N595JB

Part: BATTERY — FAILED (ZONE 200) · airframe 76,894 hrs · 27,806 cycles

FLT#591, BOS-TPA. "EMERGENCY LIGHT BATTERY (10WL) FAILED TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (10WL) IAW AMM 33-51-38 OPS CHK GOOD. A/C OK CONT SVC."

Part: BATTERY — FAILED (ZONE 200) · airframe 76,894 hrs · 27,806 cycles

FLT#591, BOS-TPA. "EMERGENCY LIGHT BATTERY (12WL) FAILED TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (12WL) IAW AMM 33-51-38 OPS CHK GOOD. A/C OK CONT SVC."

Part: APU — LEAKING (APU) · airframe 74,370 hrs · 26,837 cycles

FLT#1643, JFK-BON. 'CABIN ODOR REPORTED BY FA DURING SHORT FINAL CABIN ODOR REPORTING FORM ATTACHED ( PACKS ); FOLLOWING TSM TASK 05-50-00-810-085. FOUND OIL ON INLET PLENUM AND COMPRESSOR AREA OF APU. REF TO MDDR # 567522 FOR APU DEFERRAL. APU BLEED WAS THE SOURCE OF ODOR. ACCOMPLISHED LEVEL B DECONTAMINATION OF THE ECS IAW AMM 21-21-41. NO SMELL NOTED PACK 1 NOW OPERATIONAL. THIS CLEARS THE MDDR. MX-4 UPDATED PLACARD RMVD.'

Part: ENGINE — ABNORMAL (ENGINE #1) · airframe 74,128 hrs · 26,750 cycles

FLT#2224, MCO- DCA- (AIRCRAFT DIVERTED TO RDU).' MULTIPLE ENG 1 ENG FAULTS IN FLIGHT/ ENG 1 MODE FAULT AUTO THRUST OFF ENG 1 REVERSER FAUT / ENG 1 EGT OVR TEMP SHORT FINAL.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: OIL SYSTEM — LEAKING (APU) · airframe 74,020 hrs · 26,693 cycles

FLT#69, BOS-FLL. 'DIRTY SOCK SMELL REPORTED BY FA 1 JUST PRIOR TO LANDING; COMPLIED WITH INFO NOTECE 2017-T015 SECTION B2 . IDENTIFIED ODOR DUE TO APU LEAK INTO INLET . DECONTAMINATION LEVEL B WAS ACCOMP PER TSM 21-00-00-615-803A . A/C OK FOR SERVICE.'

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 RH DOOR STOP FITTING 7 UPPER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00017) REF AEROMAN WO: 2024 253/1 WCC# 2024-501348. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FITTING #7 I.A.W A320 SRM 53-11-12-300-010, THIS REPAIR IS CATEGORY A, NO REQUIRED FURTHER INSPECTION, THIS REPAIR IS CONSIDERED PRIMARY STRUCTURE I.A.W A320 SRM 51-11-12. DONE BY AE TECH# 90036 BUYBACK AE RII QC# 329.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE, PRESSURE BULKHEAD FWD SIDE AT FR35 & STGR30L CRACKED FASTENER HOLES REFERENCE: /1/ AEROMAN EA 53-9036-24 REV. 0 (COVER + PART 1-3) /2/ AIRBUS RDAF 81452909/003/2024#A /3/ AIRBUS RI R533-70268 ISSUE C /4/ AIRBUS RI R533-70269 ISSUE D. DESCRIPTION: DURING C7 CHECK ON N595JB (MSN 02286) AT SAL DATED AUG 2024, WHILE PERFORMING INSPECTION PER MPD 533186-01, TWO CRACKED HOLES - HOLES#6 (FRAME WEB LAYER ONLY) AND HOLE #2 (FWD SKIN LAYER ONLY) WERE REPORTED AT FR35 & STGR30LH PRESSURE BULKHEAD FWD SIDE ATTACHMENT. SEE REF /1/ EA FOR MORE DETAILS. THERE IS NO OEM MANUAL TO REPAIR THIS TYPE OF DAMAGE. THEREFORE, AIRBUS WAS CONTACTED FOR ASSESSMENT AND PROVIDED REPAIR INSTRUCTIONS REF /4/ RI AT HOLE #6 TO PERFORM CUTOUT AND INSTALL REINFORCED FITTING WITH REPAIR FILLER, AND REF /3/ RI AT HOLE #2 TO PERFORM REAMING AND COLDWORKING AND INSTALL OVERSIZED FASTENER. THESE INSTRUCTIONS ARE APPROVED BY REF /2/ RDAF AS A CAT B PERMANENT REPAIR WITH ADDITIONAL INSPECTION REQUIRED. - EC A24-1138-01 ACCOMPLISHED REPAIR INSTRUCTION PER THE REF /1/ EA AND COMPLIES WITH REF /2/ RDAF WITHOUT DEVIATION. - EC A24-1138-02 TRACKS POST REPAIR INSPECTION AT HOLE W1 (POST REPAIR HOLE #6) (THRESHOLD: 13 100 FC / 26 200 FH, INTERVAL: 13 100 FC / 26 200 FH, METHOD: EDDY CURRENT) - EC A24-1138-03 TRACKS POST REPAIR INSPECTION AT HOLE #2 (THRESHOLD: 34 700 FC / 69 400 FH, INTERVAL: TBD, METHOD: TBD) - EC A24-1138-04 TRACKS POST REPAIR INSPECTION AT REPAIR FITTING (THRESHOLD: 48 500 FC / 97 000 FH, INTERVAL: TBD, METHOD: TBD) SUBSTANTIATION: THIS REPAIR IS APPROVED AS A CAT B PERMANENT REPAIR PER REF /2/ RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-1138-01)

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 68 LH LOWER INBD HOLEN OF DOOR STOP FITTING N1 AREA CRACK D = 0.135INCH; REF AEROMAN N/R 2024- 501342, PERFORMED REPAIR IAW A320 SRM 53-41-12-300-011. REF FUR A320 -53-1712.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 LH DOOR STOP FITTING 7 LOWER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00015) REF AEROMAN WO: 2024 253/1 WCC# 2024-501346. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FITTING #7 I.A.W A320 SRM 53-11-12-300-010, THIS REPAIR IS CATEGORY A, NO REQUIRED FURTHER INSPECTION, THIS REPAIR IS CONSIDERED PRIMARY STRUCTURE I.A.W A320 SRM 51-11-12. DONE BY AE TECH# 8621321 BUYBACK AE RII QC# 273.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 844 AFT RH SIDE. CRACK LENGTH = 0.100 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501292 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME / REINFORCE DOOR STRUCTURE -MODIFICATION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 834 AFT LH SIDE. CRACK LENGTH = 0.164 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501291 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH EEH) FRAME / REINFORCE DOOR STRUCTURE -MODIFICATION.

Part: FRAME — CRACKED (ZONE 100) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 35 PRESSURE BULKHEAD FWD FACE LH SIDE, FROM LOWER OUTBOARD FASTENER AT LEVEL OF STGR30, CRACK LENGTH IS 0.095 INC H APROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN N/R 2024-501382, ACCOMPLISHED REPAIR HOLE LOCATED ON FRAME 35 PRESSURE BULKHEAD FWD FACE LH SIDE, FROM LOWER OUTBOARD FASTENER AT LEVEL OF STGR30LH, IN FWD CARGO COMPARTMENT, I.A.W AEROMAN EA#53-9036-24 REV 0 REPAIR DWG R533-70268 ISSUE C, REPAIR DWG R533-70269 RDAF 81452909/003/2024 )A) EC A24-1138-01.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 RH DOOR STOP FITTING 7 LOWER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00016) REF AEROMAN WO: 2024 253/1 WCC# 2024-501347. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FITTING #7 I.A.W A320 SRM 53-11-12-300-010, THIS REPAIR IS CATEGORY A, NO REQUIRED FURTHER INSPECTION, THIS REPAIR IS CONSIDERED PRIMARY STRUCTURE I.A.W A320 SRM 51-11-12. DONE BY AE TECH# 90036 BUYBACK AE RII QC# 329.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 LH DOOR STOP FITTING 7 UPPER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00014) REF AEROMAN WO: 2024 253/1 WCC# 2024-501345. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FITTING #7 I.A.W A320 SRM 53-11-12-300-010, THIS REPAIR IS CATEGORY A, NO REQUIRED FURTHER INSPECTION, THIS REPAIR IS CONSIDERED PRIMARY STRUCTURE I.A.W A320 SRM 51-11-12. DONE BY AE TECH# 8621321 BUYBACK AE RII QC# 273.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 833 FWD LH SIDE. CRACK LENGTH = 0.177 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501290 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD LH EEH) FRAME / REINFORCE DOOR STRUCTURE -MODIFICATION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 73,691 hrs · 26,560 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENT 1 (FWD AND AFT) OF THE E MERGENCY EXIT HATCH DOOR 843 . FWD RH SIDE. CRACK LENGTH = 0.152 INCH APROX; REF: ARM W/O 2024 253/1 N/R 2024-501289 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD RH EEH) FRAME / REINFORCE DOOR STRUCTURE -MODIFICATION.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,576 hrs · 25,716 cycles

FLT#1761, LGA-PBI. (AIRCRAFT DIVERTED TO JFK) 'ENG STALL # 2; PERFORMED BSI ON ENG 2 OF THE HPC STAGES 3, 6 AND 7 IAW AMM 72-00-00-200-016. NO DEFECTS NOTED AT THIS TIME.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,927 hrs · 25,442 cycles

FLT#1079, LAS-LAX. ' CABIN CREW REPORTED TO NEW FLIGHT CREW ABOUT FUME EVENT DURING INBOUND FLIGHT FUME WERE EXPERIENCED BY CREW & PAX & CLEANERS DURING CLIMB, DESCENT AND LANDING THROUGHOUT CABIN; PERFORMED INFO NOTICE 2017-T015J. FOUND APU BAY CONTAMINATED WITH OIL. PERFORMED DECONTAMINATION OF PACK 1 & PACK 2. NO ODOR NOTED. APU PLACED ON MEL. LOG PAGE 3670645, ITEM 1.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,172 hrs · 25,165 cycles

FLT#636, SJU-MCO. 'MX-270 AIRBUS CABIN ODOR REPORTING FORM COMPLETED; VERIFIED TO BE TYPE 1 A AMBIENT AIR. "COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A ISOLATED FAULT TO TYPE I C PER TSM 05-50-00-810-085-B / TSM 05-50-810-085-D AIRCRAFT IS OK FOR SERVICE."

Part: BATTERY — FAILED (11WL-BATT) · airframe 69,932 hrs · 25,068 cycles

FLT#2752, SJU-TPA. 'EMER LIGHT EMER L BATTERY FAIL TEST; REMOVED AND REPLACED PER AMM 33-51-00.'

Part: NONE — NONE · airframe 67,084 hrs · 23,938 cycles

FLT#879, LAS-LAX. ' DIRTY SOCK SMELL AT 1000FT; COMPLIED WITH INFO NOTICE 2017-T015 I, SECTION A, ISOLATED FAULT TO TYPE 10 PER TSM 05-50-00-810-085. VERIFIED TEMPORARY/TRANSIENT ODOR. A/C OK FOR SERVICE.'

Part: APU — ODOR · airframe 66,739 hrs · 23,805 cycles

FLT#1079, LAS-LAX. ' DIRTY SOCK SMELL ( APU BLEED AIR SUPPLY SYSTEM ) DIRTY SOCK SMELL REPORTED BY INFLIGHT IN REAR OF CABIN DURING INITIAL DESCENT AND FINAL APPROACH.' (SUPPLEMENTAL TO FOLLOW).

Part: SLIDE RAFT — FAILED (7500MM) · airframe 66,243 hrs · 23,618 cycles

FLT#1134, SJU-MCO. 'AFTER LH O/W SLIDE CHNG - DURING EMER LT CHECK FAULT MSG ESPU INT LOAD FWD L MSG & ESPU EXT LOAD FWD MSG; REFERRENCE LOG PAGE 3337111 ITEM 2 FOR R1 SLIDE OPS CK OF EPSU BITE CK GOOD REF 33-51-00. 3337111 ITEM 2: REMOVED AND REPLACED R1 ESCAPE SLIDE RAFT PACK REF MM 25-62-44-400-803A. OK FOR SERVICE. SEE LP 3337110 ITEM 1 FOR EMER LT OPS CHECK.'

Part: NONE — NONE · airframe 66,243 hrs · 23,618 cycles

FLT#1134, SJU-MCO. ' DURING T/S OF ESPU MSG'S FOUND BROKEN WIRES TO EMER EXIT LIGHT ON KICK PLATE, FWD LOWER FRAME OF L1 DOOR; REPAIR SPLICE CRIMP OPS CKS NORMAL IAW ESPM 20-43-13.'

Part: STRINGER — CORRODED (FRMS 57-58 S43L) · airframe 64,263 hrs · 22,931 cycles

DURING HEAVY MAINTENANCE, CORROSION STRINGER 43L LOC BTW FR57 TO FR 58 IN AFT CARGO COMPARTMENT; REMOVED CORROSION ON AFFECTED AREA IAW A320 SRM 51-74-00 AND EVALUATED REWORK AREA AND FOUND OUT OF LIMITS IAW SRM A320 53-41-13-283-002 FIGURE 1 SHEET1 THEN PERFORMED REPAIR ON STGR 43L BTW FR 57 TO FR 58 IAW A320 SRM 53-00-13-300-001 THIS REPAIR IS A CATEGORY B INSPECTION THRESHOLD FROM TIME TO ADL/REPAIR EMBODIMENT FC 60000 FH 120000 SUBSEQUENT INSPECTION AT INTERVALS TBD INSPECTION METHOD TBD IAW SRI 53-00-13-205-001. CLASSIFIED AS MAJOR REPAIR.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,966 hrs · 2,285 cycles

FLT 466, RSW-BOS. CREW REPORTED A DIRTY SOCK SMELL IN THE COCKPIT AND CABIN DURING CLIMB OUT, STRONGER IN THE CABIN, WITH THE AFT CABIN DESCRIBING AS BURNING EYES. THE AIRCRAFT WILL BE REMOVED FROM SERVICE FOR AN ECS SYSTEM DECONTAMINATION AND TROUBLESHOOTING OF THE SOURCE OF THE ODOR; SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 62,529 hrs · 22,343 cycles

FLT NR 320 SLC-FLL: AFT EMERGENCY LIGHT BATTERY AULT ON SELF TEST. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY, IAW AMM 33-51-00. ALL FUNCTION NORMAL, NO FAULT LIGHT.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 62,529 hrs · 22,343 cycles

FLT NR 320 SLC-FLL. LT EMERGENCY LIGHT BATTERY FAULT. REMOVED AND REPLACED LT EMERGENCY LIGHT BATTERY, IAW AMM 33-51-00. OPERATIONS CHECK GOOD, NO FAULTS NOTED.

Part: LIGHT — MALFUNCTIONED (EMERGENCY CABIN) · airframe 62,528 hrs · 22,342 cycles

FLT 320, SLC-FLL. AFTER PUSHBACK EMERGENCY OVERHEAD LIGHTS (EXIT) DID NOT ILLUMINATE. AFTER CYCLING SWITCH WAS ABLE TO GET THEM TO OPERATE. AFTER GEAR RETRACTION LIGHTS STAYED ON (SHOULD BE OFF). DURING DESCENT PAX AND CREW SMELLED STRONG ELECTRICAL ODOR FROM CABIN. SELECTED SYS OFF. PERFORMED OPERATION TEST OF THE EMERGENCY LIGHTED EXIT SIGNS, IAW AMM 33-51-00. OPERATIONS CHECK NORMAL. PERFORMED OPERATIONAL CHECK OF THE OVERHEAD EXIT SIGNS ILLUMINATION WITH THE NO SMOKING SWITCH. EXIT SIGNS AND NO SMOKING SWITCH. OPERATIONS CHECK NORMAL. INSPECTED THE CONDITION OF ALL SSBX'S (ROWS 1-27, LT AND RT), PER AMM LTV-521 TASK 44-20-17-210-801. NO DEFECTS FOUND. INSPECTED THE CONDITION OF ALL SEAT-TO-SEAT CABLES (ROWS 1-27, LT AND RT), PER AMM LTV-521 TASK 44-20-21-210-801. NO DEFECTS FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,521 hrs · 22,338 cycles

FLT 1569, CUN-LAX. FLIGHT DECK AND BOTH IN FLIGHT CREWMEMBERS REPORTED STRONG SMELL. FRONT OF CABIN FRIST 5 ROWS ELECTRICAL IN NATURE, COMPLIED WITH TSM 24-00-00-810-823-A. NO FAULTS NOR BURNING SMELL FOUND AT THIS TIME. RAN AIRCRAFT APU WITH PACKS FOR OVER AN HOUR. CHECKED FWD AVIONICS. NO FAULTS FOUND. A/C OK TO CONTINUE SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 62,273 hrs · 22,250 cycles

FLT 606, FLL-EWR. DOOR LEFT EMERGENCY EXIT AFT OVERWING EXIT INTERMITTENT (ECAM DOOR PG OVERWING EXITS OPEN IND--SLIDE IND ON ECAM OK). ADJUST PROXIMITY SWITCH OF OVERWING AFT LEFT EMERGENCY EXIT DOOR AND PERFORMED OPERATIONAL TEST, IAW AMM 52-71-00, TEST OK AT THIS TIME. MDDR CLEARED, MX-4 UPDATED, PLACARD REMOVED MCC NOTIFIED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,860 hrs · 20,646 cycles

FT # 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED BATTERIES AT 10WL AND 12WL; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT 10WL AND 12WL PER AMM 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,860 hrs · 20,646 cycles

FT # 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED BATTERIES AT 10WL AND 12WL; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT 10WL AND 12WL PER AMM 33-51-38.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 57,156 hrs · 20,413 cycles

FLT 892, TPA-BOS. EMERGENCY EXIT SIGN AT L2 DOOR DOES NOT ILLUMINATE; R & R EPSU AND BATTERY BACK UP IAW AMM 33-51-38, NO HELP. DISCOVERED MISWIRED LAMPS IN L2 DOOR OVERHEAD AND CORRECTED WIRING, OPS CHECK GOOD.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 57,156 hrs · 20,413 cycles

FLT 892, TPA-BOS. EMERGENCY EXIT SIGN AT L2 DOOR DOES NOT ILLUMINATE; R & R EPSU AND BATTERY BACK UP IAW AMM 33-51-38, NO HELP. DISCOVERED MISWIRED LAMPS IN L2 DOOR OVERHEAD AND CORRECTED WIRING, OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (FRAME 66) · corrosion level 2 · airframe 57,129 hrs · 20,404 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL AT LEVEL STR 23R AND FR 66 AT AFT GALLEY AREA; REPLACED LOWER SILL AT LEVEL STR 23R BTW FR 66 AND FR 68 AT GALLEY AREA PER RM 51-72-11. WORK ACCOMPLISHED ON NR 2019-74709

Part: WEB — CORRODED (FRAME 69) · corrosion level 2 · airframe 57,129 hrs · 20,404 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON WEB LOC. BTW FR 69 TO FR 70 AT LEVEL STR 23L AT GALLEY AREA; REPLACED WEB BTW FR 69 TO FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA PER A320 SRM 51-72-11. WORK ACCOMPLISHED ON AEROMAN NR 2019-74688

Part: WEB — CORRODED (FRAME 66) · corrosion level 2 · airframe 57,129 hrs · 20,404 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON WEB LOC. BTW FR 69 TO FR 70 AT LEVEL STR 23R AT GALLEY AREA; REPLACED WEB LOC BTW FR 69 TO FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA. WORK ACCOMPLISHED ON AEROMAN NR 2019-74687.

Part: EPSU — FAILED (CABIN) · airframe 55,712 hrs · 19,848 cycles

FLT 405, BOS-LGB. DURING EMERG LIGHT TEST LT OVWNG EPSU FAILS. REMOVED AND REPLACED FIN 11WL EPSU AS PER AMM 33-51-38. OPS CKS NORMAL.

Part: UNKNOWN — ODOR · airframe 55,714 hrs · 19,851 cycles

FLT 148, LGB-OAK. CLIMBING THROUGH 17,000 FT, SMELLED ELECTRICAL SMELL. INSPECTED AIRCRAFT AND FLIGHT DECK USING TSM 05-50-00-810-831-A. ODOR DEFINED TO TYPE 9 ITEM 2. FOUND NO DEFECTS. ALSO INSEPECTED AIRCRAFT USING TSM 24-00-00-810-823-A. FOUND NO DEFECTS. AIRCRAFT OKAY FOR CONTINUED SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, MAIN CABIN FWD WET AREA FLOOR SUPPORT FRAMES 12 TO 24, Y1292 CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-69) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, MAIN CABIN AFT WET AREA SEAT TRACK Y1292 CORRODED AT FRAMES 64 TO 69. R & R THE SEAT TRACK IAW SRM 51-42-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415 AFT WET AREA FLOOR SUPPORT Y765 CORRODED FR 64 TP FR 70. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415 AFT WET AREA FLOOR SUPPORT Y765, FR 68 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, MAIN PASSENGER CABIN, -Y1292 FLOORBEAM AT FRAME 66 HAS CORROSION. R & R THE FLOORBEAM IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, MAIN CABIN AFT WET AREA L-2 DOOR SILL Y1732 CORRODED AT FRAME 66 TO FRAME 68. R & R L2 DOOR SILL IAW SRM 51-72-11 AND SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, MAIN CABIN AFT WET AREA FLOORBEAM -Y1292 CORRODED AT FRAME 68. R & R Y1292 FLOORBEAM IAW SRM 51-72-11.

Part: STRINGER — CORRODED (FRAME 59-60) · corrosion level 2 · airframe 44,538 hrs · 15,713 cycles

FLT 6415, STRINGER 32L BETWEEN FR 59 AND FR 60 CORROSION. REPAIRED THE STRINGER IAW SRM 53-00-13.

Part: LIGHT — INOPERATIVE (ROW 13) · airframe 42,639 hrs · 14,989 cycles

ROW 13 EMERGENCY LIGHT INOPERATIVE AND COVER OFF. R & R LIGHT ASSEMBLY AT ROW 13 IAW 33-51-19, OPS CHECK GOOD.

Part: SOCKET — FAULTY (EMERGENCY LIGHT) · airframe 41,686 hrs · 14,642 cycles

DURING MAINTENANCE, FOUND ROW 15 EMERGENCY LIGHT INOPERATIVE. R & R ROW 15 EMERGENCY LIGHT SOCKET. OPS CHECK GOOD IAW AMM 33-51-18.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 39,045 hrs · 13,717 cycles

DURING SPECIAL DETAILED INSPECTION OF NR 1 ENGINE FWD MOUNT FITTING ATTACHMENT BOLT HOLES AT OTBD LWR ARM COMMON TO LWR SPAR & LWR BOOM, A CRACK INDICATION WAS NOTED. ACCOMPLISHED THE REPAIR OF EDGE DAMAGE AND REPLACED LOWER BOOM, PN D54610024200 TO NR 1 LT PYLON TO ENGINE. ALL WORK ACCOMPLISHED IAW EC A14-286-01.

Part: VALVE — FAILED (AC SYSTEM) · airframe 32,409 hrs · 11,384 cycles

FLT 134 RSW-JFK, AIRCRAFT DIVERTED TO TPA DUE TO AVIONICS VENT FAULT. ECAM ACTION WAS COMPLETED. THEN A SECOND FAULT (EXHAUST) OCCURRED, IT WAS RESET, THEN WE HEARD A LOUD BANG. CABIN KEPT CLIMBING 6-800 FPM, CABIN WENT TO 10,200. AIRCRAFT DESCENDED AND LANDED TO TPA. FOUND AIR EXTRACT DUCT COLLAPSED. REMOVED AND REPLACED AIR EXTRACT DUCT, CHECK VALVE AND SKIN AIR INLET VALVE. SYSTEM OPS CHECK NORMAL IAW 21-26-52 AND 21-26-56.

Part: COMPUTER — FAILED (NR 1) · airframe 31,297 hrs · 10,995 cycles

FLT 221 DCA-MCO, AT 190KTS FLAPS 1 WITH HALF SPEED BRAKES ON AUTOPILOT FLAPS 2 SELECTED A/C ROLLED 15 DEGREES BANK LEFT FOR 3 SECONDS THEN CORRECTED WHEN SPEED BRAKES RETRACTED. A/C AGAIN ROLLED LEFT 1 MINUTE LATER WITH NO CHANGES TO CONFIG AUTO PILOT DISCONNECTED NO FURTHER ROLLS. PERFORMED TSM TASK 27-93-00-810-950 REMOVED AND REPLACED ELAC1 (2CE1) PER AMM 27-93-34 BITE/OPS CHECK OK.

Part: TRANSDUCER — FAILED (NR 2 ENGINE) · airframe 30,143 hrs · 10,577 cycles

FLT 1221 BOS-RDU, ON TAKEOFF ENGINE INDICATIONS WERE ALL IN LINE. SHORTLY AFTER ROTATION ENG 2 OIL PRESS DROPPED QUICKLY TO 3.2 AND FLASHED ADV. CREW DECLARED AN EMERGENCY AND RETURNED TO BOS. THE OIL PRESS EVENTUALLY ROSE TO 8.0 AND NO OTHER NUMBERS WERE OUT OF LINE. LANDED AND SHUTDOWN THE ENGINE NORMALLY. LANDED OVERWEIGHT 144,000LBS. OVERWEIGHT CHKLST COMPLETED. T/S PER TSM 79-33-00-810-823-A. REMOVED & REPLACED NR 2 ENG OIL PRESSURE TRANSDUCER AS PRECAUTIONARY PER AMM 79-33-15. ENG OIL PRESSURE OPS CHECK NORMAL AT THIS TIME. ACFT OK FOR SERVICE.

Part: HEATER — FAILED (LAVATORY) · airframe 23,889 hrs · 8,337 cycles

FLT 198 LAS-JFK, ELECTRICAL FUMES SMELLED BRIEFLY WHEN HOT WATER SELECTED IN FWD LAV HOT WATER HEATER TURNED OFF SMOKE AND FUME ALARM WENT OFF FOR 2 SEC AT LEVEL OFF. REMOVED AND REPLACED FWD LAV HEATER AS PER AMM 38-12-16. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (AC PACK) · airframe 20,149 hrs · 7,000 cycles

FLT 743 - MCO-SJU, RETURN TO MCO, EXTREME CABIN V/S FLUCTUATION IN CLIMB PLUS 2000 FT TO MINUS 1500 FT. NO ECAM SWITCHED TO MAN SYS 1, SYS 2 WITH NO EFFECT. CABIN PRESSURE WENT TO 9800 FT AT 370. INITIATED DESCENT AND FLUCTUATIONS IMMEDIATELY STOPPED. SYSTEM NORMAL FOR REST OF FLIGHT. PERFORMED TSM 21-61-00. REMOVED AND REPLACED PACK 1 CONTROLLER REF AMM 21-61-34 AND PACK 2 CONTROLLER PRECAUTIONARY. PERFORMED BLEED AIR SYS TEST REF 36-11-00 AND CPC TEST REF 21-30-00. ALL CHECKS OK. OK FOR SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 19,825 hrs · 6,890 cycles

FLT 1249 - BOS-IAD - CAB PR 1 FAULT FOLLOWED BY 2 ENGINES SURGING AT CRUISE FL300, DIVERTED TO JFK. REPLACED CAB PRESS CONTROLLER NR 1 IAW AMM 21-31-34-04, OPS TEST OK. DUE TO CABIN PRESS FLUX WITH SYSTEM 1 FAIL AND SYS 2 IN CONTROL, PRECAUTIONARY REMOVED AND REPLACED CPC2 IAW AMM 21-31-34-04, OPS TEST OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,775 hrs · 6,868 cycles

FLT 1783, JFK-MCO, F/A REPORTS HOT ELECTRICAL SMELL AROUND ROW 12. COMPLIED WITH TSM TASK 24-00-00-810-823. NO DEFECTS OR SMELL NOTED. LIVE TV COMPLIED WITH TSM TASK 23-39-00-810-801. NO DEFECTS NOTED.