N4058J

Part: IGNITION SYS — FAULTED (NR 1 ENGINE) · airframe 16,138 hrs · 2,418 cycles

FLT 123, JFK-LAX. (ETOPS) ENG 1 IGN FAULT ( IGNITION SYSTEMS A) SYSTEM A ); REMOVED AND REPLACED ENG 1 IGN A IGNITER PLUG PER AMM 74-21-01. TEST OK NO FAULTS NOTED. THIS CLEARS MDDR 600069 PLACARD REMOVED MX-4 UPDATED. ENGINE: IAE, PW1133GAJM, SERIAL: P772351

Part: ACTUATOR — FAILED (NR 2 COMPRESSOR) · airframe 15,558 hrs · 2,329 cycles

FLT#20, LHR-JFK. (ETOPS) ON APPROACH RECIEVED ENG 2 COMPRESSOR VANE ECAM; REF LOGPAGES 4532479 ITEM 1 AND 2 AND 4532481 ITEM 1 FOR ENG 2 HPC SVA(REMOVED AND REPLACED AND ALL OPERATIONAL CHECKS A/C OK FOR CONT SVCR/R OF ENG 2 HPC SVA REQ PER T/S TSM 75-31-00-810-813/822A; REMOVED AND REPLACED OF ENG 2 HPC SVA IAW AMM 75-31-02 LEAK CHKS GOOD NO FAULTS NOTED.)

Part: COFFEEMAKER — ODOR (ZONE 900) · airframe 15,163 hrs · 2,269 cycles

FLT # 1908. CDG-JFK. (ETOPS) FAS REPORTED TO US THEY NOTICED AN INTERMITTENT BURNING SMELL BETWEEN ROWS 2-8. STARTED RIGHT BEFORE DESCENT. THEY DIDNT NOTICE ANYTHING FROM LAVS AND OVENS.; ACCOMPLISHED INFO NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10(FOUND FWD GALLEY COFFEE POT BURNT(#105). REPLACED COFFEE POT. ALSO ACCOMPLISHED TSM 05-50-00-810-085B AND 05-50-00-810-085D. AC OK FOR SVC

Part: VALVE — FAILED (ZONE 400) · airframe 14,830 hrs · 2,221 cycles

FLT#2260, MAD-BOS. (ETOPS) "FAN AIR VALVE BODY HAS BEEN BROKEN CONNECTING ROD TO ACTUATOR ON #1 ENG; REMOVED AND REPLACED #1 ENG FAN AIR VALVE BODY IAW AMM 36-11-54. OPS CHK AND GROUND VERIFICATION OK."

Part: ACTUATOR — FAILED (BLEED VALVE) · airframe 14,830 hrs · 2,221 cycles

FLT#2260, MAD-BOS. (ETOPS) "FAN AIR VALVE ACTUATOR REQUIRES REPLACEMENT DUE TO BROKEN FAN AIR VALVE BODY CONNECTING ROD #1 ENG; REMOVED AND REPLACED #1 ENG FAN AIR VALVE ACTUATOR IAW AMM 36-11-54. OPS CHK AND GROUND VERIFICATION OK."

Part: HOSE — DAMAGED (ZONE 400) · airframe 14,159 hrs · 2,124 cycles

FLT#1621, LHR-BOS. (ETOPS)' ENG 2 EDP SUCTION HOSE FOUND TO BE DAMAGED DURING ENG 2 LOOP INSP; REMOVED+REPLACED ENG2 EDP SUCTION HOSE IAW AMM 29-11-49; OPS CHECK GOOD AC OK FOR SVC'

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 14,146 hrs · 2,122 cycles

FLT# 1621, LHR-BOS. (ETOPS) 'ENG 2 FIRE LOOP B FAULT (ENGINE FIRE DETECTION SYSTEM 2) LOOP B). REMOVED AND REPLACED ENG #2 CORE AGB LOOP B IAW AMM 26-12-17. REF LOGPAGE 4352300 ITEM #1 BY JB MX. OPS TEST OK. ETOPS GROUND VERIFICATION PERFORMED AMM 26-12-00-710-002A. BITE TEST OK. NO FAULT FOUND. FAULT HAS NOT RETURNED.

Part: FDU — FAULTED (NR 2 ENGINE) · airframe 13,729 hrs · 2,057 cycles

FLT#32, AMS-BOS. '(ETOPS) ' ENG 2 FIRE LOOP B FAULT ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); (RESOLVED ON W/O: 1406593 TASKCARD: NR-00001 ) REMOVED AND REPLACED FDU PER TECH SUPPORT IAW AMM 26-12-34. OPS CHECK NORMAL WITH NO FAULTS THIS ACTION CLEARS MDDR 579863 MX 4 UPDATED PLACARD REMOVED MCC NOTIFIED.

Part: FIRE DETECTOR — SHORTED (NR 1 ENGINE) · airframe 13,672 hrs · 2,049 cycles

FLT#2220, LHR -JFK. (ETOPS) 'ENG 1 FIRE LOOP A CAUTION); T/S PER TSM 26-12-00-810-852-A FOUND CORE AGB LOOP A (4002WD1) SHORTED TO SHIELD. REMOVED AND REPLACED ENG 1 CORE AGB LOOP A IAW AMM 26-12-17. FAULT CLEARED. TEST OK.'

Part: FIRE DETECTOR — FAULTED (ZONE 400) · airframe 13,377 hrs · 2,000 cycles

FLT#20, LHR-JFK. (ETOPS) 'ECAM ENG FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); REF TSM 26-12-00-810-912-A FOUND AGB LOOP A TERMINALS A/C SHORTING TO DETECTOR CASE. REPLACED ENG 1 FIRE LOOP A 4001WD1 IAW AMM 26-12-17. OPS CHK OK. FAULT CLEARED. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.'

Part: SPINNER — DAMAGED (NR 2 ENGINE) · airframe 13,325 hrs · 1,991 cycles

FLT#2288, JFK-AMS. (ETOPS)' ON ENG # 2 SPINNER CONE SHOWS LITTLE COATING MISSING; REMOVED AND REPLACED ENG #2 SPINNER INLET CONE IAW AMM 72-11-01-400-801-A. NO DEFECT NOTED ON SPINNER, MX-4 UPDATED, PLACARD REMOVED, THIS CLEARS MDDR #576332.'

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 12,937 hrs · 1,931 cycles

FLT#2288, JFK-AMS. (ETOPS) 'ENG 1 LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); REF LOGPAGE 4065393, ITEM 2 (REF TSM 26-12-00-810-808-A. FOUND ENG #1 CORE AGB LOOP A SHORTED ON DETECTOR TERMINAL A/C TO OUTER CASE. REMOVED AND REPLACED AGB LOOP A IAW AMM 26-12-17. OPS CHECK GOOD. NO FAULTS PRESENT. MEL REMAINS OPEN TO MONITOR IF FAULT RETURNS.) REMOVED AND REPLACED AGB FIRE LOOP OPS CHECK OK. FAULT HASN'T RETURNED SINCE R+R DATED 02-03-25.

Part: CIRCUIT BREAKER — TRIPPED · airframe 12,815 hrs · 1,909 cycles

FLT#1515, JFK-SFO. 'SHORTLY AFTER TAKEOFF RECEIVED ECAM MSG ANTI ICE CAPT TAT STS DISPLAYS CAPT TAT INOP; CHECK TAT PHC 1 PFR HIT ON PHC 1 FOUND TAT 1 C / B Z12 OUT-RESET C / B Z12 BITE CHECKED PHC 1 TEST OK--- MONITORED TAT 1 C / B REMAINED IN--- NO HISTORY IAW AMM 30-31-710-001 . GROUND VERIFICATION FOR CAPTAIN TAT SATISFACTORY.'

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 12,808 hrs · 1,907 cycles

FLT#1621, LHR-BOS. (ETOPS) ' FOUND HARNESS ELECTRONIC CONTROL (WC08) CHAFFED AND BURNT; REMOVED AND REPLACED WCO8 HARNESS IAW AMM 73-21-68. OPS CHECK GOOD.'

Part: TUBE — DAMAGED (NR 2 EEC) · airframe 12,809 hrs · 1,908 cycles

FLT#8363, BOS-JFK. (ETOPS) ' UPON INSP OF #2 ENG FOUND EEC SENSING TUBE DAMAGED; REPLACED SENSE LINE REF AMM 73-21-49 OK FOR CONT SVC.'

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 12,808 hrs · 1,907 cycles

FLT#1621, LHR-BOS. (ETOPS). 'PFR- 73-11-01 ENG1D-0720-BDCU TEST ABORT COUNT WARNING 78-00 ENG 1 HEAT SYS DOWNGRADED (REPORTED IN BOSTON) ( HEAT SYS DEGRAD CAUTIONS ON ECAM E/WD ); INATALLED NEO INTEGRATED FUEL PUMP AND CONTROL UAW AMM 73-11-01 OPS CHECK GOOD. MX UPDATED REF 4219707, ITEM 2 (571375 FOR CONTINUE OF INSTALLATION.) FOR REMOVAL .'

Part: FCU — FAILED (2CA) · airframe 12,669 hrs · 1,886 cycles

FLT#948, LAS-JFK. (ETOPS) 'FCU RIGHT CRTR BOTTOM DAMAGE; REMOVED AND REPLACED FCU AS PER AMM 22-81-12 OPS CHECKED OK.'

Part: FIRE LOOP — FAULTED (ZONE 400) · airframe 12,162 hrs · 1,903 cycles

FLT#1915, JFK-SFO. (ETOPS) 'POST FLIGHT, ENG 1 FIRE LOOP A FAULT. INFO NOTED DUE TO ENG #1 LOOP A FAULT MEL RE-APPLY 26-12-01A SEE LOGPAGE 4110407-1. R/R 4181KS ENG 1 LOOP A GREEN HI-TEMP HARNESS, R/R 4181KS ENG 1 LOOPA WHITE HI-TEMP HARNESS, R/R 4182KS ENG 1 LOOP A RED HIGH TEMP HARNESS, R/R 4182KS GREEN HI-TEMP HARNESS IAW AMM 26-12-61, R&R 4001WD1 ENG 1 LOOP A CORE VENT DETECTOR & 4002WD1 ENG 1 LOOP A CORE AGB DETECTOR REF AMM 26-12-17, R/R 31WD1 & 32WD2 ENG 1 LOOP A PYLON HIGH TEMP HARNESS REF AMM 26-12-63, AFTER ACCOMPLISH OF TSI, HARD FAULT FOR ENG 1 LOOP A ON ECAM, PIN J/K AT FDU 2WD1 CONNECTOR READS 12 OHMS. PERFORMED OPS TEST OF IGN SYS PER AMM 74-00-00 OPS CHK OK.

Part: A/C PACK — ABNORMAL (UNKNOWN) · airframe 12,217 hrs · 1,814 cycles

FLT#2010, LAX-PBI. 'FUME EVENT "DIRTY SOCK" SMELL INFLIGHT REPORTED SMELL ON APPROACH WHEN LDG GEAR WAS EXTENDED; COMPLIED WITH INFORMATIION NOTICE 2017-T015 SEAT B2 IDENTIFIED ODOR AS TRANSIENT. LEVEL DECONTAMINATION ACCOMPLISHED PER TSM 21-00-00-615 AIRCRAFT OK FOR SERVICE.'

Part: CONTROL PANEL — FAULTED (FIRE DETECTION) · airframe 12,065 hrs · 1,785 cycles

FLT#33, BOS-CDG. (ETOPS) 'ENG 1 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: FIRE LOOP — FAULTED (ZONE 400) · airframe 11,955 hrs · 1,765 cycles

FLT#1107, JFK-LHR. (ETOPS) ENG 1 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); MCC MONITORED A/C FOR ENG # 1 FIRE LOOP A FAULTS, NO FAULTS SINCE INITIAL HIT ON 11/02/24. OPS TEST GOOD REF AMM 26-12-00 MDDR CLEARED PLACARD REMOVED UPDATED MX-4.

Part: RADAR — FAILED (WX RADAR) · airframe 11,906 hrs · 1,758 cycles

FLT#1621, LHR-BOS. (ETOPS) 'CIDS 2 MAINTENANCE MESSAGE; ITEM ALREADY DEFERRED, REF LOG PAGE 4170932, ITEM 1 (REMOVED AND REPLACED GPWC IAW AMM 34-48-34. OPS CHECK GOOD. LATEST SOFTWARE (642) INSTALLED).'

Part: LIMITER — FAILED (BATTERY) · airframe 11,866 hrs · 1,752 cycles

FLT#32, AMS-BOS. (ETOPS) 'ELEC BCL 1 FAULT; REMOVED AND REPLACED BCL #1 PER AMM 24-38-34-000-001-A ALL OPS CHECK GOOD ACCOMPLISHED ETOP'S GROUND VERIFICATION TEST PER 24-38-00-710-001-A BITE TEST.'

Part: UNKNOWN — ODOR (CABIN) · airframe 11,793 hrs · 1,742 cycles

FLT#2220, LHR-JFK. 'INTERMITTENT RUBBER SMELL COMING FROM COCKPIT AND FORWARD GALLEY; INSPECTION OF F/D + FWD D1L AREA C/OUT AND INSPECTIONS OF AVIONICS BAY AND AVIONICS VCENT AREAS DUE TO SUSPICION OF BURNING RUBBER ODOR. NO EVIDENCE OF FAILED EQUIPMENT OF BURNING IN INSPECTION FOUND IAW AMM TSM 24-00-00-810-823-A. A/C SATIS FOR CONT'D SERVICE.'

Part: UNKNOWN — ODOR (CABIN) · airframe 11,530 hrs · 1,701 cycles

FLT#8668, JFK-JFK. ' LEVEL 2 ODOR EVENT; ACCOMPLISHED LVL 2 DECONTAMINATION PER AMM 21-00-00-615-803A POSSIBLE SOURCE WAS ENG 2 PEROREMED NO TRACES OF OIL FOUND REF LP 4142794, ITEM #1 (PER AMM 72-31-00-290-802/803 PERFORMED BSI ON #2 ENG HPC 2-3/HPC-2 WEEP HOLES NO SIGNS OF OIL) ENG 1 BORO PERFORMED LP 4142796 (PER AMM 72-31-00-290-802 PERFORMED BSI PN #1 ENGINE LPC 2,3 / HPC 2 WEEPHOLES NO SIGN OF OILS) NEITHER ENGINE SHOWED SIGNS OIL CONTAM APU GVI PERFORMED NO TRACES OF OIL LP 4142792 ITEM 2 ECS AND PACK BURNED PERFORMED NO ODOR PRESENT. '

Part: COMPUTER — FAILED (1HA1) · airframe 11,529 hrs · 1,700 cycles

FLT#8417, BOS-JFK. (ETOPS) 'BMC1 FUNCTIONAL TEST NOT RESPONDING; REMOVED AND REPLACED BMC1 COMPUTER IAW AMM 36-11-00. OPS CHECK GOOD. A/C OK FOR CONT SVC.'

Part: TRANSDUCER — FAULTED (BLEED AIR) · airframe 11,529 hrs · 1,700 cycles

FLT#8417, BOS-JFK. (ETOPS) 'REF W/O 1360802 TSI- 67847-1 NR-00001 THA1 XDCR REQUIRES REMOVAL AND REPLACEMENT; REMOVED AND REPLACED 7HA1 BLEED PRESS XDCR IAW AMM 36-11-15. REQUIRES LEAK CHECK AND BITE TEST.'

Part: SENSE LINE — FAILED (ZONE 400) · airframe 11,530 hrs · 1,701 cycles

FLT#8417, BOS-JFK. (ETOPS) 'REF MDDR 561406 (REF LP 4142783-2 *** EVF FLIGHT UNSUCCESSFUL** DUE TO AIR BLEED CLASS II MX MESSAGE . ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY AIR BLEED )) CLASS II AIR BLEED; R/R SENSE LINE FROM 7HA1 IAW AMM 36-11-86 AND REMOVED AND REPLACED FLEX LINE PRV ECS SENSE LINE IAW AMM 36-11-49. LEAK CHECK GOOD, HOWEVER FURTHER T/S REQ. REF L/P 4142786 ITEM 1 (DURING LEAK CHKS FOUND BLEED LEAK COMING FROM TUBE ASSY - ECS - SENSE PYLON-HPV. REMOVED SENSE LINE IAW 36-11-86. REQ'S INSTALLATION , OPS CHECK AND LEAK CHECK. WORK ON GOING) AND ITEM 2 (INSTALLED TUBE ASSY ECS SENSE PYLON HPV IAW AMM 36-11-49. PERFORMED ENG IDLE RUN IAW AMM 71-00-00. NO LEAKS NOTES. NO CLASS II MSG'S NOTED. NO FAULTS NOTED. AS PRECAUTIONARY, PERFORMED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00. NO DEFECTS , FAULTS NOTED. ALL PARAMETERS OK.) .

Part: COMPUTER — FAILED (1HA2) · airframe 11,529 hrs · 1,700 cycles

FLT#8417, BOS-JFK. (ETOPS) 'BMC FUNCTIONAL TEST NOT RESPONDING; REMOVED AND REPLACED BMC2 COMPUTER IAW AMM 36-11-00. OPS CHECK GOOD. A/C OK FOR CONT SVC.' (SUPPLEMENTAL ADDED TO CORRECT DESCRIPTION)

Part: COMPUTER — FAILED (1HA2) · airframe 11,529 hrs · 1,700 cycles

FLT#8417, BOS-JFK. (ETOPS) 'BMC1 FUNCTIONAL TEST NOT RESPONDING; REMOVED AND REPLACED BMC2 COMPUTER IAW AMM 36-11-00. OPS CHECK GOOD. A/C OK FOR CONT SVC.'

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 11,520 hrs · 1,698 cycles

FLT#1621, LHR- BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LHR). 'AIR ENG 1 BLEED FAULT APPEARED SHORTLY AFTER TAKE OFF . FOLLOWED SOP AND QRH PROCEDURES ATTEMPTED ONE RESET PER FCOM 1 MESSAGE REMAINED . COULD NOT CONTINUE TO ETOPS FLT AND RETURNED TO LAND AT DEPARTURE AIRPORT. ( BLEED AIR SUPPLY SYSTEMS ) ( HIGH PRESSURE VALVES (HPV) ); REMOVED AND REPLACED #1 ENG HP VALVE IAW AMM 36-11-41. OPS CHECK/ LEAK CHK GOOD. MX-4 UPDATED. PLACARD REMOVED.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 10,611 hrs · 1,563 cycles

FLT#1107, JFK-LHR. (ETOPS) ' ENGINE 1 FIRE LOOP FAULT CAME ON 3 TIMES DURING FLIGHT FOR AN INSTANT. ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); FOUND CORE AGB LOOP A (4002WD1) DEFECTIVE AFTER FOLLOWING TSM 26-12-00-810-803-A. REPLACED CORE AGB LOOP A (4002WD1) IAW AMM 26-12-17, OPS CHECK OK. THIS CLEARS MDDR, PLACARD REMOVED, MX-4 UPDATED. A/C OK TO CONTINUE SERVICE.

Part: CONTROL LEVER — UNKNOWN · airframe 10,534 hrs · 1,552 cycles

FLT#44, LGW-JFK. (ETOPS). ;CLASS 2 MAINT MSGF FUEL ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY FUEL ); TROUBLESHOT PER TSM 28-46-00-810-818A, NO FAULTS NOTED ON FUEL TRANSFER, REMOVED AND REPLACED FLSCU 1 IAW AMM 28-46-34. NO FAULTS NOTED. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.

Part: FDU — FAULTED (NR 1 ENGINE) · airframe 10,520 hrs · 1,550 cycles

FLT#2289, AMS-JFK. (ETOPS) 'ENG #1 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); PERFORMED TSM 26-12-00-810-803-A. NO HARD FAULTS ON ECAM FAULT. PERFORMED GVI ON LOOPS, NO DEFECTS NOTED. PERFORMED RESISTANCE CHECK ON FDU BETWEEN JULIET AND KILO. RESISTANCE AT 1.4 KILO OHMS. WITHIN LIMITS. REPLACED FDU AS PRECAUTIONARY IAW AMM 26-12-34. OPS CHECK NORMAL.

Part: HYDRAULIC LINE — LEAKING (NR 2 HYD) · airframe 10,506 hrs · 1,548 cycles

FLT#1621, LHR-BOS. (ETOPS) 'HYD LINE ON ENG #2 EDP LEAKING FLUID; REPLACED ENG #2 HYD EDP SUCTION HOSE IAW AMM 29-13-49. OPS CHECK GOOD. NO LEAKS NOTED.'

Part: CONTROLLER — FAILED (FUEL) · airframe 10,372 hrs · 1,528 cycles

FLT#2289, AMS-JFK. (ETOPS) 'JUST PRIOR TO PUSH FUEL ACT XFER FAULT ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ); TSM TASK 28-51-00-810-808-A CARRIED OUT REMOVED AND REPLACED AFMC (2QN) IAW AMM 28-51-35. SYSTEM TEST OK THIS CLEARS THE MDDR MX-4 UPDATED. PLACARD REMOVED.'

Part: FIRE DETECTOR — FAILED (ZONE 400) · airframe 10,198 hrs · 1,501 cycles

FLT#43, JFK-LGW. (ETOPS) 'ENG 1 FIRE LOOP A FAULT ECAM DURING CRUISE ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); FOUND BREAK IN ENG 1 AFT CORE FIRE LOOP A. REMOVED AND REPLACED AFT CORE LOOP A IAW AMM 23-12-17. OPS CHECK OK. MX-4 UPDATED PLACARD REMOVED, MDDR CLEARED.

Part: DATA UNIT — FAILED (1TX1) · airframe 10,178 hrs · 1,498 cycles

FLT#2104, BOS-LGW. (AIRCRAFT DIVERTED TO JFK) 'ENROUTE TO LGW CPDLC FAILED MSG WAS DATA LINK ASTU FAULT UNABLE TO RESET.ALSO VHF 3 SHOW --- IN FREQUENCY WIWOOW NOT DATA.VHF 3 VOIC WAS OPERATIONAL; REMOVED AND REPLACED ATSU IAW AMM 46-21-00. PERFORMED ASTU UPLOAD ALL OPS NORMAL NO FAULT FOUND.

Part: VALVE — FAULTED (AIR TRIM) · airframe 10,099 hrs · 1,486 cycles

FLT#2288, JFK-AMS. (ETOPS) 'ON TAXI OUT COND TRIM AIR SYS FAULT COCKPIT TRIM AIR VALVE ( HOT AIR PRESS REGUL VLV - N703 AND UP, OPEN POSITION; REMOVED AND REPLACED TRIM AIR VALVE 11HK IAW AMM 21-63-51.OPS CHECK GOOD. THIS CLEARS MDDR MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED

Part: BLADE — FAILED (NR 1 ENG FAN) · airframe 9,685 hrs · 1,427 cycles

FLT#1408, CDG-JFK. (ETOPS) FOUND NR 1 ENGINE FAN BLADE S/N JB1AEA1140 DAMAGED AND OUT OF LIMITS. REMOVED AND REPLACED NR 1 ENG FAN BLADE #8 IAW AMM 72-11-03. REF LP 3982379, ITEM #2 FOR REQUIRED ENG RUNS.

Part: SLIDE RAFT — FAILED (R1 DOOR) · airframe 8,801 hrs · 1,301 cycles

FLT#2288, JFK-AMS. 'UNABLE TO ARM R1 DOOR AFTER 4 HRS CHECK. (PRECAUTIONARY 4HRS FAIL, HANDLE DON'T GO DOWN ALL THE WAY); REMOVED AND REPLACED R1 DOOR SLIDE ESCAPE IAW AMM 25-62-44. BLEW OUT GIRT BAR ATTACHING POINTS 4 MECHANISUM FOR POSSIBLE MOSITURE BUILD UP AND LUBRICATED FITTINGS. OPS CHECK GOOD AT THIS TIME REF L/P 3884567, ITEM #1 FOR VERIFICATION OF DOOR ARMING WITHNIN NEXT 4 HRS.'

Part: DEU — FAILED (UNKNOWN) · airframe 8,483 hrs · 1,256 cycles

FLT#20, LHR-JFK. (ETOPS) 'FAP CAUTION LIGHT ( CIDS SYSTEM - CIDS DEU B ); REMOVED AND REPLACED DEU FIN 300RH8 PER AMM 23-73-47. OPS CHECK GOOD AT THIS TIME. MX-4 UPADTED. PLACARD REMOVED.

Part: SENSOR — FAILED (CABIN TEMP) · airframe 8,476 hrs · 1,255 cycles

FLT#007, JFK-LHR. (ETOPS) 'AIR PACK 2 REG FAULT AFTER TAKEOFF ( ECAM INDICATION ON BLEED PAGE PACK COMPRESSOR OUTLET TEMPERATURE ); REMOVED AND REPLACED PACK 2 COMPRESSOR TEMP SENSOR IAW AMM 21-61-11. OPS CHECK GOOD. MDDR CLEARED. MX-4 UPDATED. PLCRD RMVD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,896 hrs · 1,025 cycles

FLT#2220, LHR-JFK. (ETOPS) 'COCKPIT TEMP. THE CONTROL NOT WORKING PROPERLY. TEMP IS ERRATIC, PRIMARILY TOO COLD, BUT AT TIMES OVER-CORRECTS TO TOO HOT; FOUND OBSTRUCTION OF COCKPIT TEMP. SENSOR. CLEARED AS REQUIRED. OPS CHECK GOOD PER AMM 21-63-00.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,650 hrs · 989 cycles

FLT#1621, LHR-BOS. (ETOPS) FUEL ACT XFR FAULT ((MEL 28-40-09I CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT). REMOVED AND REPLACED ACT VENT VALVE ACTUATOR (91QH) IAW AMM 28-28-72. PERFORMED OPS TEST OF THE ACT AUTOMATIC TRANSFER SYSTEM IAW AMM 28-28-710-005-A. ALL OPS TESTS OK. NO FAULTS NOTED. A/C RETURNED TO THE ORIGINAL GROUND CONFIGURATION. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.

Part: UNKNOWN — FAILED (UNKNOWN) · airframe 6,589 hrs · 980 cycles

FLT#43, JFK-LGW. (ETOPS) 'WXR R/T #1 FAILED INFLIGHT ( WEATHER RADAR SYSTEMS ). REPLACED TRU TRANSMITTER RECEIVER UNIT FIN 135QI. PER MM 34-41-51. OPS CHECK OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,394 hrs · 952 cycles

FLT#1107, JFK-LHR. (ETOPS) 'FUEL ACT TRANSFER FAULT ON ECAM ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT) ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: PUMP — FAILED (APU) · airframe 6,361 hrs · 947 cycles

FLT#020, LHR-JFK. (ETOPS) 'APU CLASS II MX MESSAGE ON ECAM STATUS PAGE. ( CLASS II MAINTENANCE MESSAGES DISPLAYED ); REMOVED AND REPLACED APU FUEL PUMP 4QC PER AMM 28-22-51. THE OPS CHECK IS GOOD. MDDR CLEARED. MX-4 UPDATED, PLACARD REMOVED. REPLACED RELAY 9QC PER ESPM 20-46-50.'

Part: EEC — FAULTED (ENGINE-1) · airframe 5,591 hrs · 892 cycles

FLT#2220, LHR-JFK. (ETOPS) '#1 ENG EEC P/N 1020420-2-120 S/N 5007902 REMOVED AMM 73-21-00. FOR ENGINE ONE FAULT AND AIR TURBINE COOLING FAULT; INSTALLED NEW EEC ON #1 ENGINE IAW AMM 73-21-01 OPS TEST GOOD.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,591 hrs · 892 cycles

FLT#2220, LHR-JFK. (ETOPS) 'ON TAKEOFF AND CLIMB RECVD ENG 1 HIGH VIBRATION WITH A MAX N2 VIBE OF 6.4 ECAM CLEARED WHILE CLIMBING THROUGH FL 170. REMOVED AND REPLACEMENT OF #1 ENG ACCOMPLISHED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,450 hrs · 812 cycles

FLT#1107, JFK-LHR. (ETOPS) 'HYD RAT FAULT CAME ON AS AC ENGINE WERE SHUTDOWN WHEN BLOCKING IN ( ECAM WARNINGS & CAUTIONS 8) RAT FAULT ); REMOVED AND REPLACED RAT PRESSURE SWITCH PER AMM 29-22-53. OPS CHECK & LEAK CHECK ARE GOOD. THIS CLEARS MDDR # 506076. MX-04 UPDATED. PLACARD REMOVED. MCC NOTIFIED.'

Part: NONE — FAILED (5QT) · airframe 5,035 hrs · 750 cycles

FLT#43, JFK-LGW. (ETOPS) 'DURING AIRCRAFT REFUELING RECEIVED FUEL ACT XFR FAULT ACT TANKS LOADED EVENLY -NOT ACCORDING TO NORMAL DISTRIBUTION ( FUEL QUANTITY PRESELECTOR SYSTEM ); REMOVED AND REPLACED FUEL QUANTITY PRESELECTOR (5QT) IAW AMM 28-42-21. OP'S CHECK IS GOOD. MDDR CLEARED.'

Part: OUTFLOW VALVE — FAILED (NOT ENTERED) · airframe 4,788 hrs · 715 cycles

FLT#2144, LGW-JFK. (ETOPS) 'ON COCKPIT POWER UP ECAM: AVIONICS VENT FAULT. UNABLE TO RESET. FOUND SKIN AIR OUTLET VALVE SEIZED IN OPEN POSITION. UNABLE TO SECURE VALVE CLOSE; REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM 21-26-53. OP'S CHECK IS GOOD. A/C OK FOR SERVICE.

Part: INDICATOR — FAILED (22FN) · airframe 3,895 hrs · 587 cycles

ETOPS FLT # 44, LGW-JFK) STDBY ATTITUDE INDICATOR (ISIS) AIRSPEED INDICATION SLOW (LAGGED) DURING INITIAL TAKE OFF ROLL. CA+ FO AIRSPEEDS WERE INDICATING 53 KTS WHEN ISIS STARTED REGISTRING 40 KTS ISIS QUICKLY JUMPED UP TO 20 70 KTS TO MATCH CA+ FO AFD. ISIS AIRSPEED WORKED NORMALLY REMAINDER OF FLIGHT. IT IS NOTE WORTHY THAT WINDS WERE APPROX 60 DEGREES LEFT OF NOSE AT 21 GUSTING 30 KTS. VERY ROUGH AIR WITH MODERATE RAIN. RECOMMEND BLOWING OUT PITOT STATICS AS A PRECAUTION.; T/S NOT DUPLICATE FAULT. R/R'D ISIS IND. PRECAUTIONARY. REFER AMM 34-22-25. PERFORMED PITOT/ STATIC PUMP UP REF AMM 34-13-00 AND 34-22-25. NO LEAKS NOTED. ALL PITOT AND STATIC VALUES VALUES WITHIN TOLERANCE. A/C OK FOR SERVICE. (SUPPLEMENTAL INFORMATION FOR ETOPS ACKNOWLEDGEMENT)

Part: ENGINE — FAILED (ENGINE-1) · airframe 3,328 hrs · 498 cycles

FLT#8351, BOS-JFK. (ETOPS) '#1 ENG NEEDS TO BE REMOVED SERVICEABLE DUE TO CONUS RESTRICTION; PER WO#1204304, REMOVED AND REPLACED ENGINE #1. '

Part: NONE — NONE · airframe 3,137 hrs · 469 cycles

FLT#44, LGW-JFK. (ETOPS) 'AIR PACK 2 REGULATOR FAULT UPON SHUTDOWN; PERFORMED AIR CONDITIONING TEMP CONTROL TEST REF AMM 21-63-00 TEST OK, PACK #2 OPERATES NORMAL, MSG NO PRESENT. '

Part: COMPUTER — FAULTED · airframe 3,110 hrs · 465 cycles

FLT#44, LGW-JFK. (ETOPS) 'CREW REPORTS FMGC 1 FAULTED IN FLIGHT; PERFORMED AFS TEST AND LAND CAT II TEST PER AMM 22-01-00. OPS CHECK IS GOOD. NO FAULTS NOTED.'

Part: NONE — FAILED (ENGINE-2) · airframe 2,752 hrs · 411 cycles

FLT#44, LGW-JFK. (ETOPS) ' REF TSI ON WO 1190881, REPLACE N1 SPEED PROBE; REMOVED AND REPLACED OF ENG 2 N1 SPEED PROBE IAW AMM 77-11-21. SEE L/P 3389619 (ACCOMPLISHED OP'S CHECK OF N1 SPEED SENSOR IAW AMM 77-11-21-720-050-A. OP'S CHECK OK FOR CONTINUED SERVICE.) FOR OPS CHECK.' (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)

Part: EEC — FALSE INDICATION · airframe 2,752 hrs · 411 cycles

FLT#44, LGW-JFK. (ETOPS) ' REF WO# 1190881 NR-00001 EEC WO3 HARNESS WAS REMOVED AND ROUTED IN PLACE PER AMM 73-21-63-400-802-A INSTALLATION CONTINUATION REQUIRED; FINALIZED HARNES CONNECTIONS (WO3 HARNESS) TO BIFI PER AMM SUBTASK 73-21-63-420-052-13. PART A (3) (F) REQ. REF TEM 2 FOR CONTINUATION OF LOG PAGE 3389617 (INSTALLED ENG 2 LOWER BIFI IAW AMM 72-21-11-400-801-A. REF LOG PAGE 3389618, ITEM 1 (INSTALLED SEALANT, BOLT AND BUSHING, AND SAFETIED LOWER BIFI ASSV IAW AMM 72-21-11-400-801-A.) FOR CONTINUATION. PERFORMED OPS TEST NO. 7 PER 73-21-63-400-802-A. TEST OK.).

Part: NONE — NONE · airframe 2,503 hrs · 375 cycles

FLT#20, LHR-JFK. (ETOPS) ' CABIN CREW UNABLE TO ARM SLIDE ON DOOR 2R; PERFORMED OP CHECK OF DOOR 2R IAW 52-13-00. REV 01 FEB 2022 OPS SATIS.'

Part: NONE — FAILED (6DA1) · airframe 2,100 hrs · 317 cycles

FLT#20, LHR-JFK. (ETOPS) 'ANTI ICE: CA TAT ECAM; REPLACED PHC#1 REF AMM 31-30-34. OPS CHECK OK.

Part: NONE — NONE · airframe 1,863 hrs · 283 cycles

FLT#20, LHR-JFK. (ETOPS) ' AIR PACK 1 REGULATOR FAULT IN FLIGHT (PACK COMPRESSOR OUTLET TEMP IND-BLEED PG).' (SUPPLEMENTAL TO FOLLOW)

Part: NONE — NONE · airframe 1,212 hrs · 191 cycles

(ETOPS) FLT # 20, LHR-JFK. TEMPERATURE IS DROPPING TO 60 IN ALL ZONES WHEN PACK IS ON LOW OR MEDIUM . INCREASES TO SELECTED TEMPERATURE ON HIGH; PERFORMED OPS TEST OF COCKPIT + CABIN TEMP CONTROL WITH CFDS/MCDU IAW AMM 21-63-00-710-004-A TEST PASSED. NO FAULTS NOTED. ABLE TO CONTROL CABIN TEMP WITH NO ISSUES. NO FAULTS REPORTED BY THE MCDU IN THE LAST LEG + PREVIOUS LEG REPORTS. NO CLASS 3 FAULTS. PER TSM 21-63-00-810-822-A PERFORMED OPS CHECK OF TEMP CTRL WITH MCDU PER AMM 21-60-00-710-004. NO FAULTS FOUND. ALL OPERATION + INDICATIONS NORMAL. ABLE TO CONTROL + VERIFY TEMPERATURES. TEMP CTL TEST PASSED. LAST LEG + PREVIOUS LEG REPORTS INDICATE NO FAULT. ALL INDICATED PRESSURES + TEMPS NORMAL (SUPPLEMENTAL FOR ADDITIONAL INFORMATION AND TO PROBLEM DESCRIPTION)

Part: IGNITION SWITCH — FAILED (#1 ENG) · airframe 913 hrs · 149 cycles

FLT #20, LHR-JFK. ENG 1 HUNG START; REMOVED & REPLACED IGNITER PLUG FOR IGNITION A ON #1 ENG. ENGINE RAN 3 TIMES ALL SUCCESSFULLY PER AMM 74-21-01. OK FOR CONT SERV REF AMM 71-00-00 FOR RUN

Part: GENERATOR — FAILED (APU) · airframe 913 hrs · 149 cycles

FLT # 20, LHR-JFK. NO POWER FROM APU GENERATOR; R/R APU GENERATOR REF AMM 24-23-51. OPS CHECK NML. OK FOR SVC

Part: ENGINE — FALSE INDICATION (#1) · airframe 913 hrs · 149 cycles

FLT # 20, LHR-JFK. HUNG START ENG 1 ; PERFORMED TSM 71-00-00-810-865-A. NO FAULTS FOUND. NO MESSAGES GENERATED AFTER ENGINE STARTS. OK FOR CONT SVC

Part: ENGINE — HOT START (LEFT) · airframe 913 hrs · 149 cycles

FLT# 20, LHR-JFK. HOT START NO INDICATION EGT OVERTEMP NO INDICATION AVIED BY AC TO THE LEFT THAT ENG 1 ON FIRE TAIL FOLLOWED BY INITIAL. ON FIRE INDICATION, FIRED BOTTLE ; REF LOGPAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-210-817-A TO COMPLETION. NO DEFECTS NOTED AT THIS TIME. PERFORMED TSM 71-00-00-810-861-A.NO MESSAGES PRODUCED AFTER ENG IDLE RUN. OK FOR CONT. SVC AT THIS TIME.REF LOG PAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-210-817-A TO COMPLETION. NO DEFECTS NOTED AT THIS TIME. PERFORMED TSM 71-00-00-810-861-A.NO MESSAGES PRODUCED AFTER ENG IDLE RUN. OK FOR CONT. SVC AT THIS TIME.REF AMM 72-00-00-210-817A C/W ALLL TASK UP TO STEP 5 NO DEFECTS FOUND REF AMM 70-27-00-910-806A NO DEFECTS FOUND. REMOVED AND REPLACED #1 ENG FOR EXT BOTTLE #1 CARTRIDGE IAW AMM 26-21-41-000-004-A-C + 26-21-41-400-004-C ALL CHECKS GOOD. INSTALLED ENG 1 FIRE EXT. BOTTLE #1 IAW AMM 26-21-41-400-001-E. REF LOG PAGE 3277497 ITEM #2 FOR CORRESPONDING SQUIB/CARTRIDGE. ALL CHECKS GOOD.

Part: ENGINE — HOT START (NR 1) · airframe 913 hrs · 149 cycles

FLT# 20, LHR-JFK. HOT START NO INDICATION EGT OVERTEMP NO INDICATION AVIED BY AC TO THE LEFT THAT ENG 1 ON FIRE TAIL FOLLOWED BY INITIAL. ON FIRE INDICATION, FIRED BOTTLE ; REF LOGPAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-210-817-A TO COMPLETION. NO DEFECTS NOTED AT THIS TIME. PERFORMED TSM 71-00-00-810-861-A.NO MESSAGES PRODUCED AFTER ENG IDLE RUN. OK FOR CONT. SVC AT THIS TIME.REF LOG PAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-210-817-A TO COMPLETION. NO DEFECTS NOTED AT THIS TIME. PERFORMED TSM 71-00-00-810-861-A.NO MESSAGES PRODUCED AFTER ENG IDLE RUN. OK FOR CONT. SVC AT THIS TIME.REF AMM 72-00-00-210-817A C/W ALLL TASK UP TO STEP 5 NO DEFECTS FOUND REF AMM 70-27-00-910-806A NO DEFECTS FOUND. REMOVED AND REPLACED #1 ENG FOR EXT BOTTLE #1 CARTRIDGE IAW AMM 26-21-41-000-004-A-C + 26-21-41-400-004-C ALL CHECKS GOOD. INSTALLED ENG 1 FIRE EXT. BOTTLE #1 IAW AMM 26-21-41-400-001-E. REF LOG PAGE 3277497 ITEM #2 FOR CORRESPONDING SQUIB/CARTRIDGE. ALL CHECKS GOOD.

Part: CIDS — FAILED · airframe 861 hrs · 142 cycles

(ETOPS) FLT 7, JFK-LHR. ECAM STATUS PAGE SHOWS SMOKE FWD CARGO INOP SMOKE AFT CARGO INOP STATUS MESSAGE CIDS 2 SMOKE; PER SHOWS 23-73-34 DIR 2 (102RH) SDF2 (102RH) AS PER MCC INSTRUCTIONS CIDS DIRECTOR RESET & TEST IAW TSM 26-16-00-810-821-A REV 01 NOV 2021 TEST OK OPS CHK OF FWD & AFT CARGO SMOKE DET C/O IAW AMM 26-16-00-710-802-A REV 91 TEST OK ALL MESSAGE NOW CLEARED. COMPLETED ON WORK ORDER 1154724 TSI 39811 FOLLOWING INSTRUCTIONS AS SO. PLEASE ASSIGN TO JFK AFTER FLIGHT 20 WHERE PART IS AVAILABLE. 2. REMOVE AND REPLACE # 2 CIDS DIRECTOR AS PER AMM 23-73-34. 3. PLEASE REFER TO ALL AMM / GMM FOR ALL REQUIRE DOCUMENTATION IN THE A/C LOG BOOK AND TRAX. R/R CIDS #2 DIR. IAW AMM 23-73-34.(ADDITIONAL SUPPLEMENTAL INFORMATION IN DESCRIPTION)

Part: SENSOR — FAILED (ENGINE-2) · airframe 580 hrs · 101 cycles

(ETOPS) FLT # 44, LGW-JFK. ENG 2B-0448-N1 SPEED SNSR FAIL ; RAR ENG#2 N1 SPEED SNSR IAW EMM TASK 77-11-21-520-000. PERFORMED OPS CHK BY ENG#2 IDLE RUN IAW AMM 71-00-00. OPS CHK GOOD. NO FAULTS PRESENT. RAR SNSR PER MCC JAIME #17939 REQUEST

Part: FCU — FAULT MESSAGE · airframe 409 hrs · 76 cycles

FLT 20, LHR-JFK. "AUTO FLT FCU 1 FAULT" ECAM MSG ON DESCENT TROUGH 10,000 FT. ; TROUBLESHOT PER TSM 22-81-00-810-802-A. R/R FCU PER AMM 22-81-12. ALL FUNCTIONAL TESTS PASSED AT THIS TIME. TSI C/W.

Part: SENSOR — FAILED (NR 1 ENG N1) · airframe 213 hrs · 45 cycles

FLT 2824, LAX-JFK. ENG FADEC 1 CAME ON INFLIGHT FOR ABOUT 3 MINUTES. NO OTHER UNUSUAL PARAMETERS; PERFORMED TROUBLESHOOTING PER TSM 77-11-00-710-057-A NO FAULTS FOUND. NO MAINTENANCE MESSAGE ON MCDU EXAMINED HARNESS. NO FAULTS FOUND. OK FOR CONT SVC. TROUBLESHOT PER TSM 77-11-00-810-808A NO DAMAGE TO W03 HARNESS FOUND. R/R N1 PROBE (4046KS) PER AMM 77-11-21. OPS CHKS PASSED. NO DEFECTS AT THIS TIME P1 TSI – ENG 1 FADEC SYS FAULT ***ETOPS SIG SYSTEM*** THE AIRCRAFT HAS A HISTORY OF ENG 1 FADEC FAULTS WITH THE FOLLOWING FAULT IN AIRMAN // ENG1B-0448-N1 SPEED SNSR FAIL //. PRIOR T/S STATS HARNESS WAS INSPECTED AND NO FAULTS FOUND. REF TSM 77-11-00-810-808-A N1 SENSOR ELECTRICAL FAILURE B. VERIFY THERE IS NO DAMAGE TO THE W03 HARNESS IF NONE IF FOUND REPLACE THE N1 PROBE (4046KS) PER AMM 77-11-21. DUE TO PREVIOUS WRITEUPS AND INABILITY TO VERIFY THIS CONDITION ON THE GROUND A ETOPS VERIFICATION FLIGHT IS REQUIRED PER GMM 17.5.3. UPON COMPLETION OF THIS TSI CONTACT MCC TO DOWNGRADE THIS AIRCRAFT FROM ETOPS STATUS AND EVF AUTHORIZATION. ALL WORK PERFORMED ON SIGNIFICANT SYSTEMS WHILE ACCOMPLISHING THIS TSI MUST BE DOCUMENTED IN DETAIL IN THE AIRCRAFT LOGBOOK AS WELL AS IN THE RESOLUTION OF THIS TSI. REF GMM 17-32. C/W ALL GMM BUYBACK AND RII REQUIREMENTS SOURCE: REPEAT. (RESOLVED ON W/O: 1141819 TASKCARD: NR-00002 ) TROUBLESHOT PER TSM 77-11-00-810-808A. NO DAMAGE TO W03 HARNESS FOUND. R/R N1 PROBE (4046KS) PER AMM 77-11-21 OPS CHKS PASSED. NO DEFECTS AT THIS TIME.

Part: FIRE LOOP — FAULTED (NR 2) · airframe 192 hrs · 41 cycles

FLT 2824, LAX-JFK. (FOLLOW-UP) ENG #2 FIRE LOOP INTERMITTENT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ) ;ENG 2 FIRE LOOP A PLACED ON MEL 26-12-01A MDDR # 451768 MX-4 UPDATED MCC NOTIFIED REF MDDR # 451769 FOR ETOPS RESTRICTION ; ON 10/09/19 RE-SECURED ENG #2 PYLON FIRE LOOP A (3WD2) TERMINAL STUD REF AMM 26-12-01. ON 10/09/21 R/R ENG 2 CORE LOOP A (4001WD1) FIRE DETECTOR IAW AMM 26-12-17 ON 10/09/21 REPLACED ENG#2 PYLON LOOP A (3WD2) DETECTOR IAW AMM 26-12-16. ON 10/09/21 R/R ENG 2 CORE LOOP A (4001WD1) FIRE DETECTOR IAW AMM 26-12-17. ON 10/17/21DUE TO CHRONIC HISTORY, ENG 2 “A” LOOP FAULT, AIRBUS PROVIDED A TECHNICAL ADAPTATION (RDAS) PART OF WHICH IS INCORPORATED IN EC A21-1146-01. SINCE THE FAULT HAS SWAPPED OVER TO THE ENG 2 “B” LOOP, THIS INDICATES THE FAULT EXISTS BETWEEN THE FDU AND TB 405VT2. SEE LP 3141292, ITEM 1 FOR RECLASSIFICATION OF THE MEL FROM 26-12-01-A TO MEL 26-12-01-B. ON 10/18/21 WO # 1141036 ACCOMPLISHED (EA A21-1146-02) FIRE PROTECTION - ENGINE FIRE & OVERHEAT DETECTION - SWAP ENGINE 2 FIRE LOOP WIRING CONNECTIONS TO TROUBLE ON-GOING CHRONIC LOOP A FAULT ON 10/21/21 SWAPPED PIN BACK TO NORMAL CONFIG. RECLASSIFIED TO MEL 26-12-01A MDDR 452602 ENG #2 LOOP A DEFER. REF WO # 1141492 FOR PIN SWAP. (EA A21-1146-05 FIRE PROTECTION - ENGINE FIRE & OVERHEAT DETECTION - SWAP ENGINE 2 FIRE LOOP WIRING CONNECTIONS TO TROUBLE ON-GOING CHRONIC LOOP A FAULT) ON 10/21/21 C/W WO # 1141492 AS REQ'D SWAPPED ENG #2 FIRE LOOP PIN TO ORIGINAL POSITION WIRE #2612-0220 IS @ 450VT2 MODULE #1 PIN C WIRE #2612-0221 IS @ 450VT2 MODULE #1 PIN H, WIRE #2612-0232 IS @ 450VT2 MODULE #5 PIN H WIRE #2612-0235 IS @ 450VT2 MODULE #5 PIN B. ON 10/24/21 REF LG PG EC A21-1146-06. ACTION TAKEN SUCCESSFUL. NO FAULTS NOTED. THIS CLEARS MDDR 452602. MX-4 UPDATED. (EC A21-1146-06): FIRE PROTECTION - ENGINE FIRE & OVERHEAT DETECTION - SWAP ENGINE 2 FIRE LOOP WIRING CONNECTIONS TO TROUBLE ON-GOING CHRONIC LOOP A FAULT

Part: FIRE LOOP — FAULTED (NR 2) · airframe 164 hrs · 35 cycles

FLT # 2823, JFK-LAX. (ETOPS) IN-FLIGHT 3 FALSE INDICATIONS OF ENG #2 FIRE ENG 2 FIRE LOOP A FAULT - INTERMITTENT ENG 2 FIRE DET FAULT - INTERMITTENT ENG 2 FIRE LOOP B FAULT - INTERMITTENT ALL FAULTS CLEARED WITHIN 45 MINS OF DEPARTURE AND NO FURTHER FOR REST OF FLIGHT ; SWAPPED PIN BACK TO NORMAL CONFIG. RECLASSIFIED TO MEL 26-12-01A MDDR 452602 ENG #2 LOOP A DEFER. REF WO # 1141492 FOR PIN SWAP

Part: FDU — FAILED (NR 2 ENGINE) · airframe 65 hrs · 15 cycles

FLT# 2824, LAX-JFK. " ENG 2 FIRE LOOP A FAULT " ECAM MESSAGE INTERMITTENTLY DISPLAY ; R/R ENG #2 FDU (2WD2) IAW AMM 26-12-34 ALL OPERATIONAL CHKS ACCOMPLISHED NO DEFECTS NOTED A/C OK FOR CON`T SVC

Part: FIRE LOOP — INTERMITTENT (NR 2) · airframe 75 hrs · 17 cycles

FLT# 2824, LAX-JFK. ENG #2 FIRE LOOP INTERMITTENT. FIRE LOOP A REPLACED ENG#2 PYLON LOOP A (3WD2) DETECTOR IAW AMM 26-12-16.

Part: FIRE LOOP — FALSE INDICATION (NR 2 ENGINE) · airframe 70 hrs · 16 cycles

FLT# 2823, JFK-LAX. ENG 2 FIRE LOOP A FAULT ECAM DISPLAY INTERMITTENTLY W/O CHIME OR MASTER CAUTION ; PERFORMED ENG #2 FIRE TEST PER AMM 26-12-00 NO FAULTS NOTED.

Part: DOOR — OUT OF ADJUST · airframe 35 hrs · 9 cycles

FLT# 2324, LAX-JFK. ON LOWER ECAM DOOR/OXY PAGE, OVERWING EXITS NOT SHOWING ARMED ; REMOVED LH + RH OWE EXIT DOOR LININGS TO CHECK POSITION OF DISARM SLIDE-RELEASE MECHANISM. FOUND ALL LEVERS, IN THE "DISARMED" POSITION. PLACED ALL 4 IN THE ARMED POSITION. PERFORMED OPS TEST OF THE WARNING SYS REF AMM 52-73-00-710-002-E. TESTS OK. ALSO VERIFIED INFLATION RESERVOIRS ARE NOT PINNED.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 25 hrs · 7 cycles

FLT # 2324, LAX-JFK. AIRCRAFT HAS REPORTED IN AIRMAN AN ENG 2 FIRE LOOP A FAULT IN CRUISE WITH ASSOCIATED "CHECK ENG 2 FIRE LOOP A AGB" CFDS FAULT; REF WO 1137418 NR-0001 TSI ENG 2 FIRE LOOP A FAULT. T/S PER TSM 26-12-00-810-858-A RESISTANCE VALUE OF CORE AGB LOOP A FIRE DETECTOR (4002WD1) WITHIN LIMITS 6845OHM BETWEEN PINS A AND C. R+R 4002WD1 FIRE DETECTOR PER AMM 26-12-1 AS PRECAUTIONARY PER TSI.

Part: CONTROL UNIT — FAILED (NR 2 THROTTLE) · airframe 13 hrs · 4 cycles

ETOPS: FLT 6414, JFK-VQQ. ENG 2 ONE TLA FAULT DISPLAYED ON ECAM ( THRUST LEVER POSITION SENSORS ); T/S PER TSM 76-11-00-810-825-A. FOUND WIRE 7325-7314 BROKEN BETWEEN FRAMES 33 AND 34 ( ABOVE SEAT 6F, ROUTE 2S. PER ESPM FIGURE 20-53-22-0004, REPAIR TYPE IS 2-F. PERFORMED REPAIR IAW ESPM 20-53-22-0014. SELF TEST OF THE FADEC PASSED, MDDR CLEARED PLACARD