N640JB

Part: UNKNOWN — ODOR (CABIN) · airframe 72,146 hrs · 25,808 cycles

FLT#2321, BOS-PBI. "DESCENDING THROUGH 9,000 AFT FLIGHT ATTENDANT REPORTED HOT PLASTIC ODOR EMITTING FROM AFT GALLEY THE ODOR WAS TRANSIENT. FOLLOWED A320 ODOR RECOGNITION & ISOLATION GUIDANCE FCOM PAGE 4-54 STEPS 1,2,14; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10 CONTAMINATION (CABIN ITEMS ACCOMPLISHED FULL VISUAL INSPECTION OF COFFEE MAKERS AND GALLEY WIRING NO FAULT FOUND). COULD NOT DUPLICATE TRANSIENT ODOR. LEVEL 1 DECONTAMINATION ACCOMPLISHED PER TSM 05-50-00-810-B/05-50810-055D . AIRCRAFT IS OK FOR SERVICE."

Part: UNKNOWN — ODOR (CABIN) · airframe 71,805 hrs · 25,678 cycles

FLT#1310, JAX-BOS. "ELECTRICAL BURING SMELL BETWEEN ROWS 19-24 REPORTED BY FLIGHT ATTENDANTS AND PAX. NO SMOKE VISIBLE DURING TROUBLESHOOTING FA TURNED OFF PED AND SMWLL DISSAPTED. BURNING SMELL LASTED APPROX 5 MIN DURING CRUISE. ( THALES-AVANT IFE (ENTIRE SYSTEM) ); REMOVED CB COLLERS AND REACTIVATED AVANT IFE SYS. EXAMINED AVANT IFE AT ROWS 19-24 AND FOUND NO EVIDENCE OF BURING SMOKE OR SMELL. COULD NOT DUPLICATE. AVANT IFE SYS. OPS CHK GOOD IAW 44-21-00. MDDR CLR MX-4 UPDATED AND PLACARD REMOVED."

Part: CONTROL UNIT — DAMAGED (WX RADAR) · airframe 68,769 hrs · 24,502 cycles

FLT#255, JFK-PLS. (AIRCRAFT DIVERTED TO FLL) 'INFLIGHT WX RADAR FAILURE DIVERT TO FLL THUNDER STORMS AND HURRICANE OSCAR IN THE AREA OF PLS; REMOVED AND REPLACED WX RADAR CONTROL UNIT IAW AMM 34-41-12 OPS CHECK GOOD. WEATHER RADAR CHECK GOOD.'

Part: CONTROL SYSTEM — FAULTED (SPOILERS) · airframe 68,034 hrs · 24,224 cycles

FL698, MCO-LGA. (AIRCRAFT DIVERTED TO JFK) 'SPOILER 3/4 FAULT ( GRND SPOILER CNTRL SYS -1 & 2 OR 3 & 4 ). OPEN

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 67,364 hrs · 23,972 cycles

FLT#2836, LAX-SFO. (AIRCRAFT DECLARED AN EMERGENCY INTO SFO) ' HYD Y RSVR LO LVL ECAM; FOUND PINCHED O-RING ON PUT MANIFOLD, REPLACED O-RING PER AMM 29-13-15. PERFORMED OPS CHECK NO LEAKS NOTED, OK FOR SVC, REPLACED HYD LOW & HIGH FILITERS, OPS CK GOOD, NO LEAKS NOTED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,590 hrs · 23,293 cycles

FLT#128, MCO-EWR. 'EPSU (EMERGENCY POWER SUPPLY UNIT) AT 11WL INOP; REMOVED AND REPLACED LH AFT EMERGENCY LIGHT AFT LAMP IAW AMM 33-51-15. OPS CHECK GOOD.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR32 BTW STR40R TO STR41R I N FWD CARGO COMPARTMENT (CPCP REFER TO THE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00012 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640725 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC. FR32 BTW STR40R TO STR41R IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11, AND DWG D53231585.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H1 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (2 EA); REF AEROMAN W/O 2023 280/1 WCC 2023-640742 REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FR 16 LH SIDE AT LEVEL DOOR STOP FITTING #7 IAW A320 SRM 51-42-11 AND DWG D53112300. WORK C/OUT BY AEROMAN TECH 8600804 RII: QC273.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR31 BTW STR40R TO STR41R I N FWD CARGO COMPARTMENT (CPCP REFER TOTHE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00011 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640715 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC. FR31 BTW STR40R TO STR41R IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11, AND DWG D 53231375.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR28 BTW STR41L TO STR42L IN FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00007 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640699 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC. FR28 BTW STR41L TO STR42L IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53231375. WORK ACCOMPLISHED BY AEROMAN TECH 8673420 RII: QC329.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION SPLICE LOC. BTW FR30 TO FR31 AT LEVEL STR41R IN FWD CARGO COMPARTMENT (CPCP REFER TO THE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00013 ) REMOVED AND REPLACED SPLICE LOC. BTW FR30 TO FR31 AT LEVEL STR41R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND A320 SRM 51-72-11, DWG D53231586 WORK ACCOMPLISHED ON AEROMAN NRC 2023-640714 WO 2023 280/1.' (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC FR28 BTW STR41R TO STR42R IN FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00008 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640698 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC FR28 BTW STR41R TO STR42R IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53231375. WORK ACCOMPLISHED BY AEROMAN TECH 8673420 RII: QC329.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOASTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC 2023-640741. REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FR 16 RH SIDE AT LEVEL DOOR STOP FITTING #7 IAW A320 SRM 51-42-11 AND DWG D53112300. WORK C/OUT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR30. BTW STR40R TO STR41R IN FWD CARGO COMPARTMENT (CPCP REFER TOTHE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00010 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640701 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC. FR30. BTW STR40R TO STR41R IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11, AND DWG D53231375.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 O CLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC 2023-640743 REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FR 16 LH SIDE AT LEVEL DOOR STOP FITTING #7 IAW A320 SRM 51-42-11 AND DWG D53112300.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 O CLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC 2023-640743 REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FR 16 LH SIDE AT LEVEL DOOR STOP FITTING #7 IAW A320 SRM 51-42-11 AND DWG D53112300. WORK C/OUT BY 8600804 RII: QC273.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,423 hrs · 23,236 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR30 BTW STR40L TO STR41L I N FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00009 ) REF AEROMAN W/O 2023 280/1 WCC 2023-640700 REMOVED AND REPLACED TIE CLIP (CLEAT) LOC. FR30 BTW STR40L TO STR41L IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53231212. WORK ACCOMPLISHED BY AEROMAN TECH 8632015 RII: QC230.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,317 hrs · 22,432 cycles

FLT#751, JFK-CUN. '#3 #4 F/A'S BOTH NOTICED A STRONG BURNING ODOR FROM THE AFT GALLEY ON DESCENT; C/W INFORMATION NOTED 2017 -T015J, SECTION A, ISOLATED FAULT TO TYPE 10A1 C TSM 05-50-00-810-085-B TSM 05-50-00-810-085-D. A/C OK FOR SERVICE AND PERFORMED TSM 24-00-00-810-824. A/C OK FOR SERVICE.'

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 833 CRACK LENGTH 0.380 INCH AND LOCATED AT SIXTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-114-01 ON EMERGENCY EXIT DOOR 833 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE. (WO#1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF; AEROMAN WO# 2022-167/1 WCC#2022-351253 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON AFT INNER FRAME SEGMENT (1) LOC EMERG EXIT DOOR 844. CRACK LENGTH 0.150" AT FOURTEENTH FASTENER. CRACK LENGTH 0.250 INCH LOCATION FIFTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC# A320-52-1144-04 ON EMERG EXIT DOOR 844 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE (WO#1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO#2022-167/1 WCC#2022-351258 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON FWD INNER FRAME SEGMENT (1)LOC. EMERG EXIT DOOR 834. CRACK LENGTH 0.300 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE, CRACK LENGTH 0.335 INCH LOC AT FOURTEENTH FASTENER L= 0.250" LOC AT FIFTEENTH FASTENER CRACK L= 0.370 INCH AT SIXTEENTH FASTENER CRACK L= 0.280" AT SEVENTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC# A320-52-1144-03 ON EMERG EXIT DOOR 834 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE. (WO#1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO# 2022-167/1 WCC#2022-351255 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 843. CRACK LENGTH 0.030 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-1144-02 ON EMERGENCY EXIT DOOR 843 FOR REPLACEMENT FO FRAME REINFORCE DOOR STRUCTURE. (WO#1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO#2022-167/1 WCC#2022-351251 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON AFT INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 843 CRACK LENGTH 0.240 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-1144-02 ON EMERGENCY EXIT DOOR 843 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE(WO# 1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF; AEROMAN WO#2022-167/1 WCC# 202-351252 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND ON AFT INNER FRAME SEGMENT(1) LOC EMERG EXIT DOOR 833. CRACK LENGTH 0.100 INCH AND LOCATED AT SIXTEENTH FASTENER FROM UPPER SIDE AND SEVENTEENTH FASTENER FROM UPPER SIDE, CRACK LENGTH 0.120 INCH; ACCOMPLISHED EC#A320-52-1144-01 ON EMERG EXIT DOOR 833 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE. (WO#1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO#2022-167/1 WCC#2022-351254 FOR ORIGINAL FINDING.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 844. CRACK LENGTH 0.350 INCH AND LOCATED AT FIFTH FASTENER FROM UPPER SIDE CRACK LENGTH 0.315 INCH LOC AT FIFTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC# A320-52-1144-04 ON EMERG EXIT DOOR 844 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE. (WO# 1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO#2022-167/1 WCC#2022-351257.

Part: FRAME — CRACKED · airframe 60,572 hrs · 21,402 cycles

DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON THE AFT INNER FRAME SEG(1)LOC. EMERG EXIT DOOR 834. CRACK LENGTH 0.325 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE. CRACK LENGTH 0.335 INCH LOC AT SEVENTH FASTENER, CRACK LENGTH 0.290" LOC AT EIGHTH FASTENER, CRACK L= 0.370 INCH AT SIXTEENTH FASTENER, CRACK L= 0.280" AT SEVENTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC# A320-52-1144-03 ON EMERG EXIT DOOR 834 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE. (WO# 1175016) AEROMAN RII QC220AE -MAJOR REPAIR REF AEROMAN WO#2022-167/1 WCC# 2022-351256 FOR ORIGINAL FINDINGS.

Part: A/C PACK — ODOR (CABIN) · airframe 56,803 hrs · 20,086 cycles

FLT 165, BOS-RSW. ON TAKE OFF & DECENT AROUND 5K HAD A STRONG SMELL IN THE CABIN. ALMOST LIKE VHEMICAL OF SOME KIND. FA SAID MAYBE DIRTY SOCK SMELL. SEEMS NOW AT GATE APU RUNNING HERE FAINT DIRTY SOCK SMELL. ( APU BLEED VALVE ); REACTIVATED APU AFTER ECS DECONTAMINATION IAW AMM 49-51-00. OPS CHECK GOOD. MDDR CLEARED. PLACARD REMOVED. MX-4 UPDATED. REF TSI 433661 FOR DECONTAMINATION

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 51,884 hrs · 18,296 cycles

FT # 1692, LIR-JFK. SEAT MOUNTED EMR LIGHT AT SEAT 3C AND 7C FOUND INOP; R & R OF SEAT MOUNTED EMER LIGHT AT SEAT 3C AND 7C IAW AMM 33-51-18. NO HELP. R & R OF EPSU & EMER LIGHT BATTERY AT 11WL IAW AMM 33-51-38. ALL OPS NML OK FOR SVC.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 51,884 hrs · 18,296 cycles

FT # 1692, LIR-JFK. SEAT MOUNTED EMR LIGHT AT SEAT 3C AND 7C FOUND INOP; R & R OF SEAT MOUNTED EMER LIGHT AT SEAT 3C AND 7C IAW AMM 33-51-18. NO HELP. R & R OF EPSU & EMER LIGHT BATTERY AT 11WL IAW AMM 33-51-38. ALL OPS NML OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,547 hrs · 17,788 cycles

FT # 878, LAS-BOS. RH OVERWING EMERGENCY LIGHTS INOP; R & R RH OVER-WING EMERGENCY LIGHT BATTERY IAW AMM 33-51-00, OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 46,170 hrs · 16,123 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE SEAT TRACK -Y1292, BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACT IAW SRM 51-72-11.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 43,709 hrs · 15,190 cycles

DURING ROUTINE WEEKLY CHECK, A FAULTY EPSU BATTERY WAS FOUND. R & R THE BATTERY IAW AMM 31-51-00. OPS CHECK PASSED.

Part: BATTERY — FAILED (CABIN) · airframe 41,538 hrs · 14,381 cycles

DURING ROUTINE MAINTENANCE, EMERGENCY LIGHT FAILED TEST; R & R EMERGENCY LIGHT BATTERY 12WL. PERFORMED BITE CHECK. BITE CHECK PASSED.

Part: SWITCH — FAILED · airframe 40,947 hrs · 14,164 cycles

PILOT REPORTED EMERGENCY LIGHTS CAME ON AFTER 2ND ENGINE START. REPLACED EMERGENCY LIGHT ARM SWITCH, TOGGLE, 4WL IAW AMM 33-51-08. PERFORMED OPS CHECK AND ENGINE RUN. NO FAULTS FOUND.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 40,505 hrs · 13,992 cycles

DURING MAINTENANCE IT WAS DISCOVERED THAT EMERGENCY LIGHTS TEST FAILED FOR THE FWD LT, R & R EPSU BATTERY AT 10 WL IAW AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPS CHECK WAS PERFORMED IAW AMM 33-51-38-710-052-B AND OPS CHECK PASSED.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

MAIN CABIN AFT WET AREA SHEAR PLATE HAS CORROSION, LOCATION: Y1732, FRAME 69+8", STR 23 LT. R & R SHEAR PLATE IAW SRM 51-42-11 AND 53-41-14.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

AFT CABIN FLOORBEAM, 765, FRAME 68, STR 23 RT, HAS CORROSION; R & R FLOORBEAM IAW SRM 53-42-11.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

MAIN CABIN FLOORBEAM, LOCATION: 1292, FRAME 68, STR 23L, HAS CORROSION. R & R MAIN CABIN FLOORBEAM 1292, FRAME 68, STR 23L.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

MAIN CABIN FLOORBEAM, 1292, FRAME 68, STR 23R, HAS CORROSION; R & R FLOORBEAM IAW SRM 51-42-11, 53-41-14 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

AFT CABIN FLOORBEAM HAS CORROSION, 765, FRAME 68, STR 23L. R & R FLOORBEAM IAW SRM 53-00-14, 51-41-14, 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

LEFT PASSENGER DOOR SILL LOWER, 1762, FRAME 16, STR 23LT, AFT TWO HOLES HAS CORROSION. SPOTFACED AREA AND INSTALLED REPAIR WASHERS IAW SRM 53-11-14.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

AFT MAIN CABIN FLOORBEAM HAS CORROSION, 765, FRAME 68. R & R AFT MAIN CABIN FLOORBEAM 765 FRAME IAW SRM 51-42-11 & 53-00-14.

Part: FLOOR SUPPORT — CORRODED (FRAME 67) · corrosion level 2 · airframe 40,505 hrs · 13,992 cycles

AFT CABIN FLOOR SUPPORT HAS CORROSION, LOCATION: Y1292, FR 67 +10", R & R FLOOR SUPPORT SRM 51-44-11, 53-41-14, 53-00-14.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 34,185 hrs · 11,790 cycles

CREW REPORTED EMERGENCY LIGHT AT 9C INOPERATIVE. REPINNED CONNECTOR 7261VC1A IAW AWM 33-51-07. OPS CHECK OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 34,185 hrs · 11,790 cycles

CREW REPORTED THAT EMERGENCY EXIT FLOOR LIGHTING RED LIGHT AFT END OF AISLE IS INOPERATIVE. IDENTIFIED LIGHT TO BE INSTALLED ON LAV D WALL. REPAIRED WIRING IAW ESPM 20-43-00. LIGHT OPS CHECK NORMAL.

Part: FAN — FAILED (NR 1) · airframe 31,241 hrs · 10,757 cycles

DURING MAINTENANCE, ELECTRICAL BURNING ODOR IN THE CABIN WAS NOTED. FUTHER TROUBLESHOOTING INDICATED ODOR COMING FROM RECIRCULATING FAN NR 1. R & R NR 1 FAN IAW AMM 21-21-51-000-001-A, OPS CHECK OK. NO ODOR NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,319 hrs · 10,445 cycles

DURING WEEKLY CHECK, CIDS MESSAGE FOR EXTERNAL POWER SUPPLY UNIT EXT LOAD EMERGENCY RT POPPED UP. SLAVED IN RT OVER WING ESCAPE SLIDE IAW FIM TASK 33-51-00-810-808-A. NO HELP RE-INSTALLED ORIGINAL SLIDE. FOUND OVER WING LIGHT ASSEMBLIES AT FAULT. REPLACED LAMP ASSEMBLIES. OPS CHECK GOOD, REF FIM 33-51-00-810-808-A.

Part: COMPUTER — FAILED (NR 1) · airframe 22,676 hrs · 7,969 cycles

FLT NR 6103, AIRCRAFT DIVERTED DUE TO A/C WAS IN LEFT BANK DURING STRAIGHT LEVEL FLIGHT, RUDDER SHOWED 2.6L DEFLECTION. REMOVED AND REPLACED ELAC 1 IAW AMM 27-93-34. ADJUSTED LT WING BLUE AND GREEN AILERON SERVOS PER AMM 27-14-00. ADJUSTED THREE RUDDER SERVOS DUE SLIGHTLY OUT OF TRIANGLE, ADJUSTED ALL THREE RUDDER SERVO SPRING RODS PER MM 27-24-00. OPS CHK OK.

Part: CABLE ASSY — FAILED (EMERGENCY EXIT) · airframe 22,621 hrs · 7,948 cycles

FLT 6439, DURING HEAVY MAINTENANCE - RT EMERGENCY EXIT CABLE TEST FAILED. REPLACED EXIT CABLE AS PER A320-53-1227-02 & 25-62-43-400-001. OPS CHECK OK.

Part: CABLE ASSY — FAILED (EMERGENCY EXIT) · airframe 22,621 hrs · 7,948 cycles

FLT 6439, DURING HEAVY MAINTENANCE- LT EMERGENCY EXIT CABLE TEST FAILED. REMOVED AND REPLACED LT EMERGENCY CABLE AS PER 320-53-1227-02. & 25-62-43-400-001. OPS CHECK OK.

Part: SENSOR — FAILED (AC PACK) · airframe 20,197 hrs · 7,117 cycles

FLT 968 FLL-BOS, ON DESCENT OUT OF 25,000 FEET CREW REPORTED ECAM MESSAGE PACK 1 FAULT WITH PACK 2 ALREADY IN MEL THE CREW DESCENDED TO 10,000 FEET. PACK 1 WAS UNSTABLE AND TEMP INDICATION AMBER XXX'S. TECHNICIAN REMOVED AND REPLACED COMPRESSOR TEMP SENSOR ON PACK NR 1 IAW AMM 21-61-11-04. ALL OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 17,266 hrs · 6,098 cycles

FLT 120 MSY-JFK LP 708734 - EMERGENCY EXIT LIGHT AT LT ROW 7 INOP. FOUND BROKEN WIRE UNDER SEAT, EMERGENCY LIGHT 33-50-19 CHECKS OK. SPLICED PER ESPM 20-41-00.

Part: SLIDE — FAILED (L2 DOOR) · airframe 11,973 hrs · 4,226 cycles

DURING ACCOMPLISHMENT TASK CARD A320-25-62-00-720-001, DOOR ESCAPE SLIDE OPERATIONAL CHECK OF L2 DOOR SLIDE. SLIDE FAILED TO DEPLOY PROPERLY. FURTHER INSPECTION REVEALED SLIDE FORWARD RELIEF VALVE CAUGHT ON SLIDE PACK COVER. REMOVED AND REPLACED L2 EMERGENCY SLIDE PER TASK CARD A320-25-62-44-400-007 AND SERVICED DOOR ASSIST BOTTLE AS PER TASK CARD A320-52-10-00-610-001.

Part: HYDRAULIC LINE — LEAKING (NR 1 PYLON) · airframe 9,569 hrs · 3,352 cycles

IN CRUISE, INBOUND SJC-JFK, LOSS GREEN HYD SYS PRESSURE, FOUND HYDRAULIC CASE RETURN LINE LEAKING IN NR 1 ENGINE PYLON. REMOVED AND REPLACED NR 1 ENG HYDRAULIC CASE RETURN LINE & REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRECAUTIONARY DUE TO TOTAL HYD FLUID LOSS PER AMM 29-11-51-04. SERVICED GREEN SYSTEM HYD RESERVOIR PER AMM 12-12-29-611-001, OPS LEAK CHECK OK.

Part: ELECTRICAL BOX — MALFUNCTIONED (CABIN) · airframe 7,673 hrs · 2,669 cycles

FLT 704, SJU-JFK, F/A REPORTED BURNING SMELL AROUND ROW 11. LIVE TV MASTER TURNED OFF AND SMELL STOPPED. PERFORMED LTV ELECTRICAL ODOR SYSTEM INTEGRITY CHECK. REMOVED AND REPLACED XEB 10 RT. ALL AS PER LIVE TV MM 23-39-00. ALL OPS CHECK NORMAL.