N374NW

Part: GENERATOR — FAILED (WASTE VACUUM) · airframe 68,756 hrs · 32,859 cycles

AFTER PUSHBACK AND ENGINE START FA'S IN AFT GALLEY REPORTED A STRONG BURNING ELECTRICAL ODOR FROM THE AFT CENTER LAV AREA. FLIGHT RETURNED TO THE GATE AND DEPLANED. LAVATORY WASTE SYSTEMS VACUUM GENERATOR. C/W MSI PREVENTION PROGRAM STEPS A - G FOUND VACUUM GEN CB POPPED IN REAR CB PANEL FWD VACUUM GEN TO MEL 38-30-01D "M" PROCEDURES C/W MEL & PLACARD INSTALLED. (LP: 8081427)

Part: OXYGEN BOX — FAULTED (ZONE 900) · airframe 68,713 hrs · 32,832 cycles

AFT LT LAV O2 MOD DOOR WILL NOT CLOSE LAVATORY OXYGEN MODULE. AFT LAV (LT) O2 MASK DROPPED ON LANDING IN DTW. C/A: FWD TO MCC , MEL 35-21-02 , "M" PROCEDURE CW , DISPATCH APPROVED , PLACARD INSTALLED. REMOVED AND REPLACED 203 LAV O2 CONTAINER ASSY PER AMM 35- 21. CHECKS GOOD. MEL AND PLACARD REMOVED. M PROCEDURES REMOVED. (LP: 7792992)

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 68,284 hrs · 32,589 cycles

SHIP 3274 - ATB - DUE TO CABIN PRESSURE ISSUES AND LOW CABIN DIFFERENTIAL PRESSURE MESSAGE. CREW WAS ABLE TO REGAIN PRESSURE USING MANUAL CONTROL. CORRECTIVE ACTION: REPLACED OUTFLOW VALVE AND CPC 2. (LP: 7368374)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 67,931 hrs · 32,407 cycles

ONE ROW 17 MASKS DROPPED ABC. REPACKED AND RESTOWED OXY MASKS IAW AMM 35-21. A/C OK FOR SVC.

Part: FITTING — DAMAGED (ZONE 200) · airframe 67,920 hrs · 32,400 cycles

PERFORM ER/A 628229-14AD FOR REPLACEMENT OF CONTINUITY FITTINGS ON WINDSHIELD AREA. COMPLIED WITH ER/A 628229-14AD REV. ORIGINAL; MATCHES WITH ALL STEPS ON PRI ER/A 628229-14AD REV. 0 AND PRI ER/A 628229-14AD REV.1. IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FUSELAGE FRAMES AND FORMERS WINSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTINGS IAW ER/A 628229-14AD REV. ORIGINAL SECTION I HAS BEEN COMPLIED WITH.

Part: WINDOW FRAME — DAMAGED (ZONE 200) · airframe 67,920 hrs · 32,400 cycles

PERFORMED ER/A 571984-14AD REV C ON WINDSHIELD CENTER POST AREA. COMPLIED WITH ER/A 571984-14AD REV. C MATCHES WITH ALL STEPS ON ER/A 571984-14AD REV.C PRI REV.0, REV.1 REV.2 REV.3 REV.4, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT AS PER ER/A 571984-14AD REV. C SECTIONIII HAS BEEN COMPLIED WITH. APPROVED DATE:02-SEP-25.

Part: WINDOW FRAME — NONE (ZONE 200) · airframe 67,920 hrs · 32,400 cycles

INSPECTION ERA 571984-14AD REV C. REPAIR AT AREA 2, WINDSHIELD FRAMING. ACCOMPLISHED FOLLOW ON INSPECTIONS OF AREA 2 WINDSHIELD FRAMING PER ERA 571984-14AD SECTION IV PRIOR TO 59,392 TOTAL FLIGHT CYCLES AND EVERY 4,700 FLIGHT CYCLES THEREAFTER. ASSOCIATED AA 5311-01226.

Part: NONE — NONE (NONE) · airframe 67,920 hrs · 32,400 cycles

DTE ERA 571984-14AD REV C. REPAIR OF AREA 3 (MIRROR FITTINGS) IS TIME LIMITED REQUIRING DTE FOLLOW UP PRIOR TO 92,392 TOTAL FLIGHT CYCLES. REVISE AND UPDATE ERA 571984-14AD WITH DTE RESULTS PRIOR TO 92,392 TOTAL FLIGHT CYCLES.

Part: NONE — NONE (NONE) · airframe 67,920 hrs · 32,400 cycles

DTE ERA 571984-14AD REV C. REPAIR OF HOLE D IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 61,092 TOTAL FLIGHT CYCLES. C/A: REVISE AND UPDATE ERA 571984-14AD WITH DTE RESULTS PRIOR TO 61,092 TOTAL FLIGHT CYCLES.

Part: FITTING — NOT REPORTED · airframe 67,906 hrs · 32,392 cycles

DTE ERA 628229-14AD REVISION ORIGINAL. REPLACEMENT OF CONTIUITY FITTINGS REQUIRES DTE FOLLOW UP PRIOR TO 61,892 TOTAL FLIGHT CYCLES. REVISE AND UPDATE ERA 628229-14AD WITH DTE RESULTS PRIOR TO 61,892 TOTAL FLIGHT CYCLES. (LP: 1176486)

Part: DAMPENER — INOPERATIVE (ZONE 800) · airframe 67,906 hrs · 32,392 cycles

EMERGENCY DOOR DAMPER 842 DOESN`T WORK CORRECTLY, REF. AMDS CARD 5210-7089-RA. RII). REPLACED EMERGENCY DOOR DAMPER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,561 hrs · 32,221 cycles

SHIP 3274 DISC: ON TAKEOFF, STRUCK RAISED ARRESTING CABLE @ APPROX. 80 KTS. C/A: PERFORMED WALKAROUND OF AIRCRAFT WITH NO DEFECTS NOTED. PERFORMED INSPECTION OF ALL WHEEL + TIRE ASSYS PER A320 AMM 32- 41-11. NO DEFECTS NOTED. (LP: 5712658)

Part: OUTFLOW VALVE — INOPERATIVE (ZONE 100) · airframe 67,297 hrs · 32,085 cycles

SHIP 3274 - ATB - DUE TO AIRCRAFT UNABLE TO PRESSURIZE (CAB PR EXCESS CAB ALT AND VENT SKIN VALVE FAULT ECAM WARNINGS). SKIN AIR OUTLET VALVE PLACED ON MEL. OK FOR SERVICE. LATER REPLACED SKIN AIR OUTLET VALVE (22HQ). (LP: 7184225)

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 66,876 hrs · 31,864 cycles

SHIP 3274 DISC: FA REPORTS EXIT DOOR LIGHT 2R FLICKERING. C/A: PERFORMED OPS TEST OF EMER LIGHTING IN THE CABIN W/ THE EMER EXIT LT SWITCH IAW A320 AMM 33-51, ALL OPS NORM A/C OK FOR SVC. (LP: 6374363)

Part: SERVO VALVE — FAULTY (AUTOBRAKE SYS) · airframe 66,743 hrs · 31,799 cycles

SHIP 3247 - MISC - DECLARED EMERGENCY DUE TO AN AUTO BRAKE FAULT ECAM MESSAGE WITH ASSOCIATED FAILURE MESSAGE OF NORMAL BRAKE SERVO VALVE 18GG. CORRECTIVE ACTION: REPLACED SERVO VALVE 18GG AND BSCU. (LP: 6374305)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 65,673 hrs · 31,265 cycles

SHIP 3274 DISC: EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:22D COVER TO EMERGENCY LIGHTING BROKEN, HANGING ONTO FLOOR, WIRES EXPOSED. C/A: REPLACED EMERGENCY LIGHT HOUSING BELOW SEAT 22D, CKS GOOD. (LP: 0619167)

Part: MODULE — BROKEN (OXYGEN) · airframe 65,463 hrs · 31,152 cycles

SHIP 3274 DISC: LAVATORY OXYGEN MODULE FIRST CLASS LAV O2 MODULE BROKEN. C/A: FWD TO MEL 35-21-02, "M" PROCEDURES C/W, MAY NEED PN 22G150150460400 STK N 33-3500-3-0059. PLACARDS INSTALLED. R&R F/C LAV OXY BOX ASSY IN REF TO A320 AMM 35-21, OPS CK GOOD. THIS CLEARS MEL, PLACARDS REMOVED. (LP: 6433256)

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 65,406 hrs · 31,125 cycles

SHIP 3274 DISC: OUTBOARD FLAP LEFT WING ABOUT 6' FROM OUTBOARD EDGE, ABOUT 5" LONG DENT ON THE UNDERSIDE OF FLAP. C/A: PER A320 SRM 57-53 DENT MEASURES 3.90 LENGTH X 2.00' (WIDTH) X .120" DEPTH. AREA "C" NOTED TEMP REPAIR NOT REQUIRED PERMANENT REPAIR W/IN 1000 FLT CYCLES.(FROM FLT 2463 MSP) INSP FOR CRACKS REQ. HFEC'D CRACK PER NDT A320 MANUAL 51-10-078 NO DEFECTS NOTED QC5220 DECAL APPLIED PER PS 900-5-1 NO 4. (LP: 6433250)

Part: LIGHT — DAMAGED (SEAT) · airframe 64,610 hrs · 30,699 cycles

SHIP 3274 DISC: EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP. C/A: PERFORMED OPS CHECK FOR FA READING LIGHTS IAW A320 AMM 33-27.401 JUMP SEAT READING LIGHT WORKS NML.OK FOR SVC. (LP: 0391993)

Part: UNKNOWN — ODOR (CABIN) · airframe 64,298 hrs · 30,540 cycles

SHIP 3274 DISC: UNUSUAL ODOR SMELLED. COULD BE DIRTY SOCK SMELL UNSURE. C/A: REF LOGS 0331022 AND 0331510 FOR C/A. (LP: 5352066)

Part: INLET — CONTAMINATED (APU) · airframe 64,253 hrs · 30,515 cycles

SHIP 3274 DISC: AT PUSH BACK APU BLEED WAS SELECTED ON. STRONG "DIRTY SOCK" SMELL IN COCKPIT APU BLEED WAS SELECTED OFF. WHEN MX BOARDED AIRCRAFT MECHANIC SAID SMELL WAS PRESENT IN FWD GALLEY AND BY EXIT ROW. APU WAS SELECTED OFF AND SMELL DISIPATED. C/A: FOUND APU INLET OIL SOAKED. REQUIRES APU CHANGE WIP 854736 JB. REF LOG 5352059 FOR APU DEFERAL. REMOVED AND REPLACED OZONE FILTERS PER A320 AMM 21-51. C/W AMDS W/C 0550-2002 AND 4900- 2001 AND 2100-2005. C/W NO GO ODI STEPS ATA 21-72. JOB COMPLETE OK FOR SVC. (LP: 5352058)

Part: PLENUM — CONTAMINATED (APU) · airframe 64,115 hrs · 30,446 cycles

WHEN SWITCHING TO APU BLEED AFTER ENGINE SHUTDOWN WE SMELLED STRONG FUEL SMELL. PERFORMED GVI OF APU COMP/T, FOUND FUEL INGESTED IN PLENUM AND WICKING OUT OF ACCESS DOORS. FOUND NO BAD FUEL LINES/LEAKS ON APU ASSY. SUSPECT BAD BAD DRAIN ASSY BELLOWS ON APU PLENUM DOOR ASSY. DEBRIEFED CREW FUEL ODOR IN COCKPIT ONLY/APU BLEED ON. CROSSBLEED OFF. PACK BOTH ON AND BOTH ENG OFF. PERFORMED PACK ECS BURNOUT PER TC 2100-2005. AFT BULKHEAD PANELS OF FWD CARGO PIT REQ INSTALLATION WIP BF545168. INSTALLED FWD CARGO AFT BULKHEAD PANELS WIP 724033. WORK CARDS 0550-2002, 4900-2001, & 2100-2005 ALL COMPLETED. (LP: 5846265)

Part: SNUBBER — BROKEN (OVERHEAD BIN) · airframe 64,007 hrs · 30,392 cycles

SHIP 3274 DISC: 32F OVERHEAD BIN HAS 2EA BROKEN SNUBBERS. EMERGENCY EQUIP COMPARTMENT. C/A: R/R OVERHEAD BIN ASSY AT 32F IAW A320 AMM 25-24. OVERHEAD BIN ROBBED FROM AC 3232. MEL AND PLACARD REMOVED. M PROC REVERSED. OK FOR SVC. (LP: 5846219)

Part: APU — ODOR · airframe 64,033 hrs · 30,405 cycles

SHIP 3274 DISC: F/A REPORTED DIRTY SOCK SMELL FROM EXIT ROWS TO AFT GALLEY. C/A: FLT CREW DEBREIFED. SMOKE AND FUMES QUESTIONNAIRE FILLED OUT. WHILE WORKING WORKCARD 0550-2002 NOTED. OIL CONTAMINATION IN APU INLET. NO EVIDANCE OF OIL COMING FROM EXTERNAL SOURCE. WILL REQUIRE APU PLACED ON MEL AND COMPLETION OF WORKCARD 2100-2005 FOR REVERSE FLOW ECS DECONTAMINATION WORK CARD 0550-2002 UP TO STEP 5. C/W NO GO ODI PREVENTION UP TO STEP D. PERFORMED DUCT AND PACK BURNOUT AND REPLACED RECIRC FILTERS PER AMDS WORK CARD 2100-2005. NO SMELL PRESENT. A/C OK FOR SERVICE.

Part: LIFE RAFT — LOW PRESSURE (AFT CABIN) · airframe 63,656 hrs · 30,211 cycles

SHIP 3274 DISC: AFT LIFE RAFT LOW PRESSURE. C/A: REMOVED AND REPLACED LIFE RAFT IN AFT AS PER A320 AMM 25-66. REMOVED MEL AND PLACARD. OK FOR SVC. (LP: 4550460)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,666 hrs · 29,671 cycles

SHIP 3274 PAX O2 MASK DROPPED IN FLT ON THERE OWN ON ROW 16ABC SIDE. CORRECTIVE ACTION: REPLACED O2 MASK PANEL AND RE-PACKED MASKS. OK FOR SERVICE. (9651072)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 WEAR ON TAB LUG OF HINGE FITTING 4 OF LH ELEVATOR HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED TAB LUG ON HINGE FITTING #4 LH ELEVATOR PER A320 SRM 55-26-41-300-002. (2969609)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 EXISTING REPAIR ON FASTENERS HOLES 3,4,5,6,7 AND 8. DOCUMENTED ERA 571938-14AD REV. ORIGINAL. LOCATION ON FRAME 16 RH AT DOOR STOP 7 LEVEL. CORRECTIVE ACTION: COMPLIED WITH ERA 571938-14AD REV A. (2967981)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION ON LOWER SURFACE OF UPPER SKIN TRAILING EDGE AT LEVEL RIB 7 LH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 611211-14 REV ORIGINAL. (2967968)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK INDICATION ON FRAME 16 RH SIDE IN CROSSBEAM SPLICING AREA OPEN FASTENER HOLE H2. CORRECTIVE ACTION: COMPLIED WITH ERA 610969-14AD REV. ORIGINAL. (2967963)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 INOP EPSU 13WL AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED EPSU 13WL AT AFT GALLEY AREA PER A320 AMM 33-51. (2967222)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK INDICATION ON FRAME 16 RH SIDE IN CROSSBEAM SPLICING AREA OPEN FASTENER HOLE H3. CORRECTIVE ACTION: COMPLIED WITH ERA 610969-14AD REV. 0 AND PRI 610969-14AD REV. 1. (2968062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACKS FOUND IN HOLE #2 AND HOLE #3 OF CROSSBEAM SPLICE AT FR16 RHS. CORRECTIVE ACTION: COMPLIED WITH ERA 610969-32. (2965836)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK INDICATION ON FRAME 20 RH SIDE UPPER JOGGLE AREA IN OPEN FASTENER HOLE C. CORRECTIVE ACTION: COMPLIED WITH ERA 611000-14AD REV ORIGINAL. (2966587)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 REPAIR AT FR20 RH, DOOR STOP #7 AT DOUBLE JOGGLE LEVEL REQUIRES FOLLOW UP INSPECTIONS PRIOR TO 38,442 TOTAL FLIGHT CYCLES AND EVERY 4,500 FLIGHT CYCLES THEREAFTER PER ERA 611000-14 SECTION II. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. NO TROUBLE FOUND. CONTINUE ON MON. (2964681)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 FUSELAGE / FRAMES / FR16RH AT DOOR STOP # 1 & # 7 LEVEL, DOUBLE JOGGLE AREA / FASTENER HOLES / REPAIR-MODIFICATION. CORRECTIVE ACTION: COMPLIED WITH ERA 571938-14, REV A. (2964874)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 GOUGE ON WEB LOC. UPPER PYLON BTW RIB08 TO RIB09 IB SIDE ON RH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 611339-14 REV. ORIGINAL. (2963121)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 WEAR ON FRAME 70 AND Y300 APPROX UPPER AREA AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 611380-14 REV. ORIGINAL. (2963117)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 EXCESSIVE PLAY ON BEARING ATTACH FITTING INTERCONNECTING STRUT I/B FLAP RH WING. CORRECTIVE ACTION: REPLACED FITTING PER A320 SRM 51-42-11 AND SRM 51-72-11. (2956338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION ON LOWER SURFACE OF UPPER SKIN TRAILING EDGE AREA AT LEVEL RIB 8 LH WING. CORRECTIVE ACTION: FOUND CORROSION WITHIN LIMITS. (2953223)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION INTERCONNECTING STRUT IB FLAP TARGET ON RH WING. CORRECTIVE ACTION: R/R STRUT PER WORK CARD 2750-1020-RT. (2950343)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION INTERCONNECTING STRUT IB FLAP TARGET ON LH WING. CORRECTIVE ACTION: R/R STRUT PER WORK CARD 2750-1020-LT. (2950350)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 3 AT DOOR-STOP FITTING 7 POSITION. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING PER A320 SRM 51-42-11 AND 51-72-11. (2946592)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON O/B FITING ACTUATOR LUG I/B ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON O/B FITTING ACTUATOR I/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2945100)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 5 I/B LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #5 OF I/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2944982)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON O/B FITING ACTUATOR LUG I/B ON RH WING. CORRECIVE ACTION: REPLACED BUSHING ON AILERON O/B FITING ACTUATOR LUG I/B ON RH WING PER A320 CMM 57-61-21. (2943053)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 5 I/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #5 OF I/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940020)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 5 O/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING PER A320 CMM 57-61-21. (2940047)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 3 O/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #3 OF O/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940028)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 3 I/B LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #3 OF I/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2940044)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 4 I/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #4 OF I/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940027)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 3 O/B LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #3 OF O/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2940040)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 4 I/B LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #4 OF I/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2940037)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION SHEAR TIE AT LEVEL FRAME 28 AND BETWEEN STRINGER 41RH TO STRINGER 42RH IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11. (2939666)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 2 O/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #2 OF O/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940034)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON BUSHING HINGE 2 O/B LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #2 OF O/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2940042)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 4 O/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #4 O/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940025)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 2 I/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #2 OF I/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940036)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON I/B FITING ACTUATOR LUG I/B ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON AILERON I/B FITTING ACTUATOR LUG I/B ON RH WING PER A320 CMM 57-61-21. (2939681)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 3 I/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING ON HINGE FITTING #3 OF I/B LUG ON AILERON RH WING PER A320 CMM 57-61-21. (2940030)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK ON FWD LOAD TRANSMITTING PROFILE OF FWD EMERGENCY EXIT DOOR LH PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11. (2934888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON I/B FITING ACTUATOR LUG I/B ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING (1 E/A) ON I/B FITING ACTUATOR OF I/B LUG ON AILERON LH WING PER A320 CMM 57-61-21. (2934916)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION AILERON HINGE 1 I/B LUG ON RH WING. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON HINGE FITTING #1 OF I/B LUG ON AILERON RH WING AS PER AIRBUS CMM 57-61-21. (2934909)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR 63 TO FR 64 AND STR 21L TO STR 22L UPPER FUSELAGE. CORRECTIVE ACTION: REINSPECTED REPAIR. OK FOR SERVICE. (2934924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION ON BORE OF SPIGOT RECEPTACLE FITTING ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING ON LH PYLON PER A320 SRM 54-51-12. (2934668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CRACK ON AFT LOAD TRANSMITTING PROFILE OF AFT EMERGENCY EXIT DOOR RH PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11. (2934884)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 INHIBIT INSPECTION BY EXISTING REPAIR (1EA) EXTERNAL FUSELAGE SKIN BTW FR47 TO FR70 FROM STR23 LH/RH TO BOTTOM CENTERLINE. CORRECTIVE ACTION: COMPLIED WITH ERA 611050-14AD, REV. ORIGINAL. (2934454)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION SEAT TRACK -Y765 AT LEVEL OF FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PER A320 SRM 51-42-00 AND 51-72-11. (2933002)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION SEAT TRACK -Y765 AT LEVEL OF FR 20 AT FWD GALLEY AREA. REPLACED SEAT TRACK PER A320 SRM 53-11-15. (2933020)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION ON SPIGOT RECEPTACLE FITTING ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING ON RH PYLON PER A320 SRM 54-51-12. (2931018)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 PULLING UP ON FUSELAGE LOC. FR 52 TO FR 70 BTW STR 19 L/H TO STR 19 R/H. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-11. (2929766)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION FIXED BUSHING ELEVATOR FITTING INBOARD LUG OF OUTBOARD SERVO CONTROL ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHING PER A320 CMM 55-21-15. (2927688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION ELEVATOR FITTING OUTBOARD LUG OF INBOARD-SERVO CONTROL ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHING PER A320 CMM 55-21-15. (2927692)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION FIXED BUSHING ELEVATOR FITTING OUTBOARD LUG OF OUTBOARD SERVO CONTROL ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHING PER A320 CMM 55-21-15. (2927685)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION FLOOR BEAM +Y1292 FR 16 HARD POINT AREA AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11, AND SRM 51-42-11. (2923261)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION SEAT TRACK -Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-42-00 AND SRM 51-72-11. (2923312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION FLOOR BEAM -Y1162.5 AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11-801 AND, SRM 51-72-11-911. (2921243)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 CORROSION FLOOR BEAM BTW -Y1292 AND -Y1162.5 BTW FR 66 AND FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BETWEEN FR66 TO FR 68 RH SIDE AFT GALLEY AREA AS PER A320 SRM 51-42-11-801, AND SRM 51-72-11-911. (2921193)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 MISSING MATERIAL FLOOR BEAM +Y512 AT LEVEL OF FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y512 LOCATED AT LEVEL OF FR 68 AT AFT GALLEY AREA PER A320 SRM 51-42-11-801 AND A320 SRM 51-72-11. (2919954)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 PASSENGER CREW DOOR 842 NOT WORKING CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2919372)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 EXCESSIVE PLAY PASSENGER CREW DOOR 832 ON BUSHINGS BETWEEN UPPER CONNECTION LINK AND SUPPORT ARM. CORRECTIVE ACTION: REPLACED BUSHINGS. OK FOR SERVICE. (2911092)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 PASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-11-21. OK FOR SERVICE. (2909377)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 PASSENGER CREW DOOR 832 OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED PER A320 AMM 52-13-14. OK FOR SERVICE. (2907518)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,423 hrs · 29,542 cycles

SHIP 3274 PASSENGER CREW DOOR 842 DAMPER DOES NOT WORK CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2906830)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,864 hrs · 29,229 cycles

SHIP 3274 AFT LAV OXYGEN INOP. CORRECTIVE ACTION: DEFERRED, NEW O2 GENERATOR TO BE INSTALLED. (9648334)

Part: TEST BUTTON — BROKEN · airframe 59,269 hrs · 27,801 cycles

SHIP 3274 WHILE PERFORMING W/C: 2527-01041-02 (O2 PSU PANEL DROP), FOUND TEST STOP BUTTON DAMAGED (SPRING BROKEN) IN LAV 203 (LAV D). CORRECTIVE ACTION: REPLACED O2 PSU PANEL TEST STOP BUTTON SPRING IN LAV 203 PER A320 CMM 35-22-40. OK FOR SERVICE. (2256337)

Part: MASK — INOPERATIVE · airframe 59,264 hrs · 27,798 cycles

SHIP 3274 DURING TEST O2 MASKS DID NOT DROP AT L/H SEAT ROWS 23;25. R/H SEAT ROWS 11, 15, 23, 31; 32. DOOR 2R (F/A AFT R/H). CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (2256275)

Part: NONE — NONE · airframe 58,029 hrs · 27,103 cycles

SHIP 3274 SEAT ROW 15D EMERGY LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY PATH LIGHT ASSY PER A320 CMM 25-23-51. OPS CK GOOD. (2051291)

Part: PANEL — NO TEST (PSU) · airframe 55,843 hrs · 25,917 cycles

SHIP 3274 DURING TEST FOUND PSU OXY PANEL 12DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7565564)

Part: PANEL — NO TEST (PSU) · airframe 55,843 hrs · 25,917 cycles

SHIP 3274 DURING TEST FOUND PSU OXY PANEL 2 CD DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7565565)

Part: PANEL — NO TEST (PSU) · airframe 55,843 hrs · 25,917 cycles

SHIP 3274 DURING TEST FOUND PSU OXY PANEL 16ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: OIL SYSTEM — LEAKING (APU) · airframe 55,775 hrs · 25,881 cycles

SHIP 3274 ON BASE LEG SMELLED A "DIRTY SOCK" SMELL. FA REPORTED STRONG " DIRTY SOCK" SMELL IN ENTIRE CABIN. NO SMOKE JUST SMELL. CORRECTIVE ACTION: FOUND INTERNAL OIL LK FROM APU. REPAIRED OIL LEAK PER DELTA WORK CARD 0550-2002 AND 4900. (7565524)

Part: TRANSMITTER — MALFUNCTIONED (DOOR PRESSURE) · airframe 55,277 hrs · 25,653 cycles

IRF STATES DOOR RT FWD CABIN ECAM DIF PRESSURE NORMAL IRO MESSAGE. CORRECTIVE ACTION: CLEANED R1 DOOR SENSOR. R1 DOOR INDICATION OPERATES NORMAL.

Part: LATCH — BROKEN (OXYGEN BOX) · airframe 55,214 hrs · 25,622 cycles

FOUND PSU LATCH BROKEN ON AFT LEFT LAV LAVATORY OXYGEN MODULE. CORRECTIVE ACTION: REMOVED AND REPLACED AFT LEFT LAV PSU OXYGEN MASK/ GENERATOR CONTAINER. OPERATIONS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 55,185 hrs · 25,607 cycles

OXYGEN PANEL MASK DEPLOYED. CORRECTIVE ACTION: R & R F/C LAV EMERGENCY OXYGEN CONTAINER. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT DOOR) · airframe 55,059 hrs · 25,528 cycles

DOOR RT FWD CABIN CAUTION MESSAGE AT FL340. CABIN DIFF PRESSURE OF 7.9 PSI. CABIN ALTITUDE STEADY AT 6650 FT. CORRECTIVE ACTION: PERFORMED DETAILED VISUAL INSPECTION OF RT FWD DOOR LATCHING MECHANISM POWER, PER A320 AMM 24-00.

Part: WATER HEATER — MALFUNCTIONED (LAVATORY) · airframe 54,943 hrs · 25,456 cycles

DIV - DUE TO ELECTRIC SMELL COMING FROM F/C LAV NO VISIBLE SMOKE. ISOLATED TO OVERHEATING OF LAVATORY WATER HEATER THERMOSTAT. CORRECTIVE ACTION: DEFERRED WATER HEATER TO MEL AND LOCKED OUT FWD LAVATORY. (10/8 ATL) REPLACED HOT WATER HEATER AND THERMOSTAT. (10/9 ATL) INSTALLED NEW O-RINGS AT HOT WATER HEATER. NO LEAKS AND NO BURNING SMELL, ALL WORK PERFORMED PER AMM 38-12.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 52,635 hrs · 24,277 cycles

EMERG LIGHT LENS FOR ENTRY LT AT R2 DOOR MISSING, INSTALLED LENSE COVER

Part: COOLING FAN — LEAKING (APU) · airframe 50,756 hrs · 23,373 cycles

CREW REPORTS ON TAXI IN WITH SINGLE ENGINE RUNNING FLIGHT ATTENDANTS SAW HAZE THROUGHOUT THE CABIN WITH AN ODOR. FOUND APU LEAKING OIL FROM COOLING FAN AREA. PERFORMED DECONTAMINATION OF ECS WITH APU INOP. AFTER COOLING FAN AND TRANSFER TUBE REPLACEMENT, APU STILL LEAKING. PERFORMED ECS DECONTAMINATION AGAIN. NO CONTAMINATION NOTED. COMPLY WITH NO GO ODI PREVENTION. APU REPLACED.

Part: EPSU — INOPERATIVE (CABIN) · airframe 50,685 hrs · 23,337 cycles

(LP 0798099) EPSU (12WL) INOPERATIVE IN PASSENGER CABIN. REMOVED AND REPLACED SAME. OPERATIONS CHECKS OKAY.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,681 hrs · 23,335 cycles

(LP 0787452) CRACK INDICATION ON FRAME 16 IN OPEN INBOARD UPPER HOLE AT DOOR STOP FITTING NR 7 RIGHT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING NR 7 IAW SRM 51-72-11 AND DWG D53112300.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,681 hrs · 23,335 cycles

(LP 0787455) CRACK INDICATION ON FRAME 16 IN OPEN INBOARD LOWER HOLE AT DOOR STOP FITTING NR 7 RIGHT HAND SIDE AT FORWARD GALLEY AREA . REPLACED INTERCOSTAL FITTING NR 7 IAW SRM 51-72-11 AND DWG D53112300.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 50,681 hrs · 23,335 cycles

CRACK INDICATION ON FRAME 16 IN OPEN INBOARD UPPER HOLE AT DOOR STOP FITTING NR 7 LEFT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING IAW SRM 5-72-11 AND DWG D53112300.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0783091) CORROSION FLOORBEAM -Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. (SSI 531189) REPLACED IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0781408) CORROSION FLOOR BEAM _Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189) REPLACED IAW SRM 51-72-11 AND DWG D 53110920.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0781394) CORROSION FLOORBEAM Y81 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FORWARD GALLEY AREA (SSI 531189) REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112829.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0781772) CORROSION FLOORBEAM +Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. (SSI 531189) REPLACED IAW SRM DWG D53110984.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779706) CORROSION SEAT TRACK -Y765 FRAME 41 TO 47 IN PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0778953) CORROSION WEB LOCATED BETWEEN FRAME 20 TO FRAME 24 AT LEVEL STRINGER 23L AT FORWARD GALLEY AREA (SSI 534189). REPLACED IAW SRM 51-72-11 AND DWG D53112783.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779770) CORROSION SEAT TRACK +Y765 FRAME 41 TO 47 IN PASSENGER CABIN. REPLACED SEAT TRACK +Y765 FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779681) CORROSION SEAT TRACK -Y765 ON FRAME 36 TO FRAME 41. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D5370500.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779644) CORROSION FLOORBEAM +Y1225 LOCATED FRAME 66 TO FRAMED 68 AT AFT GALLEY AREA (SSI 534147) REPLACED IAW SRM 51-72-11 AND DWG D53472780.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779745) CORROSION SEAT TRACK +Y765 FRAME 36 TO 41 IN PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

(LP 0779642) CORROSION FLOOR BEAM -Y189 LOCATED BETWEEN FRAME 20 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189). REPLACED IAW SRM 51-72-11 AND DWG D 53111406.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

CORROSION FLOORBEAM +Y503.2 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND SRM 51-72-11 AND DWG D53112825.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

CORROSION WEB LOCATION BETWEEN FRAME 20 TO FRAME 24 AT LEVEL STRINGER 23R AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53112806.

Part: NOT REPORTED — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,681 hrs · 23,335 cycles

CORROSION WE LOCATED FRAME 69 TO FRAME 70 AT LEVEL STRINGER 23L AT AFT GALLEY AREA. REPLACED IAW SRM 51-2-1 AND DWG D53474180.

Part: COOLING FAN — LEAKING (APU) · airframe 50,681 hrs · 23,335 cycles

ODOR IN CABIN WITH APU AND PACKS ON. OIL LIKE SMELL. FOUND APU COOLING FAN LEAKING OIL. REMOVED AND REPLACED COOLING FAN IAW AMM. OPERATION AND LEAK CHECK OK.

Part: TUBE — LEAKING (NR 1 ENGINE) · airframe 50,678 hrs · 23,334 cycles

WHEN POWER CAME BACK AT TOP OF DESCENT A SHARP PUNGENT SMELL FILLED THE FLIGHT DECK AND REMAINED THRU SHUTDOWN. MAINTENANCE INSPECTED APU AND FOUND INTAKE ASSEMBLY WITH OILY RESIDUE. REMOVED RIGHT APU DOOR FOR CLEANING AND FOUND NR 1 ENGINE FORWARD SUMP PRESSURIZATION TUBE LEAKING OIL. REQUIRES ENGINE CHANGE. COMPLIED WITH NR 1 ENGINE CHANGE ON 7900-2001 AND 4916-2001. INSTALLED RIGHT APU DOOR. FOUND RIGHT PACK PLENUM DELAMINATED. REMOVED AND REPLACED SAME. LEAK AND OPERATIONS CHECK GOOD.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 46,006 hrs · 21,065 cycles

CRACK ON FWD LATERAL SEGMENT FRAME INBD ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN. REPLACED FWD LATERAL SEGMENT FRAME IAW SRM 51-72-11 AND DWG D52279010.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 46,006 hrs · 21,065 cycles

CRACK ON AFT LATERAL SEGMENT FRAME INBD ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN, REPLACED AFT LATERAL SEGMENT FRAME IAW SRM 51-72-11 AND DWG D52279010.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 42,186 hrs · 19,263 cycles

CORROSION FOUND ON STRINGER 43L BETWEEN FRAME 56 AND 57. REPAIRED IAW ER/A 541087-14, REV O AND SRM 53-00-13, FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND LIGHTNING STRIKE ON EXTERNAL SKIN FR 21+5" AND 3" ABOVE STR 38R APROX, FWD FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 21+5" AND 3" ABOVE STR 38R APROX, FWD FUSELAGE IAW SRM A320 53-00-11, FIG 232.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER LOC FR 27+19" AND STR 41R LOWER FUSELAGE. PERFORMED PERMANENT REPAIR LOC. FR 27+19" AND STR 41R LOWER FUSELAGE IAW SRM A320 53-21-11, PARA 5J FIG 2013 (SHEET 2) PAGES 327/328.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LT SIDE FR 68 AFT PAX CABIN. REPLACED LOWER SILL LOCATED LT SIDE BETWEEN FR 66 TO FR 68 AT LEVEL STR 23L AFT PAX CABIN IAW SRM 51-72-11 AND DWG 53480019.

Part: STRUCTURE — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER FR 66 AT LEVEL OF STR 23R AFT PAX CABIN. REPLACED IAW 51-72-11 AND DWG D53480505.

Part: FLOORBEAM — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION, BEAM -Y1192 FR 67 AFT PAX CABIN SSI 534147 L=1.644" W=0.950" D=0.028". REPLACED BEAM -Y1192 FR 67 TO FR 68 AFT PAX CABIN IAW SRM A320 51-72-11 AND DWG D53472040.

Part: HINGE — WORN (RUDDER) · airframe 33,933 hrs · 15,272 cycles

DURING BEARING REMOVAL OF RUDDER HINGE NR 7 THE BORE FOUND WITH WEAR. THERE IS NO ALLOWABLE DAMAGE NOT REPAIR ON ANY MANUAL, HINGE NR 7 MUST BE REPLACED. REPLACED HINGE NR 7 AND FASTENERS IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTIO, FOUND CORROSION ON LOWER SILL RT SIDE FR 66 AFT PAX CABIN. REPLACED LOWER SILL AND LOCK FASTENERS. R2 FR 66 TO FR 68 AFT. PAX CABIN IAW SRM A320 51-72-11 AND DWG D53480019.

Part: STRUCTURE — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FR 68 AT LEVEL OF STR 23R AFT PAX CABIN. REPLACED AFT LOWER CORNER LOC. ON FR 68 AT LEVEL OF STR 23R AFT PAX CABIN SRM A320 51-72-11 AND DWG 53480505.

Part: FLOORBEAM — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM FR 66 -Y464 AFT PAX CABIN. REPLACED FLOORBEAM IAW SRM 51-42-11 AND SRM 51-72-11, DWG D53472816.

Part: FLOORBEAM — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON BEAM -Y1160 FR 68 AFT PAX CABIN SSI 534147, L=1.205", W=0.752", D=0.033". REPLACED BEAM IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOORBEAM — CORRODED · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON BEAM -Y1292 FR 66 AFT PAX CABIN SSI 534147, L=0.438", W=0.118", D=0.028". REPLACED BEAM -Y1292, FR 64 TO FR 66 AFT PAX CABIN IAW SRM 51-72-11 AND DWG D53472000.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

AFTER REMOVED SHEAR PLATE IAW ROUTINE CARD 5320-01089-01, FOUND CORRODED WEB AT LEVEL, STR 23R AND BETWEEN FR 69 TO FR 70. REPLACED WEB AT LEVEL STR 23R AND BETWEEN FR 69 TO FR 70 IAW SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON BEAM FR 67-68 Y765 AFT PAX CABIN. REPLACED BEAM Y765 LOC FR 67 TO FR 70 AND FASTENER IN AFT PAX CABIN IAW SRM A320 51-72-11.

Part: FITTING — CORRODED (PAX DOOR SILL) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING RT LOWER SILL AFT PAX CABIN SSI 534147 L=1.667" W= 0.575, D=0.094". REPLACED CENTER FITTING RT LOWER SILL AND FASTENER IN AFT PAX CABIN IAW SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING OF LT LOWER SILL FR 66 AND FR 68 AFT PAX CABIN. REPLACED CENTER FITTING AND FASTENER OF LT LOWER SILL FR 66 AND FR 68 AFT PAX CABIN IAW SRM 51-72-11 AND DWG D53480009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK FR 64+5", FR 66 Y765 AFT PAX CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 33,933 hrs · 15,272 cycles

DURING INSPECTION, FOUND CORROSION ON BEAM FR 67-68 -Y765 AFT PAX CABIN. REPLACED BEAM -Y765 LOC FR 67 TO FR 70 AFT PAX CABIN IAW SRM 51-42-11, 51-72-11.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 33,625 hrs · 15,130 cycles

DURING SERVICE CHECK FOUND EPSU 13WL FAULT MESSAGE ON PROGRAM TEST AND BATTERY FAULT ON EPSU 13WL. MX REPLACED BATTERY AND OPS CHECK WAS NORMAL.

Part: LUG — DAMAGED (RT MLG) · airframe 35,780 hrs · 16,172 cycles

RT FWD LUG FOR RT MLG DAMAGED DURING BUSHING INSTALATION DAMAGED RT WING. BORED TO REMOVE DAMAGE AND RE-ESTABLISHED CHAMFERS. ACCOMPLISHED IAW PRI ER/A 49778-14, AD 142948 COMPLIED WITH STEP 2 IAW PRI/ER/A 497778-14AD. NO DEFECTS NOTED INSTALLED BUSHINGS. ACCOMPLISHED IAW ERA 49778-14AD, REV 1.

Part: CONNECTOR — LOOSE (CABIN) · airframe 4,825 hrs · 2,094 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY EXIT PATH LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE RECONNECTED LOOSE CONNECTION AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,857 hrs · 12,930 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT 13WL INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 28,751 hrs · 12,884 cycles

DURING A NON ROUTINE CHECK, FOUND THE AFT RIGHT EPSU FAULT MESSAGE ON CIDS PANEL FOR 13W. MAINTENANCE REPLACED THE SLIDE ASSEMBLY AT DOOR 2R AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 27,836 hrs · 12,507 cycles

FWD DUMMY RAIL +Y503.2 IS CORRODED AT FRAME. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=2.2" W=2.1" MAX DEPTH=0.079", ORIGINAL MATERIAL THICKNESS =0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 103. R & R DUMMY RAIL IAW SRM 51-42-11. INSTALLED NEW RAIL IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 27,836 hrs · 12,507 cycles

FWD CABIN FLOORBEAM -254 IS CORRODED AT FR 18. ORIGINALTHICKNESS .079" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED FLOORBEAM AND SPLICE IAW SRM 51-42-11. RECEIVED NEW FLOORBEAM AND MACHINED BEAM AFT END TO FIT SPLICE IAW ER/A 489275-14. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-44-11. INSTALLED NEW FLOORBEAM AND SPLICE IAW TRM 53-21-01 AND SRM 51-42-11. ACCOMPLISHED FINAL ER/A 489275-14 SECTION I, PERMANENT REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,836 hrs · 12,507 cycles

NEED TO REMOVE FLOOR PANEL 221FF TO ACCESS STRINGER REPAIR. REMOVED FLOOR PANEL 221FF IAW AMM 53-12-12. UPON REMOVAL OF FLOOR PANEL 221FF FOUND CORROSION ON BOTTOM OF PANEL. NO ALLOWABLE LIMITS FOR PANEL. INSTALLED NEW FLOOR PANEL IAW AMM 53-12-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,836 hrs · 12,507 cycles

FWD CABIN FLOORBEAM +Y1292 IS CORRODED AT FR 16 BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=7.0" W=1.5" D=0.045", ORIGINAL MATERIAL THICKNESS 0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED FLOORBEAM IAW SRM 51-42-11. INSTALLED NEW FLOORBEAM IAW SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 27,836 hrs · 12,507 cycles

FWD CABIN DUMMY RAIL, Y-189 IS CORRODED AT FRAME 20. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=2.0" W=1.0", D=0.051". ORIGINAL MATERIAL THICKNESS 0.080", FOUND TO BE OUTOF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED DAMAGED DUMMY RAIL IAW SRM 51-42-11, INSTALLED NEW RAIL IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,836 hrs · 12,507 cycles

FWD CABIN FLOORBEAM -1292 IS CORRODED BETWEEN FR 16 ANDFR 20. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=3.0" W=1.0 D=0.070" ORIGINAL MATERIAL THICKNESS 0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED FLOORBEAM IAW SRM 51-42-11, INSTALLED NEW FLOORBEAM IAW SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 26,570 hrs · 11,917 cycles

DURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131AF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14 PAGE 401.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 26,570 hrs · 11,917 cycles

DURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131EF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14, PAGE 401.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 25,525 hrs · 11,470 cycles

DURING A NON ROUTINE CHECK, MX FOUND ROW 19 EMERGENCY SEAT LIGHT INOPERATIVE. MX FOUND PIN PUSHED BACK IN CONNECTOR, REINSTALLED PIN AND OPS CHECK WAS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 24,499 hrs · 11,112 cycles

TEST OF EMERGENCY LIGHTS FOUND SEAT 4 PATH LIGHT INOP, REPAIRED BROKEN WIRE UNDER SEAT AND CHECKS OK.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 50,771 hrs · 22,590 cycles

DURING "H" CHECK, FOUND PUNCTURE IN FORWARD CARGO DOOR INNER SKIN. REPAIRED PER EA 32-210218 SECTION I SECTION II OF EA 32-210218 TO BE ACCOMPLISHED WITHIN 180 DAYS.

Part: THERMOSTAT — UNKNOWN (CUSTOMER AIR) · airframe 15,355 hrs · 6,958 cycles

AIR ENGINE NR 1 AND NR 2 BLEEDS FAULTED AT FLIGHT LEVEL 390. STARTED LOSING CABIN PRESSURIZATION, ATC CLEARED AND EXECUTED RAPID DESCENT, DURING WHICH CABIN ALTITUDE WENT TO 12500 FEET. BLEEDS RECOVERED AT 10,000 FEET. MASKS WERE NOT DROPPED, AND AIRCRAFT LANDED UNEVENTFULLY AT DESTINATION. NR 2 BLEED, FAN AIR VALVE AND PNEUMATIC TEMP CONTROL THERMOSTAT (TCT) REPLACED. NR 1 BLEED, BLEED MONITOR COMPUTER (BMC) REPLACED. CHECKS NORMAL.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 11,527 hrs · 5,175 cycles

AT CRUISE ALTITUDE OF 37,000 FEET RECEIVED A CAB PR SYS 1 FAULT. MOMENTS LATER RECEIVED CAB PR 1 & 2 FAULT. REQUESTED IMMEDIATE DESCENT WITH ATC. CABIN PRESSURE WAS HOLDING STEADY AT 7,000 FEET. REPORTED TO ATC THAT CABIN PRESSURE WAS HOLDING AND RECEIVED CLEARANCE TO LEVEL AT 19,000 FEET. NO EMERGENCY WAS DECLARED, CABIN O2 MASKS DID NOT DEPLOY. UNEVENTFUL LANDING. REMOVED AND REPLACED OUTFLOW VALVE 32-2130-9-0009, S/N OFF 91680.