N634JB
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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FLT 767, MCO-PSA (AIR RETURNED TO MCO) HYD Y REVR OVHT PASSING FL 220.; TROUBLESHOT PER TSM 29-13-00-810-802-A. R & R CHECK VALVE Y FIN (3083GM) PER AMM 29-24-21. ALSO REPLACED FILTER CARTRIDGE FOR LP & HP FILTERS (3002GM) & (3048GM) IAW AMM 29-13-43. LEAK AND OPS CHKD GOOD.
FLT#488, MCO-ORH. (AIRCRAFT DIVERTED TO BOS). 'EXTREMELY LOUD SQUEAL DEVELOPED OVERHEAD BY THE COCKPIT DOOR, AT FL 370, CABIN PRESS 7400 FT. DESCENDED TO FL 330, CABIN PRESS 6050 FT SQUEAL STOPPED AFTER 10-15 MIN; REF LPG 4324310 ITEM 2 AND LPG 4324311 ITEM 2 R+R RIVET AT FR 16 STR 1R AND PRESSURIZATION TEST FOR LEAK CHECK PERFORMED SATISFACTORILY PER SRM 51-42-11. AND AMM 05-53-00. A/C OK FOR CONTINUED SVC.'
FLT#592, TPA-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO TPA). 'HYD G RSVR LO LVL COMPLETE LOSS OF HYD G SYSTEM IN FLIGHT. EMERGENCY GEAR EXTENSION POR GRH; REF L/P 4168061-2 (FOUND RH OUTBOARD LOCKSTAY ACTUATOR HOSE BROKEN REMOVED AND REPLACED LOCKSTAY ACTUATOR HOSE IAW AMM 32-11-22-400-001. SERVICED GREEN SYS HYD PERFORMED LEAK TEST OF ACT HOSE NO LEAKS NOTED. FUNCTIONAL TEST REQUIRED ) FOR REPLACEMENT OF R/H MLG O/B LOCKSTAY HOSE. REF L/P 4168062-1(PUT LANDING GEAR SYSTEM BACK TO NORMAL MOVE AFTER FREE FALL EXTENSION IAW AMM 32-00-00-860-003-A.) FOR RETURNING L/G TO NORMAL MODE AFTER EMERGENCY GEAR EXTENSION. REF L/P 4168063-1 (ACCOMPLISHED FUNCTIONAL CHK OF LDG EXTENSION AND RETRACTION IAW AMM 32-31-00-720-002-A. OPS CHECK GOOD, MDDR CLEARED, MX-4 UPDATED. VMO SWITCH RETURNED TO NORMAL CONF.) LANDING GEAR RETRACTION SYSTEM PLACED ON MEL DUE TO GEAR SWING REQ'D FOR LOCKSTAY HOSE REPLACEMENT FUNCTIONAL CHECK.'
FLT#987, ORH-MCO. 'OIL SMELL IN FLIGHT DECK ONLY. APU BLEED WAS ON; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A ISOLATED FAULT TO TYPE 10 EVIERMENTAL PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085-D REVIEWED PAST 30 DAYS FOR HISTORY NO HISTORY FOUND FOR ODOR EVENT. AIRCRAFT IS OK FOR SERVICE.'
FLT#8445, DEN-JFK. ' L2 EMERGENCY EXIT LIGHT BURNED OUT ( EXIT MARKING SIGNS (WITHOUT PASSENGERS) ); REPLACED L1 AND L2 EMERGENCY LIGHTS. RELAMPED IAW AM 33-51-11. OPS CHK GOOD IAW AMM 33-51-00-710-001. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.'
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH JOOGLE AREA FROM HOLE ÃA AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA (CRACK LENGTH IS 0.111 INCH AND CRA CK DIRECTION IS 2:00 O CLOCK); REF AEROMAN NR 2023-481375 WO 2023 273/2 PERFORMED PERMANENT REPAIR ON FRAME 16 LH JOOGLE AREA FROM HOLE #A AT DOOR STOP FITTING 7 IAW REPAIR DRAWING R53113041 ISSUE E, TOOLS USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D, SN: 220272512, DUE DATE: DEC-17-2023, MICROMETER P/N:293-344-30; S/N:71690646; DUE DATE: NOV-29-2023 AND SMALL P/N:154-901; S/N: AE-412975; DUE DATE: SEP-05-2023, DIGITAL CALIPER P/N: 500-196-30, S/N: A22344320, DUE DATE: JUL-13-2024, CALIPER P/N: 700-113-10, S/N: 0019306, DUE DATE: NOV-21-2023, CALIPER P/N 500-196-30 S/N B21140348 DUE DATE JUL-21-2024, SMALL HOLE GAUGES P/N: 154-901, S/N: AE-411361, DUE DATE: JAN-27-2024, EQUIPMENT P/N: 45MG, S/N: 221859911, DUE DATE: NOV-07-2023. DONE BY R. FIGUEROA 8620311 CHECKED BY E. NARVAEZ 8632715.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH JOOGLE AREA FROM HOLE Ã4 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA (CRACK LENGTH IS 0.088 INCH AND CRA CK DIRECTION IS 7:30 O CLOCK); REF AEROMAN NR 2023-481371 WO 2023 273 /1 PERFORMED PERMANENT REPAIR LOC ON FRAME 20 RH JOOGLE AREA FROM HOLE #4 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA IAW REPAIR DRAWING # R53113041. TOOL USED: EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. TOOL USED MICROMETER P/N:293-344-30; S/N:71690646; DUE DATE:NOV-29-2023 AND SMALL P/N:154901; S/N:AE-412975; DUE DATE: SEP-05-2023. TOOL USED CALIPER P/N= 500-196-30, S/N= B21140348, DUE DATE: JUL-21-2024. SMALL HOLE GAUGES P/N= 154-901, S/N= SE-411361, DUE DATE= JAN-27-2024. TOOL USED: KIT TOOL P/N: FTI-A320-52-1071-1,S/N= AE-27068, DUE DATE: JAN-19-2024. COMBINATION GAGE P/N= CBG-8-1-N-1, S/N= AE-410430, DUE DATE; NOV-01-2023. DONE BY R. TREJO 8617713 CHECKED BY C. RAMIREZ 8649208.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 LH JOOGLE AREA FROM HOLE ÃB AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA (CRACK LENGTH IS 0.058 INCH AND CRA CK DIRECTION IS 9:00 O CLOCK; REF AEROMAN NR 2023-481373 WO 2023 273/1 PERFORMED PERMANENT REPAIR LOC FRAME 20 LH JOOGLE AREA FROM HOLE #B AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA IAW REPAIR DRAWING # R53113041. TOOL USED: EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. TOOL USED MICROMETER P/N:293-344-30; S/N:71690646; DUE DATE:NOV-29-2023 AND SMALL P/N:154-901;S/N:AE-412975; DUE DATE: SEP-05-2023. TOOL USED CALIPER P/N 500-196-30 S/N B21140348 DUE DATE JUL-21-2024, SMALL HOLE GAUGES P/N 154-901 S/N AE-411361 DUE DATE JAN-27-2024. DONE BY R. TREJO 8617713 CHECKED BY E. ARGUETA 8619800.
DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE FITTING LOC AT FR65 BTW STR 42L TO STR 42R IN AFT CARGO COMPARTMENT ( 1EA );(RESOLVED ON W/O: 1240603 TASKCARD: NR-00018 ) REF AEROMAN WO 2023 273/ 1 NR 481489 REMOVED AND REPLACED FITTING LOC. AT FR65 BTW STR43L TO STR43R IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DRAWING D53480054.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1 .1MM APPROX); REF AEROMAN WO 2023 273/1 NR 481368 -- REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1.1 MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N:154-901;S/N:AE-411361; DUE DATE: JAN-27-2024, MICROMETERS P/N:293-345-30;S/N:71699858; DUE DATE:NOV-21-2023, EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. DONE BY Y. MENA 8672120 CHECKED BY
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H1 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1 MM APPROX ); REF AEROMAN WO 2023 273/1 NR 2023-481369 --REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H1 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED: SMALL HOLE GAUGES P/N:154-901, S/N:AE-411361, DUE DATE: JAN-27-2024, MICROMETERS P/N:293-345-30;S/N:71699858; DUE DATE:NOV-21-2023, EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. DONE BY Y. ME.
DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE FITTING LOC AT FR65 BTW STR 42L TO STR 42R IN AFT CARGO COMPARTMENT ( 1EA ); REF AEROMAN WO 2023 273/ 1 NR 481489 REMOVED AND REPLACED FITTING LOC. AT FR65 BTW STR43L TO STR43R IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DRAWING D53480054. COMPLETED MX-220 FORM BY CPCP PROGRAM. DONE BY E. RODRIGUEZ 8633115. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H1 LOCATED AT FRAME 20 LH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1 MM APPROX); REF AEROMAN WO 2023 273/ NR 481363- REMOVED AND RE-INSTALLED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H1 LOCATED AT FRAME 20 LH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED: SMALL HOLE GAUGES P/N:154-901;S/N:AE-411361; DUE DATE: JAN-27-2024, MICROMETERS P/N:293-344-30;S/N:71690646; DUE DATE: NOV-29-2023, EDDY CURRENT EQUIPMENT, PN:NORTEC 600D, SN:220272512, DUE DATE: DEC-17-202 DONE BY Y.MENA 8672120.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H3 LOCATED AT FRAME 16 LH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0 .7 MM APPROX); REF AEROMAN W.O. 2023 273/1 NR481365--REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0.7 MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N:154-901, S/N:AE-411361,DUE DATE: JAN-27-2024, MICROMETERS P/N:293-344-30;S/N:71690646; DUE DATE:NOV-29-2023, EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D, SN: 210138203, CAL DUE DATE: JUN-09-2024. DONE BY Y. MENA 8672120.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H1 LOCATED AT FRAME 16 LH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0 .73MM APRROX); REFERENCE AEROMAN WO2023 273/1 NR481366 -- REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H1 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0.73 MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N:154-901;S/N:AE-411361; DUE DATE: JAN-27-2024, MICROMETERS P/N:293-344-30;S/N:71690646; DUE DATE:NOV-29-2023, EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D, SN: 210138203, CAL DUE DATE: JUN-09-2024. DONE BY Y. MENA 8672120.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOL E H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1 .1MM APPROX); REF AEROMAN WO 2023 273/1 NR 481368 -- REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1.1 MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N:154-901;S/N:AE-411361; DUE DATE: JAN-27-2024, MICROMETERS P/N:293-345-30;S/N:71699858; DUE DATE:NOV-21-2023, EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. DONE BY Y. MENA 8672120 CHECKED BY
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH JOOGLE AREA FROM HOLE Ã6 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA (CRACK LENGTH IS 0.128 INCH AND CRA CK DIRECTION IS 9:00 O CLOCK); REF AEROMAN NR 2023 481372 WO 2023 273/1 PERFORMED PERMANENT REPAIR LOC FRAME 20 RH JOOGLE AREA FROM HOLE #6 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA IAW REPAIR DRAWING # R53113041. TOOL USED TOOL USED: EDDY CURRENT EQUIPMENT PN 600D SN 220272512 DUE DATE DEC-17-2023. TOOL USED MICROMETER P/N:293-344-30; S/N:71690646; DUE DATE:NOV-29-2023 AND SMALL P/N:154-901;S/N:AE-412975; DUE DATE: SEP-05-2023. TOOL USED CALIPER P/N= 500-196-30, S/N= B21140348, DUE DATE: JUL-21-2024. SMALL HOLE GAUGES P/N= 154-901, S/N= SE-411361, DUE DATE= JAN-27-2024. TOOL USED: KIT TOOL FTI-A320-52-1071-1, S/N= AE-27068, DUE DATE: JAN-19-2024. COMBINATION GAGE P/N= CBG-8-1-N-1, S/N= AE-410430, DUE DATE; NOV-01-2023.
DURING HEAVY MAINTENANCE: TOOL MARK ON EXTERNAL SKIN LOC ON FR 58 AND BTW STR36L TO STR 37L AT L OWER FUSELAGE; EVALUATED TOOL MARK ON EXTERNAL SKIN LOC ON FR 58 AND BTW STR36L TO STR 37L AT LOWER FUSELAGE AND FOUND WITHIN LIMITS IAW SRM A320 51-73-11 PARAGRAPH 5, THIS ADL IS CLASSIFIED CATEGORY A, AND NOT FURTHER INSPECTION IS REQUIRED TOOL USED: DEPTH GAGES P/N: 20915A21 S/N: 009279 DUE DATE: MAR-05-2024; CALIPER P/N: 500-197-30 S/N: B16144234 DUE DATE: MAR-27-2024.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON WEB FRAME 20 COMMON TO DOOR STOP FITTING 1 FROM HO LE H1 LOCATED AT FRAME 20 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1.8MM APPROX); REF. AEROMAN WO 2023 273/1 NR 481370-- REMOVED AND RE-INSTALLED INTERCOSTAL COMMON TO DOOR STOP FITTING 1 FROM HOLE H1 LOCATED AT FRAME 20 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 1MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N: 154-901, S/N:AE-411361, DUE DATE: JAN-27-2024 MICROMETERS P/N:293-345-30, S/N:71699858; DUE DATE:NOV-21-2023, EDDY CURRENT EQUIPMENT, PN: NORTEC 600D, SN: 220272512 DUE DATE DEC-17-2023. DONE BY Y. MENA 8672120.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL COMMON TO DOOR STOP FITTING 1 FROM HOL E H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0 .8MM APPROX); REF. AEROMAN WO 2023 273/1 NR 2023-481367 -- REMOVED AND REPLACED INTERCOSTAL COMMON TO DOOR STOP FITTING 7 FROM HOLE H3 LOCATED AT FRAME 16 RH SIDE AT FWD GALLEY AREA (CRACK LENGTH IS 0.8 MM APPROX ) IAW A320 SRM 51-42-11 AND DWG D53114097. TOOL USED SMALL HOLE GAUGES P/N:154-901, S/N:AE-411361, DUE DATE: JAN-27-2024, MICROMETERS P/N:293-345-30;S/N:71699858; DUE DATE:NOV-21-2023, EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 220272512 DUE DATE DEC-17-2023. DONE BY Y. MENA 8672120.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH JOOGLE AREA FROM HOLE Ã8 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA (CRACK LENGTH IS 0.124 INCH AND CRA CK DIRECTION IS 9:00 O CLOCK); REF AEROMAN NR 2023-481374 WO 2023 273/1 PERFORMED PERMANENT REPAIR ON FRAME 16 RH JOOGLE AREA FROM HOLE #8 AT DOOR STOP FITTING 7 LEVEL AT FWD GALLEY AREA IAW REPAIR DRAWING R53113041 ISSUE E, TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D, S/N: 220272512 DUE DATE DEC-17-2023, MICROMETER P/N:293-344-30; S/N:71690646; DUE DATE: NOV-29-2023 AND SMALL HOLE GAGE P/N:154-901; S/N: AE-412975; DUE DATE: SEP-05-2023, DIGITAL CALIPER P/N: 500-196-30, S/N: A22344320, DUE DATE: JUL-13-2024. DONE BY R. FIGUEROA 8620311 CHECKED BY E. NARVAEZ 8632715.
FLT#2110, SDQ-JFK. 'WET DOG ODOR FROM PACKS IN AFT CABIN ( APU BLEED AIR SUPPLY SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#2901, JFK-FLL. 'F/A REPORTS CABIN LIGHTS FLICKERED AND A BURNING ELECTRICAL SMELL; PERFORMED INSPECTION OF FWD GALLEY AREA, LIVE TV EQUIPMENT, NO ELECTRICAL BURNING AREA FOUND IAW AMM 24-00-00.'
DURING HEAVY MAINTENANCE: FUSELAGE / TAIL CONE / FR 83-85 & STGR 3L-6L / IMPACT DAMAGE -PRELIMINARY INSPECTIONS. (SUPPLEMENTAL TO FOLLOW)
FLT#1957, FLL-BOG. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' WEATHER RADAR FAULTY. ON X OFF FAILURES SHOWED & CYCLED BETWEEN WX ANT IN RED X WX RF IN RED. TURNING WX OFF WILL FIX THE ISSUE FOR A FEW MINUTES THEN FAULTY AGAIN; REMOVED AND REPLACED DRIVE WEATHER RADAR ANTENNA IAW AMM 34-41-11. OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME. A/C OK TO CONTINUE TO SERVICE.'
DURING HEAVY MAINTENANCE, L1 DOOR SLIDE FAILS EMERGENCY LIGHT TEST; REF AEROMAN NR 2022-233167 W/O 2022 8/1: REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-62-44-000-012-A, AMM 25-62-44-400-007-A, AND AMM 33-51-00-710-001. OPS CHECKS GOOD.'
DURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AT OVERWING EXIT DOOR (AFT RH EEH DOOR 844) L=0.133"; REF AEROMAN NR 2022-233226 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.
DURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AFT OVERWING EXIT DOOR FWD RH EEH DOOR (843) L= 0.130"; REF AEROMAN NR 2022-233223 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.
DURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AFT OVERWING EXIT DOOR (FWD LH EEH DOOR 833) L= 0.128"; REF AEROMAN NR 2022-233224 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.
DURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AT OVERWING EXIT DOOR (AFT LH EEH DOOR 834) L=0.135"; REF AEROMAN NR 2022-233225 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.
DURING HEAVY MAINTENANCE, R1 DOOR SLIDE FAILS EMERGENCY LIGHT TEST; REMOVED AND REPLACED R1 DOOR SLIDE REF AEROMAN NR 2022-233166 W/O 2022 8/1: IAW AMM 25-62-44-000-804-A, AMM 25-62-44-400-803-A AND AMM 33-51-00-710-001. OPS CHECKS OK.'
FLT#2511, JFK-FLL.' HYD G RESERVOIR LOW LEVEL IN FLIGHT; REF LINE CHANGE LOG PAGE 3247689-1 SYS SERVICED AS REQUIRED ALL OPS AND LEAK CHECKS ACCOMPLISHED. NO DEFECTS WERE NOTED. 27-00-00-28.LOG PAGE 3247689-1: INSTALLED PRESSURE LINE AS REQUIRED IAW 29-11-49.'
DURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN VACUUM VALVE BETWEEN FR 60 TO FR 70 RT SIDE LOWER FUSELAGE, REF AEROMAN N/R 2020-375163 WO 2020 88/1. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE LOCATED BETWEEN FR 69 TO FR 70 AND STR 30R TO STR 33R, IAW A320 SRM 53-41-11-300-004. THIS IS A CATAGORY A MAJOR REPAIR AND NOT FURTHER INSPECTION IS REQUIRED.
DURING HEAVY MAINTENANCE, ITEM TRANSFERRED FROM AEROMAN WO 2020 88/1 NR 2020-375134 DURING OPERATIONAL CHECK OF THE SLIDE RAFT. THE SLIDE RAFT TOUCHED THE FUSELAGE SKIN ON DOOR 841, AS PER AMM 25-62-44-803-A PROCEDURE 4B 12(B) REF AEROMAN NR 2020-375134 WO 2020 88/1. REMOVED AND REPLACED SLIDE RAFT DOOR 841, IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-000-803-A.
DURING HEAVY MAINTENANCE, ITEM TRANSFERRED FROM AEROMAN WO 2020 88/1 NR 2020-375059 DURING OPERATIONAL CHECK OF THE SLIDE RAFT. THE SLIDE RAFT TOUCHED THE FUSELAGE ON DOOR 831, AS PER AMM 25-62-44-400-007-A PROCEDURE 4B 12(B) REF AEROMAN NR 2020-375059 WO 2020 88/1. REMOVED AND REPLACED SLIDE RAFT DOOR 831, IAW AMM 25-62-44-000-012-A AND AMM 25-62-44-400-007-A.
DURING HEAVY MAINTENANCE, ITEM TRANSFERRED FROM AEROMAN WO 2020 88/1 NR 2020-375137 DURING OPERATIONAL CHECK OF SLIDE RAFT. THE SLIDE RAFT TOUCHED THE FUSELAGE ON DOOR 842, AS PER AMM 25-62-44-400-803-A PROCEDURE 4B 12(B) REF AEROMAN NR 2020-375137 WO 2020 88/1. REMOVED AND RPLACED SLIDE RAFT DOOR 842, IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A.
DURING HEAVY MAINTENANCE, ITEM TRANSFERRED FROM AEROMAN WO 2020 88/1 NR 2020-375135. DURING OPERATIONAL CHECK OF THE SLIDE RAFT. THE SLIDE RAFT TOUCHED THE FUSELAGE ON DOOR 832, AS PER AMM 25-62-44-400-007-A PROCEDURE 4B 12 (B) REF AEROMAN N/R 2020-375135 WO 2020 88/1. REMOVED AND REPLACED SLIDE RAFT DOOR 832, IAW AMM 25-62-44-000-012-A AND AMM 25-62-44-400-007-A.
FLT 1334, DIVERTED. DURING DESCENT WHEN OUTER TANK FUEL TRANSFER VALVES OPENED, FUEL FROM RIGHT TANK OUTER CELL DID NOT TRANSFER TO THE INNER CELL EVEN THOUGH THE VALVE SHOWED OPEN ON ECAM. POSSIBLE MOMENTARY ECAM FOR FUEL R WING TK LO LVL. TOO BRIEF TO KNOW FOR SURE. AT ROUGHLY 10000FT FUEL STARTED TO FLOW FROM INNER CELL AND COMPLETED AT 1500' (INTER CELL TRANSFER VALVES RT WING, ONE INOP. PERFORMED BITE TEST OF INTERCELL TRANSFER VALVES. NO FAULTS DISPLAYED ON MCDU. TEST DONE IAW AMM 28-15-00-740-002-A.
FT # 170, FLL-BOS. EPSU BATTERIES IN LOCATIONS 11WL, 12WL, 13WL FAILED SYSTEM TEST; R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHK OK. REF AMM 33-51-38. R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHK OK. REF AMM 33-51-38.
FT # 170, FLL-BOS. EPSU BATTERIES IN LOCATIONS 11WL, 12WL, 13WL FAILED SYSTEM TEST; R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHK OK. REF AMM 33-51-38. R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHK OK. REF AMM 33-51-38.
FT # 170, FLL-BOS. EPSU BATTERIES IN LOCATIONS 11WL, 12WL, 13WL FAILED SYSTEM TEST; R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHK OK. REF AMM 33-51-38. R & R EPSU BATTERIES IN FIN LOCATION 11WL, 12WL, 13WL. OPS CHECK OK. REF AMM 33-51-38.
EMERGENCY LIGHT BATTERY 10WL FAILS TEST; R & R BATTERY 10WL IAW AMM 33-51-38. OPS CKS OK.
DURING HEAVY MAINTENANCE, DURING CURRENT C7 CHECK A/C WAS FOUND WITH 2 QTY CORROSION DAMAGES TO THE RT WING TOP SKIN UPPER SURFACE @ STR-11R, BETWEEN RIBS 4-5 & RIBS 10-11. SEE REF /6/ FIGURES. THE DAMAGE WAS FOUND OUTSIDE SRM LIMITS AND WAS CONTACTED. PROVIDED REF /2/ RDAS & REF /3/ TD WHICH PROVIDES APPROVAL & INSTRUCTION TO REPAIR THE DAMAGED AREAS AS PER REF /4/ & /5/ REPAIR DRAWINGS. REF /2/ RDAS ALSO PROVIDES INSTRUCTION OF 4 QTY POST REPAIR INSPECTIONS. ISSUED REF /1/ REO TO ACCOMPLISH THE REPAIR AS PER REF /2/ RDAS & REF /3/ TD WITHOUT DEVIATION. EC A19-244-01 ACCOMPLISHES THE REPAIR AS PER REF /1/ REO WITHOUT DEVIATION. EC A19-244-02 ACCOMPLISHES POST REPAIR INSPECTION NR 1 (EXTERNAL DET AT RIBS 4-5; THRESHOLD 30000 FC / 41900 FH; INTERVAL 25000 FC / 34900 FH). EC A19-244-03 ACCOMPLISHES POST REPAIR INSPECTION NR 2 (TBD AT RIBS 4-5; THRESHOLD 51200 FC / 90300 FH; INTERVAL TBD). EC A19-244-04 ACCOMPLISHES POST REPAIR INSPECTION NR 3 (EXTERNAL DET AT RIBS 10-11; THRESHOLD 25000 FC / 34900 FH; INTERVAL 25000 FC / 34900 FH). EC A19-244-05 ACCOMPLISHES POST REPAIR INSPECTION NR 4 (TBD AT RIBS 10-11; THRESHOLD 54600 FC / 81700 FH; INTERVAL TBD); THIS PERMANENT REPAIR HAS BEEN APPROVED BY REF /2/ RDAS AND IS CLASSIFIED AS MAJOR.
DURING HEAVY MAINTENANCE, L/H MID EPSU FAILS PTP TEST; REMOVED & REPLACED EPSU IAW AMM 33-51-38. OPS CHECK SATISFACTORY IAW AMM 33-51-00-710-001. SUPPLEMENTAL INFORMATION TO FOLLOW.
DURING HEAVY MAINTENANCE, CABIN SEAT TRACK Y1292 FR 28-29 HAD AREA OF SCRATCHES AND GOUGES BEYOND SRM LIMITS; REF. HAECO N/R 440567-22434 - REPAIRED CABIN SEAT TRACK Y1292 BETWEEN FR 28 - FR 29 IAW A320 SRM 53-00-15-300-001 FIG. 001. CAT A REPAIR.
DURING HEAVY MAINTENANCE, CABIN SEAT TRACK Y-1292 FR 30-31 HAD AREA OF SCRATCHES AND GOUGES BEYOND SRM LIMITS; REF. HAECO N/R 440567-22436 - REPAIRED CABIN SEAT TRACK Y-1292 FR 30-31 I/A/W A320 SRM 53-00-15-300-001.
DURING HEAVY MAINTENANCE, CABIN SEAT TRACK Y-1292 FR 27 HAD AREA OF SCRATCHES AND GOUGES BEYOND SRM LIMITS; REF. HAECO N/R 440567-22435- REPAIRED CABIN SEAT TRACK Y-1292 FR 27 I/A/W A320 SRM 53-00-15-300-001.
DURING HEAVY MAINTENANCE, MAIN CABIN SEAT TRACK -Y765 FR 54-62 SCRATCHES AND GOUGES BEYOND LIMITS PER SRM REQ. REPAIR; REF. HAECO N/R 440567-22449 - REMOVED AND REPLACED MAIN CABIN SEAT TRACK -Y765 FR 47-62 I/A/W A320 SRM 51-72-11-911-001 CAT A REPAIR.
DURING HEAVY MAINTENANCE, MAIN CABIN SEAT TRACK Y765 FR 60 + 12 " SCRATCHES AND GOUGES BEYOND LIMITS PER SRM REQ REPAIR; REF. HAECO N/R 440567-22448 - REMOVED AND REPLACED SEAT TRACK SECTION FROM FR 60-FR63 IAW A320 SRM 53-41-15-300-002.
DURING HEAVY MAINTENANCE, MAIN CABIN SEAT TRACK Y1292 FR 62 HAD AREA OF SCRATCHES AND GOUGES BEYOND SRM LIMITS, REQUIRES REPAIR; REF. HAECO N/R 440567-22472 - FABRICATED AND INSTALLED SEAT TRACK REPAIR AT MAIN CABIN SEAT TRACK Y1292 FR 62 IAW A320 SRM 53-41-15-300-002.
DURING HEAVY MAINTENANCE, CABIN SEAT TRACK Y765 FR 25 HAD AREA OF SCRATCHES AND GOUGES BEYOND LIMITS; REF. HAECO NR 440567-22431 - REPAIRED CABIN SEAT TRACK Y765 FR 25 IAW A320 SRM 53-00-15-300-001.
DURING HEAVY MAINTENANCE, CABIN SEAT TRACK Y765 FR 34 HAS AREA OF SCRATCHES + GOUGES BEYOND SRM LIMITS; REF HAECO NR 440567-22432- INSTALLED PLUG REPAIR CABIN SEAT TRACK Y765 @ FR 34 IAW A320 SRM 53-00-15-300-001.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT -Y254, FRAMES 12 TO 24 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D5311008.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM, +Y512, FRAME 66. REPAIRED IAW SRM 51-72-11 AND DRAWING D53472094.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR PLATE STRINGER 23R IN THE AFT GALLEY AREA, FRAMES 69 TO 70. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DRAWING D53474180.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATED FRAME 16, STRINGER 23R AT THE FWD GALLEY AREA. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53110339.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PLATE STOP FITTING ON THE EMERGENCY DOOR IN PASSENGER CABIN. REPLACED THE STOP FITTING IAW SRM 51-42-11, AND DRAWING D52279040.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE SHEAR PLATE, STRINGER 23L IN THE AFT GALLEY AREA FROM FRAMES 69 - 70. REPLACED SHEAR PLATE IAW SRM 51-42-11, 51-72-11, AND DRAWING D53474180.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON WEB BETWEEN FRAMES 69 & 70, STRINGER 23R. REPLACED THE WEB IAW SRM 51-72-11, AND DRAWING D53474180.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT -Y1292, FRAMES 12 TO 24 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW 51-72-11, AND DRAWING D53110984.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK -Y765, FRAMES 66 TO 64 +7. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472816.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y1162 AT AFT GALLEY AREA IN FRAME 68. REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND DRAWING D53472780.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, +Y1225, FRAMES 66 TO 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DRAWING D53472000.
DURING EMERGENCY LIGHT TEST, FWD EPSU FAULTED. REPLACED FWD EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
MAIN CABIN AFT WET AREA FLOOR SUPPORT Y1292 CORRODED AT FRAME 67 AND FWD OF FRAME 68; R & R FLOOR SUPPORT IAW 51-42-11 AND 51-72-11.
MAIN CABIN AFT WET AREA FLOORBEAM -Y1292 AT FRAME 67; REPLACED FLOORBEAM IAW SRM 51-42-11, 51-72-11.
MAIN CABIN AFT WET AREA LATERAL SHEAR WEB CORRODED AT FRAME 68 TO FRAME 70 RT SIDE. R & R THE SHEAR WEB IAW SRM 51-42-11.
AFTER LANDING, AVIONICS SMOKE ECAM, NO SMOKE SEEN OR SMELLED. TSM 26-15-00-810-803A R & R AVIONICS SMOKE DETECTOR IAW AMM 26-15-15 ALL CHECKS NORMAL.
ENROUTE, NR 2 ENGINE FADEC ALTERNATOR ILLUMINATED ON ECAM. ACFT RETURNED TO DEPARTURE,. FOUND NR 2 ENGINE DEDICATED ALTERNATOR STATOR BAD. R & R ALTERNATOR. ACCOMPLISHED ENGINE RUN, GOOD REF AMM 72-22-38-000-010-B. OPS CHECK GOOD.
MAINTENANCE CHECK FOUND CIDS PANEL DISPLAYS "EPSU BATTERY FWD L" FAILURE MESSAGE. R & R FWD LT EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-710-052B.
FLT 746 SJU-MCO, ELECTRICAL FUMES AT ROW 17 REPORTED BY CUSTOMER OCCURED ON FINAL. LTV FOUND TO BE SUSPECT. PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW AMM 23-39-00. FOUND 18 DEF WITH BLACK SCREENS. REMOVED AND REPLACED XEB AT 18R IAW 23-39-00. OPS CHECK GOOD.