N4022J
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
FLT # 332, MXP-BOS. (ETOPS) PACK 2 REG. FAULT; ACCOMPLISHED TSM 21-671-00-825-A , REPLACED NR 2 PACK COMP. OUTLET TEMP SENSOR 32HH PER AMM 21-61-11-400-001-A ,NO FAULTS AT THIS TIME.
FLT # 7, JFK-LHR. (ETOPS) AC GEN CLASS II MESSAGE ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN ).
FLT 32, AMS-BOS. (ETOPS) ENG L FIRE LOOP B FAULT ECAM AFTER LANDING. ENGINE FIRE DETECTION SYSTEMS LOOP B. OPEN
FLT# 123, JFK-LAX. (ETOPS) AC GEN MAINTENANCE MSG AT GATE PRIOR TO ENGINE START. REMOVED AND REPLACED ENG # 2 IDG IAW AMM 24-21-51. OPS CHK NORMAL. NO LEAKS NOTED. NO DEFECTS NOTED AT THIS TIME.
FLT 31 BOS -AMS. COCKPIT & CABIN ODOR PASSING 10K IN DESCENT IN COCKPIT & CABIN PILOTS & F/A'S NOTICED LVEL 2 ON ODOR LEVEL CHART.; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10, (AMBIENT AIR ODOR), PER TSM 05-50-00-810-085-D. NO FUMES OR ODOR AFTER EACH ENGINE RUN. NO SIGNS OF OIL ON THE ENGINES AND APU. AIRCRAFT IS OK FOR SERVICE.
FLT 31 BOS-AMS (ETOPS). MAINTENANCE AC GEN MESSAGE ON STS PAGE ( CLASS II MX MSG - GPCU OR AC GEN ).
FLT 31 AMS-BOS (ETOPS). MAINTENANCE AC GEN MESSAGE ON STS PAGE ( CLASS II MX MSG - GPCU OR AC GEN ). OPEN
FLT # 2220 LHR- JFK (ETOPS)."RADAR CONTINUOSLY PAINTS WXR, ALTHOUGH THERE IS NONE.ECHO RETURNING LIGHTNING STRIKES.; FOUND FAULTY WXR TRANSCEIVER/PROCESSOR.R/R 1SQ1 IAW AMM 34-41-33-400-003-A.FAULT CLEARED.OK FOR SVC."
FLT 034, CDG -BOS (ETOPS). NR 2 ENG OIL SENSOR ON 19.5 ON GROUND OUT OF PARIS THEN ONE HOUR INTO THE FLIGHT DROPPED TO 12 THEN CLIMB TO 13 THEN ON LANDING WENT TO 20.5. SO 19.5 ON THE GROUND IN PARIS THEN 20.5 ON THE GROUND IN BOS ( OIL QUANTITY INDICATIONS ).; (RESOLVED ON W/O: 1468625 TASKCARD: NR-00001 ) REMOVED AND REPLACED ENG #2 OIL QUANTITY SENSOR IAW EMM 79-31-21 OPS CHK GOOD. LEAK CHK OK THIS CLEARS MDDR 606232 MX-4 UPDATED. ORIGINAL SUBMISSION DATE: 01/14/2026
FLT 1107, JFK-LHR (ETOPS). AIR BLEED MX MAINTENANCE MESSAGE AFTER PUSHBACK, I MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1, FAULTS INDICATED BY AIR BLEED.; (RESOLVED ON W/O: 1469094 TASKCARD: NR-00001 ) C/W TSM 36-11-00-810-993 RAR RELAY 22HV. OPS CHECK SATISFACTORY. THIS CLEARS MDDR 605987. MX4 UPDATED PLACARD REMOVED. REF ITEM #1 LOG PAGE 4470190 FOR GROUND VERIFICATION. ( LP 4470190- EFERENCE MDDR 605987 AIR BLEED CLASS II.; ACCOMPLISHED GROUND VERIFICATION OF APU AIR BLEED PER 36-12-00. GROUND VERIFICATION SATISFACTORY.
FLT 1408 CDG- JFK (ETOPS). " DUE TO REMOVAL AND REPLACEMENT OF CARGO FIRE BOTTLE 4010-WX, CARTRIDGE 4011-WX REQ. REPLACEMENT.; REMOVAL AND REPLACMENT OF CARTRIDGE 4011-WX IN REF W/ AMM 26-23-41. OPC GOOD. NO DEFECTS NOTED."
FLT#123, JFK-LAX. AFTER PARKING TOW INFLIGHT CREW MEMBERS REPORTED DIRTY SOCK SMELL IN THE AFT GALLEY FROM DESCENT THROUGH 10,000 UNTIL TOUCHDOWN. APU WAS OFF. ENTERED A CLOUD LAYER AT ABOUT 5,000' TILL 400' , SMELL INTENSITY REPORTED AS MILD. ONE FWD FA ALSO REPORTED THE MILD SMELL AT 2,500; PER CAQE REPORT, APU IS THE PROBLEM CAUSE OF THE SOURCE. INSPECTED APU, APU COMPARTMENT NO OIL LEAKS FOUND/NOTED. INSPECTED BOTH M/L/G WHEEL WELLS AND BELLY AREA UP TO APU INLET. NO EVIDENCE OF FLUID LEAKS NOTED. PERFORMED BOTH ENGINE RUNS. ISOLATED EACH BLEED SOURCE. NO ODOR NOTED. NO SMELL NOTED. PER INFO NOTICE 2017-T015L. SECTION A ISOLATED ODOR TO TYPE 10, TRANSIENT ENVIRONMENTAL, ODOR, A/C IJ FOR SERVICE.
FLT#8485, BHM-BOS. (ETOPS) "APU LOOP A FAILED ( APU FIRE DETECTION SYSTEM LOOP A . REMOVED AND REPLACED APU LOOP IAW AMM 26-13-15 OPS CHECK GOOD. MX-4 UPDATED, STICKER REMOVED AC OK TO SVC.
DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / RHS SKIN PANEL AT FR63 - FR64 AND STGR40R STGR42R / DENTS AND GOUGES - TIME-LIMITED REPAIR; REFERENCES: /1/ DAMAGE REPORT, MAPPING, AND REQUEST /2/ SRM TASK 53-41-11-283-024 - ADL /3/ AIRBUS DOSSIER 81653487 /4/ AIRBUS DRAWING E53478902010 ITEM 540 (RIVETS) /5/ AIRBUS RDAF 81653487/006/2025#A. DESCRIPTION: ON 05-SEP-2025 @ BOS DURING PREFLIGHT MX ACTIVITIES ON N4022J (MSN: 10303), A LAV GSV IMPACTED THE A/C, RESULTING IN THREE (3) DENT AND GOUGE DAMAGES ON THE REAR FUSELAGE RHS SKIN PANEL LOCATED BETWEEN FR63 - FR64 AND STGR40R STGR42R. SEE REF /1/ FOR FULL DETAILS. THE DAMAGES WERE ASSESSED AND ALL GOUGES/SCRATCHES WERE BLENDED SMOOTHLY PER SRM 51-73-00 AND MRT PER THE NTM WAS ACCOMPLISHED. THE FINAL DIMENSIONS OF ALL DENTS AND MATERIAL LOSS ARE REPORTED AS FOLLOWS: 1. DAMAGE 1 AT STGR 40R, DENT: L=2.0" , W=1.5", D=0.008". A.THIS DAMAGE IS OUT OF SRM ALLOWABLE LIMITS OF DUE TO PROXIMITY TO DAMAGE 2 & 3. 2.DAMAGE 2 AT STGR 41R, DENT + GOUGE: DENT DIMENSIONS - L= 4.6" , W= 1.7", D=0.015", REWORK DIMENSIONS - MIN MRT = 0.045". 3.DAMAGE 3 AT STGR 42R, DENT + GOUGE: DENT DIMENSION - L= 0.75", W= 0.125", D=0.008", REWORK DIMENSIONS - MIN MRT = 0.045". EXTERNAL AND INTERNAL DVIS IAW NTM 51-90-00 CONFIRMED NO ADDITIONAL/INTERNAL DAMAGES, AND HFEC INSPECTIONS IAW NTM 51-10-08 WEREACCOMPLISHED AT DAMAGE AREAS 2 AND 3 REVEALING ANOMALIES, BUT THEN A FPI IAW NTM 51-80-00 CONFIRMED NO CRACK FINDINGS. THE SRM REF /2/ WAS REVIEWED FOR ADL AND WAS OOL DUE TO BEING IN AN EXCLUDED AREA. AIRBUS WAS CONTACTED REQUESTING DISPOSITION AND REPAIR INSTRUCTIONS VIA REF /3/ DOSSIER AND PROVIDED CONFIRMATION THAT THE DAMAGE IS ACCEPTABLE AS-IS ON A TEMPORARY BASIS OF 200FC CONTINGENT ON NO REWORKED AREAS OF THE FASTENER HEADS EXCEEDING 0.02MM DEPTH AS PER SRM 51-73-11, PARA. 4.C.(2). MX REPORTED FEEDBACK THAT DAMAGE AREA 2 (LAP JOINT AREA) EXCEEDED THIS LIMIT. AIRBUS CONFIRMED THAT THE AFFECTED FASTENERS (FOUR (4) TOTAL) MUST BE R/R IAW SRM 51-42-11, SRM 51-43-00 & SRM 51-44-11, AND AIRBUS DRAWING REF /4/. EC A25-831-01 IS ISSUED TO PERFORM THIS TEMPORARY REPAIR VALID FOR 200FC AS AUTHORIZED IAW REF /3/ DOSSIER AND WAS REPORTED TO AIRBUS FOR ISSUANCE OF REF /5/ RDAF. THIS EC A25-831-02 IS ISSUED TO TRACK THE PERMANENT REPAIR DUE IN 200FC IAW THE LIMITATIONS PER REF /5/ RDAF. SUBSTANTIATION: THIS PERMANENT REPAIR IS CURRENTLY PENDING OEM APPROVAL AND IS CLASSIFIED AS OTHER.* REV 01* /7/ AIRBUS D/81653487/045/2025 ISSUE A /8/ REPAIR INSTRUCTION FOR CPC APPLICATION R53070555 A /9/ A321 (ST2) SRM TASK 53-00-11-300-059 ON 9/20/2025, AIRBUS PROVIDED REF /7/ TD TO DO THE PERMANENT DOULBER REPAIR AS PER REF /9/ PRINCIPLES. THE REF /7/ TD REPAIR CONSISTS OF CUT-OUT LAY-OUT, MATERIAL AND THICKNESS OF THE DOUBLER AND FILLER, FASTENERS INFORMATION AND APPLCATION OF SURFACE PROTECTION. AIRBUS ALSO PROVIDED REF /8/ RI TO MAKE SURE THE CORRECT APPLICATION OF THE CORROSION PREVENTION COMPOUND. THIS EC IS BEING REVISED TO ENCOMPASS REF /7/ TD INSTRUCTIONS. NOTE - INITIAL TEMPORARY REPAIR DONE AS PER A25-831-01 AND REF /5/ RDAF IS STILL VALID FOR 200FC FROM 9/7/2025. - ONCE THE REPAIR IS DONE AS PER REF /7/ TD AND EC/TC A25-831-02 REV 01, REPORT BACK TO AIRBUS TO GET THE RDAF. *REV 02* /10/ TRM 81653487/061 ON 9/26/2025, AIRBUS PROVIDED REF/10/ TRM 061, WHICH ADDRESSED A CONCERN ABOUT THE REPAIR COVERAGE FOR DAMAGE #1(TRM /054). PER FIGURE 2 OF THE REF/7/ TD, THE REPAIR DOUBLER CONTOUR WILL END RIGHT AT THE EDGE OF THE DAMAGE AND MAY NOT FULLY COVER IT. AIRBUS STATED, SINCE DAMAGE #1 IS A SHALLOW DENT (D=0.02MM) AND THE NOMINAL THICKNESS REMAINS THE SAME, THE DOUBLER DOES NOT NEED TO BE EXTENDED. IF DEFORMATION REMAINS, AIRBUS PROVIDED DRESS BACK INSTRUCTIONS PER REF /10/ TRM 061 AS REQUIRED. AN ADDITIONAL ISSUE WAS FOUND DURING THE LAYOUT OF THE CUTOUT PER REF/7/ TD SINCE THE CUT OUT COULD NOT FIT ALL 5 FASTENERS AT FR 42RH(TRM /056). IN REF /10/ TRM, AIRBUS CONFIRMED IT IS ACCEPTABLE TO TAPER THE LOWER PORTION OF THE CUT-OUT TO INCLUDE ONLY 3 FASTENERS AT STGR42RH AS LONG AS ALL THE DAMAGE IS REMOVED AND ALL OTHER REQUIREMENTS PER REF/7/ TD ARE MET. TC A25-831-02 IS BEING REVISED TO ENCOMPASS THESE INSTRUCTIONS. NOTE: THESE ADDITIONAL INSTRUCTIONS/DEVIATIONS WILL BE EMBODIED IN EITHER A TD REVISION OR RDAF ONCE THE REPAIR IS COMPLETE.*REV 03* REFERENCES: /11/ AIRBUS RDAF 81653487/050/2025 ISSUE A (200FC LIMITATION). DESCRIPTION: ON 10/6/2025, AIRBUS PROVIDED THE REF /11/ RDAF AUTHORIZING THE REPAIR ACCOMPLISHED PER EC A25-831-02 AS TIME-LIMITED FOR 200FC PENDING FURTHER DTA. AS A RESULT THE FOLLOWING EC/TCâS ARE REVISED/RELEASED: - EC/TC A25-831-02 IS BEING REVISED TO DOCUMENT THE ISSUANCE OF THE REF /11/ RDAF AND ALLOW THE AIRCRAFT TO RTS. NOTE: AIRCRAFT CAN FULLY RTS ONCE RDAF FOR AIRBUS DOSSIER 81660383 IS ALSO RECEIVED.- EC/TC A25-831-03 IS BEING RELEASED TO TRACK THE PERMANENT REPAIR DUE WITHIN 200FC (PENDING FURTHER DTA). SUBSTANTIATION: THIS TIME-LIMITED REPAIR IS APPROVED AS PER REF /11/ RDAF AND REMAINS CLASSIFIED AS MAJOR. (E/C: A25-831-02)
FLT#1621, LHR-BOS. (ETOPS) L-1 TSI ELEC GEN 1 FAULT-DUE TO ELEC GEN 1 FAULT ON PFR IN LHR & GCU1 SHOWING THE AT FAULT, REMOVED AND REPLACED GCU NR 1 IAW AMM 24-22-34. OPS CHK GOOD. TSI CLOSED. GROUND VERIFICATION C/W PER AMM 24-22-34.
FLT#1621, LHR-BOS. (ETOPS) L1 TSI - ENG 1 IGN A FAULT, APPROVAL REQUIRED FOR RESOLUTION, DUE TO PREVIOUS ENGINE 1 IGNITION A FAULT IN LHR AND THE INABILITY TO MEL SYSTEM A ON THE ETOPS FLEET PLEASE REPLACE ENG#1 SYSTEM A EXCITER, IGNITER AND LEAD REF AMM 74-11-01, 74-21-01 AND 74-21-61. ENSURE ALL GMM AND RII REQUIREMENTS ARE COMPLIED WITH; (RESOLVED ON W/O: 1439029 TASKCARD: NR-00002) REMOVED AND REPLACED BOTH IGNITER PLUGS PER EMM 74-21-01, R/R'D IGN-A LEAD PER EMM 74-21-61 & R/R'D IGN EXCITER PER EMM 74-11-01. OPS CK'D SATIS AND NO FURTHER ISSUE WAS OBSERVED.
FLT#1621, LHR-BOS. (ETOPS) L1 TSI - ENG 1 IGN A FAULT, APPROVAL REQUIRED FOR RESOLUTION, DUE TO PREVIOUS ENGINE 1 IGNITION A FAULT IN LHR AND THE INABILITY TO MEL SYSTEM A ON THE ETOPS FLEET PLEASE REPLACE ENG#1 SYSTEM A EXCITER, IGNITER AND LEAD REF AMM 74-11-01, 74-21-01 AND 74-21-61. ENSURE ALL GMM AND RII REQUIREMENTS ARE COMPLIED WITH; (RESOLVED ON W/O: 1439029 TASKCARD: NR-00002) REMOVED AND REPLACED BOTH IGNITER PLUGS PER EMM 74-21-01, REMOVED AND REPLACED IGN-A LEAD PER EMM 74-21-61 & R/R'D IGN EXCITER PER EMM 74-11-01. OPS CK'D SATIS AND NO FURTHER ISSUE WAS OBSERVED.
FLT#1023, JFK-LAX. (ETOPS) ENG 1 LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); REMOVED AND REPLACED FIRE LOOP A CORE IAW AMM 26-12-17 OPS CHK GOOF MX-4 UPDATED PLACRD REMOVED MDDR CLEARED.
FLT#1908, CDG-JFK. (ETOPS) "REF T/C A3625040-01 ON WO 1423764 FAN AIR VALVE REQ REPLACEMENT; REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-54 OPS CHK GOOD."
FLT#1107, JFK-LHR. (ETOPS) 'NAV PRED W/X DET FAULT ON TAXI OUT ( WEATHER RADAR SYSTEMS ).' T/S PER TSM 34-41-00-810-810-A. REMOVED AND REPLACED 13SQ1 PER AMM 34-51-00. ALL OPS NORMAL AT THIS TIME. THIS CLEARS MDDR MX-4 UPDATED PLACARD REMOVED.
FLT#2220, LHR-JFK. (ETOPS) (AIRCRAFT PERFORMED AN AIRTURN BACK TO LHR) .' AFTER T/O ECAM MESSAGE FOR ENG1 BLEED FAULT APPEARED ON. WE FOLLOWED ECAM ACTIONS AND MESSAGE CAME BACK. WE CALLED MX AND DID RESET PROCEDURES AND MESSAGE WAS NOT CLEARED; TROUBLESHOT PER TSM 36-11-54 AND FOUND FN AIR VALVE ROD END DAMAGED REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-54 .OPS CHECK GOOD A/C OK FOR SVC.
FLT#1408, CDG-JFK. (ETOPS)GREEN HYD PUMP (ENG) INDICATION INOP ( ECAM HYD PAGE INDICATIONS 9) (G/B/Y) HYD SYS LABEL VERTICAL LINE LINKS ); RE-PINNED CONTACTORS AND CONNECTOR IAW ESPM 20-44-10. OPS CHECK GOOD. NO FAULT NOTED. MDDR CLEAR. MX-4 UPDATED PLACARD REMOVED.
FLT#1107, LHR-JFK. (ETOPS) GREEN HYD ENG PUMP INDICATION STAYS ON ( ECAM HYD PAGE INDICATIONS 7) PUMPS ); REMOVED AND REPLACED G HYD ENG PUMP PRESSURE SWITCH IAW AMM 29-11-17. OPS CHECK GOOD. MDDR CLEARED. PLACARD REMOVED. MX-4 UPDATED.
FLT#711, JFK-LHR. (ETOPS) HYD SD PAGE ON ECAM PANEL GREEN HYD SYS SHOWS ENG 1 HYD PUMP ON AND GREEN MOST OF THE HYD LINE ENG 1 OFF ( ECAM HYD PAGE INDICATIONS 7) PUMPS ); RE-PINNED CONNECTOR IAW ESPM 24-25-24. OPS CHECK GOOD. NO DEFECTS NOTED. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED. MDDR CLEARED
FLT#1107, JFK-LHR. (ETOPS) ENG 1 MINOR FAULT ( MINOR FAULT CAUTIONS ON ECAM EWD ); REMOVED AND REPLACED AUXILIARY OIL PRESSURE SENSOR FROM ENG #1 REF AMM 79-33-24.
FLT#2289, AMS-JFK. (ETOPS) ' ENG #1 HYDRAULIC PUMP INDICATOR STAY GREEN WHEN ENGINE IS SHUTDOWN; REF TSM 29-11-00-810-806-A. REMOVED AND REPLACED #1 ENG PUMP PRESSURE SWITCH IAW 29-11-17. PERFORMED OPS TEST OF GREEN HYDRAULIC SYSTEM. OPS CHECK GOOD. NO LEAKS NOTED. THIS CLEARS THIS MDDR. PLACARD REMOVED. MX-4 UPDATED.
FLT#2220, LHR-JFK. (ETOPS). 'REF MDDR 561337 (GREEN HYD SYS - LINK LINE FOR PRESS INDICATION SHOWS AMBER WHEN NOT PRESSURIZED ( AMBER LINE ) ( ECAM HYD PAGE INDICATIONS 9) (G/B/Y) HYD SYS LABEL VERTICAL LINE LINKS )) GREEN SYS SHOWS PRESS; REMOVED AND REPLACED GREEN HYD PRESS SWITCH 1151GN PER AMM 29-32-12. NO HELP MDDR REMAINS OPEN. REMOVED AND REPLACED #1 ENGINE GREEN SYSTEM PRESSURE SWITCH IAW 29-11-17. OPS CHECKS GOOD. THIS CLEARS MDDR 561337. MX-4 UPDATED PLACARD REMOVED.
FLT#2288, JFK-AMS. 'FA REPORT DIRTY SOCK POSSIBLE FUMES IN MID CABIN TO AFT GALLEY; COMPLIED WITH INFORMATION NOTICE 2019-T025SECTION A. ISOLATED FAULT TO TYPE 40 (40CR-A) AMBIENT AIR DOOR. BOTH ENGINE IDLE RUNS G/O LTP 50% N1, NO ODORS (SMELL NOTICED). PER TSM 05-50-00, 240-085-B TSM 05-50-00-810-085-D.'
FLT#1908, CDG-JFK. (ETOPS) 'AIR PACK 1 REG FAULT ( ECAM INDICATION ON BLEED PAGE PACK COMPRESSOR OUTLET TEMPERATURE ); FROM TSM 21-61-00-801-824-A OPS TEST OF PAC SYS PASSED ,AS PRECAUTION CLEANED TEMP SENSOR IAW 21-61-00-100-801,RE RAN TEST AND TEST PASSED. MX-4 UPDATED. MDDR CLEARED. AC OK TO SVC.
FLT#20, LHR-JFK. (ETOPS) 'UPON LANDING ENG 1 HEAT SYS DEGRADED ( HEAT SYS DEGRAD CAUTIONS ON ECAM E/WD ); REMOVED AND REPLACED ENG #1 IFPC IAW AMM 73-11-01 OPS CHECK AND LEAK CHECK GOOD THIS CLEARS THE MDDR PLACARD REMOVED MX-4 UPDATED.'
FLT#20, LHR-JFK. (ETOPS) 'VENT EXTRACT FAULT IN FLIGHT FOLLOWED QRH PROCEDURE; REMOVED AND REPLACED VENT EXTRACT (18HQ) IAW AMM 21-26-51. PERFORMED OPS TEST IAW AMM 21-26-00-710-001, TEST OK.'
FLT#1407, JFK-CDG. (ETOPS) 'IN CRUISE AT FL330 WE RECEIVED A VENT EXTRACT FAULT WE COMPLIED WITH QRH ANDCONTACTED MCC. A MUTUAL DECISION TO CONTINUE WAS MADE AS THE BLOWER WAS ON MEL; AEVC OPERATIONAL TEST CARRIED OUT IAW AMM 21-26-00 TEST SHOWS BLOWER FAN FAULT ONLY AS STATED ON MDDR 553979 (REMOVED AND REPLACED BLOWER VENT FAN ( 20HQ) IAW AMM 21-26-51, PEROFRMED OPS TEST IAW AMM 21-26-00-710-001, TEST OK, THIS CLEARS MDDR 553979, MX-4 UPDATED, PLACARD REMOVED).
FLT#1407, JFK-CDG. (ETOPS) 'ACT XFER FAULT ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ); REF TSM 28-28-00-810-874-A. ACCOMPLISHED FUEL TRANSFER BETWEEN ALL TANKS IAW AMM 28-25-00. OPS CHECK GOOD. NO FAULTS/MSGS NOTED. THIS CLEARS MDDR. ALL CONFIGU'S NORMAL. PLAC REMOVED. MX-4 UPDATED. MCC NOTIFIED.
FLT#7, JFK-LHR. (ETOPS) 'BLOWER VENT FAULT ( BLOWER FAN - NO AVNCS SYS FAULT ECAM CAUTION ); REMOVED AND REPLACED BLOWER VENT FAN ( 20HQ) IAW AMM 21-26-51, PERFORMED OPS TEST IAW AMM 21-26-00-710-001. TEST OK, THIS CLEARS MDDR 553979, MX-4 UPDATED, PLACARD REMOVED.
FLT#1408, CDG-JFK. (ETOPS). 'HYD G ENGINE 1 PUMP LO PR INFLIGHT; SYSTEM TROUBLESHOT IAW TSM 29-11-00-810-804-A AND FOUND ENGINE DRIVEN HYDRAULIC PUMP DRIVE SHAFT SPLINE WORN. REMOVED AND REPLACED EDP IAW AMM 29-11-51-400-805. INSPECTED CASE DRAIN FILTER, HP FILTER AND LP FILTER DPI. NO DEFECTS NOTED. OPS CHECK GOOD. NO DEFECT NOTED. A/C OK FOR SVC.'
FUEL ACT XFER FAULT ECAM MESSAGE. ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ); T/S PER TSM 28-28-00-810-874-A AND PERFORMED FUNCTIONAL TEST OF THE ACT AUTO XFER SYSTEM. NO DEFECTS NOTED OPS TEST GOOD MDDR CLEARED PLACARD REMOVED UPDATED MX-4 REF AMM 28-28-00.
FLT#44, LGW-JFK. (ETOPS)' REF LOG PAGE 3970765, ITEM 1 POWER PLANT ENGINEERING AFTER BSI OF #2 ENG REVIEW ADVISED ENGINE REQUIRES REPLACEMENT; REF DEFECT 3970767, ITEM 1 (REM/INS ENG 2 PER TC A320-71-00-51-400-802-1. TESTS OK. A/C OK FOR SERVICE) FOR REPLACEMENT OF ENG 2.' (SUPPLEMENTAL TO FOLLOW)
FLT#44, LGW-JFK. ' DIRTY SOCK SMELL AFT GALLEY DURING FINAL APPROACH PHASE; COMPLIED WITH INFORMATION NOTICE 2017-T015K, SECTION B2. IDENTIFIED ODOR AS TYPE 1. DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM TASK 05-50-00-810-831-A. AIRCRAFT IS OK FOR SERVICE. INSP OF APU DID NOT REVEAL ANY EVIDENCE OF LEAKS. NO ODORS NOTED DURING OPERATION OF APU NOR ENGINES.'
FLT#7, JFK-LHR. (ETOPS) ' NO POSITION ON FMS 2 ATTEMPTED RESET UNSUCCESSFUL ( FLIGHT MANAGEMENT SYSTEM (FMS) 2) FMS2 ); FMGC 1 AND 2 RERACK C/O IAW 22-83-34. AFS OP TEST C/O IAW 22-96-00. MDDR 547933 CLOSED. MCC NOTIFIED.'
FLT#20, LHR-JFK. (ETOPS). 'FAULT LT WILL NOT EXT IN MODE SELECTED ON ACT TRF PNL. ACT XFR FAULT (ACT) ); PERFORMED FIM TASK 28-46-00-810-879-A. TEST PASSED BUT SHOWS HISTORY OF FAULT. REMOVED AND REPLACED AFMC IAW AMM 28-51-35. OPS CHECK GOOD AT THIS TIME. MX-4 UPDATED AND PLACARD REMOVED.
FLT#1620, BOS-LHR. 'AFTER TAKE OFF AMBER CLOG UNDER FUEL USED FOR #2 ENGTMG IT WENT AWAY CLIMBING OUT OF FL230; PFR MSG 73-11-06 ENG 2 D - 0257- FUEL FLTR IMP CLOG # 2 ENG FUEL FILTER REPLACED IAW AMM 73-11-06 PB 401 CONF 21 AND TEST #13 IDLE POWER TEST PERFORMED SATIS WITH NIL LEAKS IAW AMM 71-00-00-720-811 REV 21 FEB 24 MATERIALS USED QTY 1 FUEL FILTER P/N 1020930-5 AND QTY 1 PACKING P/N M83485-1-246.'
FLT#1408, CDG-JFK. (ETOPS) 'APU AUTO SHUTDOWN; T/S IAW TSM 49-00-81-810-821-A. REMOVED AND REPLACED IGNITER PLUG IAW AMM 49-41-41 AND IGNITER LEAD IAW AMM 49-41-43 AND EXCITER BOX UNIT IAW AMM 49-41-33. ALL OPS CHECK OK. APU RAN CONTINUOUSLY WITH NO ISSUES NOTED. FAULT COULD NOT BE DUPLICATED.
FLT#43, (ETOPS) ECAM MSG AC GEN MAINTENANCE ( CLASS II MX MSG - GPCU OR AC GEN ); REMOVED AND REPLACED GCU #2 PER AMM 24-22-34. OPS CHECK GOOD AT THIS TIME.
FLT#20, LHR-JFK. (ETOPS) 'ENG 2 FIRE LOOP A FAULT ILLUMINATED IN FLIGHT; REMOVED AND REPLACED ENG #2 AGB LOOP A IAW AMM 26-12-17. DUE TO FLUCTUATING RESISTANCE VALUE WHEN VIBRATED. OPS CHECK NORMAL, NO FURTHER FAULTS NOTED.
DURING HEAVY MAINTENANCE: EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHEET 1) FIGURE 005 (SHEET 1) DIAGRAMA 001(SHEET 1) THIS REPAIR IS CATEGORY B PERMANENT AND INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AT 1300 FC / AND SUBSEQUENT INSPECTION AT INTERVALS OF 1300 FC. INSPECTION METHOD. GENERAL VISUAL INSPECTION I.A.W SRI 53-41-11-205-052. (RESOLVED ON W/O: 1289336 TASKCARD: NR-00007) EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHEET 1) FIGURE 005 (SHEET 1) DIAGRAMA 001(SHEET 1) THIS REPAIR IS CATEGORY B PERMANENT AND INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AT 1300 FC / AND SUBSEQUENT INSPECTION AT INTERVALS OF 1300 FC.
DURING HEAVY MAINTENANCE: EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHEET 1) FIGURE 005 (SHEET 1) DIAGRAMA 001(SHEET 1) THIS REPAIR IS CATEGORY B PERMANENT AND INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AT 1300 FC / AND SUBSEQUENT INSPECTION AT INTERVALS OF 1300 FC. INSPECTION METHOD. GENERAL VISUAL INSPECTION I.A.W SRI 53-41-11-205-052. EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHEET 1) FIGURE 005 (SHEET 1) DIAGRAMA 001(SHEET 1) THIS REPAIR IS CATEGORY B PERMANENT AND INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AT 1300 FC / AND SUBSEQUENT INSPECTION AT INTERVALS OF 1300 FC. INSPECTION METHOD. GENERAL VISUAL INSPECTION I.A.W SRI 53-41-11-205-052 AND TOOL USED: CALIPER, P/N 500-197-30, S/N 15120588, DUE DATE: NOV-24-2024 AND EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D, S/N: 220272712, DUE DATE: 28-NOV-24 AND ULTRASOUND THICKNESS GAGE P/N: 45MG, S/N: 232017609, DUE DATE: 22-SEP-24.
FLT#20, ETOPS, ECAM ENG 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); AEROMAN INSPECTED AND TESTED #2 ENGINE FIRE, LOOP A IAW AMM 26-12-00-200-802-A WITH NO DEFECTS NOTED
FLT#1407,JFK-CDG. (ETOPS) 'SPUIOUS ENG 2 FIRE LOOP A FAULT MSG CYCLING IN FLT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); REF TSM 26-12-00-810-805A, AWM 26-12-06 AND AWM 71-51-75. CHECK WIRING, FDU 2WD2 PIN A/K AND A/J = 1481 K OHMS. WIRING CHECK GOOD. ACCOMPLISHED A VISUAL INSPECTION OF THE BLOCK 450VT2 AND FIRE LOOP ELEMENTS FOR SIGNS OF DAMAGE OR COMTAMINATION, FIND NO EVIDENCE. REMOVED AND REPLACED FDU 2WD2 AS A PRECAUTIONARY/ T/S. '
FLT#1107, JFK-LHR. (ETOPS)' ENG 1 FIRE LOOP B FAULT; REFERENCE TSM 26-12-00-810-804A BITE CHECK OF FDU OK. PERFORMED RESISTANCE CHECKS ACROSS AGB CORE AND PYLON LOOPS "B". ALL WITHIN ALLOWABLE LIMITS. NO DAMAGES NOTED TO LOOPS DURING VISUAL INOP. AS PRECAUTIONARY REPLACED ENG #1 FDU AGB LOOP B AND CORE VENT LOOP B. MDDR CLEARED. MX-4 UPDATED.'
FLT#20, LHR-JFK. (ETOPS) 'ENG 1 FIRE LOOP A FAULT ECAM ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); PERFORMED TSM 26-12-00-810-852-A. INSPECTED AGB LOOP A FIRE DET CORE LOOP. FOUND LOOP BROKEN. REPLACED PER AMM 26-12-17. ALL OPS NORMAL. BITE TEST OK. THIS CLEARS MDDR. MX-4 UPDATED. PLACARD REMOVED. MCC HAROON.'
FLT#43, JFK-LGW. (ETOPS) 'FUEL CLASS II 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 FUEL LEVEL SENSING CONTROL UNIT. OPS CHK GOOD PER AMM 28-46-34. MX-4 UPDATED PLACARD REMOVED.
FLT#8518, JFK-BOS. (ETOPS) ENG 2 FIRE LOOP B FAULT ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ). AFTER REPAIRING WIRE 2612-0278 ON #2 ENG AND REMOVAL AND REPLACEMENT OF AGB AND CORE CHANNEL B LOOPS. A SUCCESFUL OPS TEST WAS ACCOMPLISHED PER AMM 26-12-00. THIS MDDR IS CLEARED. PLACRD REMOVED. UPDATED MX-4.
ENG 2 FIRE LOOP B FAULT MSG SELF CLEARS THEN COMES BACK HAPPENED THROUGHOUT ENTIRE FLIGHT; REF L/P 3852479, ITEM 1 (REMOVED AND REPLACED FIRE DETECTOR LOOP A AND LOOP B FIRE DETECTOR RAMP ASSY IAW AMM 26-12-16 REF LOGPAGE 3852481, ITEM 1 FOR REQUIRED INSTALLATION OF PYLON FORE DETECTOR RAMP ASSY.) AND 2 (REMOVED AND REPLACED FIRE DETECTION SYS HARNESS 4001WD2/4002WD2 PER AMM 26-12-17.). REMOVED AND REPLACED LOOP A AND LOOP B FIRE DETECTOR RAMP ASSY & REMOVED AND REPLACED OF HARNESS 4001WD2 /4002WD2. OPS CHECK NORMAL THIS CLEARS MDDR 527728. MX-4 UPDATED AND PLACARD REMOVED.
FLT#1407, JFK-CDG. (ETOPS) 'ENGINE 2 FIRE LOOP B FAULT ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); REF LP 3820829, ITEM 1 (REMOVED AND REPLACED ENG 2 PYLON LOOP B FIRE DETECTION HARNESS 41WD2 AND 42WD2 IAW AMM 26-12-63. ALL OPS NORMAL. ) AND 2 (PERFORMED TEMPORARY REPAIR ON ENG 2 PYLON LOOP B FIRE DETECTION HARNESS WIRE END 42WD2 PER EC N. A23-966-01. WILL REQUIRE REPLACEMENT WITHIN 7 DAYS WHEN WIRE PART NUMBER EN2346-005A004 IS IN STOCK. REF L/P 3820832-1) FOR CORRECTIVE ACTION. MDDR CLEARED MX-4 UPDATED. PLACARD REMOVED.' ORIGINAL SUBMISSION DATE: 10/16/2023
FLT#8123, JFK-LAX. (ETOPS) ' ENG 2 FIRE LOOP B FAULT INTERMITTENTLY ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); R/R 4001WD2 CORE LOOP AS PER TSM 26-12-00-810-806A AS WELL AS TERMINAL BLOCK 450VT2 BLOCK 5. REF TRAX FOR SPECIFIED WIRE CHECKS/ LOOP CHECKS. OPS TEST OK AT THIS TIME/ REF ESPM 20-44-51 FOR BLOCK REMOVAL AND REPLACEMENT. REF LOGPAGE 3820815, ITEM 2 FOR FURTHER T/S. THESE ITEMS CLEAR THIS MDDR. MX-4 UPDATED. PLACARD REMOVED. '
FLT#2289, AMS-JFK. (ETOPS) ' ENG 2 FIRE LOOP B FAUL SHOWS ON EICAS INTERMITTENTLY; TSM TASK 26-12-00-810-806-A CARRIED OUT FAULT NOT CONFIRMED ON GROUND VISUAL INSPECTION CARRIED OUT NO DAMAGE NOTED. AS PRECAUTIONARY REPLACED ASSEMBLY FIRE HARNESS (4166KS) IAW AMM 26-12-62. ALL CHECKS GOOD FAULT NOT ACTIVE A/C OK FOR CONTINUED SERVICE.'
FLT#1408, YQX-JFK. (ETOPS) ENGINE 2 FIRE LOOP B FAULT ECAM INTERMITTANTLY. ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B ); REF LOGPAGES 3793278, ITEM 2 AND LOGPAGE 3793279, ITEM 1 AND ITEM 2(PERFORMED OPS TEST IAW AMM 26-12-04. TEST PASSED OK FOR SVC) FOR CORRECTIVE ACTION. MX-4 UPDATED PLACARD CLEARED.
FLT#8008, CDG-JFK. (ETOPS) '#1 EGN NO.3 BEARING CARBON SEAL FAILED BSI AND PER PRATT ENGIE REQUIRES REMOVAL AS UNSERVICEABLE; INSTALLED #1 ENG IAW TASK CARD A320-71-00-51-400-802-A REF WO # 1282086.'
FLT#7, JFK-LHR. (ETOPS) ' #1 LP FUEL SHUT OFF ACTUATOR WILL NOT CLOSE WITH ENG FIRE PUSH BUTTON SWITCH; REMOVED AND REPLACED #1 LP FUEL SHUT OFF ACTUATOR IAW AMM 28-24-51. OPS CHECK GOOD.'
FLT#7, JFK-LHR. (ETOPS) (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' WET DIRTY SOCKS SMELL OBSERVED IN COCKPIT, FRONT GALLEY AND AFT GALLEY DURING TAXI. SMELL INTENSIFIED AND CHANGED TO A SLIGHTLY BURNING SMELL AFTER TAKEOFF. DURING DESCENT SMELL CHANGED BACK TO DIRTYU SOCKS AND INCREASED IN INTENSITY. SMELL DURING ALL PHASES OCCURRED WHILE ENGINES FOR BLEED AIR; T/S SHOT TO #1 ENG AT FAULT REF LOG PAGE 3727248-2 (REF WO 1278279 FOR ALL WORK ACCOMPLISHED & INSPECTION ITEMS FOR REMOVAL AND REPLACEMENT OF #1 ENG) FOR REPLACEMENT. PERFORMED ECS DECONTAMINATION PER AMM 21-00-00-615-802-A OPERATED PACKS USING ENGINE/ APU BLEED NO ORDOR PRESENT.
FLT#1621, LHR-BOS. (ETOPS) 'WHILE DESCENDING THRU 8000' WITH THRUST AT IDLE A STRONG DIRTY SOCK SMELL APPEARED. ODOR WAS STRONG ENOUGH IN CABIN FOR IN-FLIGHT TO CALL TO REPORT IOT. ODOR THROUGHOUT OUT CABIN AND COCK PIT ODOR PERSISTED TO THE GATE NO TROUBLESHOOTING ATTEMPTED; REF DEFECT 3727229 (ACCOMPLISHED TSM 05-50-00-810-831-A. C/W INFO NOTICE 2017-T015J AND SUBTASK TSM 05-50-00-810-085-D. APU OVERSERVICED. REMOVED OIL FROM APU. DECONTAMINATION ACCOMPLISHED.) FOR RESOLUTION, ALSO REPLACED OZONE FILTER #2 PER AMM 21-51-41.- A/C GOOD FOR SERVICE.'
FLT#1408, CDG-JFK. (ETOPS) (AIRCRAFT DIVERTED TO LHR) 'FLIGHT MANAGEMENT COMPUTERS GIVING ERRONEOUS INFORMATION IN FLIGHT. BOTH COMPUTERS WERE HAVING FLUCTUATIONS IN BOTH TIMES TO FIXES AND DISTANCES. DESTINATION DISTANCES RANGED FROM 3000 MILES TO 9999 MILES. TIMES VARIED FROM 1 TO 10 HOURS. FUEL VARIED FROM 8.0 AT LANDING TO -56.0 AT LANDING; REMOVED ADN REPLACED FMGC #1 IAW AMM 22-82-34. OPS TEST OK. CROSSLOAD COMPLETED AND ALL SOFTWARES MATCH. A/C OK TO CONTINUE FOR SERVICE
FLT#20, LHR-JFK. (ETOPS) 'ENG 1 MAIN OIL FILTER CAP DAMAGED; REMOVED AND REPLACED ENG 1 MAIN OIL FILTER CAP IAW TASK CARD NO. A320-79-21-06-960-801-A.' (SUPPLEMENTAL INFORMATION ADDED)
FLT#44, LGW-JFK. (ETOPS) 'WO# 1274801 TSI P2 REGUR FAUL ASSIGNED; ACCOMPLISHED WO 1274801 TSI PACK 2 TEM CONTROL R/R OPS CHECK NORAML REF AMM 21-61-11.'
FLT#1620, BOS-LHR. (ETOPS) 'DETEC FAULT ECAM AT 7000 DURING CLIMB OUT FOLLOWED QRH PROCEDURE ACCOMPLISHED RESET PROCEDURE ACCORDING TO MCC INSTRUCTIONS MESSAGE WENT AWAY BUT RETURNED BRIEFLY SEVERAL TIME DURING FLIGHT ( CIDS SYSTEM - DIRECTOR N703-UP. REMOVED AND REPLACED CIDS DIRECTOR #1 IAW AMM 23-73-34. PERFORMED ORBU SOFTWARE UPLOAD VIA FAP IAW AMM 23-73-00-869-001-A. FAULT CLEARED. OPS CHECK GOOD. MDDR CLEARED.
FLT#1621, LHR-BOS. (ETOPS) CIDS 2 CLASS II MX ( CLASS II MX MSG DISPLAYED - CIDS ). REMOVED AND REPLACED CIDS DIRECTOR #1 IAW AMM 23-73-34. PERFORMED ORBU SOFTWARE UPLOAD VIA FAP IAW AMM 23-73-00-869-001-A. FAULT CLEARED. OPS CHECK GOOD. MDDR CLEARED.
FLT#1621, LHR-BOS. (ETOPS) 'AUTO FLT FCU 2 FAULT X2 (RESET ON GROUND, UNSUCCESSFUL RESET IN FLIGHT); REMOVED AND REPLACED FCU. OPS CHECK GOOD REF AMM 22-81-12.'
FLT#44, LGW-JFK. (ETOPS) 'ENG 2 FIRE LOOP A FAULT; T/S PER TSM: 26-12-00-810-805-A. #2 ENGINE LOOP " HARNESS CHANGED DUE TO DAMAGE, REF L/P 3764382-1 (REF TSM 26-12-00-810-805-A, UPON VISUAL INSPECTION, FOUND CORE -AGB LOOP A, FIRE DETECTOR (4002WD1) HARNESS DAMAGED AND CLAMP DAMAGED, ON ENG 2. ORIGINAL WRITEUPREMAINS OPEN.) AND 3764384-2 (REMOVED AND REPLACED AGB CORE DET RAIL AND CABLE ASSEMBLIES 4181KS & 4182KS AIW AMM 26-12-61. OPS CHECK FAILED, ENG #2 LOOP A FAULT STILL PRESENT. FURTHER T/S REQUIRED. REF LOG PAGE 3764380 ITEM1 FOR THE MAIN ITEM. REF AMM 26-10-00 BITE TEST OF LOOP B NORMAL ). FURTHER T/S FOUND #2 ENGINE LOOP "A" AGB CORE FIRE DETECTOR SHORTING TO SHIELD ON BOTH PINS A+C. REMOVED AND REPLACED AGB CORE FIRE DET ( 4002WD1) PER AMM 26-12-17. OPS TEST OF FIRE AND O/H DETECTION GOOD, NO FAULTS OF ECAM MESSAGES, AMM 26-12-00.'
FLT#2104, BOS-LGW. (ETOPS) 'ENGINE 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ); REMOVED AND REPLACED FDU #2 AS PER AMM 26-12-34 AND PER UPPER LEADERSHIP. OP'S CHECK IS GOOD. MX-4 UPDATED. PLACARD REMOVED. MDDR CLEARED.'
FLT#44, LGW-JFK. (ETOPS) ' ENG 1 IGNITION B INOP ( IGNITION SYSTEMS - SYSTEM B ); REMOVED AND RELACED ENG 1 IGN B IGNITOR IAW PW MM 74-21-61. THE OPS CHECK IS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.
ETOPS. FLT# 2220, (LHR-JFK). EPSU BATT (10WL) OVER TEMP; R/R EPSU BATT 10WL IAW AMM 33-51-00.
ETOPS. FLT# 2220, (LHR-JFK). EPSU BATT (11WL) OVER TEMP; R/R EPSU BATT 11WL IAW AMM 33-51-00.
FLT#1620, BOS-LHR. (ETOPS) 'FUEL ACT TRANSFER FAULT MESSAGE APPEARED AGAIN DURING THE CRUISE. FUEL WAS TRANSFERRED MANUALLY PER QRH PROCEDURE THERE WERE 3400 LBS OF FUEL LEFT IN ACT 1 WHEN THE MESSAGE CAME UP ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ). PERFORMED OPS TEST OF THE ADDITIONAL CENTER TANK AUTO TRANSFER SYSTEM IAW AMM 28-28-00-710-005-A. OPS TEST IS GOOD. AS PRECAUTIONARY REMOVED AND REPLACED ALSCU IAW AMM 28-46-35. MDDR CLEARED. PLACARD REMOVED. UPDATED MX-4.
FLT#2104, BOS-LGW. (ETOPS) 'NO.1 ENG AFT ACCOUSITIC LINER AT 5 O' CLOCK AFT LOOKING FORWARD, SMALL PUNCTURE IN LINER, APPROX 5MM DIAMETER. PERFORMED REPAIR TO ENG 1 ACOUSTIC (REAR) LINES AT 5 O'CLOCK POSITION IAW AMM 72-21-01. MDDR CLEARED. MX-4 UPDATED.
FLT#1107, JFK-LHR. (ETOPS) ' ECAM ENG 2 FIRE LOOP A FAULT; TROUBLESHOOTING. CARRIED OUT IAW TSM 26-12-00-810-805A REV 01FEB2023 AND OPERATIONAL TEST OF ENG FIE AND OVERHEAT DETECTION CARRIED OUT IAW AMM 26-12-00-710-002A REV -01FEB 2023. NO FAULTS RECORDED.'
FLT#7, JFK-LHR. (ETOPS) 'MAINT AIR BLEED MSG ( 36-00-00-C CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY AIR BLEED ). NO ACTIVE FAULTS NO ECAM NOTED; BITE CHECK PERFORMED OF BMC'S NO FAULTS NOTED REF AMM 36-11-00-740-802A; OK FOR CONTINUED SERVICE. MDDR CLEARED. MX-4 UPDATED. MCC NOTIFIED.
FLT#20, LHR-JFK. (ETOPS) 'ON HYD PAGE ENG 2 EDP SHOWS IN LINE GREEN WITH HYD ENG 2 PUMP PUSH BUTTON SWITCH IN AUTO .- DEPRESSUIZTION FUNCTION (ENGINE DRIVEN PUMP SYS - DEPRESS FUNC); REF AWM 29-13-02, CHK WIRING AT FIN 3074GD SHIELDING AND WIRE. THE CONTINUITY CHECK IS GOOD. REMOVED AND REPLACED ENG 2 PUMP PRESS SWITCH FIN 3074GD AS A PRECAUTIONARY T/SHOOTING IAW 29-12-00. RAN ENG 2 AT IDLE AND OPS TEST YELLOW HYD SYS IAW 29-13-00 WITH FLT CONTROLS OPS TEST. ALL OPS CHECK IS NORMAL. CLEARED MDDR# 493753. MX-4 UPDATED AND MCC NOTIFIED.'
FLT # 43, JFK-LGW. SMOKE FWD CRG DET FAULT & AFT CRG DET FAULT ECAM IN FLIGHT ; TSM 26-16-00-810-809A REV NOV 08/ 2022 PERFORMED, RESET OF CIDS SDF CARRIED OUT. GROUND SCAN CARRIED OUT + SYSTEM TEST CARRIED OUT. NIL FAULTS
FLT#43, JFK-LGW. (ETOPS) 'FUEL ACT XFR FAULT ON ECAM ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT)); FOUND AFT 1 ACT NOT TAKING ANY FUEL WHILE REFUELING, RESEATED PIN "G" AT TB 40009VT4. AFT1 ACT IS NOW TAKING FUEL. OPS TEST GOOD REF AMM 28-28-00-710-005-A. MDDR CLEARED, PLACARD REMOVED. UPDATED MX-4.
FLT#1926, LGW-BOS. (ETOPS) 'HYDRAULIC FLUID LEAKING FROM RH WING PANEL 674BB. PANELS 674BB AND 674AB WERE REMOVED; FOUND O-RING ON YELLOW ENG DRIVEN PUMP HYD PULSATION DAMPER LEAKING. REPLACED O-RING ON HYD PULSATION DAMPER. OPS & LEAK CHECKS ARE GOOD. NO LEAKS NOTED AT THIS TIME. REF AMM 29-13-53. RT WING PNL INSTALLATION 674BB & 674AB TRANSFERRED TO L/P # 3438424, ITEM 1 (INSTALLED R WING PANELS 674 AB AND 674BB IAW AMM 57-51-37.).' (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)
(ETOPS)FLT# 44, LGW-JFK. TEMP CTL 1 CLASS 2 MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 4) FAULT(S) INDICATED BY TEMP CTL 1 (2) ); ITEM PLACED ON MEL 21-00-00, CAT'C', PER MCC ACKEEM, MDDR 479640, MX4 UPDATED AND PLACARD INSTALLED. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE IAW AMM 21-51-51. OPS CHK OK. MDDR 479640 CLEARED. (SUPPLEMENTAL INFORMATION)
FLT# 44, LGW-JFK. CLASS 2 MAINTENANCE MESSAGE CIDS 1 DIRECTOR INOP. ( CLASS II MX MSG DISPLAYED - CIDS ); REMOVED + REPLACED CIDS DIRECTOR # 1 FIN 101RH IAW AMM 23-73-34 THIS CLEARS MDDR
FLT#44, LGW-JFK. (ETOPS) ' WHEN STARTING ENG 1 WE RECEIVED MULTIPLE WARNINGS INCLUDING "STALL, RETARD, AND TRAFFIC ALERTS. ALSO, MULTIPLE ECAM MESSAGES APPEARED INCLUDING ALL ENG FAIL, L&R EIU FAULT, B&Y SYSTEM LO PR, G&B SYS LO PR, AND LFRWD OVERWING FAULT. INOP SYSTEM INCLUDES OVERWING AND CVR; FWC 1 & 2 RESET C/OUT IAW AMM 31-52-00. ENG 1 &2 EGR IDLE POWER FOR OPSCHK C/OUT IAW AMM 72-00-00. NO FAULT WAS REPORTED, AND ENG RUN WAS PERFORMED BY THE FLIGHT CREW. '
FLT#44, LGW-JFK. (ETOPS) 'MCDU 2 NOT PROVIDING SNED PROMPT (*) FOR FLIGHT PLAN-RELATED REQUESTS. SPECIFICALLY: NO PROMPT FOR: INIT / INIT REQUEST AND F.PLN / WIND TEMP/ WIND / TEMP REQUEST. MCDU 2 DID PROVIDE SEND PROMPTS FOR ACARS-DRIVEN FUNCTIONS; RESET FMGC #2 PERFORMED AFS TEST REF AMM 22-96-00. NO FAULTS RE-ALIGNED ADIRS ALL FUNCTIONS ON MCDU ON FO'S NORMAL.' (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)
FLT#20, LHR-JFK. (ETOPS) 'CANNOT TRANSFER FUEL OUT OF ALL ACT USING MANUAL TRANSFER. THE PUMP DOES NOT TURN ON; FOUND 122 QH RELAY AT FAULT. REMOVED AND REPLACED 122 QH RELAY IAW ESPM 20-46-50. OPS CHECK NORMAL. FUEL TRANSFER OPS NORMAL GFI FUNCTION. OPS CHECK NORM PER TASK A320-28-18-00-710-803-A.'
FLT#20, LHR-JFK (ETOPS).' AFT TEMP SENSOR READING NOTABLY WARMER THAN ACTUAL WAS ABLE TO MAINTAIN AN ACCEPTABLY COMFORTABLE TEMP BY ADJUSTING FLT DECK CONTROLS; ACCOMPLISHED RESET OF TEMP CONTROL SYSTEM AND OPS CHECK. CFOS CHECK GOOD REF AMM 21-63-00-710-004. CABIN TEMP IN AFT FELT NORMAL W/SW IN CM POSITION IN COCKPIT.'
FLT#20, LHR-JFK (ETOPS). ' TEST OF EMERGENCY O2 SYSTEM DUE TO TSI 41316 ACCOMPLISHED; ACCOMPLISHED TEST OF EMERGENCY O2 SYSTEM IAW AMM 35-23-00. TEST OK.'
(ETOPS) FLT #43, JFK-LGW. ENG 2 MINOR FAULT ( MINOR FAULT CAUTIONS ON ECAM EWD; PLACED ENG 2 MINOR FAULT ON CA-MEL 73-30-05, CAT C. PLACARD INSTALLED. MCC DAVID NOTIFIED. MX-4 UPDATED); R/R EEC #2 ENG IAW AMM 73-21-01. OPS CHECK GOOD. THIS CLEARS MDDR 468999. MX-4 UPDATED. MCC NOTIFIED). (ON 4/2/2022, WHEN THE DEFECT WAS DEFERRED, NO ETOPS SIGNIFICANT SYSTEM WAS DISTURBED. HOWEVER, AFTER TROUBLESHOOTING ON 4/10/ 2022, THE #2 ENG EEC WAS CHANGED, WHICH DISTURBED AN ETOPS SIGNIFICANT SYSTEM. AS SUCH, THE ITEM NOW MEETS THE ETOPS SIGNIFICANT SYSTEM REPORTABLE CRITERIA).
FLT#43, JFK-LGW. (ETOPS).' DURING THE START OF ENGINE 1, RECEIVED ENGINE START FAULT. NO IGNITION ON IGN A. ECAM/QRH COMPLIED WITH. TORCHING NOTED BY GROUND CREW ODOR NOTED FROM P ACKS AFTER START ATTEMPT; ACCOMPLISHED T/S IAW AMM 71-00-810-850-A SUSPECT IGN A DID NOT LIGHT OFF. ITEM CLEARED ON L/P 3298968 ITEM #2 FOR REMOVAL AND REPLACEMENT OF IGNITION PLUG A. A/C OK FOR RETURN TO SERVICE.' (SUPPLEMENTAL ADDED TO THE FLIGHT NUMBER AND TIME/CYCLE). (SUPPLEMENTAL TO FOLLOW)
(ETOPS) FLT # 44, LGW-JFK. FORWARD & AFT CARGO DET FAULT ; SDF SYS #2 SHOWS CIDS 1 SDF 1 FAULT - RESET CIDS DIR 1 & 2 PER TSM 26-17-00-810-823-A RESET NORMAL REF L/P 3295059-2 FOR GROUND VERIFICATION OF SYSTEM. PERFORMED GROUND VERIFICATION OF CIDS 1, CIDS 2, SDF 1, SDF 2 PER AMM 26-10-00-710-801-A AND CARGO SMOKE PTT TEST IAW AMM 26-16-00-710. OPS CHECK OK. A/C OK FOR CONT SVC
(ETOPS) FLT 20, LHR-JFK. P1-TSI R/R FCU DUE TO PREVIOUS WRITE-UP, PLEASE REMOVE AND REPLACE THE FCU PER AMM 22-81-012. PLEASE MARK THE OLD UNIT AS SOS. ; (RESOLVED ON W/O: 1146268 TASKCARD: NR-00001 ) R/R FCU REF AMM 22-81-12/
(ETOPS) FLT 7, JFK-LHR. CREW REPORTED FCU 1 FAULT; PERFORMED POWER DOWN AND POWER UP OF AIRCRAFT. MESSAGE CLEARED. PERFORMED OPS CHECK PER AMM 22-96-00-710-001-A. NO FAULTS NOTED.
ETOPS: FLT 2824,LAX-JFK.P2 TSI - FUEL X FEED VALVE FAULT N4022J HAS HAD REPEAT HITS IN AIRMAN FOR FUEL X FEED VALVE FAULT. THIS IS AN ETOPS SIGNIFICANT SYSTEM. MESSAGE IS ALSO A NO DISPATCH CONDITION ACCOMPLISH TSM 28-23-00-810-801A. ENSURE WIRE CHECKS ARE ACCOMPLISHED PRIOR TO ANY PART REPLACEMENT. ****ETOPS SIG SYSTEM**** ENSURE GMM AND RII REQUIREMENTS ARE COMPLIED WITH. ; ACCOMPLISHED TSM 28-23-00-810-801A (WIRING CHECKS ACCOMPLISHED) NO DEFECTS FOUND. AS PRECAUTIONARY R+R CROSSFEED VALVE ACTUATOR 5QE IAW AMM 28-23-51. OPS CHECK GOOD
ETOPS: FLT 7, JFK-LHR. RECEIVED ECAM FOR ENGINE #2 START FAULT. AUTOCRANK AND AUTO RESTART SUCCESSFUL. RESULTED IN TANGENTIAL FAILURE ECAM FOR ENGINE #2 IGNITION "A" FAULT; R & R ENG #1 IGNITER A REF AMM 74-21-01. IGNITER TEST AND IDLE ENGINE RUN REF AMM 71-00-00 SUCCESSFUL
ETOPS: FLT 20, LHR-JFK. FLIGHT ATTENDENT CIDS CATION LIGHT COMES ON IT FLICKERS OR RESET ITSELF. CABIN LIGHTS COME ON/OFF WITH ASSOCIATED RH ATTENDENT CID PANEL CAUTION LIGHT ; R & R CIDS #1 IAW AMM 73-34-04 ALL OPS CHECKS GOOD AND SOFTWARE LOADS
ETOPS: FLT 2023, JFK-LAX. SMOKE AFT CRG DET FAULT MESSAGE; R & R SMOKE DETECTOR 10WH, AFT CARGO, PER AMM 26-16-15 GROUND SCANNING ON SDF 1 AND 2 DISPLAYS LRU INFORMATION. NO NEW FAULTS DETECTED DURING TEST.
ETOPS: FLT 324, LAX-JFK. OIL LEAKING FROM # 2 ENG IDG VENT/BREATHER; R & R ENG 2 IDG. LEAK AND OPS TEST GOOD. ALL PARAMETERS OK. NO LEAKS NOTED. REF MM 24-21-51.