N559JB
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
86 reports on file, 2005-01-01 – 2024-10-05.
Part: FITTING — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL FITTING LAYER AT THE UPPER AND LOWER INBOARD HOLES OF DOOR STOP FITTING 7 LOCATED FRAME 16 RH AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00055) REF AE W/O# 2024-214/1. N/R# 2024 - 446432. REMOVED AND REPLACED INTERCOSTAL FITTING LOCATED DOOR STOP FITTING 7 FRAME 16 RH AT FWD GALLEY AREA I.A.W. A320 SRM 53-11-12-300-010, A320 SRM 51-72-11, DWG D53114223 AND EC NO. 2022-02-11-FAA STEP 21. ACCOMPLISHED BY AE TECH# 8608018. AE QC INSP# 329.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 2, LOCATED ON CROSSBEAM SPLICING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.106 INCHES, CRACK DIRECTION: 1 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00051) REF AE W/O# 2024-214/1. N/R# 2024 - 446364. PERFORMED PERMANENT REPAIR ON FASTENER HOLE 2, LOCATED ON CROSSBEAM SPLICING AREA FR16 LH SIDE ON PASSENGER CABIN I.A.W REPAIR DWG R53112926 AND A320 SRM 51-49-00. ACCOMPLISHED BY AE TECH# 8658318. AE QC INSP# 381.
Part: STRINGER — CORRODED (ZONE 100) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC, BWT FR, 55 TO FR, 57 IN AFT CARGO COMPARTMENT (CPCP FINDING);(RESOLVED ON W/O: 1311389 TASKCARD: NR-00057) REF AE W/O# 2024-214/1. N/R# 2024 - 446603. REMOVED AND REPLACED STRINGER 43L LOC, BET FR 55 TO FR 57 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-42-11, A320 SRM 51-72-11, AND DRAWING E53470342. ACCOMPLISHED BY AE TECH# 901023. AE QC INSP# 420.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00056) REF AE W/O# 2024-214/1. N/R# 2024 - 446437. PERFORMED PERMANENT REPAIR ON HOLE C OF JOGGLE AREA ON FRAME 16 LH AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA I.A.W A320 SRM 53-11-12-300-012 PARAGRAPH 2.A. (1). FIGURE 001, FIGURE 004, FIGURE 005 AND FIGURE 008. DIA: 8.420 MM (0.3315 INCH). THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 6800FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 5900 FC (FH NOT RELEVANT) IAW A320 SRI 53-11-12-205-008 TABLE 1. ACCOMPLISHED BY AE TECH# 8620918. AE TECH# 329. FUR-A320-53-01720 ASSIGNED.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00048) REF AE W/O# 2024-214/1. N/R# 2024 - 446433. PERFORMED PERMANENT REPAIR ON FRAME 20 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. I.A.W A320 SRM 53-11-12-300-012 ITEM 2.A(1) FIGURE 001.FIGURE 002.FIGURE 004 AND FIGURE 008. THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT 8900 FC (FH NOT RELEVANT)FROM TIME OF ADL/REPAIR EMBODIMENT AND SUBSEQUENT INSPECTIONS AT INTERVALS OF 8900FC (FH NOT RELEVANT) IAW A320 SRI 53-11-12-205-008. TABLE 2. ACCOMPLISHED BY AE TECH# 8629318. AE QC# 259. FUR-A320-53-01717 ASSIGNED.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00054) REF AE W/O# 2024-214/1. N/R# 2024 - 446436. PERFORMED PERMANENT REPAIR ON HOLE 6 OF JOGGLE AREA LOC. ON FR16 LH AT LEVEL OF DOOR STOP FITTING 7 FWD GALLEY AREA IAW A320 SRM 53-11-12-300-012 PARAGRAPH 2.A.(1), FIGURE 001, FIGURE 004, FIGURE 005 AND FIGURE 008. DIA A = 12.445 MM (0.4899 INCH). THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 6800FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 4700FC (FH NOT RELEVANT) IAW A320 SRI 53-11-12-205-008 TABLE 1. ACCOMPLISHED BY AE TECH# 8623121. AE QC INSP# 276. FUR-A320-53-01716 ASSIGNED.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE A OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00052) REF AE W/O# 2024-214/1. N/R# 2024 - 446434.PERFORMED PERMANENT REPAIR ON HOLE A OF JOGGLE AREA LOC. ON FR16 RH AT LEVEL OF DOOR STOP FITTING 7 FWD GALLEY AREA IAW A320 SRM 53-11-12-300-012 PARAGRAPH 2.A.(1), FIGURE 001, FIGURE 004, FIGURE 005 AND FIGURE 008. DIA A = 8.420 MM (0.3315 INCH). THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 6800FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 5900FC (FH NOT RELEVANT) IAW A320 SRI 53-11-12-205-008 TABLE 1. ACCOMPLISHED BY AE TECH# 8671520. AE QC INSP# 238. FUR-A320-53-01713 ASSIGNED.
Part: SUPPORT WEB — CORRODED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CORROSION SUPPORT WEB LOCATED BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1311389 TASKCARD: NR-00043) REF AEROMAN WO 2024 214/1 NR 2024-446422. REMOVED AND REPLACED NEW SUPPORT WEB LOCATED BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53474180 TOOL USED CALIPER PN: 500-197-30, SN: A18109027, DUE DATE: JAN-17-2025. COMPLETED MX-220 FORM BY CPCP PROGRAM.DONE BY J. PALACIOS 8671520 CHECKED BY 320.
Part: SUPPORT WEB — CORRODED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CORROSION SUPPORT WEB LOCATED BTR FR 69 AND FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1311389 TASKCARD: NR-00042) REF AEROMAN WO 2024-214/1 NR 2024-446420. REMOVED AND REPLACED SUPPORT WEB LOCATED BTW FR 69 AND FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53474180 TOOL USED CALIPER P/N: 700-113-10 S/N: 0016656, DUE DATE: MAR-04-2025.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00053) REF AE W/O# 2024-214/1. N/R# 2024 - 446435. PERFORMED PERMANENT REPAIR ON HOLE C OF JOGGLE AREA LOC. ON FR16 RH AT LEVEL OF DOOR STOP FITTING 7 FWD GALLEY AREA IAW A320 SRM 53-11-12-300-012 PARAGRAPH 2.A.(1), FIGURE 001, FIGURE 004, FIGURE 005 AND FIGURE 008. DIA A = 10.585 MM (0.4167 INCH). THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 6800FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 4100FC (FH NOT RELEVANT) IAW A320 SRI 53-11-12-205-008 TABLE 1. ACCOMPLISHED BY AE TECH # 8623121. AE QC INSP#238. FUR-A320-53-01715 ASSIGNED.
Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE, REAR FUSELAGESB53-1491 DOOR STOP FITTING NR 1 STR 22L FR 68 HOLE FILLET RADIUS CRACKED PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS 1-4) /2/ AIRBUS RDAF 81468047/003/2024#B /3/ AIRBUS DOSSIER 81468047 /4/ AIRBUS TD REF 81468047/027/2024#B. DESCRIPTION: DURING CURRENT CHECK ON N559JB (MSN: 01917) @ SAL, DURING THE ACCOMPLISHMENT SB A320-53-1491 REV 02 AND SB A320-53-1288 REV 02, TWO CRACKS WERE FOUND AT FR 68 LH. (1) CRACK ON THE FR 68 LH DOOR STOP FITTING #1, LOWER I/B HOLE AND (2) CRACK ON THE FR 68 LH HORIZONTAL FLANGE RADII. SEE REF /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS) FOR MORE DETAILS. REPAIRS CONSISTED OF DAMAGE ON CRACK (1) AT THE FR 68 LH DOOR STOP FITTING #1, LOWER I/B HOLE WAS REAMED AS PER SRM 53-41-12-300-008 WITH A REPAIR BUSHING INSTALLED. CRACK (2) ON FR 68 LH HORIZONTAL FLANGE RADII DAMAGE WAS REMOVED AS PER TD 850533481/006/2020#C. AIRBUS ADVISED PROCEEDING WITH REPAIR IN ACCORDANCE TO TASK 53-41-12-300-022. THIS WAS APPROVED THROUGH AIRBUS THROUGH REF /3/ AIRBUS DOSSIER 81468047 AND REF /4/ AIRBUS TD REF 81468047/027/2024#B. AIRBUS PROVIDED DISPOSITION VIA REF /2/, RDAF, INCLUDING FULL REPAIR DISPOSITION AND INSPECTION METHOD/INTERVAL. EC A24-1250-01 IS ISSUED TO ACCOMPLISH THE PERMANENT REPAIR IAW REF /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS) EC A24-1250-02 IS ISSUED TO ACCOMPLISH POST REPAIR INSPECTION AT EXTERNAL SURFACES OF THE FRAME WEB (FWD FACE) AND REPAIR PART WEB (AFT FACE) PER AIRBUS RDAF, REF /2/. TH = 60000 FC (FH NOT RELEVANT). INTERVAL = TBD, METHOD TBD. EC A24-1250-03 IS ISSUED TO ACCOMPLISH POST REPAIR INSPECTION (FASTENERS HOLES AT FRAME INNER CAP AND MACHINED REPAIR PART ATTACHMENT), PER AIRBUS RDAF, REF /2/. TH = 71400 FC (FH NOT RELEVANT). INTERVAL = TBD, METHOD = TBD. EC A24-1250-04 IS ISSUED TO ACCOMPLISH POST REPAIR INSPECTION AT (FASTENER HOLES AT FRAME WEB, MACHINED REPAIR PART AND SEAL PROFILE / BRACKETS ATTACHMENT.), PER AIRBUS RDAF, REF /2/. TH = 82900 FC (FH NOT RELEVANT). INTERVAL = TBD, METHOD = TBD. EC A24-1250-05 IS ISSUED TO ACCOMPLISH POST REPAIR INSPECTION AT (REPAIR PART HORIZONTAL FLANGE AND INNER CAP FILLET RADIUS)PER AIRBUS RDAF, REF /2/. TH = 48700 FC (FH NOT RELEVANT). INTERVAL = 19700, METHOD = HFEC AS PER NTM 51-10-08. SUBSTANTIATION: THIS CATEGORY B PERMANENT REPAIR WITH INSPECTIONS REQUIRED IS APPROVED PER REF /2/ RDAF AND IS CLASSIFIED AS MAJOR IAW WITH JETBLUE GMM CHAPTER 8.6. (E/C: A24-1250-01)
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH & RH LOWER FASTENERS AREA / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9035-24 COVER REV.0 & PART 1-6 /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03) /3/ AIRBUS RDAF 81453413/003/2024#A /4/ AIRBUS RI R531-13430 ISSUE F /5/ AIRBUS RI R53113672 ISSUE B /6/ R53112919 ISSUE J & R53113426 ISSUE F (GAIN ACCESS) /7/ AIRBUS DOSSIER 81453413. DURING CURRENT (9/2024) M2 CHECK ON N559JB (MSN 01917) AT SAL, WHILE ACCOMPLISHING REF /2/ SB NDT INSPECTIONS ON THE WINDSHIELD FRAMING CENTER POST, CRACKS WERE FOUND ON THE LOWER ATTACHMENT ON AREAS A (BOTH SIDES), C (RH SIDE) & D1 HOLES (BOTH SIDES). THE CRACK WAS REMOVED BY HAND REWORK AND THE REWORK AS PER REF /5/ REPAIR INSTRUCTIONS. THE CRACK DIMENSION AND LOCATIONS ARE AS FOLLOWS: 1. AREA A1 LHS: L=9.36MM AND W=6.85, 2.AREA D1 HOLE LHS: FINAL DIAMETER 8.249MM, 3.AREA A1 RHS SPOT FACE CRACK: L= 9.24MM AND W=7.68MM 4.AREA C1 RHS CORNER CRACK: L= 9.24MM AND W=6.10MM 5.AREA D1 RHS HOLE CRACK: FINAL DIAMETER14.173MM. THERE WAS NO REFERENCE TO REPAIRING THIS TYPE OF DAMAGE PER OEM MANUALS. THEREFORE, AIRBUS WAS CONTACTED VIA REF /7/ DOSSIER FOR ASSESSMENT WITH THESE FINDINGS. AIRBUS PROVIDED REPAIR INSTRUCTIONS TO PERFORMING REWORKS AND INSTALLING REINFORCEMENT FITTING PER REF /4/ RI AND REPLACING CONTINUITY FITTINGS PER REF /6/ RI. EC A24-1231-01 ACCOMPLISHES PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH REF /3/ RDAF WITHOUT DEVIATION. EC A24-1231-02 TRACKS POST REPAIR INSPECTION ON THE CONTINUITY FITTING (HFEC INSPECTION, THRESHOLD: 29500 FC, INTERVAL: 8700 FC). EC A24-1231-03 TRACKS POST REPAIR INSPECTION ON THE WINDSHIELD FRAMING (HFEC INSPECTION, THRESHOLD: 27000 FC, INTERVAL: 4700 FC). EC A24-1231-04 TRACKS POST REPAIR INSPECTION ON OTHER AREAS (TBD, THRESHOLD: 60000 FC, INTERVAL: TBD) NOTE: SB 53-1331 WILL NO LONGER BE APPLICABLE AFTER REPAIR ACCOMPLISHMENT. THIS WILL BE REFLECTED ON EC 2020-17-03-FAA. SUBSTANTIATION: THIS REPAIR IS APPROVED AS CAT B REPAIR PER REF /3/ RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-1231-01)
Part: WEB — CRACKED (ZONE 100) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH WEB AFT FACE HORIZONTAL FLANGE LEVEL OF STR 22L. CRACK L= 0.580 INCH; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00068) PERFORMED REPAIR ON FR68 LH WEB AFT FACE HORIZONTAL FLANGE LEVEL OF STR 22L I.A.W. EC NO. A24-1250-01 AND EA NO. 53-9041-24. THIS REPAIR IS CATEGORY B I.A.W. 81468047/003/2024#B. TOOL USED PN: NORTEC 600D, SN: 200048001. DUE DATE: MAY-28-2025. TOOL USED SMALL HOLE GAUGE P/N : 154-901, S/N: AE-403298, DUE DATE: SEP-23-2024 AND MICROMETER P/N: 293-344-30, S/N: 77011100, DUE DATE: MAR-31-2025. TOOL USED DIGITAL CALIPER P/N: 500-196-30, S/N: A21033544, D/D: APR-09-2025. TOOL USED, P/N: 45MG, S/N: 130066701, DUE DATE: JUL-12-2025. OUTSIDE MICROMETER PN: 293-344-30, SN: 77021048, DUE DATE: FEB-28-2025. TELESCOPING GAUGES P/N: MTEE6, S/N: AE-411147, DUE DATE: DEC-14-2024 ALL WORK ACCOMPLISHED ON AEROMAN WO 2024-214/1 NR 2024- 446474.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STO P FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00067) PERFORMED REPAIR ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STOP FITTING 1 AT AFT GALLEY AREA, I.A.W. EC NO. A24-1250-01 AND EA NO. 53-9041-24. THIS REPAIR IS CATEGORY B I.A.W. 81468047/003/2024#B. TOOL USED PN: NORTEC 600D, SN: 200048001. DUE DATE: MAY-28-2025. TOOL USED SMALL HOLE GAUGE P/N : 154-901, S/N: AE-403298, DUE DATE: SEP-23-2024 AND MICROMETER P/N: 293-344-30, S/N: 77011100, DUE DATE: MAR-31-2025. TOOL USED DIGITAL CALIPER P/N: 500-196-30, S/N: A21033544, D/D: APR-09-2025. TOOL USED: , P/N: 45MG, S/N: 130066701, DUE DATE: JUL-12-2025. OUTSIDE MICROMETER PN: 293-344-30, SN: 77021048, DUE DATE: FEB-28-2025. TELESCOPING GAUGES P/N: MTEE6, S/N: AE-411147, DUE DATE: DEC-14-2024 ALL WORK ACCOMPLISHED ON AEROMAN WO 2024-214/1 NR 2024 446439.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68RH SIDE AT LOWER I/B HOLE OF DOOR STOP FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00066) REF: ARM W/O 2024 214/1 N/R 2024-446438. PERFORMED REPAIR ON FRAME 68 RH SIDE AT LOWER INBOARD HOLE OF DOOR STOP FITTING 1 AT AFT GALLEY AREA I.A.W. A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT 37900FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 5300FC (FH NOT RELEVANT)I.A.W. SRI 53-41-12-205-010, TOOL USED PN: NORTEC 600D, SN: 200048001. DUE DATE: MAY-28-2025, TOOL USED SMALL HOLE GAUGE P/N : 154-901, S/N: AE-403298, DUE DATE: SEP-23-2024 AND MICROMETER P/N: 293-344-30, S/N: 77011100, DUE DATE: MAR-31-2025. TOOL USED DIGITAL CALIPER P/N: 500-196-30, S/N: A21033544, D/D: APR-09-2025, TOOL USED: , P/N: 45MG, S/N: 130066701, DUE DATE: JUL-12-2025. TOOL USED COMBINATION GAUGE P/N:CBG-4-4-N-1 S/N:AE-38007 DUE DATE:APR-08-2025 MANDREL GAUGE P/N:CBMG-4-4-N S/N:AE-24223S DUE DATE:APR-23-2025,MANDREL GAUGE P/N:CBMG-6-1-N,COMBINATION GAUGE P/N:CBG-8-1-N-1 S/N:AE-418148 DUE DATE:FEB-28-2025 MANDREL GAUGE P/N:CBMG-8-1-N S/N:314602A DUE DATE:JUN-14-2025Q. FUR-A320-53-01779 ASSIGNED.
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA LH SIDE FROM UPPER TENSION BOLT IN I/B VERTICAL FLANGE. CRACK DIRECTION IS 2 O'CLOCK LENGTH IS 0.140 INCH APPROX IN COCKPIT; ARM W/O 2024 214/1 N/R 2024-446172ACCOMPLISHED REPAIR OF THE CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT ON AREAS A (BOTH SIDES), C (RH SIDE) AND D1 (BOTH SIDES) I.A.W. EC A24-1231-01 AND EA 53-9035-24 (COVER PLUS PARTS 1 THRU 6) AND AIRBUS RDAF 81453413/003/2024#A. THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 27000FC (FH NOT RELEVANT) FROM TIME OF SOLUTION EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 4700FC (FH NOT RELEVANT), METHOD OF INSPECTION HFEC AS PER NTM 53-11-29 OF WINDSHIELD FRAMING AFTER REMOVAL OF MIRROR FITTINGS I.A.W. AIRBUS RDAF 81453413/003/2024#A. TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D, SN: N500X11290U021704, DUE DATE: APR-14-2025; ET EQUIPMENT, P/N: NORTEC 600D, S/N: 60009161631 DUE DATE: MAR-11-2025; CALIPER P/N: 500-196-30,S/N: A21126170 DUE DATE DEC-06-2024; ULTRASONIC THICKNESS GAGE, P/N: 45MG, S/N: 130064101 DUE DATE: DEC-13-2024 AND OUTSIDE MICROMETER PN: 293-344-30, SN: 71975635, DUE DATE: JUL-02-2025. FUR-A320-65-01778.
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 80,942 hrs · 29,027 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA RH SIDE FROM UPPER TENSION BOLT IN INBORD VERTICAL FLANGE. CRACK DIRECTION IS 10 O'CLOCK, CRACK LENGTH IS 0.080 INCH APPROX IN COCKPIT; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00064) REF: ARM W/O 2024 214/1 N/R 2024-446171 ACCOMPLISHED REPAIR OF THE CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT ON AREAS A (BOTH SIDES), C (RH SIDE) AND D1 (BOTH SIDES) I.A.W. EC A24-1231-01 AND EA 53-9035-24 (COVER PLUS PARTS 1 THRU 6) AND AIRBUS RDAF 81453413/003/2024#A. THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 27000FC (FH NOT RELEVANT) FROM TIME OF SOLUTION EMBODIMENT AND SUBSEQUENT INSPECTION AT INTERVALS OF 4700FC (FH NOT RELEVANT), METHOD OF INSPECTION HFEC AS PER NTM 53-11-29 OF WINDSHIELD FRAMING AFTER REMOVAL OF MIRROR FITTINGS I.A.W. AIRBUS RDAF 81453413/003/2024#A. TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D, SN: N500X11290U021704, DUE DATE: APR-14-2025; ET EQUIPMENT, P/N: NORTEC 600D, S/N: 60009161631 DUE DATE: MAR-11-2025; CALIPER P/N: 500-196-30,S/N: A21126170 DUE DATE DEC-06-2024; ULTRASONIC THICKNESS GAGE, P/N: 45MG, S/N: 130064101 DUE DATE: DEC-13-2024; FEELER GAUGE P/N: 2ZVC8, S/N: AE-419546, D/D: MAR-28-2025. FUR-A320-56-01777 ASSIGNED.
Part: WARNING MESSAGE — ILLUMINATED · airframe 80,210 hrs · 28,753 cycles
FLT#1584, MCO-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) ' HYD Y RSVR LO LVL ECAM NO HYDL FLUID INDICATED ON ECAM.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
Earlier reports · 2005–2023 · 68 reports
2023
Part: NONE — NONE · airframe 76,402 hrs · 27,259 cycles
FLT#87, ALB-FLL. 'INFLIGHT ADVISED DURING DESCENT THAT THERE WAS A STRONG AND PERSISTENT DIRTY SOCK ODOR. MX -270 FILLED OUT; PERFORMED LEVEL B REMOVAL OF THE CONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM (ECS) IAW AMM 21-00-00-615-803A. REMOVED AND REPLACE AIR CONDITION RECIRCULATION FILTER IAW AMM 21-21-42.'
2022
Part: NONE — NONE · airframe 74,277 hrs · 26,446 cycles
FLT#149, JFK-CHS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' R1 DOOR SHOWED DISARMED AFTER TAKEOFF. SLIGHT PRESSURE ON THE ARMING LEVER WOULD SHOW ARMED BUT WOULD NOT STAY; PERFORMED VISUAL INSPECTION OF R1 DOOR SLIDE, FOUND THE RIGHT TELESCOPIC FORK NOT FULLY ENGAGING TO LOCK GIRT BAR IN THE FLOOR FITTING AND RE-INSTALLED GIRT BAR WITH FULL TELESCOPIC FORK ENGAGEMENT PER AMM 25-62-44-420-065A STEP 4.'
Part: PROXIMITY SENSOR — FAILED (12GA) · airframe 74,107 hrs · 26,382 cycles
DURING HEAVY MAINTENANCE, AFTER TAKE-OFF AFTER GEAR RETRACTION ECAM MESSAGE: L/G GEAR NOT UPLOCKED FOLLOW ECAM ACTIONS AND QRH PROCEDURES STILL L/G NOT LOCKED UP. AT GEAR EXTENSION NORMAL GEAR DOWN AND LOCK 3 GREEN LIGHTS; PERFORMED TSM OF LG UPLOCK TGT POSITION FAULT ON NLG IAW TSM 32-31-00-810-837-A. DUE TO FAULT CONFIRMATION REMOVED AND REPLACED SENSORS 12GA,13GA, AND 37GA IAW AMM 32-31-73-000-005-A AND AMM32-31-73-400-005-A. PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR IAW AMM 32-31-00-720-002-A CHECK AND TEST ARE OK. AEROMAN TECH 8623008, AEROMAN INSPECTOR 8606312.
Part: IDG — FAILED · airframe 73,839 hrs · 26,271 cycles
FLT#1597, JFK-DEN. 'DESCENDING ON ARRIVAL OUT 13,00 FEET GEN #1 FAILED ALSO A/P2 AND AUTO THRUST DISCONNECTED AS WELL AS FLIGHT DIRECTORS. THE TOP MCDU SCREEN FAILED MOMENTARILY ALSO. ( IDG 1 DISCONNECTED (N503-N655) ); REPLACED #1 ENG IDG IAW AMM 24-21-51. OPS CHECK AND LEAK CHECK OK. REMOVE MDDR 473853. MX-4 UPDATED. PLACARD REMOVED.'
2021
Part: ELEVATOR SYSTEM — OUT OF RIG · airframe 71,404 hrs · 25,421 cycles
FLT 222, PBI-BOS. AIRCRAFT VIBRATION ON CLIMBOUT FROM PBI STARTED AROUND FL170 FILLED OUT AIRCRAFT VIVRATION SURVEY FOR MORE DETAILS VIBRATION INTENSITY SCALE 4; PERFORMED AMM TASK 05-50-00-810-801-A. FOLLOWED DECISION TABLE AND LEAD TO BELIEVE ELEVATORS ARE THE PROBLEM. FOUND L & R ELEVATORS OUT OF RIG. PANEL 344AT - TOP OF RIGHT ELEVATOR MISSING 4 FASTENERS. INSTALLED NEW SCREWS REF AMM 27-34-00. ADJUSTED L INBOARD AND OUTBOARD ELEVATOR ACTUATORS IAW AMM 37-34-0-820-003-B. L ELEV WITHIN LIMITS AT THIS TIME.
2020
Part: FLAP TRACK — FAILED (TE FLAPS) · airframe 69,593 hrs · 24,739 cycles
FLT 789, EMERGENCY DECLARED. ON APPROACH TO LANDING RECEIVED A FLAPS FAULT WHEN GOING FROM FLAP 1 TO FLAP 2. SLATS DEPLOYED BUT FLAPS DID NOT. ECAM RECYCLE DID NOT WORK. NORMAL LANDING WITHOUT FLAPS. R & R THE FLAP TRACK IAW AMM 27-54-49 & ADJUSTED FLAP TRACK IAW AMM 27-54-00. VERIFIED FLAP RIGGING IAW AMM 27-54-00. PERFORMED AN OPS CHECK OF THE PPUS ON THE CFDS IAW 27-54-49. PERFORMED OPERATIONAL TEST IAW AMM 27-54-00.
2019
Part: FAN — FAILED (E/E BAY) · airframe 67,624 hrs · 24,014 cycles
FT # 227, EWR-JFK. EMERGENCY DECLARED. DIVERTED TO JFK. AVIONIC SMOKE ECAM WITH ASSOCIATED LOUD NOISE AND ELECTRICAL BURNING SMELL. AFTER LANDING NOTED CABIN EXTRACT FAN CIRCUIT BREAKER POPPED; R & R AVIONIC FAN EXTRACT IAW AMM 21-26-51. OPS CHK GOOD. NO DEFECTS NOTED. PERFORMED INSPECTION FOR ELECTRICAL BURNING SMELL IN COCKPIT IAW TSM 24-00-00-810-823-A. NO FURTHER DAMAGE DETECTED. A/C OK FOR SVC
Part: UNKNOWN — ODOR (COCKPIT) · airframe 66,261 hrs · 23,508 cycles
FT # 179, AFTER LANDING F/A'S COMPLAINED ALONG WITH PAX THROUGHOUT CABIN OF MUSTY/DIRTY SOCK SMELL AS DESCENT STARTED INTO LGB AT APPROXIMATELY 8000 UPON LANDING IN LGB FLIGHT CREW NOTICED SMELL ONCE COCKPIT DOOR WAS OPEN. C/W INFO NOTICE 2017-T015E, T/S TO BE A LEVEL 1 ENVIROMENTAL SYS ODOR. RAN PACKS NO ODOR NOTED. A/C OK FOR CONT SVC.
Part: UNKNOWN — ODOR (CABIN) · airframe 66,167 hrs · 23,462 cycles
FT # 477, LEVEL ONE ODOR DETECTED BY INFLIGHT CREW ON DESCENT BETWEEN 10.000 AND THE SURFACE, ROW 15 TO AFT OF CABIN DESCRIBED AS DIRTY SOCKS ODOR. STRONG BUT CLASSIFIED AS TRANSIENT AS IT DISSIPATED UPON LANDING; COMPLIED WITH INFORMATION NOTICE 207-T015D SECTION A. AIRCRAFT IS OK FOR SERVICE. NO ABNORMAL ODORS. NOTED ON GROUND DURING PACK OPERATION.
Part: FILTER — FAILED (OZONE) · airframe 65,763 hrs · 23,320 cycles
(RESOLUTION): FT # 71, FUMES IN AFT CABIN TURNED OFF PACK 2 AND FUMES DISSIPATED. FUMES CLAMINATION CHECK LIST C/W. ( PACKS - SINGLE (SPEEDBRAKES OK) (N503-N665) ); R & R RH OZONE FILTER IAW AMM 21-51-41. OPS CHECKED NORMAL MX-4 UPDATED PLACARD REMOVED.
2018
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 FR66+3; REF NR 440500-30452: CORR BEYOND BLEND LIM AFT CABIN FLR BEAM RPL ON NR 30453.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 AT FR67+10; REMOVED AND REPLACED BEAM IAW SRM 53-41-14 REF NR 30444 FOR ALL WORK ACCOMPLISHED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR RT AFT SHEAR ANGLE FITTING AT FR69-70 HAS LOWER SURFACE CORROSION. REMOVED & REPLACED RT AFT SHEAR WEB ANGLE FITTING IAW SRM 51-72-11-911-001.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 AT FR67+16; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30445 FOR WORK ACCOMPLISHED.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, THE LT AFT EMERGENCY LIGHT FAILED TO ILLUMINATE WITH THE SWITCH IN THE ARMED POSITION AND C/B PULLED. REMOVED AND REPLACED THE BATTERY PACK & EPSU 13WL IAW AMM 31-51-38-00-001A, AND 33-51-38-400-001. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-38-710-052B. OPEN
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y765 AT FR66+2; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30456 FOR ALL WORK ACCOMPLISHED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1162.5 AT FR 66. REMOVED AND REPLACED FLOORBEAM Y1162.5 AT FR 66 STR 23L IAW SRM 51-42-11 & 53-00-14-283-002.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL. CORROSION AT AFT GIRT BAR BOLT ATTACH HOLE FR 66 +18 STR 23R; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-283-002. WORK ACCOMPLISHED ON NR 440500-30433.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 DOOR SILL FWD GIRT BAR. CORROSION AROUND GIRT BAR AFT INBD HOLE FR 67 + 18 STR 23L; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-283-002. WORK ACCOMPLISHED ON NR 440500-30441.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR68; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30455 FOR ALL WORK ACCOMPLISHED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y81 FR17 +16. RPL FWD CABIN FLOORBEAM -Y81 PER SRM 53-11-14, 51-44-11.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL. CORROSION AT FWD GIRT BAR BOLT ATTACH HOLE FR 66 +2 STR 23R; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-283-002. WORK ACCOMPLISHED ON NR 440500-30434.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL AT FR66. REMOVED CORROSION ON R2 DOOR SILL AT FR66 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-283-002 FIG 001 SHT 01. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-11 AND 51-72-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512.5 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30462 FOR WORK ACCOMPLISHED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR 66. REMOVED CORROSION. OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED & REPLACED FLOORBEAM IAW SRM 53-41-14 FIG 016.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512.5 AT FR 65; REPLACED FLOORBEAM IAW SRM 53-00-14-283-002. WORK ACCOMPLISHED ON NR 440500-30448.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 FR66+2. RPL AFT CABIN FLOORBEAM Y1292 PER SRM 53-00-14-283-002.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL AFT AFT GIRT BAR. CORROSION AROUND GIRT BAR FWD INBD BOLT HOLE FR 67 +18 STR 23L; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-283-002.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM ANGLE BRACKET AT FLOORBEAM -Y1732 AND FRAME 18. REMOVED & REPLACED FLOORBEAM ASSEMBLY - Y1732 IN ACCORDING TO SRM 51-42-11.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 DOOR SILL. CORROSION AROUND AITBD ATTACH HOLE FR 66 STR 23; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-12-283-002. WORK ACCOMPLISHED ON NR 440500-30436.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM - Y 81 AT FR 17 + 10". REMOVED CORROSION VERIFIED BEYOND .024" LOSS LIMITS IAW SRM 53-11-14-283-004. REMOVED & REPLACED BEAM -Y81 AT FR 17 + 10" ON NR 440500-30481.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 DOOR SILL FWD GIRT BAR. CORROSION AROUND FASTENER HOLE FR 66 =1 STR 23L; REMOVED AND REPLACED DOOR SILL IAW SRM 53041014-283-002. WORK ACCOMPLISHED ON NR 440500-30438.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 AT FR68 +9. AFT CABIN FLOORBEAM -Y1292 FR68 +9 CORR RPL ON NR 30453.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30458 FOR ALL WORK ACCOMPLISHED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y1732 AT FR18; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30482 FOR ALL WORK ACCOMPLISHED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR RT AFT SHEAR ANGLE FITTING AT FR69-70 HAS LOWER SURFACE CORROSION. REMOVED & REPLACED RT AFT SHEAR WEB ANGLE FITTING IAW SRM 51-72-11-911-001.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 FR66 +6. REPLACED BEAM -Y1292 FR66+6 IAW SRM 51-42-11.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR LT AFT SHEAR WEB ANGLE FITTING AT FR69+17 LOWER SURFACE CORROSION. REMOVED & REPLACED SHEAR WEB ANGLE FITTING AT LT FR 69 IAW SRM 51-72-11 PARA C.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512 AT FR 66 +3; REPLACED FLOORBEAM IAW SRM 53-00-14-283-002. WORK ACCOMPLISHED ON 440500-30457.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 DOOR SILL FWD GIRT BAR. CORROSION AROUND GIRT BAR HOLE FR 66 +6 STR 23L; REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-283-001. WORK ACCOMPLISHED ON NR 440500-30439.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL. CORROSION AT FLOORBOARD ATTACH HOLE 67 +20 STR 23R; REPLACED R2 DOOR SILL. REF NR 440500-30461.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR66+8 TO 67+8; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30454 FOR WORK ACCOMPLISHED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,119 hrs · 22,306 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y765 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30447 FOR WORK ACCOMPLISHED.
2017
Part: UNKNOWN — ODOR (CABIN) · airframe 59,378 hrs · 20,862 cycles
BELOW 5,000 FEET, A DIRTY SOCK ODOR WAS PRESENT. DONNED OXYGEN MASKS FOR LANDING. COMPLIED WITH INFORMATION NOTICE 2017-T015A SECTION B TABLE ONE. NO FINDINGS. PERFORMED BORESCOPE INSPECTION OF THE NR 1 AND 2 ENGINES AND APU. PERFORMED BORESCOPE INSPECTION OF NR 1 AND 2 ENGINES LPC STAGES 1.5, 2.0, 2.3, 2.5 IAW AMM 72-00-00-200-017-B AND HPC STAGE 3 BEARING COMP HOUSING AND BLADES IAW AMM 72-00-00-200-016-B01. NO OIL CONTAMINATION FOUND IN EITHER ENGINE. PERFORMED INSPECTION OF THE APU IAW 49-00-81-810-136-B . NO OIL CONTAMINATION FOUND IN APU INTAKE. ALL ENGINE STAGES WERE ACCESSED THROUGH THE N1 STATOR BLADES. NO COWLINGS WERE OPEN AND NO BORESCOPE ACCESS PORTS WERE REMOVED. AIRCRAFT IS OK FOR SERVICE.
Part: APU — ODOR · airframe 58,751 hrs · 20,597 cycles
APU INOPERATIVE DIRTY SOCK ODOR. WHILE ON THE GROUND WITH APU ON THE WHOLE CABIN SMELLED. THE ODOR STOPPED WHEN THE ENGINES WERE RUNNING AND THE APU WAS SHUT OFF. ODOR CAME BACK IN THE DESCENT WITH APU OFF. FROM 5000-1000 FT. R & R THE APU IAW AMM 49-11-11. PERFORMED OPS AND LEAK CHECK OF THE APU IAW AMM 49-00-00. OPS CHECKED GOOD. NO LEAKS NOTED AT THIS TIME R & R 100HM AND 101HM OZONE FILTERS IAW AMM 21-51-41.
Part: FILTER — ODOR (OZONE) · airframe 58,563 hrs · 20,512 cycles
DIRTY SOCKS ODOR NOTED AT LOW ALTITUDE. ACCOMPLISHED TSM 05-50-00-810-831A AND INFO NOTICE 2017-TO15. PERFORMED POST ENGINE WASH BORESCOPE INSPECTION OF THE NR 1 AND 2 ENGINE LPC IAW AMM 72-00-00-200-17B, AND HPC IAW AMM 72-00-00-200-16B. NO ACTIVE OIL LEAKS NOTED. R & R THE LT & RT OZONE FILTERS IAW AMM 21-51-41, LEAK CHECKED OK. ACFT OK FOR SERVICE.
Part: FILTER — ODOR (OZONE) · airframe 58,563 hrs · 20,512 cycles
DIRTY SOCKS ODOR NOTED AT LOW ALTITUDE. ACCOMPLISHED TSM 05-50-00-810-831A AND INFO NOTICE 2017-TO15. PERFORMED POST ENGINE WASH BORESCOPE INSPECTION OF THE NR 1 AND 2 ENGINES LPC IAW AMM 72-00-00-200-17B, AND HPC IAW AMM 72-00-00-200-16B. NO ACTIVE OIL LEAKS NOTED. R & R THE LT & RT OZONE FILTERS IAW AMM 21-51-41. LEAK CHECKED OK. ACFT OK FOR SERVICE.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 57,902 hrs · 20,255 cycles
DURING HEAVY CHECK MAINTENENANCE, CORROSION WAS DISCOVERED ON THE RT WING UPPER SURFACE STRINGER 8, RIB 13. REMOVED THE CORROSION IAW SRM 57-21-11, & EC A17-240-01.
Part: DOOR SILL — CORRODED (FRAME 55) · corrosion level 2 · airframe 57,902 hrs · 20,255 cycles
DURING HEAVY CHECK MAINTENENANCE, CORROSION WAS DISCOVERED ON THE AFT CARGO DOOR SILL FRAME 55. R & R THE DOOR SILL IAW SRM 53-41-49.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 57,902 hrs · 20,255 cycles
DURING HEAVY CHECK MAINTENENANCE, CORROSION WAS DISCOVERED ON THE RT WING UPPER SURFACE STRINGER 11 RIB 1 + 10. REMOVED CORROSION IAW SRM 57-21-11 EC A17-240-01. MAJOR REPAIR.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 57,902 hrs · 20,255 cycles
DURING HEAVY CHECK MAINTENENANCE, CORROSION WAS DISCOVERED ON THE RT WING UPPER SURFACE STRINGER 11 RIB 1 + 10. REMOVED CORROSION IAW SRM 57-21-11, EC A17-240-01. MAJOR REPAIR.
2016
Part: CONTROL UNIT — FAILED (MLG) · airframe 56,819 hrs · 19,829 cycles
EMERGENCY DECLARED. PILOT REPORTED RECEIVING LGCIU 2 FAULT UPON GEAR EXTENSION. PERFORMED THE QRH PROCEDURE WITH A MANUAL GEAR EXTENSION. CREW DECLARED AN EMERGENCY. LANDED UNEVENTFULLY. R & R THE NR 2 LGCIU IAW AMM 32-31-71. PERFORMED GEAR SWING AS PRECAUTIONARY IAW 32-31-00. ALL OPS CHECKED OK.
2015
Part: FLOORBEAM — CORRODED (FRAME 16) · airframe 52,122 hrs · 18,123 cycles
FLOORBEAM AT Y503 AND FRAME 16 HAS CORROSION; R & R FLOORBEAM IAW SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 51,147 hrs · 17,775 cycles
DURING HEAVY MAINTENANCE, FOUND FLOORBEAM AT FRAME 68, Y765 HAS EVIDENCE OF CORROSION. R & R FLOORBEAM AT FRAME 68, Y765 IAW SRM 51-42-11. OK FOR SERVICE.
Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 51,147 hrs · 17,775 cycles
DURING HEAVY MAINTENANCE FOUND FLOORBEAM AT FR 68, Y1292 HAS EVIDENCE OF CORROSION. R & R FLOORBEAM AT FRAME 68, Y1292 IAW SRM 51-42-11. OK FOR SERVICE.
2014
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 47,284 hrs · 16,421 cycles
DURING MAINTENANCE CHECK, FOUND AFT LT EMERGENCY LIGHT BATTERY FAILED. R & R EMERGENCY BATTERY FIN 13WL IAW 33-51-38. OPS CHECKED GOOD.
Part: FITTING — LEAKING (BRAKE VALVE) · airframe 45,799 hrs · 15,929 cycles
AIRCRAFT RETURNED TO DEPARTURE DUE TO Y RESERVOIR LOW LEVEL. DURING INITIAL INSPECTION, FOUND LEAK COMING FROM FITTING ON DUAL DISTRIBUTION BRAKE VALVE BRAKE PRESSURE LINE. FOUND DETERIORATED O-RING R & R O-RING IAW MM 32-43-14. SERVICED YELLOW SYSTEM IAW MM 12-12-00 AND BLEED YELLOW SYS HYD IAW MM 29-00-00-870-004. ALSO, INSPECTED YELLOW SYS FILTER DPI'S, ALL WERE FOUND OK. SYS WAS NOT DEPLETED OPERATION AND LEAK CHECK NORMAL.
2013
Part: ACTUATOR — RUPTURED (LT MLG) · airframe 43,164 hrs · 15,030 cycles
CREW DECLARED AN EMERGENCY DUE TO HYD GREEN NR 1 ENGINE PUMP LOW PRESSURE AND HYD G SYS LOW LEVEL. ACCOMPLISHED AMM TASK 29-00-00-280-006, FOUND FLEX LINE ON LT MLG DOOR EXT/RETRACT ACTUATOR RUPTURED. R & R BOTH FLEX LINES AND JOINT SWIVEL ASSY IAW AMM 32-31-38. LEAK & OPS CHECKED OK.
Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 42,146 hrs · 14,692 cycles
FLT 399 LGA-MCO, AFTER LANDING GEAR RETRACTION ECAM BRAKES AUTO BRK FAULT BRAKE RELEASED. BRAKES ON WHEEL 3 & 4 (PAIR 2) BOTH RELEASED WHILE BRAKING OVER 20 KNOTS. REMOVED AND REPLACED BSCU (BRAKE STEERING CONTROL UNIT) 10GG IAW AMM 32-42-34. OPS CHECK SATISFACTORY.
2012
Part: SENSOR — FAILED (AC BAY) · airframe 39,319 hrs · 13,686 cycles
FLT 831 JFK-STI, AIR RETURN TO JFK DUE TO AIR PACK 2 OVERHEAT RECEIVED DURING CLIMBOUT. APPLIED ECAM/QRH PROCEDURES PACK CONTINUES TO OVERHEAT WITH PB ON OVERHEATED 3 TIMES BEFORE RTB FLOW REMAINDER OF FLIGHT WITH PB OFF. ALSO JEOPARDIZING APPLIED MEL IN EXISTENCE REQUIRING BOTH PACKS OPERATIVE. REMOVED AND REPLACED COMPRESSOR TEMP SENSOR PER 21-61-11-04. OPS CHECK OK.
2011
Part: CABLE — FAILED (EMERGENCY EXIT) · airframe 35,633 hrs · 12,450 cycles
FLT 6461 JFK-LCQ, ON HEAVY MAINTENANCE CHECK FOUND RT OVERWING EXIT SLIDE CABLE FAILED THE TRAVEL TEST. REMOVED AND INSTALLED OVERWING EMERGENCY EXIT SLIDE CABLE ASSY PER A320-53-1227-01.
Part: CABLE — FAILED (OVERWING EXIT) · airframe 35,633 hrs · 12,450 cycles
FLT 6461 JFK-LCQ, ON HEAVY MAINTENANCE CHECK FOUND LT OVERWING EXIT SLIDE CABLE FAILED THE TRAVEL TEST. REMOVED AND INSTALLED OVERWING EMERGENCY EXIT SLIDE CABLE ASSY PER A320-53-1227-01.
Part: SPLICE — DAMAGED (CABIN) · airframe 33,062 hrs · 11,561 cycles
FLT 1695 BOS-MCO, FORWARD EMERGENCY PATH LIGHTING RED ON PARTITION INOP. REPAIRED SPLICE AT FWD PARTITION AREA IAW ESPM 20-28-25. SYS OPS CHECK NORMAL IAW AMM 33-51-00.
2010
Part: CONNECTOR — DAMAGED (CIDS) · airframe 32,128 hrs · 11,211 cycles
FLT 1695 BOS-MCO, ON GROUND AT MCO - FLIGHT ATTENDANT CIDS PANEL SMOKING AS EXITING A/C AFTER DEPLANING. ALL POWER REMOVED FROM PANEL AND AIRCRAFT. PERFORMED TSM 24-00-00, FOUND CIDS FAP AND THE CONNECTOR BEHIND THE VSC DAMAGED. NOTE: WE WILL UPDATE THIS REPORT AFTER FINAL FIX IS ACCOMPLISHED.
2008
Part: ENTERTAIN SYS — ODOR (CABIN) · airframe 24,795 hrs · 8,513 cycles
FLT 504, FLL-EWR, LTV SYSTEM SMELL OF SMOKE ROW 1 THRU 5, LTV DEACTIVATED. T/S PER TR 2400001, TSM 24-00-00-810-823 & 23-39-00-810-801. NO ABNORMALITIES FOUND. INSPECTED ROW 1-7 ABCDEF. UPDATED XEB S/W. ADJUSTED RSSI FROM 4.95 TO 2.50. MONITORED SYS FOR 3 HOURS. OPS NORMAL. NO SMELLS NOTED.
2006
Part: CABLE ASSY — STIFF (E DOOR SLIDE) · airframe 14,223 hrs · 4,799 cycles
RT EMERGENCY OVERWING EXIT SLIDE BOTTLE DEPLOYMENT CABLE STIFF. REMOVED & REPLACED DEPLOYMENT CABLE AND TESTED AS PER AMM 25-62-23-43-04.
Part: CABLE ASSY — STIFF (E EXIT SLIDE) · airframe 14,223 hrs · 4,799 cycles
LEFT EMERGENCY EXIT SLIDE BOTTLE DEPLOYMENT CABLE STIFF. REMOVED AND REPLACED LT OVERWING EXIT SLIDE BOTTLE DEPLOYMENT CABLE AND TESTED AS PER AMM 25-62-43-04.
2005
Part: ELECTRICAL BOX — UNKNOWN (CABIN) · airframe 8,432 hrs · 2,871 cycles
CABIN CREW REPORTS ELECTRICAL FUMES ON SHORT FINAL. FUME DISSIPATED WHEN LIVE TV TURNED OFF. FUMES IDENTIFIED NEAR ROW 17. INSPECTED ROW 17 DEF SEB COVER AND DETECTED DRIED AND BURNT BEVERAGE RESIDUE. CLEANED RESIDUE AND REINSTALLED SEAT 17 DEF SEB COVER. DEACTIVATED LTV SYS PER MM 23-39-00. LTV SYSTEM PLACED ON MEL 25-22-03 CAT D, CTL NR L02830. COMPLIED WITH INFO NOTICE 2004-T023TR AND TSM TASK 24-00-00-810. UPON ARRIVAL AT JFK REMOVED AND REPLACED SEB AT SEAT 17 DEF IAW LTV MM 23-39-00. OPERATOIN CHECK OK.