLACED ENG 2 PYLON LOOP B/A RACK ASSY IAW AMM 26-12-16) FOR TROUBLE SHOOTING AND CORRECTIVE ACTIONS MDDR CLEARED MX-4 UPDATED PLACARD REMOVED.

Part: SUPPORT BRACKET — DAMAGED (ZONE 400) · airframe 14,836 hrs · 2,200 cycles

FLT#1621, LHR-BOS. (ETOPS) "#2 ENG FAN AIR SUPPORT BRACKET HAS ELONGATED HOLE AND WORN BEARING; REPLACED #2 ENG FAN AIR SUPPORT BRACKET REF AMM CHPT 36-11-00."

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 14,836 hrs · 2,200 cycles

FLT#1621, LHR-BOS. (ETOPS) 'REMOVED ENG #1 FAN AIR VALVE ASSY IAW AMM 36-11-54-000-803-A; REPLACED ENGINE #1 FAN AIR VALVE DUE TO EXCESSIVE PLAY IN UPPER BEARING PER TASK CARD A3625040-01, AMM TASK 36-11-54. REF LP 4300580 ITEM 1 FOR OPS CHK.'

Part: CONTROL UNIT — FAILED (ALSCU) · airframe 14,767 hrs · 2,190 cycles

FLT#1908, CDG-JFK. "L2 TSI – HIGH LEVEL SENSOR FAULT DUE TO AVIATAR REPORTING THE FOLLOWING FAULT FUEL ACT AFT 1 HI LVL IAW TSM 28-46-00-810-873-A. IF NO FAULTS ARE FOUND, REPLACE AUXILIARY LEVEL SENSING CONTROL UNIT (ALSCU) (60QJ) PER AMM 28-46-35. C/W ALL GMM BUY BACK AND RII REQUIREMENTS- THANK YOU SOURCE- AVIATAR; (RESOLVED ON W/O: 1423896 TASKCARD: NR-00001) REMOVED AND REPLACED ALSCU AT 60QJ. PERFORMED OPS CHK AND OPS CHK TEST GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. REF AMM 28-46-35."

Part: PRESSURE SWITCH — FAULTED (RAT) · airframe 14,550 hrs · 2,158 cycles

FLT#1908, CDG-JFK. (ETOPS) .'HYD RAT FAULT; REMOVED AND REPLACED ACTUATOR PRESSURE SWITCH IAW AMM 29-22-53.LEAK CHK GOOD.OPS CHK GOOD.NO FAULTS NOTED.AC OK FOR SVC.'

Part: IGNITER — FAILED (APU) · airframe 14,358 hrs · 2,129 cycles

FLT#1908, CDG-JFK. (ETOPS) 'ON START AFTER LANDING APU AUTO SHUTDOWN. HUNG AT 20%. NO EGT INCREASE; REMOVED AND REPLACED APU IGNITER PLUG W/REF TO AMM 49-41-41. PERFORMED OPS CHECK OF APU, NO FAULT NOTED. A/C OK FOR SVC.'

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL SYS) · airframe 14,035 hrs · 2,082 cycles

FLT#7, JFK-LHR. (ETOPS). FUEL CLASS II MX MSG ON ECAM ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY FUEL ); PERFORMED BITE TEST OF FLSS PER AMM SUBTASK 28-46-00-740-051-H. NO FAULT NOTED AT THIS TIME MX-4 UPDATED PLACARD REMOVED.

Part: SENSOR — FAULTED (OIL SYSTEM) · airframe 13,868 hrs · 2,057 cycles

FLT#1908, CDG-JFK. (ETOPS) 'CONUS REST DUE TO ENG 2 OIL SENSOR FAULT REPAIRS ( AIRCRAFT TECHNICAL RESTRICTION (CONUS RESTRICTION) ); REF LOG PG 4225204, ITEM #2 ENG #2 PHMU REPLACED NO FAULTS NOTED CONUS NO LONGER REQUIRED. MX4 UPDATED MCC NOTIFIED.'

Part: METERING UNIT — UNKNOWN (NR 2 ENGINE) · airframe 13,860 hrs · 2,056 cycles

FLT#1907, JFK-CDG. (ETOPS) 'ENG 2 OIL SENSOR FAULT ON DESCENT ( 5) OIL SENSOR FAULT CAUTION ON ECAM EWD ); ACCOMPLISHED TSM 77-31-00-810-807-A. ACCOMPLISHED VISUAL INSP OF W3/W4 HARNESS. NO DAMAGE NOTED. INTERROGATED CFDS, 'ENG2 PHMU INTERNAL SNSR FAULT.' REMOVED AND REPLACED ENG#2 PHMU IAW AMM 77-31-01. OPS CHECK GOOD. NO FAULTS/MSGS NOTED. ALL PARAMS NORMAL. THIS CLEARS MDDR. PLAC REMOVED. MX-4 UPDATED.'

Part: FIRE LOOP — FAILED (NR 2 ENGINE) · airframe 13,290 hrs · 1,959 cycles

FLT#34, CDG-BOS. (ETOPS) ENG 2 FIRE LOOP A FAULT INOP - REPEAT WRITE-UP ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A )'; CHECK PER TSM 26-12-00-810-805-A. FOUND DET-FIRE CORE AGB LOOP A (4002WD1) SHORTED TO GROUND. R/R DET-FIRE CORE AGB LOOP A IAW AMM 26-12-17. PERFORMED OPS CHECK. OPS CHECK GOOD. MX-4 UPDATED, MDDR CLEARED. PLACARD REMOVED.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 13,233 hrs · 1,951 cycles

FLT#20, LHR-JFK. (ETOPS) 'AFTER ENG 2 START WE GOT ENG 2 FUEL HEAT SYS FUEL RETURN VALVE OPEN; REF TSM 73-13-00-810-803A REV FEB 25. REPLACED RTRT MODULE IAW AMM 73-13-03-400-801-A & 73-13-03-000-801-A REV DEC 24.'

Part: INDICATION SYS — FAULTED · airframe 12,993 hrs · 1,917 cycles

FLT#1408, CDG-JFK. (ETOPS) 'FUEL ACT XFR FAULT ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ); PERFORMED OPS CHECK OF ACT FUEL TRANSFER SYSTEM AS PER AMM 28-28-00.OPS CHECK NORMAL.NO DEFECTS NOTED.MX-4 UPDATED PLACARD REMOVED.

Part: ENGINE — FAILED (ENGINE-1) · airframe 12,564 hrs · 1,851 cycles

FLT#524, LAX-JFK. '(ETOPS) 'FOUND OIL IN #1 ENGINE TURBINE EXHAUST; REMOVE & REPLACED #1 ENGINE REF WO 1377333 T/C A320-71-00-51-400-802A OK FOR CONT. SVC.'

Part: FIRE LOOP — FALSE INDICATION (ZONE 400) · airframe 12,160 hrs · 1,786 cycles

FLT#33, BOS-CDG. (ETOPS) 'ENG 2 LOOP B FIRE FAULT CAUTION DISPLAYED INTERMIT DURING FLIGHT ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); PERFORMED ENG 2 FIRE LOOP TEST IA WAMM 26-12-00. OPS CHECK GOOD. NO DEFECTS NOTED FAULTS DISPLAYED ON ECM. MDDR CLEARED PLACARD RMV. MX-4 UPDATED (MSG HAS NOT APPEARED WITHIN THE LAST FEW PREVIOUS FC).

Part: FUEL CONTROL — FAILED (FUEL SYS) · airframe 11,696 hrs · 1,717 cycles

FLT#44, LGW-JFK. (ETOPS) CLASS II FUEL MAINTENANCE MESSAGE ON STATUS PAGE ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY FUEL ); REMOVED AND REPLACED AFCM W/ REF TO AMM28-51-35. OPS CHECK GOOD. NO FAULTS NOTED, THIS CLEARS MDDR 560614. MX-4 UPDATED/ PLACARD REMOVED

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 11,630 hrs · 1,707 cycles

FLT#552, MCO-BOS. (ETOPS) 'ENG 1 CONSUMPTION SINCE LAST UPLIFT AND CURRENT UPLIFT AT 0.329 QPH ABOVE AMM LIMITS; R/R ENGINE #1, SEE LP 4113859 (PERFORMED ENG #1 CHANGE PER TASK CARD NO A320-71-00-51-000-802-A AND A320-71-00-51-400-802-A ON W/O 1359258), THIS CLEARS THIS DEFECT.'

Part: WIRE HARNESS — FAILED (NR 1 EEC) · airframe 11,630 hrs · 1,707 cycles

FLT#552, MCO-BOS. (ETOPS) 'RE FL/P 4113863, ITEM 2 (#1 ENG NAI UPSTREAM PT FAULT ON ENG START; REMOVED AND REPLACED #1 ENG PT NACELLE ANTI ICE IAW AMM 30-21-00 FAULT IS STILL PRESENT AT THE MOMENT.) #1 ENG NAI UPSTREAM PT FAULT; REMOVED AND REPLACED # 1 ENG EEC HARNESS W03 IAW AMM 73-21-63. OPS CHECK OK NO FAULTS PRESENT.'

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 11,630 hrs · 1,707 cycles

FLT#552, MCO-BOS. (ETOPS) 'REF ITEM 4113855-1 (ENG 1 CONSUMPTION SINCE LAST UPLIFT LP 4113851 AND CURRENT UPLIFT AT 0.329 QPH ABOVE AMM LIMITS) (ENG OIL CONSUMPTION); ENG 1 REPLACED EVF SATISFACTORY REF LP 4113870, ITEM 1. MDDR 559532 CLEARED MCC NOTIFIED CM # 61535. REMOVED AND REPLACED ENGINE #1, SEE LP 4113859 (PERFORMED ENG #1 CHANGE PER TASK CARD NO A320-71-00-51-000-802-A AND A320-71-00-51-400-802-A ON W/O 1359258), THIS CLEARS THIS DEFECT

Part: FIRE LOOP — FAULTED (NR 2) · airframe 10,952 hrs · 1,607 cycles

FLT#31, BOS-AMS. (ETOPS) 'ENG 2 FIRE LOOP B FAULT POPPED UP WHILE SITTING AT THE GATE ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); REF L/P 4067945 ITEM #2 (PERFORMED VISUAL INSPECTION OF THE ENGINE FIRE DETECTION SYSTEM IAW AMM 26-12-00-200-802, FOUND DEEP GOUGES IN DET-FIRE, CORE AGB LOOP B (4002W02), R & R CORE AGB LOOP B IAW AMM 26-12-17. REMOVED AND REPLACED FIRE HARNESS ASSY IAW AMM 26-12-62. PER MCC REQUEST) & #2 (PERFORMED OPS TEST OF ENG #2 FIRE AD OVERHEAT DETECTION W/ CFDS IAW AMM 26-12-00. OPS TEST OK) FOR REMOVAL AND REPLACEMENT OF AGB LOOP B (4002WD2), FIRE HARNESS (4166KS) AND ENG #2 FIRE DETECTION OPS TEST. MDDR CLRD, MX-4 UPDATED, PLAC REMOVED.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 10,531 hrs · 1,546 cycles

FLT#44, LGW-JFK. (ETOPS) 'ENG 1 FADEC MAINTENANCE MSG AT SHUTDOWN AT THE GATE; REF L/P 3927095, ITEM 1 (PFR SHOWED FADEC 1 FAULT IN CONJUNCTION WITH 75-32-03 ENG-1B-0701- ACTIVE HPC BLEED VLV SOL FAIL WITH MULTIPLE HITS IN THE PAST DAYS. PERFORMED TSM 75-32-00-810-849A, FOUND W3 HARNESS CHAFFED NEXT TO P57 CONNECTOR AND CHAFED AT 2ND CLIP FROM P57 CONNECTOR. REQUIRES W3 HARNESS REPLACEMENT.) FOR TROUBLESHOOTING. W03 HARNESS FOUND CHAFFED. REMOVED AND REPLACED ENG #1 W03 HARNESS IAW AMM 73-21-63. FADEC SELF TEST OK. A/C OK FOR CONT SVC. REF LP 3927098, ITEM 1 (RECONNECTED EEC AND PHMU CONNECTORS ON ENG 1 (J4, J6, J10, J14) ATER W03 HARNESS REMOVED AND REPLACED IAW AMM 73-21-63. SELF TEST OK) FOR RECONNECTION OF EEC AND PHMU CONNECTORS.'

Part: CONTROLLER — FAULTED (FUEL QTY) · airframe 10,516 hrs · 1,544 cycles

FLT#906, ORD-JFK. (ETOPS) 'FQI CH1 FAULT; REMOVED AND REPLACED FQIC IAW AMM 28-42-34 OPS TEST GOOD.'

Part: FIRE LOOP — MALFUNCTIONED (LOOP B) · airframe 10,472 hrs · 1,535 cycles

FLT#44, LGW-JFK. (ETOPS) FIRE LOOP B FAULT ECAM FLASHING FOR 3 SECONDS AND THEN GOES AWAY CAME IN TWICE 10 MINUTES APART APPROXIMATELY 45 MIN PRIOR TO LANDING ECAM DID NO RE-APPEAR AFTER THE SECOND INSTANCE. REMOVED AND REPLACED FIRE LOOP IAW AMM 26-12-17.

Part: WIRE HARNESS — FAILED (NR 2 ENGINE) · airframe 10,170 hrs · 1,491 cycles

FLT#1620, BOS-LHR. (ETOPS) 'ENG 2 MINOR FAULT, REF TSM 73-31-00-810-811-A, INSPECTED WC08 HARNESS AND FOUND HARNESS DAMAGED AND EXPOSED WIRES. REMOVED AND REPLACED WC08 HARNESS-CORE (4094 KS) IAW AMM 73-21-68. OPS CHECK OK. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.

Part: SENSOR — FAILED (NR 2 ENGINE) · airframe 10,027 hrs · 1,471 cycles

FLT#1107, JFK-LHR. (ETOPS) 'ENG 2 MINOR FAULT ( MINOR FAULT CAUTIONS ON ECAM EWD ); REMOVED AND REPLACED FUEL FLOW SENSOR ENG # 2 IAW AMM 73-31-12-400 AND PERFORMED IDLE RUM REF AMM 71-00-00-860-822. MX-4 UPDATED. PLACARD REMOVED.

Part: SMOKE WARNING — ILLUMINATED (LAVATORY) · airframe 9,840 hrs · 1,444 cycles

FLT#007, JFK-LHR. (ETOPS) 'ECAM MAINT MSG SMOKE ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 2) FAULT(S) INDICATED BY SMOKE ); PERFORMED T/S PER AMM 26-17-00-810-825-00 NO FAULTS FOUND THIS CLEARS MEL 26-00-03 MX-4 UPDATED AND PLACARD REMOVED .

Part: TRANSFER SYS — FAULTED (FUEL SYSTEM) · airframe 9,798 hrs · 1,438 cycles

FLT#1107, JFK-LHR. (ETOPS)' FUEL CTR R XFR FAULT COMPLETED ECAM/QRH IN FLIGHT ( CENTER TANK SYSTEMS 2) B) TRANSFER VALVES (WITH ACT(S)) ); PERFORMED OPERATIONAL TEST OF THE MAIN FUEL TRANSFER SYSTEM, IAW AMM 28-26-00-710-001-A. OPERATIONAL TEST GOOD NO FAULTS NOTED.FUEL TRANSFER RATE IS NORMAL. A/C OK FOR SVC. MX-4 UPDATED MCC NOTIFIED PLACARD REMOVED.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 9,666 hrs · 1,419 cycles

FLT#32, AMS-BOS. (ETOPS) 'ON DEPARTURE RECEIVED AIR ENG BLEED 2 MESSAGE COMPLIED W/ECAM & QRH. RAN RESET TABLE AND SYSTEM DID RESET. SPOKE W/MCC & ADVISED ENTERING IN BOOK PER MCC REQUEST; REF LP'S 3933133, ITEMS 1 (HP BLEED-V (4000HA2)/SENSE LINE FAULT PER TSM 36-11-00-810-976-A INSPECTED LINES FOUND OK. REMOVED AND REPLACED ENG #2 HP BLEED VALVE PER AMM TASK 36-11-51. OPS CHK GOOD. IDLE ENGINE RUN ACCOMPLISHED NO FAULT NOTED) AND 2 (PRESS REG-V (4001HA2) FAULT PER TSM 36-11-00-810-981-A. REMOVED AND REPLACED ENG #2 PRV VALVE IAW AMM TASK 36-11-52. OPS CHECK GOOD. IDLE ENGINE RUN ACCOMPLISHED NO FAULTS NOTED) FOR CORRECTIVE ACTIONS. ENG #2 HP VALVE & PRSOV VALVE REPLACED NO FAULTS NOTED. A/C OK FOR CONT SERVICE. GROUND VERIFICATION CHECKS ACCOMPLISHED, MCC NOTIFIED.

Part: CONTROL UNIT — FAILED (FUEL SYS) · airframe 9,651 hrs · 1,417 cycles

FLT#1408, (ETOPS) FUEL CLASS II MX MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY FUEL ); REMOVED AND REPLACED FUEL-LEVEL SENSING CONTROL UNIT IAW AMM 28-46-34. OPS CHECK GOOD , NO MSG DISPLAYED AT THIS TIME. MDDR CLEAR, PLACARD REMOVED & MX4 UPDATED.

Part: IGNITER — FAULTED (NR 1 ENGINE) · airframe 9,333 hrs · 1,370 cycles

FLT#31, BOS-AMS. (ETOPS) 'STARTING ENGINE 1 RECEIVED ENG 1 IGN A FAULT; REMOVED AND REPLACED #1 ENG IGNITOR PLUG IGNITION A. OPS CHECK GOOD. REF AMM 74-21-01.'

Part: FCU — FAILED (APU) · airframe 9,136 hrs · 1,340 cycles

FLT#523, JFK-LAX. (ETOPS) "APU AUTO SHUTDOWN ( APU SYSTEM A321NEO ETOPS ); REMOVED AND REPLACED FCU IAW AMM 49-41-00. PERFORMED OPS TEST OF APU PER 24-41-00 OF THE AMM. TEST NORMAL. NO LEAKS NOTED. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.'

Part: CIDS — FAILED (UNKNOWN) · airframe 8,793 hrs · 1,291 cycles

FLT#44, LGW-JFK. (ETOPS) 'CLASS II CIDS MESSAGE ( CLASS II MX MSG DISPLAYED - CIDS ). C/W REF LP 3880805, ITEM 2 (REMOVED AND REPLACED CIDS DIRECTOR 2 IAW AMM 23-73-34 OBRM DOWNLOAD PROCEDURE ACCOMPLISHED. OPS TEST SATISFACTORY. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED) FOR REMOVAL AND REPLACEMENT OF CIDS.

Part: CIDS — FAILED (101RH) · airframe 8,542 hrs · 1,254 cycles

FLT#20, LHR-JFK. (ETOPS). 'SMOKE FWD CRG DET FAULT. AFT CRG DET FAULT; ACCOMPLISHED TSM 26-17-00-810-822A. REMOVED AND REPLACED CIDS #1 IAW AMM 23-73-34. OPS TEST OK. NO-FAULT PRESENT.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,422 hrs · 1,236 cycles

FLT#1124, LAX-JFK. (ETOPS) ENG 1 IGNITION A FAULT AFTER ENGINE START ( IGNITION SYSTEMS A) SYSTEM A ). REMOVED AND REPLACED ENG 1 IGNITER "A" IRW AMM PW1000G-C-74-21-01. OPS CHECK SUCCESSFUL. PLACARD REMOVED. MX-4 UPDATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,427 hrs · 1,237 cycles

FLT#2223, JFK-LAX. (ETOPS) 'ENG 2 FIRE LOOP A ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); PER TSM 26-12-00-810-805A TESTED #2 ENG LOOP A AGB FOUND LOOP WITH HIGH RESISTANCE. REMOVED AND REPLACED LOOP A AGB IAW TSM 26-12-00-810-805A. OPS CHECK OK NO FAULT PRESENT. THIS CLEARS MDDR # 530042, PLACARD REMOVED. MX-4 UPDATED, MCC NOTIFIED.'

Part: ACTUATOR — FAILED (FUEL TRANSFER) · airframe 7,888 hrs · 1,154 cycles

FLT#2289, AMS-JFK. (ETOPS) ' FUEL ACT XFR FAULT; REMOVED AND REPLACED ACT VENT 91QH IAW AMM 28-28-62. OPS CHECK REQUIRED REF L/P 3675767, ITEM 2. ( (ITEM RESOLVE UNDER MDDR: 524937) PERFORMED OPERATIONAL TEST OF THE ACT VENT VALVE ACTUATOR IAW AMM 28-28-00-710-006 AND PERFORMED OPERATIONAL TEST OF THE ACT ASPER AMM 28-28-01C OPS CHECK OK. MX-4 UPDATED. MCC NOTIFIED. PLACARD REMOVED).'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,754 hrs · 1,135 cycles

FLT#43, JFK-LGW. (ETOPS) AC GEN MAINTENANCE STATUS MESSAGE. ( CLASS II MX MSG - GPCU OR AC GEN ); PERFORMED FUNCUTION TEST OF A/C GEN IAW AMM 24-21-51. NO MSG. OK FOR FLT SVC AT THIS TIME. MX-4 UPDATED. PLACARD REMOVED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,731 hrs · 1,129 cycles

FLT#20, LHR-JFK. (ETOPS) 'AFTER LANDING ECAM ENG 2 OIL CHIP DETECTED; REF LOG PAGE 3793104 (MX ACKNOWLEDGE EVF SUCCESSFUL FOR #2 ENG WITH NO DEFECTS. THIS CLEARS MDDR 523562. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED) #2 ENGINE REPLACED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,535 hrs · 1,100 cycles

FLT#20, LHR-JFK. (ETOPS) ' ENG 2 HIGH VIBRATION COMES DURING CLIMB POWER ONLY; REF LP 367411, ITEM 1 REMOVAL AND REPLACEMENT ENG 2 REF WO 1277461. OK FOR CONTINUED SERVICE.'

Part: SENSOR — FAILED (UNKNOWN) · airframe 7,209 hrs · 1,053 cycles

FLT#007, JFK-LHR. (ETOPS) 'AIR PACK 1 REGULATOR FAULT ( PACK COMPRESSOR OUTLET TEMP IND- BLEED PG ). REMOVED AND REPLACED PACK 1 COMPRESSOR TEMP SENSOR FIN 12HH IAW AMM 21-61-11. OPS CHECK GOOD. NO DEFECTS NOTED. CLEARS MDDR 518686. MX-4 UPDATED. PLACARD REMOVED.

Part: FDU — FAILED (UNKNOWN) · airframe 7,094 hrs · 1,035 cycles

FLT#44, LGW-JFK. (ETOPS) 'ENGINE 2 FIRE LOOP B FAULT. ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ). REF TSM 26-12-00-810-806A, AWM 26-12-08 AND AWM 71-575, CHK WIRING FDU2 PINS K&J RESISTANCE 1476 OHMS, PERFORMED A GVI OF THE FIRE LOOPB ELEMENTS NO DAMAGES NOTED. REMOVED AND REPLACED FDU 2 AS A PRECAUTIONARY T/SHOOTING, REF LOG PAGE 3715588-2, FOR CORRECTIVE ACTION. CLEARED MDDR 517296. MX-4 UPDATED AND PLACARD REMOVED.

Part: CONTROL UNIT — FAILED (UNKNOWN) · airframe 6,893 hrs · 1,006 cycles

FLT#7, JFK-LHR. (ETOPS) 'ACT XFR FAULT ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT) ); REMOVED AND REPLACED CONTROL INIT - AXILIARY LEVEL (60QJ) IAW AMM 28-46-35. TEST OK. ACCOMPLISHED OPERATIONAL TEST OF THE ACT AUTOMATIC TRANSFER SYSTEM IAW AMM 28-28-00-710-005-A. TEST OK. NO FAULTS NOTED. MX4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.

Part: FUEL CONTROL — FAILED (4005KM) · airframe 6,778 hrs · 989 cycles

FLT#1621, LHR-BOS. (ETOPS) ' APU AUTO SHUT DOWN W/ FUEL LOW PRESSURE; REMOVED AND REPLACED FCU FIN 8022KM. OPS CHECK OK IAW AMM 49-32-00.'

Part: UNKNOWN — UNKNOWN · airframe 6,369 hrs · 929 cycles

FLT#1107, JFK-LHR. (ETOPS) 'ON 2 ENGINE START DURING TAXI OUT RC'VD ENG 2 IGN A FAULT ENGINE STARTED WITH AUTO MOTORING; REPLACED #2 ENG IGNITER "A" (UPPER) IAW AMM 74-21-01. IDLE RUN PERFORMED OPS CHECK GOOD. A/C OK FOR SVC.'

Part: CONTROLLER — FAILED (FUEL) · airframe 5,964 hrs · 870 cycles

FLT#2104, BOS-LGW. (ETOPS) 'PIREP: PERSISTENT FUEL ACT XFR FAULT. ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT). REF TSM 28-46-15, ASM 28-46-01 AND AWM 28-46-19, REMOVED AND REPLACED AFMC (FIN 2QN) IAW 28-51-35 AND HI LVL SNSR ACT1 SEL SW (FIN72QJ1) IAW ESMP 20-45-21. AS A PRECAUTIONARY /T/SHOOTING PER LEADERSHIP REQUEST. TEST OF THE HI LVL SNSRS ACCOMPLISHED IAW 28-46-00, ALL OPS CHK OKAY.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 4,268 hrs · 623 cycles

FLT # 7, JFK-LHR. SMOKE FWD CRG DET FAULT AND AFT CRG DEF FAULT AMBER ON UPPER ECAM. STATUS PAGE SHOWS INOP SYS FWD CRG DET AND AFT CRG DET. HAPPENED IN CRUISE FL 330 CIDS 2 & SMOKE STATUS ; TSM 26-16-00-810-809/812-A RESET C/O CIDS-SDF 2 SYS TEST C/O IAW AMM 26-10-00-740-802-A REV AUG 01 2022. MSG'S CLEARED.

Part: CHIP DETECTOR — FALSE INDICATION · airframe 3,557 hrs · 517 cycles

FLT#20, LHR-JFK. (ETOPS) 'ETOPS GROUND VERIFICATION REQUIRED DUE TO CHIP DETECTION MSG ON ENG 2; ENG #2 GROUND VERIFICATION ACCOMPLISHED REF LOG PAGE 3521797, ITEM #1 (HIG POWER ASSURANCE TEST COMPLETED ALL ENG PARAMETERS NORMAL AND FAULTS NOT PRESENT. REF AMM 71-00-00-710-806A. ENG 2 OIL FILTER REEXAMINED AND NO DEFECTS FOUND. REF AMM 79-21-06.) FOR HIGH POWER ASSURANCE TEST. ALL OPS IS NORMAL. OK FOR CONT SERVICE.'

Part: CIDS — FAILED (101RH) · airframe 3,241 hrs · 471 cycles

FLT#44, LGW-JFK. (ETOPS) 'REF MDDR 480639 TSI CIDS FAULTS; REMOVED AND REPLACED D CIDS 1 DIRECTOR IAW AMM 23-73-34. OPS CHECK GOOD.'

Part: NONE — NONE · airframe 3,227 hrs · 469 cycles

FLT#44, LGW-JFK. (ETOPS) 'CLASS II AIR BLEED MESSAGE (36-00-00-C CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY AIR BLEED); PERFORMED OPS CHECK OF BMC 1 AND 2 IAW AMM 36-11-00. TEST OK. CLASS II FAULT MESSAGE NOT PRESENT. MDDR # 481204.' (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)

Part: NONE — NONE · airframe 2,693 hrs · 392 cycles

FLT#43, JFK-LGW. (ETOPS) ' CLASS II MX MESSAGE SMOKE ON SHUTDOWN; PERFORMED TSM 26-17-00 MSG CLEARED.'

Part: CHIP DETECTOR — WARNING MESSAGE · airframe 2,686 hrs · 391 cycles

FLT#44, LGW-JFK. (ETOPS) ' ENG 2 OIL CHIP DETECTED; TROUBLESHOOT PER TSM 79-35-00-810-808-A. INSPECTED ENG 2 MAGNETIC CHIP COLLECTORS, FOUND WITHIN LIMITS. INSPECTED ENG 2 MAIN OIL FILTER ELEMENT, FOUND WITHIN LIMITS. ACCOMPLISH ENG 2 IDLE RUN, NO LEAKS NOTED, AND NO ENG OIL CHIP DETECTED MESSAGE ON PFR. RECERTIFY THE A/C BACK TO ETOPS OPERATIONS.'

Part: NONE — FAILED (6DA1) · airframe 2,548 hrs · 371 cycles

FLT#44, LGW-JFK. (ETOPS). 'AFTER TAKE OFF, ANTI ICE CAPTAIN PITOT. CAPTAIN AOA, CAPTAIN L STAT, AND CAPTAIN R STAT; REMOVED AND REPLACED PHC-1 (6DA1) IAW AMM 30-31-34. OPS CHECK GOOD.'

Part: NONE — NONE (6DA1) · airframe 2,520 hrs · 367 cycles

FLT#44, LGW-JFK. (ETOPS) 'PROBE HEAT COMPUTER P/N 733902-1-2 S/N 733902IN11695 REMOVED FROM POSITION 6DA1 IN SERVICEABLE CONDITION FOR INSTALL ON N4058J ROB AUTHORIZED BY MCC BOB D AOG REQ 1983296 OPENED; PULLED/COLLARED 49 VU PHC 1 CB. RESET CB PHC #1 AT 49VU REF AMM 30-31-34; INSTALLED PHC #1 REF AMM 30-31-34 OPS CHK OK. NO FAULTS NOTED. (SUPPLEMENTAL INFORMATION ADDED TO CORRECT THE A/C SERIAL NUMBER AND TAIL NUMBER).

Part: FIRE DETECTOR — FAILED (NR 2 ENGINE) · airframe 1,355 hrs · 202 cycles

FLT # 7, JFK-LHR. PRIOR TO DEPARTURE ENGINE 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ) ; REF TSM 26-12-00-810-805. INSPECTED FDU #2 LOOP A CONNECTOR, AS WELL AS PYLON, FAN, CORE LOOP A CONNECTOR WITH NO FINDING, FAULT, DID NOT CLEAR PLACED ON MEL 26-12-01-A CAT C MX-4 UPDATED MCC MARIO NOTIFIED PLAACRD INSTALLED FOUND/RAIL ENG #2 AGB LOOPA @FAULT R +R IAW AMM 26-12-17. MSG CLEARED OPS TEST GOOD MDDR CLEARED, PLACARD REMOVED, UPDATED MX 4 UPDATED.

Part: CIDS — FAULTED (NR 1) · airframe 780 hrs · 119 cycles

FLT 44, LGW-JFK. SMOKE LAV DET FAULT. R+R CIDS 1 DIRECTOR IAW AMM 23-73-34, OPS CHECKED GOOD

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL TRANSFER) · airframe 53 hrs · 10 cycles

ETOPS: FLT 7, JFK-LHR. ACT XFR FUEL FAULT; TRANSFERED FUEL PER AMM 28-25-00 - NO FAULTS PRESENT ON ECAM.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL TRANSFER) · airframe 53 hrs · 10 cycles

(ETOPS): FLT 20, JFK-LHR. FUEL ACT XFR FAULT ON CLIMB QRH COMPLIED WITH ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT) ); PERFORMED OPS TEST OF THE ACT AUTO XFER SYSTEM IAW AMM 28-28-00-710-005-A OPS TEST GOOD MDDR CLEARED PLACARDS REMOVED UPDATED MX-4

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL TRANSFER) · airframe 26 hrs · 6 cycles

ETOPS: FLT 7, JFK-LHR. ACT TRANSFER FAULT AFTER FUELING; TRANSFERRED FUEL FROM ACT AFT 2. MSG CLEARED. PERFORMED OPS CHECK IAW 28-28-00. OPS CHECK GOOD.