N507JT
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JETBLUE AIRWAYS CORPORATION (YENA) | Operator | on 2019-05-28 | Operator named in NTSB report |
Accident & incident history
Operated by Jetblue Airways Corp (per NTSB report)
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.
61 reports on file, 2011-03-26 – 2025-06-24.
Part: HOOK AND LOOP — MELTED (ZONE 200) · airframe 86,106 hrs · 32,312 cycles
FLT#1911, EWR-RSW."ENTERING FLIGHT DECK SMELL/ODOR OF MELTING WIRES INSULATION BURNING SMELL/ODOR SEE PREVIOUS WRITE UP ON PAGE 4301026 (FOUND OLD HOOK AND LOOP ADVISE MELTING IN THE SUN PERMEATING FAN REMOVED & CLEARED ODOR NO LONGER DETECTED); ACCOMPLISHED INFO NOTICE 2017-T015L TSM 05-50-00-810-831A IDENTIFICATION TYPE #10 MISC. CABIN ODOR PER TABLE 2 COCKPIT ITEMS INSP RELATED ITEMS MCDU, GPCU, TRU, RMP, ELAC, EXTRACT FAN, AVIONICS BLOWER ACCOMPLISHED TSM 24-00-00-810-823A NO FUMES NOTED."
Part: SKIN — CORRODED (ZONE 600) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TIP SKIN LOWER SURFACE BETWEEN RIB 21 TO RIB 22 ON RH WING (CPCP FINDINGS); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00042) AEROMAN WO# 2025 180/1 WCC 2025-2984859 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB 21 TO RIB 22 ON RH WING IAW A320 SRM 57-21O-11-283-007. THIS REPAIR IS CAT B INSP THRESHOLD 144,000FC / 180,000 FH SUBSEQUEST INSP AT INTERVALS TBD METHOD INSP TBD A320 SRM 57-21-11-205-008. TABLE 1, PSE IAW A320 SRM 51-11-12 MX-220 COMPLETED FUR# A320-57-02321.
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10 INCHES) TO RIB 19 ON LH WING; TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCAION TRAILING EDGE TOP SKIN LOWER SURFACE RIB 18 PLUS 10 INCHES TO RIB 19 ON LH WING IAW EA57-0046-25.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 AND 12 O'CLOCK, CRACK DEPTH IS 0.110 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00032) REF AE WO# 2025-180/1. N/R# 2025 - 298874. EVALUATED DIAMETER HOLES D1 TO D4 AND FOUND WITHIN LIMITS TO REPAIR IAW SRM A320 53-41-12-300-008. PERFORMED REPAIR LOC. ON FRAME 68 RH SIDE HOLE LOWER INBOARD AT DOOR STOP FITTING 1 IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B. INSPECTION IS APPLICABLE FOR AREA 1 AND AREA 3 IAW A320 SRM 53-41-12-205-010. TABLE 06.
Part: SKIN — DAMAGED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TEOH BTWN RIB 15 - 19 / LOWER SURFACE / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0046-25 REV 0 (COVER AND PARTS 1 - 4) /2/ AIRBUS RDAF 81592930/005/2025#A /3/ AIRBUS DOSSIER 81592930 /4/ AIRBUS TECHNICAL DISPOSITION TD/81592930/012/2025#A /5/ AIRBUS TECHNICAL DISPOSITION TD/81592930/019/2025#A. DESCRIPTION: DURING CURRENT (06/2025) C9 CHECK ON N507JT (MSN: 01240) @ SAL, WHILE ACCOMPLISHING INSPECTIONS PER MPD TASK 572179-01, CORROSION WAS FOUND ON THE LH WING TOP SKIN PANEL 2 LOWER SURFACE AT THE FOLLOWING THREE AREAS, SEE REF /1/ AEM EA FOR DETAILS: 1. BETWEEN RIB 15 (WMRX 5097.109) AND RIB 16 (WMRX 5626.979). 2. BETWEEN WMRX 5855.60 AND WMRX 6401.863 (LEVEL OF RIB 17 (WMRX 6173.909)). 3. BETWEEN RIB 18 (WMRX 6695.749) AND RIB 19 (WMRX 7252.699). THE CORROSION DAMAGE WAS REMOVED AND EVALUATED AGAINST SRM TASK 57-21-11-283-007 AND WAS FOUND TO BE OUT OF LIMITS. AIRBUS WAS CONTACTED FOR DISPOSITION VIA REF /3/, DOSSIER, AND PROVIDED THE FOLLOWING REPAIR INSTRUCTIONS:â¢: â¢: ⢠FOR DAMAGE IN AREAS 1 AND 3: REPAIR IAW REF /4/ TD, CONSISTING OF ZERO STRESS JACKING, BLEND OUT IAW R572-58616 PARAGRAPH E, AND SEALING OF VOIDS PER SRM 51-76-12. ⢠FOR DAMAGE IN AREA 2: REPAIR IAW REF /5/ TD, CONSISTING OF ZERO STRESS JACKING, FASTENER REMOVAL, BLEND OUT IAW SRM 51-74-00, HFEC AND ROTOPROBE, WET-ASSEMBLED REINFORCEMENT REPAIR IAW R572-58483, SRM 51-27-11, D572-52403, AND R572-58616, CCC RESTORATION, AND SEALING OF VOIDS PER SRM 51-75-12. THESE INSTRUCTIONS ARE APPROVED PER REF /2/ RDAF AS PERMANENT WITH POST REPAIR INSPECTIONS REQUIRED IAW THE FOLLOWING SCHEDULE: ⢠RDAF SECTION 13 TABLE 1 ITEM 1 - AT THE TOP SKIN, UPPER SURFACE, AT THE REAR SPAR AND TRAILING EDGE OVERHANG BETWEEN RIBS 15-16: TH = 23000 FC / 46000 FH, INT = 23000 FC / 46000 FH, METHOD = DET, THIS INSPECTION SUPERSEDES RDTS/80917747/003/02/2021#A, MSN 1240 (RDAF REF. & IS.: 80917747/003/2021#A) ITEM NO. 2. RDAF SECTION 13 TABLE 1 ITEM 2 - AT THE TOP SKIN UPPER SURFACE, BETWEEN RIBS 16-18: UNDER THE REPAIR PLATE AT THE REAR SPAR ATTACHMENTS, FORWARD OF THE REPAIR PLATE, AND AT 3 ROWS OF ATTACHMENTS INBOARD AND OUTBOARD OF THE REPAIR PLATE: TH = 15000 FC / 30000 FH, INT = 15000 FC / 30000 FH, METHOD = SDI + DET, RDAF SECTION 13 TABLE 1 ITEM 3 - AT THE REAR SPAR TOP FLANGE AT THE FASTENERS COMMON TO THE REPAIR PLATE BETWEEN RIBS 16-18: TH = 18000 FC / 30000 FH, INT = 18000 FC / 30000 FH, METHOD = DET, RDAF SECTION 13 TABLE 1 ITEM 4 - AT THE TOP SKIN, UPPER SURFACE, AT THE REAR SPAR AND TRAILING EDGE OVERHANG BETWEEN RIBS 18-19: TH = 60000 FC / 120000 FH, INT = TBD METHOD = TBD. EC A25-574-01 ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH THE REF /2/ RDAF WITHOUT DEVIATION. EC A25-574-02 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTIONS IAW RDAF SECTION 13 TABLE 1 ITEM 1. EC A25-574-03 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTIONS IAW RDAF SECTION 13 TABLE 1 ITEM 2. EC A25-574-04 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTIONS IAW RDAF SECTION 13 TABLE 1 ITEM 3. EC A25-574-05 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTIONS IAW RDAF SECTION 13 TABLE 1 ITEM 4 AND IS CURRENTLY PENDING THE OEM. SUBSTANTIATION: THIS PERMANENT, CATEGORY B, REPAIR IS APPROVED BY REF /2/ RDAF AND IS CLASSIFIED AS MAJOR.(E/C: A25-574-01)
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT OPEN FASTENER HOLE UPPER OUTBOARD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 O'CLOCK, CRACK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00031) REF AE WO# R 2025-180/1. N/R# 2025 - 298873. EVALUATED DIAMETER HOLES D1 TO D4 AND FOUND WITHIN LIMITS TO REPAIR IAW SRM A320 53-41-12-300-008. PERFORMED REPAIR LOC. ON FRAME 68 RH SIDE UPPER OUTBOARD HOLE AT DOOR STOP FITTING 7 IAW A320 SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00029) REF AE WO# 2025-180/1. N/R# 2025 - 298871. EVALUATED DIAMETER HOLES D1 TO D4 AND FOUND WITHIN LIMITS TO REPAIR IAW SRM A320 53-41-12-300-008. PERFORMED REPAIR LOC. ON FRAME 68 LH SIDE LOWER INBOARD HOLE AT DOOR STOP FITTING 1 IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: AEROMAN WO# 180/1 NR# 2025-298911 FOR WORK PERFORMED: PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVERHANG AREA, BTW RIB 14 (PLUS 17 INCHES) TO RIB 15, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW A320 SRM 57-21-11-283-007, FIG 003 (SHEET 2) AND FIG 006 (SHEET 1), THIS REPAIR IS CATEGORY B, PERCENTAGE OF REMOVED MATERIAL IS: 43.65%, WITH AN INSPECTION THRESHOLD: 15,000FC / 30,000FH, SUB INSPECTION AT INTERVALS OF 15,000FC / 30,000FH, METHOD OF INSPECTION: DETAILED VISUAL INSPET IAW A320 SRM 57-21-11-205-006, TABLE 1 MX-220 C/W FUR#; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00054) AEROMAN WO# 180/1 NR# 2025-298911 FOR WORK PERFORMED: PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVERHANG AREA, BTW RIB 14 (PLUS 17 INCHES) TO RIB 15, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW A320 SRM 57-21-11-283-007, FIG 003 (SHEET 2) AND FIG 006 (SHEET 1), THIS REPAIR IS CATEGORY B, PERCENTAGE OF REMOVED MATERIAL IS: 43.65%, WITH AN INSPECTION THRESHOLD: 15,000FC / 30,000FH, SUB INSPECTION AT INTERVALS OF 15,000FC / 30,000FH, METHOD OF INSPECTION: DETAILED VISUAL INSPET IAW A320 SRM 57-21-11-205-006, TABLE 1 MX-220 C/W FUR#.
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 TO RIB 17 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00053) AEROMAN WO 180/1 NR# 2025-298901 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVEHANG AREA, BTW RIB 16 (PLUS 2 INCHES) TO RIB 17, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW A320 SRM 57-21-11-283-007, FIGURE 003 (SHEET 2) AND FIGURE 006 (SHEET 1). THIS REPAIR IS CATEGORY B, PERCENTAGE OF REMOVED MATERIAL IS: 20-81% WITH AN INSPECTION THRESHOLD: 23,000FC / 46,000FH, SUBSEQUENT INSPECTION AT INTERVALS OF: 23,000FC / 46,000FH. METHOD OF INSPECTION: DETAILED VISUAL INSPECTION IAW A320 SRM 57-21-11-205-006, TABLE 1 MX-220 C/W FUR#.
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10") TO RIB 19 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00044) AEROMAN WO 2025-180/1 NR 2025-298902 FOR WORK PERFORMED; PERFORMED BLEND OUT AND EVALUATE BLENDED AREA, P1 ON RIB 18, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW A320 SRM 57-21-11-283-007, FIGURE 006 / 57-21-11-283-007 (SHEET 1 ) THIS REPAIRS ARE CATEGORY B PERCENTAGE OF REMOVED MATERIAL ON P1 IS 13.70% WITH AN INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT 61,000 FC/110,000FH, SUBSEQUEST INSPECTIONS AT INTERVALS OF TBD, METHOD OF INSPECTION: TBD IAW A320 SRI 57-21-11-205-006 TABLE 1 SEE FUR# A320-57-02332 SEE NR 46 FOR SECOND BLEND AREA AND FUR AND MX-220.
Part: SKIN — CORRODED (ZONE 600) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ON RH WING IAW (CPCP FINDING); REF AEROMAN WO 2025-180/1 WCC#2025-298913 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ON RH WING IAW A320 SRM 57-21-11-283-007. THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD 144,000FC/180,000FH SUBSEQUENT INSPECTION AT INTERVALS TBD METHOD INSPECTION TBD IAW A320 SRM 57-21-11-205-008. TABLE 1 THIS REPAIR IS CONSIDERED PSE IAW A320 SRM 51-11-12. MX 220 COMPLETE. FUR COMPLETED FUR# A320-57-02320.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.090 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00030) REF AE WO# 2025-180/1. N/R# 2025 - 298872. EVALUATED DIAMETER HOLES D1 TO D4 AND FOUND WITHIN LIMITS TO REPAIR IAW SRM A320 53-41-12-300-008. PERFORMED REPAIR LOC. ON FRAME 66 LH SIDE LOWER INBOARD HOLE AT DOOR STOP FITTING 1 IAW A320 SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B.
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 (PLUS 15 INCHES) TO RIB 17 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00057) TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCATED TRAILING EDGE TOP SKIN LOWER SURFACE RIB 16 PLUS 15 INCHES IAW EA 57-0046-25 MX 220 C.W.
Part: SKIN — CORRODED (ZONE 500) · airframe 85,998 hrs · 32,272 cycles
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 15 (PLUS 16") TO RIB 16 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00055) REF TASK CARD 72179-01-1-575 JB WO# 1389906 PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE RIB 15 PLUS 16 INCHES IAW EA57-0046-25 MX-220 COMPLIED WITH.
Part: UNKNOWN — ODOR (CABIN) · airframe 85,315 hrs · 32,022 cycles
FLT#1733, DCA=PBI. 'FUMES/ODOR COCKPIT DESCENDING THROUGH 8000 THRUST IDLE. HP VALVE OPEN. PACK 1 OFF; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2 IDENTIFIED ODOR TYPE 10 TRANSITORY PRECAUTIONARY R/R 2 EA. CABIN FILTERS, DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-810-085 A/C OK FOR SVC FILTER CHANGE MM 21-21-41.'
Part: FILTER — ODOR (ZONE 200) · airframe 85,188 hrs · 31,974 cycles
FLT#87, ALB-FLL. 'ODOR EVENT DESCENDING THROUGH 4000 PERSISTED 3-5 MINUTES HP VALVES OPEN; C/W INFO NOTICE 2017-TOI5J & REF TSM 05-50-00-810-831-A PERFORMED PACK BURNS NO ODOR NOTED R/R RECIRCULATION FILTERS IAW AMM 21-21-00 NO ODOR NOTICED AT THIS TIME.'
Part: APU — ODOR (ZONE 100) · airframe 85,174 hrs · 31,969 cycles
FLT#1817, JFK-POS. 'AROUND 14K FEET A STRONG ODOR WAS SMELLED THROUGHOUT THE WHOLE AIRCRAFT. STARTED OUT STRONG AND SWEET THEN TURNED OLD AND MUSTY (DIRTY SOCK); C/W INFO NOTICE 2017-TO15K SECTION B LEVEL 2 DETERMINE APU SOURCE OF ODOR AT THIS TIME. SYS DECONTAMINATED PEPLACED ECS FILTER NO ODOR NOTED WITH ENGINES ON PER AMM 72-00-00 [ASKS RESTORED MDDR CLEAR MX-4 UPDATED.'
Earlier reports · 2011–2024 · 44 reports
2024
Part: RADAR — FAILED (WX RADAR) · airframe 84,363 hrs · 31,635 cycles
FLT#2751, TPA-SJU. (AIRCRAFT DIVERTED TO FLL) 'WX RADAR INTERMITTENT. FAILED 3 TIMES, JUST STOPPED PAINTING AND NO INDICATIONS, NO ECAMS; REMOVED AND REPLACED R.T. I.A.W AMM 34-41-33, NO FAULTS NOTED.'
Part: ENGINE — FAILED (LEFT) · airframe 83,238 hrs · 31,209 cycles
FLT#153, JFK- PBI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) .'AFTER T/O A/C HAD A SIGNIFICANT VIBRATION. WHILE TROUBLESHOOTING TOWER ADVISED SEVERAL A/C SAW DEBRIS COME OFF OUR A/C. WE RETURNED AND DIDAN OVERWEIGHT LANDING; FOUND #1 ENG DAMAGE CAUSED BY BIRD STRIKE. ENGINE REPLACED ON LOGPAGE 3943050-2 (REMOVAL AND INSTALLATION OF ENG #1 ACCOMPLISHED REF W/O 1344200 AND T/C NO. A320-71-00-20-400-040). CHP 5 INSPECTION COMPLETED ON LOGPAGE 3943045-2 AND ENGINE INSPECTION ACCOMPLISHED ON 3943046-1. OVERWEIGHT INSP ACCOMPLISHED ON 3943044-2.'
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,223 hrs · 30,446 cycles
FLT#2475, BDL-SJU. (AIRCRAFT DECALRED AN EMERGENCY INTO SJU) ' HYD Y RSVR LVL ECAM: 45 MINUTES INTO FLIGHT C FL 340. FOLLOWED ECAM QRH. CONTACTED MCC; REMOVED AND REPLACED O-RING AT HALF COUPLING FIN# 3701GM IAW AMM 29-13-15. OPT CHECK OK. NO LEAK FOUND.'
Part: SERVO CONTROL — FAILED (33CE2) · airframe 79,524 hrs · 29,789 cycles
FLT#1393, FLL- NAS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' R AILERON IS DEFLECTED UP A LITTLE. AIR RETURN TO FLL PER CO; FOUND R/H WING BLUE AILERON SERVO CONTROL AT FAULT. REF LOGPG 3740737 -2 (ACCOMPLISHED REMOVED AND REPLACED R/H WING BLUE AIRLERON SERVO CONTROL IAW AMM 27-14-51. REPLACED DUE TO FAILED R/H WING AILERON DUMPING TEST "NOT OK" IAW TSM TASK 27-10-00-810-838-A) AND LOGPG 3740738-1 (INSTALLED LOCKING CAP PIN ON AILERON JACK BRACKET PIN AND ACCOMPLISHED LEAK CHECK OF SERVO B/R AILERON REF AMM 27-14-51. ALSO ACCOMPLISHED BLEEDING ADJUSTMENT AND OPS TEST OF SERVO CONTROL REF AMM 27-14-00. THE OPS CHECK IS GOOD. NO LEAKS NOTED.)FOR REMOVAL AND REPLACEMENT. AND OPS CHECK REF AMM 27-14-51.'
2022
Part: NONE — NONE · airframe 77,141 hrs · 28,860 cycles
FLT#1279, LAS-LAX. 'STRONG CHEESE ODOR REPORTED BY FA'S ON FINAL APPROACH. ISOLATION CHECKLIST DONE AFTER LANDING; DURING T/S PER TSM 05-50-00-810-831-A, FOUND GREEN SYS HYD LINE LEAKING, CORRECTED ON LOG PAGE # 3442177, ITEM#1 (FOUND GREEN HYD LINE REGULAR BRAKE SYS UNDER AFT CARGO FWD BULK, CHAFE. REPAIRED LINE PER PERMASWAGE TYPE 1 SMALL HOLE USING ONLY ONE UNION REMOVED DAMAGE .20" AMM 20-23-11.). PERFORMED LEVEL A DECONTAMINATION OF THE ECS IAW AMM 21-00-00-615-802, ALSO REPLACED BOTH RECIRCULATION FILTERS PER MCC REQUEST. (REF.LOG PAGE# 3442181, ITEM 1 (REMOVED AND REPLACED BOTH RECIRCULATION FILTERS PER AMM 21-21-41. OPS CHECK GOOD)). A/C OK FOR SERVICE.'
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE UPPER CORNER WEB JOINT AFT FACE BETWEEN UPPER FASTENER AND STRINGER 8 RADIUS, CRACK LENGTH IS 0.2 50 INCH APPROX AT AFT GALLEY AREA (1 E/A); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00014 ) REF TO AEROMAN W/O:2022 181/1 NR 2022 - 481951, PERFORMED PERMANENT REPAIR FRAME LOC. FR 68 BTW STRG 7 R/H TO STRG 9 R/H I.A.W A320 SRM 53-41-12-300-012 AND 51-42-11 AND DRAWING #D53480505.THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM THE TIME OF REPAIR EMBODIMENT: 57700FC AND SUBSEQUENT INSPECTION AT INTERVALS OF: 2600FC, INSPECTION METHOD: REMOVE THE REPAIR PART AND PERFORM NDT INSPECTION FOR CRACK I.A.W A320 SRI 53-41-12-205-014 STEP 2. A TABLE 001. TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 210138203 DUE DATE APR-11-2023. ULTRASONIC THICKNESS GAGE PN 45MG SN 130063701 DUE DATE JUN-16-2023. CALIPER P/N: 500-197-30, S/N: A21303945, DUE DATE: MAY-06-2023. KIT AIRBUS P/N: FTI-A320-52-1071-1, S/N: AE-27068, DUE DATE: FEB-10-2023. DONE BY J. BATRES 8618913 CHECKED BY E. ARGUETA 8619800 RII BY AEROMAN QC 259 FUR-A320-53-00453.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2022-181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITY FITTING (1 E/A) LOC BTW FRAME 1 AND 2 LH SIDE IAW A320 SRM 51-72-11-911-001, SRM 51-72-11-911-001, SRM 51-42-11, SRM 51-49-00 AND REPAIR INSTRUCTION R53112919 ISSUE F. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC600D, S/N: 210138203, DUE DATE: APR-11-2023; TORQUE: P/N: QD2R200, S/N: 0312800545, DUE DATE: JAN-06-2023. DONE BY N. LIZAMA 8626912 CHECKED BY L. OSTORGA 8619517 RII AE QC 321.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 8 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481996, REMOVED AND REPLACED INTERCOSTAL FITTING LOCATED ON FR16 AT LEVEL OF DOOR STOP FITTING #7 RH SIDE IAW A320 SRM 51-42-11 AND DWG # D53112300, TORQUE APPLIED 120 LB.IN. TOOL USED PN= NORTEC 500D, SN= N500X1693P030456, DUE DATE= JAN-26-2023; DIGITAL CALIPER PN= 500-196-30, SN= B21140377, DUE DATE= OCT-14-2022; TORQUE PN= QD2R200, SN= 0621902107, DUE DATE= MAR-24-2023. DONE BY V. ANZORA 8619318 CHECKED BY L. OSTORGA 8619517.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2O22 181/1 NR 2022-481928, REMOVED AND REPLACE CONTINUITY FITTING (1 E/A) LOC BTW FRAME 1 AND 2 RH SIDE IAW A320 SRM 51-42-11, SRM 51-49-00 AND REPAIR INSTRUCTION R53112919 ISSUE F. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC600D, S/N: 210138203, DUE DATE: APR-11-2023; TORQUE: P/N: QD2R200, S/N: 0312800545, DUE DATE: JAN-06-2023. DONE BY N. LIZAMA 8626912 CHECKED BY L. OSTORGA 8619517 RII AE QC 258, QC 303, QC 259.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF AEROMAN WO 2022 181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITY FITTING (1 E/A) LOC BTW FRAME 1 AND 2 LH SIDE IAW A320 SRM 51-72-11-911-001, SRM 51-72-11-911-001, SRM 51-42-11, SRM 51-49-00 AND REPAIR INSTRUCTION R53112919 ISSUE F. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC600D, S/N: 210138203, DUE DATE: APR-11-2023; TORQUE: P/N: QD2R200, S/N: 0312800545, DUE DATE: JAN-06-2023. DONE BY N. LIZAMA 8626912 CHECKED BY L. OSTORGA 8619517 RII BY INSP AE321 A. SERMENO.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16RH SIDE IN OPEN FASTENER HOLE 2 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS AREA 6 AND 8 O CLOCK AT FWD GALLEY AREA (2EA); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00019 ) REF TO AEROMAN WO 2022 181/1 NR 2022-481995, REMOVED AND REPLACED INTERCOSTAL FITTING LOCATED ON FR16 AT LEVEL OF DOOR STOP FITTING #7 RH SIDE IAW A320 SRM 51-42-11 AND DWG # D53112300, TORQUE APPLIED 120 LB.IN. TOOL USED PN= NORTEC 500D, SN= N500X1693P030456, DUE DATE= JAN-26-2023; DIGITAL CALIPER PN= 500-196-30, SN= B21140377, DUE DATE= OCT-14-2022; TORQUE PN= QD2R200, SN= 0621902107, DUE DATE= MAR-24-2023. DONE BY V. ANZORA 8619318 CHECKED BY L. OSTORGA 8619517. RII BY AE QC 252, QC 293 AND QC 238.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 1 AND 4 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2020 181/1 NR 2022-481999, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FRAME 16 LH AT LEVEL DOOR STOP 7 IAW SRM A320 51-42-11 AND DRAWING #D53114223 EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE DATE: JAN-26-2023; TORQUE P/N: QD2R200, S/N: 0621902107, DUE DATE: MAR-24-2023. DONE BY L. OSTORGA 8619517 CHECKED BY E. ALAS 8611211 RII EA QC 284.
Part: NONE — NONE · airframe 76,915 hrs · 28,766 cycles
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 2 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2, 5, 8, AND 11 OCLOCK AT THE FWD GALLEY AREA (4 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481998, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FRAME 16 LH AT LEVEL DOOR STOP 7 IAW SRM A320 51-42-11 AND DRAWING #D53114223 EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE DATE: JAN-26-2023; TORQUE P/N: QD2R200, S/N: 0621902107, DUE DATE: MAR-24-2023. DONE BY L. OSTORGA 8619517 CHECKED BY E. ALAS 8611211 RII AE QC 284.
2021
Part: A/C PACK — CONTAMINATED · airframe 73,807 hrs · 27,617 cycles
FLT 2893, JFK-MIA. DIRTY SOCKS SMELL ON DECENT THROUGH 5000 FT. DISIPATED WITH PACK 1 OFF. PACK 1 ODOR ( PACKS ); ACCOMPLISHED WO 1132627 SVC CK AND CABIN ODOR TSM PER INFO NOTICE 2017 - T015 H SECT B2 AND AMM TASK 21-00-00 LEVEL A DECONTAMINATION. AC RESTORED TO ORIGINAL CONFIG. MX 4 UPDATED MCC NOTIFIED PLACARD REMOVED.
Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 73,090 hrs · 27,361 cycles
FLT 543, EWR-PBI. #4 F/A SMELLED THE DIRTY SOCKS SMELL BEFORE TO OUT OF EWR F/A SAID THE SMELL WENT AWAY BUT SEVERAL PAXS COMPLAINED OF THE SMELL THE SMELL CAME BACK ON DESCENT THE F/A STATED; COMPLIED WITH INFO NOTICIE 2017-T015F SECTION B. APU BLEED PLACED ON MEL 36-12-02B LP 3094198. AIRCRAFT OK FOR SERVICE. T/S ODOR EVENT W/ TSM 05-50-00-810-831-A DISCOVERED APU OVERSERVICED. DESERVICED APU AND CLEANED APU INTAKE, DIFFUSER AND ELBOW. PERFORMED LEVEL A DECOMTAMINATION OF ECS AND REPLACED BOTH RECIRC FAN FILTERS IAW AMM 21-00-00-615-802-A. MEL CLEARED, MCC NOT
Part: COMPUTER — FAILED (NR 1 ELAC) · airframe 73,091 hrs · 27,362 cycles
FLT 6122, PBI-MCO. AFTER DEPARTURE WE NOTICE THE AIRPLANE IN A SLIP AND IN A 5 DEGREE BANK RIGHT TURN WITH AUTO PILOT ON. TURNING OFF THE AUTOPILOT THE PLANE 3 BANK INCREASES FURTHER & AGRESSIVELY; PERFORMED TSM TASK 27-10-00-810-842A. R & R ELAC1 (2CE1) PER AMM 27-93-34. OPS CHK NORMAL. OK FOR SVC. CAT IIIB LAND TEST REQUIRED.
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 72,915 hrs · 27,301 cycles
DURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAILS TEST; R & R EPSU AND EPSU BATTERY AT 10WL PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-400-001-A.
Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 72,915 hrs · 27,301 cycles
DURING HEAVY MAINTENANCE, LH WING / OTBD FLAP / TRAILING EDGE / RIB 6-8 / DEBOND - PERMANENT REPAIR (PN:D575710080000 , SN: 2083); THIS REPAIR HAS BEEN APPROVED VIA THE REF /2/ RDAF. THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY ""A"" REPAIR
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 72,915 hrs · 27,301 cycles
DURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAILS TEST; R & R EPSU AND EPSU BATTERY AT 12WL PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-400-001.
2020
Part: SLIDE RAFT — FAILED (CABIN) · airframe 70,698 hrs · 26,463 cycles
DURING HEAVY MAINTENANCE, EPSU INT LOAD AND EXT LOAD FAULT SHOW ON PTP DURING EMERGENCY LIGHT TEST; REF AEROMAN N/R 2020-44268, REMOVED AND REPLACED ESCAPE SLIDE RAFT FROM DOOR 831 IAW 25-23-42 AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-001-A, TEST IS OK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,698 hrs · 26,463 cycles
DURING HEAVY MAINTENANCE, WHILE ACCOMPLISHING ITEM 13 OF TASK CARDS 320K8010 ENO -10 AND 320K8010-ENO 11, FOUND EMERGENCY LIGHTS 51WL AND 53WL INOP IN PASSENGER CABIN (2EA); REF AEROMAN N/R 2020-44247, REMOVED AND REPLACED GPSU BATTERY PACK 11WL IAW AMM 33-51-38 AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY POWER SUPPLY UNITS BY BITE CHECK IAW 33-51-00-710-001-A. TEST IS OK
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 70,698 hrs · 26,463 cycles
DURING HEAVY MAINTENANCE, CORROSION ON THRESHOLD SHEET LOCATED FR52A TO FR56 RH SIDE IN AFT CARGO COMPARTMENT; ACP ON AEROMAN W/O 2020 7/1 NON-ROUTINE 2020-44137. REMOVED AND REPLACED THRESWHOLD SHEET LOCATED FR 52A TO FR 56 RH SIDE IN AFT CARGO COMPARTMENT (1E/A) IAW A320 SRM 51-72-11 AND DRAWING D53475500.
Part: SKIN — SATURATED (RT ELEVATOR) · airframe 70,698 hrs · 26,463 cycles
DURING HEAVY MAINTENANCE, TRAPPED WATER INDICATION ON R/H ELEVATOR HOMNEYCOMB CORE STRUCTURE TOP SKIN LOC 2"" OUTBD FROM LIGHTNING STRIP N2 AND 4"" FROM T/E ( SIZE IS L=4"", W= 3""; REF AEROMAN N/R 2020-44129, PERFORMED REPAIR ON RH ELEVATOR HONEYCOMB CORE STRUCTURE TOP SKIN IAW A320 SRM 55-21-11-300-005. THIS IS A PERMANENT REPAIR, NO FURTHER ACTION REQUIRED
2019
Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 68,233 hrs · 25,545 cycles
FT # 2074, EMERGENCY FLOOR LIGHT ROW 1 HELD ON BY A BANDAID. FALLING OFF. SECURED ROW 1 EMERGENCY LIGHT LENS COVER AS REQUIRED IAW AMM 33-50-00. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 67,183 hrs · 25,144 cycles
FLT 1043, EWR-PBI. MULTIPLE EXIT SIGNS WITH BULBS BURNED OUT; RELAMPED AS REQUIRED OPS CK NORM MM 33-51-16.
2018
Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 65,855 hrs · 24,669 cycles
COCKPIT/CABIN HAD AN ODOR WHILE DESCENDING FROM 370 - 330. F/A CALLED ABOUT ODOR ROW 21-25. BURNING ELEC. METALIC ODOR IN COCKPIT. ACCOMPLISHED ODOR RECOGNITION AND ISOLATION PROCEDURE FCOM VOL-1 PACK 1 OFF 3-5 MIN. ODOR DISSIPATED, KEPT CONFIGURATION THROUGH 10,00 FT. SMELLED BURNING RUBBER ODOR THROUGH 4600 FT, PILOT SMELLED DIRTY SOCK ODOR FOLLOWED BY HEADACHE & NAUSEA. NR 3 FA REPORTED HEADACHE. ACCOMPLISHED INFO NOTICE 2017-T015C. PERFORMED TSM 05-50-00-810-831-A. ACCOMPLISHED TABLE 1 SECT C LVL 3 ENG IDLE RUN AMM 71-00-00-810-801-A. PARAG 4 FAULT ISOLATION NO DEFECT NOTED. PERFORMED ELECTRICAL BURNING ODOR & FUMES INSPECTION PER AMM 24-00-00-810-823-A. NO DEFECTS NOTED & NO ODOR DETECTED THROUGHOUT COCKPIT & CABIN. AT THIS TIME OPERATED ALL ELECTRICAL SYSTEMS, GALLEYS LAVATORIES IFE APU & A/C PACKS. NO DEFECTS FOUND. A/C OK FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,187 hrs · 24,018 cycles
DURING A CABIN EMERGENCY LIGHT TEST, FAILED FOR EMERGENCY LIGHT 12WL. REMOVED AND REPLACED THE EPSU 12WL BATTERY PACK IAW AMM 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS TESTED GOOD IAW AMM 33-54-38-805-058-A. OPEN
2017
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,808 hrs · 23,064 cycles
LENS FOR EMERGENCY EXIT LIGHT SEAT 3C MISSING. REPLACED THE EMERGENCY LIGHT LENS.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,610 hrs · 22,973 cycles
DURING A WEEKLY EMERGENCY LIGHT TEST, THE SYSTEM FAILED. FOUND THE EPSU BATTERY AT FAULT 10WL AND 13WL. R & R BOTH BATTERY PACKS IAW AMM 33-51-38. OPS TESTED OK.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,610 hrs · 22,973 cycles
DURING A WEEKLY EMERGENCY LIGHT TEST, THE SYSTEM FAILED. FOUND EPSU BATTERY AT FAULT 10WL AND 13WL. R & R BOTH BATTERY PACKS IAW AMM 33-51-38. OPS TESTED OK.
Part: ENGINE — ODOR (NR 1) · airframe 60,040 hrs · 22,382 cycles
TURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACED. NO DEFECTS NOTED AT THIS TIME AND AIR QUALITY SATIFACTORY.
Part: FILTER — ODOR (OZONE) · airframe 60,040 hrs · 22,382 cycles
TURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACED. NO DEFECTS NOTED AT THIS TIME AND AIR QUALITY SATIFACTORY.
2016
Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 57,548 hrs · 21,476 cycles
SEAT TRACK CORRODED FRAMES 12 - 24 -Y1292R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 REV. 114 TASK 53-00-14-283-002. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11 REV 114.
Part: SEAT TRACK — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 57,548 hrs · 21,476 cycles
SEAT TRACK CORRODED FRAMES 12-14 Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 57,548 hrs · 21,476 cycles
FLOOR SUPPORT CORRODED FRAMES 12 - 16, -Y1379.5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-1-14.
2015
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,202 hrs · 20,626 cycles
RIGHT EMERGENCY BATTERY FAULT. R & R RT EMERGENCY BATTERY IAW 33-51-38. OPS CHECK GOOD.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,202 hrs · 20,626 cycles
LEFT EMERGENCY BATTERY FAULTED. R & R LT EMERGENCY BATTERY IAW 33-51-38. OPS CHECK GOOD.
Part: CONTROL UNIT — FAILED (MLG) · airframe 52,174 hrs · 19,523 cycles
FLT 198, CREW DECLARED AN EMERGENCY AND AIRCRAFT DIVERTED DUE TO LGCIU FAILURE. REMOVED AND REPLACED LGCIU PER 32-31-71 OPS CHECKED OK FOR SERVICE.
2014
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 51,354 hrs · 19,243 cycles
EMERGENCY DECLARED. DURING LANDING FLIGHT CONTROL FLAPS LOCKED, SLATS AT 2 FLAPS LESS THAN 1 ON ECAM. UNLOCKED FLAP WING TIP BRAKE AND OPERATED FLAPS SEVERAL TIMES WITH NO FAULTS. PERFORMED INSPECTION OF FLAPS AND DRIVE UNITS, NO DEFECTS FOUND IAW TSM 37-51-00-810-818. ACCOMPLISHED TSI ON LT FLAP INTERCONNECTING STRUT CHECKED AND FOUND OUT OF RIG. RIGGED STRUT IAW AMM 27-51-44. INSPECTION OF ALL FLAP DRIVE SYSTEMS FOUND IN CORRECT POSITION. ALL TORQUE TUBES FOUND OK AND NO ADJUSTMENTS REQUIRED. FLAPS SYSTEM CHECKS OK IAW AMM 27-54-00.
Part: SENSOR — FAILED (NLG STEERING) · airframe 50,986 hrs · 19,111 cycles
CREW REPORTED NOSE WHEEL STEERING (NWS) FAULT. WILL NOT RESET. LOST ALL STEERING DURING LANDING. ACFT TOWED TO GATE. R & R 3GC NWS FEEDBACK SENSOR IAW AMM 32-51-19. OPS CHECK GOOD.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,473 hrs · 14,791 cycles
FLT 84 FLL-JFK, FWD, AFT & MID CABIN CEILING LEVEL EXIT IDENTIFIER EMERGENCY LIGHTS & OVER WING EXIT IDENTIFIERS HAS NUMEROUS BULBS INOP. RELAMPED ALL CEILING & OVER WING EXIT IDENTIFIER BULBS AS REQUIRED, OPS CHECK PER AMM 33-51-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,473 hrs · 14,791 cycles
FLT 84 FLL-JFK, ON GROUND MAINTENANCE CHECK FOUND EXIT IDENTIFIER EMERGENCY LIGHTS ON R1, R2, L2 DOORS HAS NUMEROUS BULBS BURNT OUT. EMERGENCY LT TEST FAILED. RELAMPED ALL EXIT IDENTIFIER AS REQUIRED PER AMM 33-51-00. OPS CHECK OK.
Part: CONTROLLER — FAULTY (AC PACK) · airframe 37,738 hrs · 14,545 cycles
FLT 136 RSW-JFK, DIVERTED TO MCO, DUE TO PACK 1 FAULT AT 30,000 FT. REMOVED AND REPLACED NR 1 PACK CONTROLLER 7HH IAW AMM 21-61-34. OPS CHECK FOUND OK.
Part: EPSU — FAILED (CABIN) · airframe 36,110 hrs · 13,982 cycles
FLT 445 BOS-TPA, ON GROUND AND WHILE PERFORMING EMERGENCY LIGHTS SYS TEST FROM PTP, FOUND EMERGENCY POWER SUPPLY LEFT FAILED. REPLACED EPSU 11WL PER AMM 33-51-38. SYS TEST GOOD.