N334NW

Part: DAMPENER — NO TEST (ZONE 800) · airframe 95,614 hrs · 44,211 cycles

NO TEST FOR DAMPER OF PAX DOOR 832. REF AMDS 5210-7089-LA. REPLACED DOOR DAMPER OF PASSENGER CREW DOOR 832 IAW FAM AMM 52-13-14-000-001-A AND AMM 52-13-14-400-001-A.

Part: DAMPENER — FAILED (ZONE 800) · airframe 95,611 hrs · 44,210 cycles

DONT PASS TEST DOOR DAMPER ON PASSENGER CREW DOOR 841 (REFFER TO AMDS CARD 5210-7089-RF). REMOVED DOOR DAMPER ON PASSENGER CREW DOOR 841 P/N FE174-0011 S/ N 1526 ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 52-11-14- 000-001-A JOB IN PROGRESS. REPLACED DAMPER AT PASSENGER CREW DOOR 841 AS PER A320 FAM AMM 52-11-14-000-001-A AND A320 FAM AMM 52-11-14-400-001-A SEEINDIVIDUAL SIGN OFF ORNRC 19/200 RII INSPECTION COMPLETE. AE375QC JOB COMPLETE. (LP: 1359969)

Part: BOTTLE — NO TEST (ZONE 800) · airframe 95,611 hrs · 44,210 cycles

DID NOT PASS TEST DOOR DAMPER OF PASSENGER CREW DOOR 831. REMOVED PASSENGER CREW DOOR DAMPER 831 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-11-14- 000-001-A, STEP 3.B THRU 4.A. REPLACED THE DOOR DAMPER IAW FAM AMM 52-11-14-000-001-A, AND FAM AMM 52-11-14-400-001. (LP: 1349178)

Part: HYDRAULIC LINE — LEAKING (ZONE 300) · airframe 94,295 hrs · 43,516 cycles

SHIP 3234 DISC: THERE IS A SMELL IN THE COCKPIT & THROUGHOUT THE AIRCRAFT. I SUSPECT SOME TYPE OF FUMES FROM THE PACKS. C/A: DURING INSPECTION FOUND A HYDRAULIC LEAK FROM RUDDER SEEPS DOWN TO INET OF APU. OPEN ACCESS PANEL ON RUDDER FOUND V-NUT LINE TUBE CONNECTION TO UPPER SERVO ACTUATOR SOUR OF LEAK REF A320 AIPC 27-24-04-09/060. TIGHTENED V-NUT PER A320 AMM 20-21. CHECK OK - NO LEAK. SEE LOG 1006044 FOR NO GO ODI PREVENTION ACTION. (LP: 5243102)

Part: LEVER — OUT OF ADJUST (ZONE 800) · airframe 92,072 hrs · 42,379 cycles

SHIP 3234 DISC: R2 DOOR ARMS WITH PIN INSTALLED. C/A: REMOVED DOOR LINING DOOR 2R OVER DISARM LEVER. WIP 416340. ADJUSTED ARMING LEVER FITTING REF A320 AMM 52-13-21. INSTALLED NEW ARMING PIN. OP CKS NORMAL AT THIS TIME. OK FOR SERVICE. SUGGEST REPLACING BALL FITTING PN 32-2500-3-0873. NIS. ALL DOOR LIMING REINSTALLED. (LP: 6184018)

Part: BLOWER MOTOR — FAILED (ZONE 100) · airframe 91,977 hrs · 42,329 cycles

SHIP 3234 DISC: STRONG BURNING ELEC SMELL IN AFT LAVS. AT GATE BEFORE BOARDING. C/A: FOUND VAC LAV BLOWER MOTOR BAD. AFT ACCESS PANEL IN AFT BAG BIN REMOVED FOR ACCESS ON AFT WALL (604034).. REPLACED LAV VAC BLOWER MOTOR A320 AMM 38-31. INSTALLED AFT WALL PANEL A320 AMM 25-55. (LP: 5137868)

Part: FILTER — ODOR (ZONE 100) · airframe 91,945 hrs · 42,309 cycles

SHIP 3234 DISC: AFTER APU START, FA'S NOTICED STRONG "DIRTY SOCK" ODOR IN AFT PORTION OF AC. FO NOTICED SAME ODOR SHORTLY AFTER. DISSIPATED SLIGHTLY AFTER APU BLEED WAS TURNED OFF, BUT CAME BACK AFTER BLEED TURNED BACK ON. C/A: RUN APU BLEED CONFIRMED "DIRTY SOCK" SMELL PERFORMED LEVEL A DECONTAMINATION OF ECS IAW W/C 2100-2-007. NO ODORS NOTED. PER MCC R/R BOTH REC. FILTERS. NOTIFIED MCC. OK FOR SERVICE. (LP: 5137856)

Part: SENSOR — FAULTED (NR 2 ACM) · airframe 91,797 hrs · 42,221 cycles

SHIP 3234 - ATO - AT APPROXIMATELY 20KTS DUE TO AIR PACK 2 OVHT ECAM MESSAGE. CORRECTIVE ACTION: PACK #2 PLACED ON MEL DEFERRAL. OK TO CONTINUE. (LP: 0436105) SUPPLEMENTAL INFO: FAULTS COMP TEMP SENSOR 32HH. R/R'D SENSOR 32HH PER A320 AMM 21- 61. RIGHT PACK WONT GO OUT OF LO MODE. R/R'D DIFFERENTIAL PRESSURE SENSOR 9HB PER A320 AMM 21-51. R/R'D COMPRESSOR PNEUMATIC OVERHEAT SENSOR 11HM9 PER A320 AMM 21-61. ALL CHECKS OK. MEL CLEARED. PLACARD REMOVED.

Part: CLAMP — LOOSE (RT A/C PACK) · airframe 91,456 hrs · 42,042 cycles

SHIP 3234 - ATO - DUE TO AIR R WING LEAK ECAM MESSAGE. CORRECTIVE ACTION: FOUND LEAK IN RIGHT PACK BETWEEN OZONE CONVERTER AND CROSS BLEED VALVE. RETIGHTENED CLAMP ON T-DUCT IN FRONT OF OZONE CONVERTER, AND R/R LOOPS 47HF AND 74HF. NO LEAKS NOTED.

Part: SKIN — HANDLER ERROR (L1 DOOR) · airframe 91,075 hrs · 41,832 cycles

SHIP 3234 DISC: JETBRIDGE CONTACTED L1 LOWER DOOR, DAMAGE TO EDGE OF LOWER SHEET METAL. C/A: REWORKED DAMAGE IAW A320 SRM 52-10-00. WITHIN ALLOWABLE LIMITS FOR ALLOWABLE REWORK TYPE 1 PER A320 SRM 52-10-00-283-001, FIG. 006. RESTORED SURFACE PROTECTION. THIS REWORK IS PERMANENT REPAIR CATEGORY B. FOLLOW ON INSPECTION REQUIRED AT 60,000 FC FROM TIME OF REWORK. SUBSEQUENT INSPECTIONS AND INSPECTION METHOD TBD. UPDATED LRU TO FTN 1W8541 DOOR, PSGR, ENTRANCE; FWD LH. (LP: 5609920)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 90,449 hrs · 41,495 cycles

SHIP 3234 DISC: EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:1C . C/A: FOUND 1C EMERGENCY FLOOR LIGHTING LENSE LOOSE, RESECURED, EMER LIGHT OPERATES NORMAL, A/C OK FOR SVC. (LP: 0194331)

Part: SKIN — CORRODED (FRM 69-70) · corrosion level 3 · airframe 90,372 hrs · 41,447 cycles

SHIP 3234 DISC: CORROSION EXTERNAL SKIN DRAIN VALVE LOC. FR 69 TO FR 70 AT LEVEL STR 31 TO STR 32 R/H AT LOWER FUSELAGE. C/A: PERFORMED REPAIR LOC. FR 69 TO FR 70 AT LEVEL STR 31 TO STR 32 R /H AT LOWER FUSELAGE AS PER A320 SRM 53-41-11-300-004 STEP 2FIGURE 001 (SHEET 1 OF 1 ) MEASURES OF CORROSION ARE: L= 3.013 INCHES; W= 2.255 INCHES TOOL USED DIGITAL CALIPER PN: 500-197-30 ;SN: A21141969; DUE DATE: 21 NOV 24. DECAL MONITOR STABLISHED.. (LP0170061)

Part: DAMPENER — NO TEST (DOOR) · airframe 90,372 hrs · 41,447 cycles

SHIP 3234 DISC: DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 831 AT FWD GALLEY AREA REFER TO AMDS CARD 5210- 7089-LF (RII). C/A: REMOVED DOOR DAMPER P/N FE174-004 S/N 407 ON UNSERVICEABLE CONDITION OF PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11- 14-000-001-A STEP 3.C AND STEP 4 JOB IN PROGRESS CYLINDER, DOOR

Part: DAMPER — NO TEST (DOOR) · airframe 90,372 hrs · 41,447 cycles

SHP 3234 DISC: DONT PASS TEST DAMPER ON PASSENGER CREW DOOR 841 REFER TO AMDS CARD 52 10-7089-RF RII AT FWD GALLEY AREA. C/A: REPLACED NEW EMERGENCY DOOR DAMPER ON SERVICEABLE CONDITION ON PASSENGER CREW DOOR 841, AS PER A320 FAM AMM-52-11-14-000-001-A, AS PER A320 FAM AMM-52-11-14-400-001-A, TOOL USED: CALIPER, P/N: 500-196-30, S/N: B21140358, DUE DATE: 24-DEC-24, TOOL USED: FEELER GAUGE, P/N: 2ZVC8, S/N: AE-412364, DUE DATE: 14-JUL-24, TOOL USED: TORQUE, P/N: QD1R200, S/N:06180901262, DUE DATE:04- MAR-24, TOOL USED: REGULADOR PRESION, P/N: 8700-2500-580, S/N: AE-31620, DUE DATE: 10-OCT-24, TOOL USED: THERMOMETERS, P/N: FLUKE 566, S/N: AE-405679, DUE DATE: 22-MAR-24 RII INSPECTION COMPLETE 0943462 AE362QC JOB COMPLETE. (LP: 0160507)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,337 hrs · 41,431 cycles

2L SLIDE DEPLOYED IN ERROR. C/A: REF. LOG 0134554 FOR 2L SLIDE REPLACEMENT, REMOVAL, REMOVED 2L DAMPER PER A320 AMM 52-13 OK TO INSTALL DELTA INSTALLED DAMPER PER A320 MM 52-13 CK'S GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,200 hrs · 41,354 cycles

SHIP 3234 DISC: FA REPORTED 2R DOOR WOULD MOVE BETWEEN ARM & DISARM WITH PIN INSTALLED INTO DOOR. C/A: FOUND 2R DOOR ARMING PIN BRACKET MISALIGNED. RE-ALIGNED BRACKET PERFORMED OPERATIONAL CHECK PER A320 AMM 52-73-00-710-001A. OPS NML (LP: 5089422)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,049 hrs · 41,269 cycles

SHIP 3234 DISC: N ARRIVAL AT GATE APU FUME SMELL APPEARED CAPT TURNED OFF APU BLEED FUMES DISAPPEARED INSTANTLY CAPTAIN AND F/A NO SMELL ADV. C/A: INSPECTED APU / ENGINE INLETS PACK INLETS NO CONTAMINATION. NOTED PREFORMED ECS DECONTAMINATION PER AMDS W/C 2100-2005 R/R RECIRC FILTERS PER A320 AMM 21-26 NO SMELL PRESENT A/C OK FOR SVC. (LP: 729177)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,069 hrs · 41,281 cycles

SHIP 3234 DISC: FOUND PAINT MISSING AT LT WING ROOT/SLAT 1 AT LOC STA 0/RIB1. C/A: COMPLIED WOTH REPETATIVE CHECK ON LT WING ROOT IAW SRM 51-77-12. NO DEFECTS NOTED. (LP 9900478)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,983 hrs · 40,708 cycles

AIRCRAFT 3234 - ATO - AT APPROXIMATELY 70 KNOTS DUE TO DOOR FWD CARGO ECAM MSG. TAKEOFF ABORTED. CORRECTIVE ACTION: FOUND CARGO DOOR HANDLE UNLATCHED. REPLACED WORN FORWARD HANDLE FLAP HOOK AND PIN MECHANISM. OPS CHECK GOOD. (LP 4131113)

Part: PANEL — OUT OF ALIGNMENT (L1 DOOR) · airframe 87,364 hrs · 39,858 cycles

DOOR 1L DISARMING PIN WILL NOT ENGAGE FULLY IN THE LOCK POSITION. CORRECTIVE ACTION: FOUND PANEL MISALIGNED WITH PIN HOLE. ADJUSTED 1L DOOR PANEL AS NEEDED. DISARMING PIN ENGAGED NML AT THIS TIME. OK FOR SERVICE. (8942272)

Part: NONE — NONE (NONE) · airframe 87,356 hrs · 39,852 cycles

SHIP 3234 NEED TO COMPLY WITH DELTA ERA 604224-14AD (MAJOR REPAIR). CORRECTIVE ACTION: COMPLIED WITH. (2534630)

Part: PIN — WILL NOT ARM · airframe 87,255 hrs · 39,806 cycles

SHIP 3234 DOOR 1L DISARM PIN WILL NOT STAY LOCKED IN. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-12. OK FOR SERVICE. (8942206)

Part: NONE — NONE · airframe 87,360 hrs · 39,855 cycles

SHIP 3234 MINOR UPDATES TO EM 5311-01244 SECTION 01 (CRACK). CORRECTIVE ACTION: COMPLIED WITH. (2471116)

Part: NONE — NONE (NONE) · airframe 92,028 hrs · 42,355 cycles

SHIP 3234 DISC: ER/A 597800-14AD HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. THE SUBJECT LOG 2432038 IS DTE RELATED. STAGE II APPROVAL PROVIDED AT REV A. THE REPAIR OF SECTION I IS PENDIN G STAGE III APPROVAL PRIOR TO THE ESTABLISHED THRESHOLD UPDATED LIMITS FROM 86937 FH AND 43361 FC TO 88200 FH AND 44100 FC PER ERA 597800-14 AD.S. (LP: 2432038)

Part: NONE — NONE · airframe 86,473 hrs · 39,353 cycles

SHIP 3234 -ATO- AT LOW SPEED DUE TO DISPLAY OF ELEC GEN 2 FAULT MESSAGE. CORRECTIVE ACTION: DEFERRED #2 IDG PER MEL 24-20-01A AND CONTINUED. (9182360)

Part: PRESSURE DECK — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON PRESSURE DECK MEMBRANE TO CENTER WING BOX FR 36 LH HOLE 2. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD REV ORIGINAL. (2211157)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (- Y765) ZONE 1 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2211203)

Part: PRESSURE DECK — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON PRESSURE DECK MEMBRANE TO CENTER WING BOX FR 36 RH HOLE 5. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD REV ORIGINAL. (2211047)

Part: PRESSURE DECK — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON PRESSURE DECK MEMBRANE TO CENTER WING BOX FR 36 RH HOLE 6. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD REV 0 REV 1 AND REV 2. (2211042)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254) ZONE 1 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14 AD REV ORIGINAL. (2211237)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 (- Y254) ZON E 2 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2210899)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (- Y765) ZONE 1 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2211204)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254) ZONE 2 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2211198)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254) ZONE 2 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2211284)

Part: PRESSURE DECK — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON PRESSURE DECK MEMBRANE TO CENTER WING BOX FR 36 RH HOLE 2. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD REV ORIGINAL. (2211208)

Part: PRESSURE DECK — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON PRESSURE DECK MEMBRANE TO CENTER WING BOX FR 36 LH HOLE 3. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD REV ORIGINAL. (2211017)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 (Y765) ZONE 1 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2210893)

Part: STRINGER — CRACKED · airframe 85,624 hrs · 38,856 cycles

SHIP 32341 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 (-254) ZONE 1 AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 597663-14AD REV ORIGINAL. (2211279)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5(- Y765) ZONE 2 AT FR36. CORRECTIVE ACTION: REPAIRED PER ER/A 597663-14 AD REV ORIGINAL. (2209696)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION INDICATION FOUND IN OPEN HOLE 4 OF THE SKIN UNDERNEATH THE HINGE FITTINGS ON FWD CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 597985-14AD REV ORIGINAL. (2210063)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION INDICATION FOUND IN OPEN HOLE 20 OF THE SKIN UNDERNEATH THE HINGE FITTINGS ON FWD CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 597985-14AD REV ORIGINAL. (2210060)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION STRINGER 31R LOCATED BETWEEN FR65 TO FR66 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11 AND 51-42-11. (2208862)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2(Y765) ZONE 2 AT FR36. CORRECTIVE ACTION: REPAIRED PER ERA 597663-14 AD REV ORIGINAL. (2209692)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND ON CONTINUITY FITTINGS RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ERA 597599-14AD REV. ORIGINAL. (2208327)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION STRINGER 41R LOCATED FR 33 TO FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 53-21-13. (2208434)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACKS WERE FOUND AT VARIOUS HOLE POSITIONS IN THE JUNCTION BETWEEN THE FLOOR BEAMS AND VERTICAL STIFFENERS AT Y-765,HOLES 1,2; Y-254,HOLES 1,2; Y254, HOLES 1,2; Y765, HOLES 1,2. CORRECTIVE ACTION: COMPLIED WITH SECTION II OF ERA 597663-14AD. (2208367)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION SHEAR TIE LOCATED FR 33 AND STR 40L TO STR 41L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11. (2208313)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 BENT INTERNAL STRUCTURE CROSS BEAM LOCATED FR 29 AND STR 38L TO STR 39R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSS BEAM PER A320 SRM 51-42-11. (2208638)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 (3) CRACKED HOLES FOUND ON RHS FR36 PRESSURE PANEL AND (2) CRACKED HOLES FOUND ON LHS FR36 PRESSURE PANEL. CORRECTIVE ACTION: COMPLIED WITH ERA 597800-14AD. (2207402)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE WEB LOCATED FR 33 TO FR 34 AND STR 38L FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-72-11. (2207337)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 EXPIRED DUE DATE FULL FACE OXYGEN MASK THIRD OCCUPANT IN COCKPIT. CORRECTIVE ACTION: REPLACED MASK PER A320 AMM 35-12-41. (2205993)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER OUTBO ARD HOLE 3 AT DOOR STOP FITTING 4 POSITION. CORRECTIVE ACTION: REPAIRED FRAME PER A320 SRM 53-41-12. (2205600)

Part: RESERVOIR — OUT OF DATE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 EXPIRED DUE DATE RESERVOIR OFFWING ESCAPE SLIDE L/H IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RESERVOIR PER A320 AMM 25-62-46. (2204176)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE WEB LOCATED FR 33 TO FR 34 AND STR 38R FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRUCTURE WEB PER A320 SRM 51-72-11. (2203031)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION SHEAR TIE LOCATED FR 33 AND STR 40R TO STR 41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11 AND 51-72-11. (2203027)

Part: ACCESS PANEL — ELONGATED · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 ELONGATED HOLE ACCESS PANEL 540JB FUEL TANK CUT OUT LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-21-11. OK FOR SERVICE. (2201559)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE SUPPORT WEB LOC BTW FR69 TO FR70 STR 23RH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT WEB AND FASTENERS PER A320 SRM 51-72-11. (2200513)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE ON SUPPORT WEB LOC BTW FR68 TO FR69 AT LEVEL STR23 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SUPPORT WEB PER A320 SRM 51-72-11 AND 51-42-11. (2200262)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND IN OPEN HOLE LOCATED AT DOOR STOP FITTING 1 LH SIDE LOWER INBOARD HOLE. CORRECTIVE ACTION: REPAIRED FRAME PER A320 SRM 53-41-12. (2200524)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y765 LOC BTW FR64 TO FR66 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE PER A320 SRM 51-42-11. (2200505)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y464 LOC BTW FR68 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2200508)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION STRINGER 43L LOCATED BTW FR55 TO FR58 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11 AND 53-41-13. (2200455)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y1162.5 AND BTW FR68 TO FR69 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2200264)

Part: BUSHING — WORN · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 842 BUSHINGS UPPER AND LOWER WORN. CORRECTIVE ACTION: REPLACED BUSHINGS ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 842 AS PER A320 AMM 52-13-21. OK FOR SERVICE. (2200515)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD HOLE 4 AT DOOR STOP FITTING 3 POSITION. CORRECTIVE ACTION: REPAIRED FRAME PER A320 SRM 53-41-12. (2200530)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE UPPER INBOA RD HOLE 2 AT DOOR STOP FITTING 4 POSITION. CORRECTIVE ACTION: REPAIRED FRAME PER A320 SRM 53-41-12. (2200560)

Part: DOOR — OUT OF ADJUST · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 842 HARD TO OPEN / OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-13-21. OK FOR SERVICE. (2200517)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION STRINGER 39L LOCATED FR 32 TO FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-21-13. (2197900)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 BENT INTERNAL STRUCTURE CROSS BEAM LOCATED FR 26 AND STR 38L TO STR 41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE CROSS BEAM PER A320 SRM 51-72-11. (2197772)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK INDICATION FOUND IN OPEN HOLE LOCATED DOOR STOP FITTING 7 UPPER INBOARD HOLE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-12. (2197919)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CRACK IN EMERGENCY EXIT DOOR 833 ON LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOAD TRANSMITTING PROFILE PER A320 SRM 51-72-11. (2197878)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE Y1292 LOC BTW FR64 TO FR66 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2197867)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 WEAR ON FIXED BUSHING ELEVATOR FITTING 1 OUTBOARD LUG ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORE LUG AND REPLACED BUSHINGS (1EA)ON OB LUG HINGE FITTING 1 RH ELEVATORS AS PER A320 SRM 55-26-41. (2194977)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION DOOR CUTOUT SEAL LOCATED AT LEVEL FR 26 TO FR 27 STR 38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOOR CUTOUT PER A320 SRM 51-42-11 AND 51-72-11. (2194933)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION STRINGER 41L LOCATED FR 33 TO FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 53-21-13 AND 51-42-11. (2194979)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 BENT INTERNAL STRUCTURE CROSS BEAM LOCATED FR 27 AND STR 38L TO STR 41 R IN FWD CARGO COMPARTMENT. REPLACED INTERNAL STRUCTURE CROSS BEAM PER A320 SRM 51-72-11. (2194859)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3270 CORROSION FLOOR STRUCTURE Y1162.5 LOC BTW FR66 TO FR68 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2187996)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y765 LOC BTW FR66 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (2187987)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION CENTER FITTING LOC.BTW FR 66 AND FR 68 STR 23 L AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING A320 SRM 51-72-11 AND 51-42-11. (2188000)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y160.5 LOC BTW FR66 TO FR68 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM AND FASTENERS A320 SRM 51-42-11. (2188005)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE Y1162.5 LOC BTW FR68 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2180048)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION LOWER SILL LOC BTW FR66 TO FR68 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 51-42-11 AND 51-72-11. (2177484)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y1292 LOC BTW FR16 TO FR20 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (2177472)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION ON RIVETS COMMON TO SHEAR TIE LOCATED FR 29 AND STR 40R TO STR 41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVETS COMMON TO SHEAR TIE PER A320 SRM 51-42-11. (2177470)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION ON RIVETS COMMON TO SHEAR TIE LOCATED FR 29 AND STR 38L TO STR 39L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVETS COMMON TO SHEAR TIE PER A320 SRM 51-42-11. (2177457)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION ON RIVETS COMMON TO SHEAR TIE LOCATED FR 29 AND STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVETS COMMON TO SHEAR TIE PER A320 SRM 51-42-11. (2177454)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE -Y1162.5 LOC BTW FR66 TO FR68 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2177496)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION ON RIVETS COMMON TO SHEAR TIE LOCATED FR 30 AND STR 40L TO STR 41L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVET COMMON TO SHEAR TIE PER SRM 51-42-11. (2177461)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION ON RIVETS COMMON TO SHEAR TIE LOCATED FR 30 AND TR 39L TO STR 40L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVETS COMMON TO SHEAR TIE PER A320 SRM 51-42-11. (2177478)

Part: SHEAR PLATE — CORRODED (FRMS 69-70) · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE SHEAR PLATE LOC BTW FR69 TO FR70 STR23 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS PER SRM A320 51-72-11 AND 51-42-11. (2170437)

Part: SHEAR PLATE — CORRODED (FRMS 69-70) · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE SHEAR PLATE LOC BTW FR69 TO FR70 AT LEVEL STR23 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS PER SRM A320 51-72-11 AND 51-42-11. (2170434)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE LOC -Y765 BTW FR16 TO FR20 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2161932)

Part: NONE — NONE · corrosion level 2 · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE LOC Y503.7 BTW FR12 TO FR16 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2159540)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 831 BUSHINGS DETERIORATED. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-11-22. OK FOR SERVICE. (2159618)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 842 DAMPER DID NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-13-14. OPS TEST GOOD. (2158541)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 841 BUSHINGS DETERIORATED. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-11-21. OK FOR SERVICE. (2159609)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 CORROSION FLOOR STRUCTURE Y1292 LOC BTW FR12 TO FR24 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (2156817)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 832 DOES NOT PASS OPERATIONAL TEST. CORRECTIVE ACTION: REPLACED DAMPER. OPS TEST GOOD. (2150961)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 EXPIRED DUE DATE RESERVOIR OFFWING ESCAPE SLIDE L/H IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RESERVOIR PER A320 FAM AMM 25-62-46. (2149357)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 832 HARD TO OPEN. CORRECTIVE ACTION: ADJUSTED DOOR RIGGING PER A320 FAM 52-13-21. OK FOR SERVICE. (2145004)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 832 OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-13-22. OK FOR SERVICE. (2145001)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 841 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2141999)

Part: NONE — NONE · airframe 85,624 hrs · 38,856 cycles

SHIP 3234 PASSENGER CREW DOOR 831 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2142009)

Part: NONE — NONE · airframe 85,615 hrs · 38,850 cycles

SHIP 3234 FIRST OFFICER OXYGEN MASK FAILED TEST. CORRECTIVE ACTION: DISCONNECTED AND RE-SEATED MASK SUPPLY LINE. OPS GOOD. NO LEAKS. (8361048)

Part: NONE — NONE · airframe 84,991 hrs · 38,507 cycles

SHIP 3234 1L DOOR ARMING PIN LOOSE. CORRECTIVE ACTION: R/R 1L DOOR ARMING PIN PER A320 AMM 52-62. (8336812)

Part: NONE — NONE · airframe 85,066 hrs · 38,551 cycles

SHIP 2894 1L DOOR DISARM PIN LOCKING BALLS INOP. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR 1L DISARMING PIN. OPS CHECK GOOD. OK FOR SERVICE (8118964)

Part: LIGHT — INOPERATIVE (SEAT 15D) · airframe 84,070 hrs · 37,976 cycles

SHIP 3234 EMERGENCY PATH LIGHT AT SEAT 15D LOOSE/INOP. CORRECTIVE ACTION: SECURED EMERGENCY LIGHT LOWER SEAT SHROUD PER A320 AMM 33-51. (7786420)

Part: DOOR FRAME — CRACKED (L1 DOORWAY) · airframe 83,192 hrs · 37,556 cycles

SHIP 3234 L-1 DOOR STOP FITTING #7, FRAME 16, HOLES #1 AND #3 SHOW CRACK INDICATIONS. CORRECTIVE ACTION: REP PER ERA 590594-14AD REV ORIG. (1758440)

Part: DOOR FRAME — CRACKED (R1 DOORWAY) · airframe 83,192 hrs · 37,556 cycles

SHIP 3234 R1 DOOR, FRAME 20, STOP # 1 SHOWS CRACK INDICATION AT # 3 HOLE IN INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ERA 590594-14AD REV ORIG. (1758340)

Part: DOOR FRAME — CRACKED (R1 DOORWAY) · airframe 83,192 hrs · 37,556 cycles

SHIP 3234 R1 DOOR, FRAME #16, FITTING #7, SHOWS CRACK INDICATIONS AT HOLE #1 (FRAME AND INTERCOSTAL) AND HOLE #3 (INTERCOSTAL). CORRECTIVE ACTION: COMPLIED WITH PRI 590594-14AD REV ORIG. AND ERA 590594-14AD REV ORIG. (1758442)

Part: PANEL — NO TEST (PSU AFT GALLEY) · airframe 83,174 hrs · 37,549 cycles

SHIP 3234 DURING TEST AFT GALLEY LT AND RT OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REMOVED AND REPLACED AFT GALLEY LT AND RT OXYGEN CONTAINER DOOR AS PER A320 CMM 35-21-74. OK FOR SERVICE. (7397074)

Part: PSU — NO TEST (SEAT 24ABC) · airframe 82,793 hrs · 37,387 cycles

DURING TEST FOUND PSU OXY PANEL FOR SEAT 24ABC WILL NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 26DEF) · airframe 82,793 hrs · 37,387 cycles

DURING TEST FOUND PSU OXY PANEL FOR SEAT 26DEF WILL NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: LIGHT — DAMAGED (SEAT 27D) · airframe 82,747 hrs · 37,362 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE NEAR SEAT 27D. CORRECTIVE ACTION: RESECURED EMERGENCY FLOOR LIGHTING. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 26 DEF) · airframe 82,642 hrs · 37,306 cycles

DURING TEST FOUND PSU AT SEAT 26 DEF WILL NOT OPEN. CORRECTIVE ACTION: REPLACED PSU PANEL. OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 5CD) · airframe 82,642 hrs · 37,306 cycles

DURING TEST FOUND PSU AT SEAT 2CD WILL NOT OPEN. CORRECTIVE ACTION: REPLACED PSU. OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 28DEF) · airframe 82,642 hrs · 37,306 cycles

DURING TEST FOUND PSU AT SEAT 28DEF WILL NOT OPEN. CORRECTIVE ACTION: REPLACED PSU. OPERATIONS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 82,139 hrs · 37,049 cycles

DESCENDING THROUGH 8K MSL GOT A DIRTY SOCK SMELL. AFTER LANDING & SHUTTING DOWN #2 ENG AIR GOT VERY HOT. AFTER PULLING INTO GATE , CABIN BECAME HAZY WITH DIRTY SOCK SMELL AGAIN . CORRECTIVE ACTION: REMOVED #2 ENG SPINNER PER A320 AMM 7221(886483) REMOVED #1 ENG SPINNER, INSPECTED AND FOUND NO OIL. REINSTALLED #1 ENG SPINNER REF A320AMM 72-21. PERFORMED DUCT BURN. HYD LK FOUND AND REPAIRED. OK FOR SVC

Part: FORK — CRACKED (CARGO DOOR) · airframe 80,849 hrs · 36,322 cycles

FWD CARGO DOOR / FRAME FORKS / CRACKED AND OVERSIZED HOLES / AD 2018-25-08, FR25 HOLE #H1 FR26(H2, H3) AND FR26A(H10, H11), REPAIR PER ER/A 579317-14AD ON SHOP WORK ORDER PR0134

Part: HOUSING — BROKEN (CABIN) · airframe 78,002 hrs · 34,923 cycles

FOUND EMERGENCY LIGHT AT SEAT 22DEF HOUSING BROKEN OFF. REMOVED AND REPLACED HOUSING. OPERATION CHECKS GOOD.

Part: CAP — LEAKING (APU OIL SYSTEM) · airframe 77,900 hrs · 34,872 cycles

(LP# 3084898) LAST 10 MINUTES OF FLIGHT, AIRCRAFT HAD A POTENTIALLY TOXIC WET SOCK SMELL THAT BEGAN NEAR FORWARD GALLEY AND MIGRATED TO BACK OF AIRCRAFT. FOUND OIL INGESTION THRU APU INLET AND OIL LEAKING FROM SERVICING CAP. TIGHTENED OIL CAP LOCKING MECHANISM. REMOVED AND REPLACED LEFT AND RIGHT RECIRCULATION FAN FILTERS, OIL CAP AND OZONE CONVERTERS. COMPLY WITH NO GO ODI STEPS. OPERATION CHECKS GOOD, NO SNELL NOTED.

Part: LIGHT — UNSECURE (CABIN) · airframe 77,819 hrs · 34,835 cycles

EMERGENCY SEAT MOUNTED LIGHT DAMAGED 26D. SECURED LIGHT.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 77,727 hrs · 34,799 cycles

EMERGENCY LIGHTS ON EXIT ROWS IN WRONG POSITIONS. REPOSITIONED LIGHT ASSEMBLIES. OPERATION CHECKS GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 77,417 hrs · 34,636 cycles

FOUND RIGHT OVERWING EPSU INOP. REMOVED AND REPLACED RIGHT OVERWING EPSU. OPERATION CHECKS NORMAL.

Part: EPSU — MALFUNCTIONED (CABIN) · airframe 77,368 hrs · 34,611 cycles

CIDS MESSAGE 33-51-38. REMOVED AND REPLACED EPSU AND DEU.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 76,452 hrs · 34,149 cycles

LESS THAN 1 MINUTE LAV SMOKE WARNING IN FIRST CLASS LAVATORY. NOW SMOKE NOTED. PASSENGER EXITED LAV JUST AS ALARM STOPPED.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 76,287 hrs · 34,066 cycles

DIV- DUE TO AN INOP CAPTAIN'S OXYGEN MASK. MASK WAS SWAPPED WITH THE NR 2 OBSERVERS MASK ASSY AND PLACED ON MEL 25-11-07. DAMAGED MASK WAS SUBSEQUENTLY REPLACED AND MEL CLEARED. SHIP WAS RETURNED TO SERVICE.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 76,280 hrs · 34,062 cycles

EMERGENCY LIGHT ASSEMBLY BROKEN AT SEATS 24D AND 32D. FWD TO MCO/PLAC PER MEL 33-50-03A. REMOVED AND REPLACED EMERGENCY LIGHT HOUSING AT SEATS 24D AND 32D. OPERATION CHECKS GOOD.

Part: SOCKET — DAMAGED (OVERWING EXIT) · airframe 74,957 hrs · 33,496 cycles

RIGHT AFT OVERWING EXIT HANDLE EMERGENCY LIGHT SOCKET DAMAGE, REPLACED LIGHT ASSY

Part: REPAIR — DEBONDED (TE FLAP) · airframe 72,261 hrs · 32,225 cycles

TAP TEST INSPECTIONS ON PREVIOUS REPAIR AND FOUND DEBONDED IAW ER/A N 538043-14 REV ORIGINAL SECTION II. PERFORMED PERMANENT REPAIR ON I/B FLAP RT WING LOWER SKIN BTW RIB 5 AND RIB 6 IAW ER/A N 53804314 REV B SECTION III AND PRI ER/A 538043-14 REV A REVISION 0,1,2,3 AND 4.

Part: SKIN — DENTED (FRAME 67) · airframe 68,761 hrs · 30,577 cycles

DENT ON EXTERNAL SKIN, FRAME 67 BETWEEN STR 4R TO STR 5R ON UPPER FUSELAGE. PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL SKIN FRAME 67 BETWEEN STR 4R TO STR 5R ON UPPER FUSELAGE IAW SRM 53-41-11, PARA 5M FIG 215.

Part: STRUCTURE — DENTED (APU BAY) · airframe 68,761 hrs · 30,577 cycles

DENT ON INTERNAL STRUCTURE FWD WALL IN APU COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED ON INTERNAL AREA STRUCTURE FWD WALL IN APU COMPARTMENT IAW PRI 539101-14, REV O AND ER/A N539101-14, REV.

Part: SEAT TRACK — OUT OF LIMITS (FRAME 47-64) · airframe 68,761 hrs · 30,577 cycles

OUT LIMIT SEAT TRACK -Y1292, FRAME 47 TO 64 EVALUATED WITH JC 2500-2032. MEASURE ARE P1 FR 58 L: 2.666", W: 0.377", D: 0.045", P2 FR 63.+16", L: 2.340", W: 0.377", D: 0.045" IN PASSENGER CABIN. REPLACED SEAT TRACK -Y1292 LOCATED FRAME 47 TO FRAME 64 IAW SRM 51-72-11 AND DWG D53472077.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 72,249 hrs · 32,218 cycles

CORROSION WAS FOUND ON STRINGER 43L, FRAMES 56 - 57. SECTION OF THE STRINGER WAS REMOVED AND REPLACED.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON SHEAR TIE AT LEVEL OF FRAME 28 AND STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. CORROSION ON SHEAR TIE AT LEVEL OF FRAME 28 AND STR 43R TO STR 44 IN FWD CARGO COMPARTMENT.

Part: CHANNEL — BROKEN (PAX DOOR) · airframe 68,761 hrs · 30,577 cycles

BROKEN CHANNEL SEAL PASSENGER CREW DOOR RT SIDE INTERNAL STRUCTURE AT FWD GALLEY: REPLACED CHANNEL SEAL PASSENGER CREW DOOR RT SIDE INTERNAL STRUCTURE AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D52110490.

Part: STRUCTURE — CORRODED (FRAMES 30-31) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON INTERNAL STRUCTURE SECTION CONNECTION BETWEEN FRAME 30 TO FRAME 31 AND STR 41R IN FWD CARGO COMPARTMENT. REPLACED INTERNAL STRUCTURE SECTION CONNECTION BETWEEN FRAME 30 TO FRAME 31 AND STR 41R IN FWD CARGO COMPARTMENT AS IAW SRM 51-72-11 AND DWG D53231586.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 68,761 hrs · 30,577 cycles

CRACK ON EMERGENCY EXIT DOOR 843 FWD LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, SSI 522102-01-1, ATTACH FORM 5100-3201. REPLACED EMERGENCY EXIT DOOR 843 FWD LOAD TRANSMITTING PROFILE IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 68,761 hrs · 30,577 cycles

CRACK ON EMERGENCY EXIT DOOR 834 FWD AND AFT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN (SSI 522102-01-1, CARD 5220-3010A ATTACH FORM 5100-3201). REPLACED SEGMENTS, LOAD TRANSMITTING 2 EA ON EMERGENCY EXIT DOOR 834 FWD & AFT POSITION IN PASSENGER CABIN IAW SRM 51-75-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 68,761 hrs · 30,577 cycles

CRACK ON EMERGENCY EXIT DOOR 844 FWD LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, CARD 5220-3010A ATTACH FORM 5100-3201. REPLACE EMERGENCY EXIT DOOR 844 FWD LOAD TRANSMITTING PROFILE IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.

Part: FITTING — DENTED (CARGO DOOR) · airframe 68,761 hrs · 30,577 cycles

DENT ON CORNER FITTING DOOR AFT LOWER POSSITION IN FWD CARGO COMPARTMENT. REPLACED CORNER FITTING IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D523-71100.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON EMERGENCY EXIT DOOR 834 AFT LOWER FITTING IN PASSENGER CABIN. REPLACED ON EMERGENCY EXIT DOOR 834 AFT LOWER FITTING IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG NR D52279040.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.995", W=0.895", D=0.003". REPLACED FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FR 12 TO FR 24 AS IAW SRM 51-72-11 AND DWGS, D53112819, D53110984.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 68,761 hrs · 30,577 cycles

CRACK ON EMERGENCY EXIT DOOR 833 FWD LOAD TRANSMITTING PROFILE IN PASSENGER CABIN. SSI 522102-01-1, CARD 5220-3010A ATTACH FORM 5100-3201. REPLACED FWD LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT DOOR SRM 51-72-11 AND DWG D52279010.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 72,249 hrs · 32,218 cycles

CORROSION ON FLOOR PANEL HARD POINTS AND INSERTS OF PANEL 261DF AT AFT GALLEY AREA. REPLACED THE FLOOR PANEL HARD POINTS AND INSERTS IAW SRM.

Part: SEAT TRACK — OUT OF LIMITS (FRAMES 41-47) · airframe 68,761 hrs · 30,577 cycles

SEAT TRACK OUT LIMITS BETWEEN FRAMES 41 - 47 -Y1292. REPLACED IAW SRM 51-72-11 AND DWG D53371000, D53476950.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y1292 FROM FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y1162 FROM FRAME 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472088.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y1162 FROM FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y1292 FROM FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPOET IAW SRM 51-72-11 AND DWG D53472090.

Part: SEAT TRACK — NOT REPORTED (FRAMES 35-36) · airframe 68,761 hrs · 30,577 cycles

SEAT TRACK -Y765 OUT LIMITS BETWEEN FRAMES 35 - 36. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371024.

Part: FITTING — CORRODED (FRAME 20) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CORNER FITTING FRAME 20 AT FWD GALLEY AREA ON STRINGER 23L. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y512 FROM FRAMES 64 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472000.

Part: FITTING — CORRODED (FRAME 20) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CORNER FITTING FRAME 20 AT FWD GALLEY AREA ON STRINGER 23R, L=0.787", W=0.567", D=0.003", SSI 531102. REPLACED CORNER FITTING LOCATION FRAME 20 AT LEVEL STR 23R FWD GALLEY AREA IAW SRM 51-72-11 AND DWG NR D53112225, REPAIRED IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CENTER FITTING AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 AND STRINGER 23L. REPLACED CENTER FITTING AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 AND STR 23L IAW SRM 51-72-11 AND DWG NR D53112225.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y765 FROM FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y765 FROM FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53110422, D53112814, D53112812, AND D53110984.

Part: FITTING — CORRODED (FRAME 16) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CORNER FITTING FRAME 16 AT FWD GALLEY AREA ON STR 23R, L=0.789", W=0.765", D=0.003". SSI 531102. REPLACED CORNER FITTING LOCATED FRAME 16 AT LEVEL STR 23R FWD GALLEY AREA FLOOR STRUCTURE IAW SRM 51-72-11 AND DWG N. D53112225.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y765 FROM FRAME 66+5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: SEAT TRACK — NOT REPORTED (FRAMES 47-64) · airframe 68,761 hrs · 30,577 cycles

OUT LIMITS SEAT TRACK +Y1292 FRAMES 47 - 64, REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23L, L=0.800", W=0.400", D=0.002". SSI 534147. REPLACED LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23L IAW SRM 51-72-11 AND DWG D53480020.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT -Y189 FROM FRAMES 20 - 23. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: FITTING — CORRODED (FRAME 66) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CORNER FITTING FRAME 66 AT AFT GALLEY AREA FROM STRINGER 22L TO STRINGER 23L L=0.700" W=0.350" D=0.004" .SSI534133. REPLACED CORNER FITTING FRAME 66 AT AFT GALLEY AREA FROM STRINGER 22L TO STRINGER 23L IAW SRM 51-72-11 AND DWG D53480020.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y765 FROM FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW 51-72-11 AND DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (FRAMES 14-16) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y940 FROM FRAMES 14 - 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112822.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOOR SUPPORT +Y765 FROM FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: SEAT TRACK — NOT REPORTED (FRAMES 47-64) · airframe 68,761 hrs · 30,577 cycles

OUT LIMITS SEAT TRACK +Y765 FRAME 47 - 64. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DWG D53470080 AND DWG 53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON FLOORBEAM +Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.985", W=0.875", D=0.003". REPLACED FLOORBEAM +Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW SRM A320 51-72-11 AND DWG D53112816, DWG D53110984 AND DWG D53110422.

Part: FITTING — CORRODED (FRAME 68) · airframe 68,761 hrs · 30,577 cycles

CORROSION ON CORNER FITTING FRAME 68 AT AFT GALLEY AREA FROM STR 22L TO STR 23L. L=0.600", W=0.350", D=0.002, SSI 534136. REPLACED CORNER FITTING FRAME 68 AT AFT GALLEY AREA FROM STR 22L TO STR 23L IAW SRM 51-72-11 AND DWG D53480020.

Part: FRAME — CRACKED (FRM 68) · airframe 68,761 hrs · 30,577 cycles

CRACK ON FRAME 68 STRINGER 23L. REPLACED THE FRAME IAW SRM 51-72-11 AND DWG D53470150.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,595 hrs · 30,506 cycles

SEAT 25 EMERGENCY LIGHT INOPERATIVE IAW ESPM 20-43. SPICED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 67,615 hrs · 30,059 cycles

DURING INSPECTION, FOUND CORRSION FOUND AT STRINGER 43 LT FRAME 56 TO 57. REMOVED FASTENERS IAW SRM 51-42-11, 500123, COMPLETED BHEC OF FASTENER HOLES IAW NDTM 51-00-00 PART 6, NO CRACKS FOUND. 270158. FABRICATED STRINGER SPLICE AND COUPLING IAW SRM 53-00-13, 874907. OK TO INSTALL SPLICE ASSY AND DOUBLER, 270158. INSTALLED STRINGER SPLICE IAW SRM 53-00-13-2-001-00/ERA 535444-14.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 72,249 hrs · 32,218 cycles

FOUND AREAS OF CORROSION COMMON TO STRINGER 43L. ALL DAMAGE IS FOUND BETWEEN FRAMES 56-57. THE DAMAGED STRINGER SECTION WAS REMOVED AND A SPLICE REPAIR INSTALLED IAW ER/A.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 64,645 hrs · 28,704 cycles

DURING SERVICE CHECK, FOUND NUMEROUS SEAT ROW LIGHTS OUT. SEATED WALL MOUNTED CONNECTORS, OPERATES NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 64,359 hrs · 28,587 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY EXIT SIGN AT L1 DOOR LWR LT CORNER INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTION AT SIGN; TIGHTENED CONNECTION AND OPS CHECK WAS NORMAL.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 63,957 hrs · 28,379 cycles

FOUND NO TEST, ON EMERGENCY LIGHTS. REPLACED ESPU OPS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 58,990 hrs · 26,000 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 20 INOPERATIVE. MAINTENANCE REPLACED BROKEN WIRE AT SOCKET ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 56,110 hrs · 24,631 cycles

DURING EMERGENCY LIGHT TEST FOUND ROW 12ABC PATH LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRE AT CONNECTOR AND TESTS OK.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 55,941 hrs · 24,541 cycles

EMERGENCY LIGHT TEST FOUND SEAT ROW 8 INOPERATIVE. REPAIRED BROKEN WIRING AND TESTS OK.

Part: WIRE — DEFECTIVE (CABIN) · airframe 55,484 hrs · 24,357 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW PATH LIGHT 17C INOP. REPLACED PIGTAIL IN SEAT AND TESTS OK.

Part: PIN — BROKEN (CABIN) · airframe 55,270 hrs · 24,272 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT 22C PATH LIGHT INOP. REPAIRED BROKEN CONTACT PIN AND TESTS OK.

Part: PIN — BROKEN (CABIN) · airframe 55,270 hrs · 24,272 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT 23C PATH LIGHT INOP. REPAIRED BROKEN CONTACT PIN AND TESTS OK.

Part: PIN — BROKEN (CABIN) · airframe 55,270 hrs · 24,272 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT 5C PATH LIGHT INOP. REPAIRED BROKEN CONTACT PIN AND TESTS OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 53,573 hrs · 23,532 cycles

DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT SEAT ROW 19 INOP, REPAIRED BROKEN WIRE AND TESTS OK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND RT FLOOR SUPPORT Y-1292 HAS CORROSION. REPAIRED IAW SRM 51-22-11, SRM 53-41-15, SRM 51-42-11, SRM 51-44-11, AND SRM 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND RT FLOOR SUPPORT Y-1292 HAS CORROSION AT FR67. REPAIRED IAW SRM 51-22-11, SRM 53-41-15, SRM 51-42-11, SRM 51-44-11 AND 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1292 AT FR66 HAS CORROSION. REPAIRED IAW SRM 53-41-15, SRM 51-22-11, SRM 51-42-11, SRM 51-44-11, SRM 51-75-12

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND FLOOR SUPPORT LBL10, CORRODED AT FR12 TO 24. REPAIRED IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CORROSION ON FRAME 28 SHEAR TIE BETWEEN S43R AND S42. REPAIRED IAW SRM 51-42-11 AND SRM 51-75-12.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CORROSION ON FRAME 20 SHEAR TIE BETWEEN S41R AND S42R. REPAIRED IAW SRM 51-42-11 AND SRM 51-75-12.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING H-CHECK FOUND CORROSION ON FRAME 29 SHEAR TIE BETWEEN S24R AND S43R. REPAIRED PER SRM 51-42-11 AND SRM 51-75-12.

Part: THRESHOLD — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CORROSION ON DOOR L1 THRESHOLD. REPAIRED IAW SRM 51-42-11, 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT FRAME 20 RBL 29. REPAIRED IAW SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND PUNCTURE IN CABIN FLOOR PANEL 232FF. REPAIRED IAW SRM 53-02-00.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CRACK IN RT FWD EMERGENCY EXIT DOOR AFT SIDE PROFILE BEAM CRACKED. REPAIRED IAW SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND PUNCTURE IN CABIN FLOOR PANEL 221AB. REPAIRED IAW SRM 53-02-00.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND PUNCTURE IN CABIN FLOOR PANEL 262EF. REPAIRED IAW SRM 53-02-00.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND DAMAGE TO FLOOR PANEL 232DF. REPAIRED IAW SRM 53-02-00, SRM 51-77-12, SRM 51-75-12 AND SRM 51-23-11.

Part: BEAM — CRACKED (EMERGENCY EXIT) · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CRACK IN RT AFT EMERGENCY EXIT DOOR AFT SIDE PROFILE BEAM. REPAIRED IAW SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK SUPPORT AT FRAME 66 TO 68 Y765. REPAIRED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND FLOOR SUPPORT Y765, FR68 HAS CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK, FOUND FLOOR PANEL 261FF HAS CORROSION. REPLACED FLOOR PANEL, IAW TASK CARD 2500-6602.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND FLOOR PANEL 221FF HAS CORROSION. REPLACED FLOOR PANEL, IAW TASK CARD 2500-0617.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 51,698 hrs · 22,781 cycles

DURING "H" CHECK FOUND FLOOR PANEL 262FF HAS CORROSION. REPLACED FLOOR PANEL, IAW TASK CARD 2500-6602.

Part: WIRE — BROKEN (CABIN) · airframe 51,661 hrs · 22,767 cycles

EMERGENCY EXIT LIGHT AT ROW 11ABC WAS OUT. FOUND AND REPAIRED A BROKEN WIRE. A/C WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,173 hrs · 18,385 cycles

EMERGENCY LIGHTS AT SEATS 1, 2, 3, 5, 6, 7 INOPERATIVE. REPLACED EPSU AT PSU PANEL 110WL1. CHECKS OK. Â

Part: POWER SUPPLY — FAILED (CABIN) · airframe 41,349 hrs · 17,986 cycles

EMERGENCY ESCAPE LIGHT POWER SUPPLY TEST FAILED AT FLT ATTENDANT PROGRAM TEST PANEL (SYSTEM OK LIGHT WILL NOT COME ON). GROUND SCANNING OF CFDS SHOWED EPSU AFT-LEFT AT FAULT. REPLACED AFT-L EPSU (POWER SUPPLY), CHECKS GOOD. Â

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,324 hrs · 17,975 cycles

OVERWING DOORS L2 AND R2 EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. SYSTEM CHECKS GOOD. Â

Part: SMOKE — DETECTED (COCKPIT) · airframe 39,244 hrs · 17,011 cycles

SMOKE IN COCKPIT WITH ASSOCIATED PRINTER FAIL ANNUNCIATION. CREW PULLED C/B J-21 PRINTER SUPPLY. SMOKE SUBSIDED. MAINTENANCE REMOVED AND REPLACED PRINTER.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 32,881 hrs · 14,175 cycles

During "L" check found corrosion on seat track at BS 765 between frames 18 and 20. Repaired per EA 32-191967.

Part: POWER SUPPLY — FAILED (CABIN)

DURING MAINTENANCE TEST OF EMERGENCY LIGHT SYSTEM, UNIT EMER RT FAULT WAS INDICATED. REPLACED RIGHT EMERGENCY POWER SUPPLY UNIT AND BATTERY, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING INTERMEDIATE LAYOVER VISIT, THE LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED TO SELF TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: EPSU — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE ACCOMPANIED BY EPSU COM EMER R. RIGHT EPSU FAULTING ALL INDICATIONS. REPLACED THE RIGHT EPSU, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE FORWARD LEFT EPSU 10 WL FAILED THE EMERGENCY LIGHTS TEST. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK OK.

Part: ECU — MALFUNCTIONED (NR 2 ENGINE)

DURING DESCENT AT 33,000 FEET, NR 2 ENGINE OVERSPEED OCCURRED. AUTO THROTTLE WAS DISENGAGED, POWER LEVER WAS PULLED BACK, AND ENGINE RPM CONTINUED TO ACCELERATE. ENGINE WAS MANUALLY SHUTDOWN. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BORESCOPE AND ENGINE OVERSPEED INSPECTION REVEALED NO DISCREPANCIES. REPLACED THE NR 2 ENGINE CONTROL UNIT, OPERATIONAL CHECK OK.

Part: ANGLE — CRACKED (BELLY FAIRING)

DURING 'C' CHECK, THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B AND THE LEFT OVERWING SLIDE PACK WAS FOUND CRACKED. THE CRACK EMANATES FROM THE FORWARD MOST EDGE TO THE SECOND FASTENER HOLE APPROXIMATELY 4 INCHES AFT OF THE FORWARD EDGE. REPAIRED PER NWA EA 32-97835.