N335NW

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 91,413 hrs · 42,067 cycles

DURING POWER TRANSFER FROM GPU TO APU, A FEW OXYGEN MASK FELL ON THE REAR OF THE AIRCRAFT. RESTOWED OXYGEN MASK IN RT AFT GALLEY. REF AMM 35-21. (LP: 8031298)

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 91,081 hrs · 41,895 cycles

L1 DOOR EMERGENCY OPERATING CYLINDER PRESS LOW. SERVICED L1 DOOR EMERGENCY OPERATING CYLINDER PER A320 AMM 52-10. NO LEAKS NOTED. (LP: 7661409)

Part: SAFETY VALVE — FAULTED (ZONE 700) · airframe 90,952 hrs · 41,832 cycles

LANDING GEAR FAILED TO EXTEND ON THE FIRST ATTEMPT CYCLED THE GEAR HANDLE PER THE ECAM. IT TOOK 90-120 SECONDS TO START THE EXTENSION. THE PREVIOUS LANDING GEAR EXTENSION IN BDL WAS NORMAL . C/A: T/S PER A320 TSM 32-31-00-810-836-A, NO FAULTS IN EITHER LGCIU 1 OR 2, LANDING GEAR DOORS OPERATED NORMALLY. CHECKED INDUCTANCE OF ALL LANDING GEAR PROX SENSORS PER A320 AMM 32-31-73-820-008-A . ALL WERE WITHIN LIMITS. PER MCC CHANGE L/G SAFETY VALVE 49GA ( WIP 460557). R/R L/G SAFETY VALVE (49GA) REF A320 AMM 32-31. OPS CHECK AND LEAK CHECK GOOD. OK FOR SVC. (LP: 7982544)

Part: ELEC CONNECTOR — CONTAMINATED (ZONE 700) · airframe 90,952 hrs · 41,832 cycles

ON ARRIVAL WHEN THE LANDING GEAR HANDLE WAS SELECTED DOWN. THE GEAR DID NOT EXTENT. AFTER 20 SECONDS THE GEAR HANDLE WAS CYCLED FROM DOWN TO UP, TO DOWN. AFTER 20 SECONDS THE GEAR EXTENDED NORMALLY. T/S IAW TSM 32-31-00-810-808-A. NO PROX SENSOR FAULTS ON PFR. NO DEFECTS DURING INSPECTION. FOUND L/G SAFETY VALVE 49GA CONNECTOR AND RECEPTACLE CONTAMINATED. CLEANED CONNECTOR AND RECEPTACLE. NO FAULTS ON LGCIU 1+2 AND BSCU 1+2. NO ADIRS FAULTS . NOTIFIED MCC. (LP: 7982542)

Part: OXYGEN MASK — DISLODGED (ZONE 200) · airframe 90,915 hrs · 41,814 cycles

OXYGEN MASKS PANEL FELL AT ROW 12DEF. DEFER O2 MASKS AT SEAT ROW 12DEF TO MEL 35-21-01A, M PROCEDURE C/W, INSTALLED PLACARD, A/C OK TO CONTINUE ON MEL. RE-SECURED PANEL DOOR OK FOR SVC PER A320 AMM 25-25. MEL CLEARED / PLACARD REMOVED M PROC REVERSED. (LP: 7982514) / S

Part: LANDING GEAR — MALFUNCTIONED (ZONE 700) · airframe 90,851 hrs · 41,778 cycles

LANDING GEAR RETRACTION SYSTEM. ON APPROACH AT LANDING, GEAR DOWN , NOTHING HAPPEN, AFTER GEAR HANDLE CYCLED LANDING GEAR CAME DOWN AND LOCKED & ALL INDICATIONS NORMAL, DOWN & LOCKED. C/A: MLG & NLG IN DOWN LOCK POSITION PER MEL 32-31-02, VMO TO LG DOWN , NLG PIN & MLG DOWN LOCK DEVICE INSTALLED & SECURED. CYCLED GEAR 10 TIMES PER A320 AMM 32-21. NO DEFECTS NOTED. ( 503183). PERFORMED OPS CHECK OF SAFETY VALVE AT 260 KTS PER A320 AMM 32-31. OPS CHK GOOD. OK FOR SVC. MEL/PLACARD REMOVED. (LP: 7372876)

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 90,828 hrs · 41,765 cycles

ON WALKAROUND POST FLIGHT INSPECTION FOUND NR 1 ENGINE AD EVIDENCE OF A BIRD STRIKE INSIDE THE ENGINE COWLING, ALL ENGINE INDICATIONS NORMAL. C/A: CW AMM 05-51-14 INSPECTION, CLEANED DEBRIS , NO DAMAGE NOTED, DEFER BOROSCOPE INSPECTION ON MON. FOR 25 FLT HR OR 10 FLT CYCLE WISHEVER COME FIRST PER PARA 4-C AMM 72-00-00-200-001-A. REMOVED PLUGS 1,4,8,13,15 AND TURNING PAD FOR BOROREFA320 AMM 72-00. COMPLIED WITH BORESCOPE INSPECTION FOR BIRDSTRIKE ON NR 1 ENGINE, NO RESTRICTIVE DAMAGE FOUND REF AMM 72-00-00-200-001 A. REF LOG 7372885 FOR ONE TIME FOLLOW UP BORESCOPE. REINSTALLED PLUGS 1,4,8,13,15 AND TURNING PAD PER A320 AMM 72-00. (LP: 7372877)

Part: MICROPHONE — INOPERATIVE (ZONE 200) · airframe 90,828 hrs · 41,763 cycles

FO O2 MASK MIC INOP. C/A: R&R'D FO'S 02 BOX OPS CK & LEAK CK GOOD PER AB320 AMM 35-10. (LP: 7372856)

Part: ENGINE — ODOR (NR 1) · airframe 89,820 hrs · 41,227 cycles

SHIP 3235 DISC: AR 2500' ON DEPARTURE DIRTY SOCK ODOR IN COCKPIT. FA DID NOT SMELL ANYTHING. QRH COMPLETED AND IN CONJUNCTION WITH MCC ISOLATED SMELL TO PACK #1. CONTINUED TO DESTINATION WITH PACK 1 OFF. AFTER LANDING TURNED PACK 1 ON AND DIRTY SOCK ODOR CAME BACK. C/A: OPERATED APU WITH NO EVIDENCE OF ODOR. INSPECTED APU COMPARTMENT & INLET WITH BLACKLIGHT, NO DEFECTS NOTED. OPERATED BOTH ENGINES AND CONFIRMED ODOR PRESENT FROM #1 ENGINE WITH NBR 1 PACK ISOLATED, REFERENCE WORKCARD 0550-2002. REQUIRES BORO AS PER W/C 7900-2001(854265). PERFORMED BORO ON #1 ENG HPC PER AMDS WORKCARD 7900-2001. FOUND OIL WETTING IN STAGES 1-6. DID NOT INSPECT FURTHER BACK AFTER CONFERENCE. ENGINE CHANGE REQUIRED. OIL QUANTITY FOR BOTH ENGINES CHECKED AND SATISFACTORY ON ARRIVAL REPLACED #1 ENGINE PER AMDS CARD 7100-9901-LT. PERFORMED ECS BUROUT PER A320 AMM 21-00-00 LEVEL B. MCC NOTIFIED. OK FOR SERVICE. (LP: 7263612)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 89,330 hrs · 40,967 cycles

SHIP 3235 DISC: ADDITIONAL INSPECTIONS ARE REQUIRED PER ER/A 619049-14, REV. A. C/A: COMPLETE SECTION II OF ER/A 619049-14, REV. A. ASSOCIATED ER/A 00-619049 ADDED FOR AC 3235. (LP: 0908232)

Part: BOTTLE — LEAKING (ZONE 800) · airframe 88,357 hrs · 40,471 cycles

SHIP 3235 DISC: ON SERVICE CHECK, FOUND L2 DOOR DAMPER LOW UPON SERVICING FOUND BOTTLE LEAKING NITROGEN. C/A: REMOVED DOOR DAMPER PER A320 AMM 52-13-14. OK TO INSTALL REPLACEMENT DOOR DAMPER QC 5364. INSTALLED DOOR DAMPER PER A320 AMM 52-13-14 UP TO 4B(22), EXCLUDING MEASUREMENTS J1 AND J4 998181. SAFETY AND SECURITY OF THE INSTALL VERIFIED QC 5364. SERVICED BOTTLE, REMOVED SAFETY PIN AND ARMED ASSIST BOTTLE. COMPLETED ALL STEPS OF A320 AMM 52-13-14. RII C/W. (LP: 6909812)

Part: SPAR — CRACKED (ZONE 600) · airframe 88,154 hrs · 40,370 cycles

TRANSFERRED FROM PAPER NON-ROUTINE CRACK FOUND AND VERIFIED BY HFEC ON RH WING AFT SPAR IB OF FLAP TRACK #4. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 007-0001:5957917/001 00001 REPAIRED RH WING AFT SPAR PER PRI 618844-14 REV 0, 1, 2, 3, 4, 5, 6, 7, 8, 9 , 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, AND ER/A 618844-14 SECTION I REV ORIGINAL. REF. LOG 0636715 FOR FOLLOW ON REQUIREMENTS.

Part: FITTING — DAMAGED (ZONE 100) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: LH MLG DOOR ACTUATOR FITTING ON THE KEEL BEAM. THE UPPER AFT FASTENER HEAD HAS SHEARED OFF. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 045-0001:5340-01075-03A/001 00032 REPAIRED PER PRI 619049-14AD REV 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11 AND ER/A 619049-14AD REV ORIGINAL SECTION I. REPAIRED PER PRI 619049-14 AD, REV O,1. (LP: 0650874)

Part: HINGE FITTING — DAMAGED (ZONE 100) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: RH MLG DOOR HINGE FITTING HAS A SHEARED FASTENER. OUTBOARD AFT FASTENER. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 048-0001:5340-01075-04B/002 00031 REPAIRED PER PRI 619053-14AD REV 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14 AND ER/A619053-14AD REV ORIGINAL SECTION I. (LP: 0650878)

Part: OXYGEN MASK — NO TEST (ZONE 200) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: WHILE PERFORMING OPS TEST FOR O2 GENERATOR AND MASK ROBS FOUND SEAT 14DEF MASK DIDN'T DROP. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2000/075 00287 RESET MASK PANEL ADJUSTED DOOR PANEL AND COMPLIED WITH OPS TEST REF. A320 AMM 25-25-43. (LP: 0649220)

Part: NONE — NONE (NONE) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: REF NR #001 INSPECT LH WING REAR SPAR NEAR FLAP TRACK #4 ATTACH POINT AND SUPPORT FITTINGS AROUND RIB 19. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2000/020 00023 COMPLIED WITH PRI 618875-14 REVISION 0,1,2 AND ER/A 618875-14 REVISION ORIGINAL. (LP: 0647619)

Part: SPAR — CRACKED (ZONE 600) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: DTE REQUIRED. ER/A 618844-14 ISSUED FOR CRACK ON THE MIDDLE REAR SPAR LOWER FLANGE BETWEEN RIB 19 AND 20 ON THE RH WING. FOLLOW ON DTE IS REQUIRED. C/A: DTE REQUIRED. SECTION I REPAIR IS LIMITED TO 6 MONTHS. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 00-618844 ADDED FOR AC 3235. (LP: 0636715)

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: DTE REQUIRED FOR REPAIR AND MODIFICATION INSTALLED ON THE LH MLG KEEL BEAM PER ER/A 619049-14AD. C/A: SECTION II IS LIMITED TO 182 DAYS AFTER 17OCT24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. DTA REQUIRED. ASSOCIATED ER/A 00-619049 ADDED FOR AC 3235 (LP: 0614718)

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: DTE REQUIRED FOR REPAIR AND MODIFICATION INSTALLED ON THE RH MLG KEEL BEAM PER ER/A 619053-14AD. C/A: DTE REQUIRED FOR REPAIR AND MODIFICATION INSTALLED ON THE RH MLG KEEL BEAM PER ER/A 619053-14AD. (LP: 0614674)

Part: SKIN — UNKNOWN (ZONE 100) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: A320 / 3235 / FUSELAGE / FR47 / STR10RH / SKIN PANEL & STRINGER / UNDOCUMENTED EXISTING REPAIR / REPLACEMENT ER/A 616897-14 REV. A REQUIRES STAGE 3 DTA APPROVAL. C/A: THIS IS A DTA MONITOR LOG FOR ER/A 616897-14 REV. A WHICH REQUIRES STAGE 3 DTA APPROVAL ON OR BEFORE 41,900 FLIGHT CYCLES OR 83,900 FLIGHT HOURS FROM SECTION I REPAIR EMBODIMENT, WHICHEVER COMES FIRST. ASSOCIATED ER/A 00-616897 ADDED FOR AC 3235. (LP: 0573517)

Part: SPAR SPLICE — UNKNOWN · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: RI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 12 PRIMER APPLICATION OF RH REAR SPAR SPLICE REPAIR PARTS ASSOCIATED ER/A 14-619729 ADDED FOR AC 3235. COMPLIED WITH PRIMER APPLICATION OF RH REAR SPAR SPLICE REPAIR PART(S) IAW PRI 619729-14 STEP 12. PROCESS WAS COMPLIED WITH AT 21:00 5AUG24, 7 HRS. 15 MINS. AFTER COMPLETION OF CHROMIC ACID ANODIZATION PROCESS MEETING TIME REQUIREMENTS OF PMS 01-02-74. (LP: 0481218)

Part: SPAR SPLICE — UNKNOWN · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 10 PRIMING OF RH REAR SPAR SPLICE REPAIR PART. COMPLIED WITH PRIMING OF RH REAR SPAR SPLICE REPAIR PART IAW PRI 619729-14 REV. 4 STEP 10. PROCESS WAS COMPLETED WITH AT 17:30 6AUG24, 9 HRS. 11 MIN. AFTER COMPLETION OF CHROMIC ACID ANODIZATION PROCESS MEETING TIME REQUIREMENTS OF PMS 01-02-74. (LP: 0481214)

Part: SPAR SPLICE — UNKNOWN · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 11 ANODIZATION OF RH REAR SPAR SPLICE REPAIR PART(S). COMPLIED WITH STEP 11 CHROMIC ACID ANODIZATION FOR RH REAR SPAR SPLICE REPAIR PART(S) IAW PRI619729-14 REV 3. PROCESS WAS COMPLETED 13:45 5AUG24. (LP: 0481217)

Part: SPAR SPLICE — UNKNOWN · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 9 ANODIZATION OF RH REAR SPAR SPLICE REPAIR PART. ASSOCIATED ER/A 14-619729 ADDED FOR AC 3235. COMPLIED WITH CHROMIC ACID ANODIZATION OF RH REAR SPAR SPLICE REPAIR PART IAW PRI 619729 REV 4 STEP 9. PROCESS WAS COMPLETED 08:19 6AUG24. (LP: 0481205)

Part: LAVATORY — ODOR (AFT) · airframe 88,054 hrs · 40,308 cycles

SHIP 3235 DISC: FA IN AFT CABIN COMPLAINED OF AN ODOR. COULD NOT BE SENSED IN FRONT OF CABIN OR FLIGHT DECK. C/A: PERFORMED W/C 0550-2002, TYPE 9 MISCELLANEOUS ODOR IN THE AFT CABIN. FOUND AFT LAVS TO HAVE A STINK SMELL, CLEANERS WERE ABLE TO CLEAN & REMOVE SMELL. NO OTHER SMELLS WERE FOUND WHILE PERFORMING W/C. A/C OK FOR SVC. (LP: 5946972)

Part: UNKNOWN — ODOR (CABIN) · airframe 87,712 hrs · 40,126 cycles

SHIP 3235 DISC: HOT/BURNING ELECTRICAL/ PLASTIC SMELL NEAR FWD GALLEY. C/A: T/S PER W/C 0550-2002, FOUND NO BURNING ELECTRICAL OR PLASTIC SMELL ON A/C, CHANGED RECIRT FAN FILTERS, OK FOR SVC, COMPLIED WITH W/C 0550-2002. (LP: 4886914)

Part: NONE — NONE (NONE) · airframe 87,712 hrs · 40,126 cycles

SHIP 3235 DISC: EXISTING REPAIR ON STR10RHS ON FR47 ON UPPER FUSELAG. FUSELAGE / FR47 / STR10RH / SKIN PANEL & STRINGER / UNDOCUMENTED EXISTING REPAIR / REPLACEMENT C/A: C/W ER/A 616897-14AD REV. ORIGINAL. (LP: 0275089)

Part: NONE — NONE (NONE) · airframe 87,684 hrs · 40,111 cycles

SHIP 3235 DISC: *DTE* AT CCK AND WHILE ACCOMPLISHING JC 5331-2032 (ALI 533191) -1) A PREVIOUS, UNIDENTIFIED REPIAR WAS FOUND AT FR47 AND STR10 RHS. REPAIR CONSISTS OF A STRINGER SPLICE REPAIR AND EXTERNAL SKIN DOUBLER REPAIR. C/A: REF ER/A 616897-14, FUSELAGE / FR47 / STR10RH / SKIN PANEL & STRINGER / UNDOCUMENTED EXISTING REPAIR / REPLACEMENT. (LP: 0273577)

Part: SKIN — DAMAGED (RT NR 2 SPOILER) · airframe 87,684 hrs · 40,111 cycles

SHIP 3235 DISC: PERFORATION LOWER SURFACE SPOILER 2 RH WING. REPAIRED LOWER SURFACE ON SPOILER 2 RH WING AS PER A320 SRM TASK 51-77-13-911-001. (LP: 0272870)

Part: FRAME — CRACKED (FRM 66) · airframe 87,681 hrs · 40,110 cycles

SHIP 3235 DISC: CRACK INDICATION ON FRAME 66 RH SIDE DOOR STOOP FITTING 7 HOLE 2 . C RACK DIRECTION 10 0.CLOCK( LOOKING FWD) CRACK DEEP = 0.050 INCH. AA 53 11-01216 AD RELATED ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT . C/A: PERFORMED PERMANENT REPAIR ON HOLE #2 DOOR STOP FITTING #7 FR66 RH SIDE AS PER A320 SRM 53-41-12-300-010.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 87,681 hrs · 40,110 cycles

CORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFACE AS NEGLIGIBLE DAMAGE IAW SRM 51-73-11. PERFORMED ULTRASONIC MEASURE DONE ON REWORKED AREA IAW NTM 51-10-04 MINIMUM REMAINING THICKNESS ARE P1. 0.226 ", P2. 0.204 ", P3. 0.204 ", P4. 0.276 ", P5. 0.276 ", P6. 0.195 ", P7. 0.158, P8. 0.190 ". RECHECK IS NOT REQUIRED DUE TO IS CLASSIFIED AS CAT A. AS PERMANENT.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 87,681 hrs · 40,110 cycles

CORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFACE AS NEGLIGIBLE DAMAGE IAW SRM 51-73-11. PERFORMED ULTRASONIC MEASURE DONE ON REWORKED AREA IAW NTM 51-10-04 MINIMUM REMAINING THICKNESS ARE P1. 0.226 ", P2. 0.204 ", P3. 0.204 ", P4. 0.276 ", P5. 0.276 ", P6. 0.195 ", P7. 0.158, P8. 0.190 ". RECHECK IS NOT REQUIRED DUE TO IS CLASSIFIED AS CAT A. AS PERMANENT.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 87,681 hrs · 40,110 cycles

CORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFACE AS NEGLIGIBLE DAMAGE IAW SRM 51-73-11. PERFORMED ULTRASONIC MEASURE DONE ON REWORKED AREA IAW NTM 51-10-04 MINIMUM REMAINING THICKNESS ARE P1. 0.226 ", P2. 0.204 ", P3. 0.204 ", P4. 0.276 ", P5. 0.276 ", P6. 0.195 ", P7. 0.158, P8. 0.190 ". RECHECK IS NOT REQUIRED DUE TO IS CLASSIFIED AS CAT A. AS PERMANENT.

Part: NONE — NONE (NONE) · airframe 87,681 hrs · 40,110 cycles

EXISTING REPAIR LOC. BTW FR 61 TO FR62 AT LEVEL OF STR 43LH TO STR43RH ON LOWER FUSELAGE. PERFORMED INSPECTION ON EXTERNAL DOUBLER REPAIR #6 LOC. BTW FR 61 TO FR62 AT LEVEL OF STR 43LH TO STR43RH ON LOWER FUSELAGE THEINSTALLATION OF SAID REPAIRS/MODIFICATIONS HAS BEEN LOCATED.TO BE MORE SPECIFIC, THE APPROVAL REFERENCES INSTALLED AS PERAA-2335-01033- 05 / SRM 53-00-11-300-029 ON 06-JULY-2009, ERA607092-14AD,PRI REV:0. REQUIRED INSPECTION THRESHOLD FROM TIME OFADL/REPAIR EMBODIMENT AT 25,000 FC/ 50,800 FH; SUBSEQUENT INSPECTION AT INTERVALS OF 4000 FC/8000 FH AS PER A320 SRI53-00 -11-205-046, STEP 2.A AND TABLE 002. INSPECTION METHOD ( EDDY CURRENT). DECAL MONITOR STABLISHED WITH LOG PAGE XXXXXX JOB IN PROGRESS. (LP: 0250816)

Part: NONE — NONE (NONE) · airframe 87,681 hrs · 40,110 cycles

SHIP 3235 DISC: EXISTING REPAIR LOC. BTW FR59 TO FR61 AT LEVEL OF STR43LHS TO STR43RHS ON LOWER FUSELAGE. C/A: PERFORMED INSPECTION ON EXTERNAL DOUBLER REPAIR LOC. BTW FR59 TO FR61 AT LEVEL OF STR43LHS TO STR43RHS ON LOWER FUSELAGE . THEINSTALLATION OF SAID REPAIRS/MODIFICATIONS HAS BEEN LOCATED.TO BE MORE SPECIFIC, THE APPROVAL REFERENCES INSTALLED AS PERAA-2335-01033- 05; A320 SRM 53-00-11-300-029 ON 06-JULY-09 , ERA607092-14AD,PRI REV:0. REQUIRED INSPECTION THRESHOLD FROM TIME OFADL/REPAIR EMBODIMENT AT 25,000 FC/ 50,800 FH; SUBSEQUENT INSPECTION AT INTERVALS OF 4000 FC/8000 FH AS PER A320 SRI53-00 -11-205-046, STEP 2.A AND TABLE 002. INSPECTION METHOD ( EDDY CURRENT). DECAL MONITOR STABLISHED WITH LOG PAGE XXXXXX JOB IN PROGRESS. (LP: 0250826)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 2C) · airframe 87,424 hrs · 39,978 cycles

SHIP 3235 DISC: O2 MASKS DROPPED ON TAKEOFF SEATS 2C + 2C. C/A: INSPECTED AND STOWED IAW A320 AMM 35-21. (LP: 5438814)

Part: PSU — DAMAGED (SEAT ROW 19EFD) · airframe 87,684 hrs · 40,111 cycles

SHIP 3235 DISC: WHILE WORKING AMDS CARD 2527-01041-02 FOUND PSU OXYGEN DOOR TEST STOP ASSEMBLY BROKEN AT 19 EFD. REPLACED OXYGEN ASSY MASK CONTAINER ON ROW 19 FED IN PASSENGER CABIN, REFER TO LOG N5438812 JOB 159 AS PER SAFRAN CMM 25-28-02 REV NO. 8 PAGE 10095 ITEM 145 FIGURE 1 PAGE 10083. THE INSTALLATION AND TEST IS TO BE ACCOMPLISHED ON AMDS CARD 2527-01042-03-DE STEPS 12, 13 AND 15. JOB COMPLETE. (LP: 5438812)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,690 hrs · 39,605 cycles

SHIP 3235 PASSENGER DEPLOYED MASK AT 32ABC. CORRECTIVE ACTION: RESECURED PANEL PER A320 AMM 35-21. OK FOR SERVICE. (4281756)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,592 hrs · 39,549 cycles

SHIP 3235 O2 MASKS FELL OUT IN ROW 12DEF. RETURNED TO GATE. CORRECTIVE ACTION: RE-PACKED MASKS & REINSTALLED CATCH CORRECTLY. OPS NML PER A320 AMM 25-25. (4558298)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,341 hrs · 38,877 cycles

SHIP 3235 "DOOR R FWD EMER EXIT " ECAM MESSAGE ENROUTE. CORRECTIVE ACTION: SECURED RT FWD EMERGENCY EXIT DOOR COVER IAW A320 25-23 ECAM MSG CLEARED. NO 30 DAYS HISTORY. A/C OK FOR SVC. (4703756)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,341 hrs · 38,877 cycles

SHIP 3235 DOOR R FWD EMER EXIT MSG ON CLIMBOUT. CORRECTIVE ACTION: ADJUSTED PROX SENSOR. OK FOR SERVICE. (4703760)

Part: UNKNOWN — UNKNOWN · airframe 84,945 hrs · 38,649 cycles

SHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14. (2673850)

Part: UNKNOWN — UNKNOWN · airframe 84,945 hrs · 38,649 cycles

SHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14AD REV A. (2673855)

Part: UNKNOWN — UNKNOWN · airframe 84,945 hrs · 38,649 cycles

SHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14. (2673858)

Part: UNKNOWN — UNKNOWN · airframe 84,945 hrs · 38,649 cycles

SHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14AD REV A. (2673863)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 ER/A 606228-14AD REVISION 'A' ISSUED FOR REPAIR PERFORMED AT FR6 8RH AT STOP 1 TO 7. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: INSPECTED. CONTINUE ON MON. (2651649)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 CRACK INDICATION FOUND AT FR 68LH STGR 22. CORRECTIVE ACTION: REPAIRED PER ERA ER/A 606234-14 AND PRI 606234-14. (2651685)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 DURING VISUAL INSPECTION PREVIOUS REPAIR WAS FOUND (REPAIR ANGLE) ON OF THE FR 68 LH AND STG 22. W/C 5311-01244-01A, SB A320-53-1491 R0, EASA PAD 21-090". CORRECTIVE ACTION: REPAIRED PER PRI 606234-14 AND ER/A 606234-14. (2651695)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 DURING VISUAL INSPECTION PREVIOUS REPAIR WAS FOUND (REPAIR ANGLE) ON OF THE FR 68 RH AND STG 22. W/C 5311-01244-01B, SB A320-53-1491 R0, EASA PAD 21-090". CORRECTIVE ACTION: REPAIRED PER ERA 606228-14 AD REV A. (2651504)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 ER/A 606234-14AD ISSUED FOR REPAIR INSTALLED AT FR68 STOP 1 TO STOP 7. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: INSPECTED. CONTINUE ON MON. (2651619)

Part: A/C PACK — ODOR · airframe 84,770 hrs · 38,542 cycles

SHIP 3235 ON CLIMBOUT GOT OILY SMELL IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH DELTA WORK-CARD 0550-2002 AND 7900-2001. OK FOR SERVICE. (9467598)

Part: NONE — NONE · airframe 84,931 hrs · 38,639 cycles

SHIP 3235 COMPLY WITH VA 99348MA. CORRECTIVE ACTION: COMPLIED WITH. (2472169)

Part: NONE — NONE · airframe 83,849 hrs · 38,028 cycles

SHIP 3235 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: READJUSTED DOOR HANDLE POSITION. DOOR LOCKED AND SECURED. OK FOR SVC. (8916270)

Part: NONE — NONE · airframe 83,375 hrs · 37,760 cycles

SHIP 3235 R/H MLG ANCHORAGE FITTING HAS PITTING IN BORE AND FACE AFTER BUSHING REMOVED. CORRECTIVE ACTION: REPAIRED RH MLG RETRACT ACTUATOR ANCHORAGE FITTING PER A320 SRM 57-26-13. (2320870)

Part: ANCHOR FITTING — CORRODED · airframe 83,375 hrs · 37,760 cycles

SHIP 3235 L/H MLG ANCHORAGE FITTING CORROSION. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-23-13. CONTINUE ON MON. (2321601)

Part: ANCHOR FITTING — DAMAGED · airframe 83,375 hrs · 37,760 cycles

SHIP 3235 L/H MLG ANCHORAGE FITTING HAS PITTING IN BORE AND FACE AFTER BUSHING REMOVED. CORRECTIVE ACTION: REPAIRED PER SRM 57-26-13. OK FOR SERVICE. (2321635)

Part: NONE — NONE · airframe 83,375 hrs · 37,760 cycles

SHIP 3235 R/H MLG ANCHORAGE FITTING PITTED AND CORRODED. CORRECTIVE ACTION: REPAIRED FITTING PER A320 SRM 57-26-13-300-008. OK FOR SERVICE. (2320701)

Part: NONE — NONE · airframe 82,393 hrs · 37,195 cycles

SHIP 3235 F/A UNABLE TO ARM DOOR 2L. CORRECTIVE ACTION: CYCLED DOOR, FOUND DEBRIS/TRASH UNDER GIRT BAR. CLEANED AREA AND LUBRICATED GIRT BAR. OK FOR SERVICE. (8001554)

Part: NONE — NONE · airframe 82,185 hrs · 37,096 cycles

SHIP 3235 1L ENTRY DOOR ARMING LEVER HARD TO OPERATE. CORRECTIVE ACTION: FOUND STRAP HANGING FROM SLIDE PACK GETTING IN THE WAY OF LINKAGE. STOWED STRAP. ARMED AND DISARMED DOOR MANY TIMES. OKAY FOR SERVICE. (2094375)

Part: NONE — NONE · airframe 81,765 hrs · 36,893 cycles

SHIP 3235 O2 MODULE DOOR BROKEN AND MASKED DEPLOYED AT 2R DOOR. CORRECTIVE ACTION: R/R AFT GALLEY EMERGENCY O2 MODULE PER A320 AMM 35-21-41. OPS TEST GOOD. (2028759)

Part: NONE — NONE · airframe 81,513 hrs · 36,741 cycles

SHIP 3235 DURING SERVICE CHECK FOUND SEVERAL ROWS EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R AFT LEFT BATTERY PACK PER A320 AMM 33-51. OPS CK GOOD. (8166346)

Part: LIFE VEST — MISSING (SEAT 31ABC) · airframe 80,164 hrs · 36,012 cycles

SHIP 3235 FOUND THREE SPARE LIFE VEST MISSING AT LOCATION 31ABC OH BIN. CORRECTIVE ACTION: INSTALLED 3 EA NEW SPARE LIFE VESTS. OK FOR SERVICE. (6449920)

Part: VHF COMM — INTERMITTENT · airframe 80,129 hrs · 35,988 cycles

SHIP 3235 - ATB - DUE TO ALL VHF COMMUNICATION BEING INTERMITTENT. OTHER AIRCRAFT FAULTS PRESENT INDICATING POSSIBLE ELECTRICAL ISSUE. CORRECTIVE ACTION: FOUND DC ESS BUS SUPPLY CONTACTOR (4PC) BAD AND REPLACED. ALSO REPLACED AC MAIN GENERATION CONTACTORS (11XU1 AND 11XU2) PRECAUTIONARY. AIRCRAFT RTS.

Part: PSU — NO TEST (SEATS 25 DEF) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 25 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665687)

Part: PSU — NO TEST (SEATS 30 DEF) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 30 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665688)

Part: PSU — NO TEST (SEATS 15 DEF) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 15 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665686)

Part: PSU — NO TEST (SEATS 14 DEF) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 14 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665685)

Part: PSU — NO TEST (SEAT 31ABC) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 31 ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665684)

Part: PSU — NO TEST (SEAT 11ABC) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 11 ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665681)

Part: PSU — NO TEST (SEAT 21 ABC) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 21 ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (1766011)

Part: PSU — NO TEST (SEAT 21 ABC) · airframe 79,995 hrs · 35,924 cycles

SHIP 3235 DURING TEST PSU/O2 PANEL IN SEAT 21 ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7665683)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 100 TO INBOARD DIRECTION FROM Y-1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV ORIGINAL. (1763570)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 28 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762987)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 5 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV.0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762740)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIPS 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 28 TO INBOARD DIRECTION FROM - Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762994)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 27 TO INBOARD DIRECTION FROM - Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762999)

Part: DOOR FRAME — CRACKED · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON DOOR STOP FITTING 1 OPEN HOLE 1. CORRECTIVE ACTION: PERFORMED PERMANENT PER A320 SRM 53-41-12. (1762319)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 17 TO INBOARD DIRECTION FROM - Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1763002)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 23 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 00-590132. (1763016)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 14 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1763018)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 16 TO INBOARD DIRECTION FROM - Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV.0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762992)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 8 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV .0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762737)

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FLOOR BEAM +Y1162.5 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (1762761)

Part: FITTING — CRACKED (STOP FITTING) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON DOOR STOP FITTING 2 OPEN HOLE 1 UPPER OUTBOARD. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE ON DOOR STOP FITTING 1, HOLE 4 AT FR.68RH AS PER A320 SRM 53-41-12. (1762817)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 20 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1763012)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 3 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV.0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762743)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 17 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV. 0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762824)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 RH SIDE AT THE CONNECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 5 TO INBOARD DIRECTION FROM Y- 1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV.0,1,2,3,4 AND ERA 590132-14AD REV. ORIGINAL. (1762748)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 LH SIDE AT THE CONECTION OF THE PRESSURE DECK PANEL TO THE CWB IN HOLE 22 TO INBOARD DIRECTION FROM Y1523 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590132-14AD REV.0,1,2,3,4 AND ERA 590132- 14AD REV. ORIGINAL. (1763009)

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON DOOR STOP FITTING 1 OPEN HOLE 4 LOWER INBOARD. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (1762048)

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FLOOR BEAM -Y765 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1762064)

Part: FLOORBEAM — CORRODED (FRM 68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FLOOR BEAM -Y1162.5 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1761969)

Part: STRAP — CRACKED (RT AILERON) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK AILERON STRAP UPPER SURFACE ON RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR DOUBLER ON AILERON STRAP UPPER SURFACE ON RH WING AS PER A320 SRM 57-61-21. (1761736)

Part: DOOR FRAME — CRACKED · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON DOOR STOP FITTING 1 OPEN HOLE 3 LOWER OUTBOARD. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER SRM 53-41-12. (1762051)

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON INTERCOSTAL LOCATED FRAME 16 RIGHT SIDE OF THE DOOR STOP 7 AFFECTED HOLE IS 1. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590358 14AD REV 0 AND ERA 590358 14AD REV ORIGINAL. (1760533)

Part: ATTACH FITTING — GOUGED (LT MLG WW) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 GOUGE ATTACHMENT FITTINGS FWD LUG KEEL BEAM AREA AT LH MAIN LANDING GEAR. CORRECTIVE ACTION: REPLACED ATTACHMENT FITTING PER A320 SRM 517211. (1760520)

Part: DOOR FRAME — CRACKED (FRM 20) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 20 LH DOOR STOP FITTING 7 AREA HOLE C. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590074-14AD PRI REV.0 REV.1 AND ER/A 590074-14AD REV. ORIGINAL. (1761189)

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON INTERCOSTAL LOCATED FRAME 16 LEFT SIDE OF THE DOOR STOP 7 AFFECTED HOLE IS 3. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590355 14AD REV. 0 AND ERA 590355 14AD REV. ORIGINAL. (1760537)

Part: ATTACH FITTING — WORN (RT MLG) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 WEAR ON ATTACHMENT FITTING FWD POSITION KEEL BEAM AREA ON RH MAIN LANDING GEAR. CORRECTIVE ACTION: REPLACED ATTACHMENT FITTING PER A320 SRM 517211. (1760521)

Part: SKIN — DAMAGED (LT WING) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 ELONGATED HOLE CUT OUT FUEL TANK LOC. BTW RIB 15 TO RIB 16 ON LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-21-11-300-002 AND SRM 51-42-11. (1761178)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 OPEN HOLE POSITION 4(-Y254) ZONE 1 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590111-14AD REV.0,1,2 AND ERA 590111-14AD SECTION I REV.ORIGINAL. (1761174)

Part: FRAME — CRACKED (ZONE 100) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 OPEN HOLE POSITION 5 (Y765) ZONE 1 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590111 14AD REV. 0, 1, 2 AND SECTION I ERA 590111 14AD REV. ORIGINAL. (1760542)

Part: FRAME — CRACKED (FWD CARGO) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 ON OPEN HOLE POSITION 2 (Y765) ZONE 1 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI: 590111-14AD. REV: 0,1 AND 2. AND ER/A: 590111-14AD SECTION I REV: ORIGINAL. (1760763)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 ON OPEN HOLE POSITION 2 (Y765) ZONE 2 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI:590111-14AD. REV: 0,1 AND 2. AND ERA: 590111-14AD SECTION I REV: ORIGINAL. (1760766)

Part: FRAME — CRACKED (FRM 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 16 RH SIDE AT THE DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP FITTING 7 ON HOLE NUMBER 6 IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590085-14AD PRI REV.0, PRI REV.2 AND ER/A 590085-14D REV. ORIGINAL. (1761180)

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION LOWER SILL RH SIDE LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 51-72-11. (1761185)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 ON OPEN HOLE POSITION 3 (Y254) ZONE 2 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI: 590111-14AD REV: 0,1 AND 2.AND ER/A: 590111-14AD SECTION I REV: ORIGINAL. (1760767)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 POSITION 5 (Y765) ZONE 1 OF THE BACK AF T SIDE OF THE HORIZONTAL FLOOR BEAM RADII IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590111 14AD REV. 0, 1, 2 AND ERA 590111 14AD SECTION I REV. ORIGINAL. (1760426)

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON INTERCOSTAL LOCATED FRAME 16 RIGHT SIDE OF THE DOOR STOP #7 AFFECTED HOLE IS NO.3. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590358 14AD REV. 0 AND ERA 590358 14AD REV. ORIGINAL. (1760445)

Part: FRAME — CRACKED (FRM 36) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 36 ON OPEN HOLE POSITION 4 (Y254) HOLE 2 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590111 14AD REV.0, 1, 2AND ERA 590111 14AD SECTION I REV ORIGINAL. (1760443)

Part: SKIN — CORRODED (UPPER) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION ADF ANTENNA 2 AREA AROUND HOLES ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590557-14 PRI REV.0 AND ER/A 590557-14 REV.ORIGINAL. (1760386)

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON CONTINUITY FITTING RH LOCATED ON WINDSHIELD FRAMING LOWER CENTER POST FRAME 2 ON COCKPIT WINDOW FRAME. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590052 14AD REV.0 AND ERA 590052 14AD REV.ORIGINAL. 90052 14AD REV.0 AND ERA 590052 14AD REV.ORIGINAL. (1760392)

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 35 AREA ON HOLE H6 AT LEVEL STR 30 LH SIDE IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A: 590106-14AD REV: ORIGINAL AND PRI: 590106-14AD REV. 0, REV 1, AND REV. 2. (1759705)

Part: SKIN — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION INTERNAL STRUCTURE UPPER SKIN CENTER WING BOX LOCATED BTW FR 41 TO FR42 AT LEVEL Y1292 IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590387-14 REV 0, AND ER/A 590387-14 REV. ORIGINAL. (1759697)

Part: INTERCOSTAL — CRACKED (FRM 20) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION FOUND ON INTERCOSTAL LOCATED FRAME 20 LEFT SIDE OF DOOR STOP NO.1. CORRECTIVE ACTION: REPLACED INTERCOSTAL PER PRI 590439-14AD REV.0 AND AS PER ER/A 590439-14AD REV. ORIGINAL. (1759699)

Part: STRINGER — CORRODED (FRAME 56) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION STRINGER 43R AT LEVEL OF FR56 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590406-14 PRI REV.0 AND ER/A 590406 REV.ORIGINAL. (1760382)

Part: FRAME — CRACKED (FRM 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON FRAME 16RH SIDE AT DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP FITTING 7 ON HOLE NUMBER 7 IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590085-14AD PRI REV.O, PRI REV.1 AND PRI REV.2 AND ER/A 590085-14D REV. (1759696)

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK INDICATION ON INTERCOSTAL LOCATED FRAME 16 LEFT SIDE OF THE DOOR STOP NO.7 AFFECTED HOLE IS 1. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 590355 14AD REV. 0 AND ERA 590355 14AD REV. ORIGINAL. (1760433)

Part: ANGLE — CRACKED (FAIRING) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK ANGLE SUPPORT BELLY FAIRING AT LEVEL FR46 RH SIDE KEEL BEAM AREA AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED ANGLE SUPPORT PER A320 SRM 53-35-11 AND SRM 51-42-11. (1758862)

Part: ANGLE — CRACKED (BELLEY FAIRING) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK ANGLE SUPPORT BELLY FAIRING AT LEVEL FR46 KEEL BEAM AREA LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED ANGLE PER A320 SRM 53-35-11. (1759239)

Part: FITTING — CRACKED (FWD CARGO DOOR) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CRACK ON DOOR LOWER AFT CORNER FITTING IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOOR LOWER AFT CORNER FITTING PER A320 SRM 514211. (1759227)

Part: BEAM — BENT (FRAMES 51-52 S44) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 BENT INTERNAL STRUCTURE BEAM BTW FR51 TO FR52 AND LEVEL OF STGR 44 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED BEAM PER A320 SRM 51-72-11. (1755302)

Part: FLOORBEAM — CORRODED (AFT GALLEY AREA) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FLOOR BEAM -Y464.8 AND FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1752100)

Part: DUMMY RAIL — CORRODED (FRMS 12-16) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION RAIL DUMMY -Y1379.5 BETWEEN FR12 TO FR16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED RAIL DUMMY PER A320 SRM 51-72-11. (1752109)

Part: WEB — CORRODED (AFT GALLEY AREA) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION ANGLE WEB FLOOR STRUCTURE LOCATED FR69 TO FR70 AND STR23R AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED ANGLE WEB PER A320 SRM 51-72-11.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,154 hrs · 40,370 cycles

SHIP 3235 DISC: DTA MONITOR INSPECTION LOG REFERENCE ER/A 531233-14 REV B SECTION III REQUIRES DTA APPROVAL ON OR BEFORE 87700 CYCLES AFTER SECTION I ACCOMPLISHMENT. C/A: NOTE THE MONITOR RECORDS / PLANNING. DISCONTINUE REVENUE SERVICE ON OR BEFORE 87700 CYCLES PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-531233 ADDED FOR AC 3235. (LP: 1752495)

Part: FLOOR SUPPORT — DAMAGED (FRAMES 66-68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 ELONGATED HOLE FLOOR BEAM +Y1227 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1751274)

Part: SKIN — SCRATCHED (FRAMES 23-24) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 SCRATCH ON EXTERNAL SKIN STATIC PORT RH SIDE BTW FR23 TO FR24 AT LOWER FUSELAGE. CORRECTIVE ACTION: REWORKED AREA AS PER A320 SRM 51-73-11. OK FOR SERVICE. (1751251)

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION SHEAR PLATE STR 23 L FR69 TO FR70 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE PER A320 SRM 51-72-11-11. (1751271)

Part: BUSHING — CORRODED (RT ELEVTR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 4 ON RH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPAIRED BORES (2E/A) OF HINGE FITTING PER AIRBUS CMM TASK 55-21-15 AND AIRBUS 320 SRM 55-26-41 AND AIRBUS A320 SRM 55-26-41. (1751438)

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION SEAT TRACK -Y1292 BTW FR12 TO FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK PER SRM 51-72-11. (1751261)

Part: ANGLE — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION ANGLE WEB FLOOR STRUCTURE LOCATED FR69 TO FR70 AND STR23L AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED ANGLE PER A320 SRM 51-72-11. (1751263)

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION SHEAR PLATE STR 23 R AND FR69 TO FR70 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE PER A320 SRM 51-72-11. (1751266)

Part: BUSHING — CORRODED (ELEVATOR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 6 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED HINGE FITTING #6 BOTH LUGS PER AIRBUS CMM 55-21-15 AND A320 SRM 55-26-41. (1748510)

Part: FLOOR SUPPORT — DAMAGED (FRAMES 66-68) · corrosion level 2 · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 ELONGATED HOLE FLOOR BEAM -Y1227 BTW FR66 TO FR68 AT AFT GALLEY. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1748504)

Part: BUSHING — CORRODED (ELEVATOR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 6 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED HINGE FITTING #6 PER AIRBUS CMM 55-21-15 AND A320 SRM 55-26-41. (1748512)

Part: BUSHING — CORRODED (ELEVATOR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 1 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED HINGE FITTING #1 I/B LUG PER AIRBUS CMM 55-21-15 AND A320 SRM 55-26-41. (1748507)

Part: BUSHING — CORRODED (ELEVATOR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 3 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED HINGE FITTING #3 BOTH LUGS PER AIRBUS CMM 55-21-15 AND A320 SRM 55-26-41. (1748514)

Part: BUSHING — CORRODED (ELEVATOR HINGE) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION FIXED BUSHING ELEVATOR FITTING HINGE 5 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORES (2E/A) OF HINGE FITTING PER AIRBUS SRM 55-26-41. (1748506)

Part: SLIDE — MISINSTALLED (PAX DOOR) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 IMPROPERLY PACKED SLIDE RAFT PASSENGER CREW DOOR 841. CORRECTIVE ACTION: R AND R SLIDE RAFT PER DELTA WORKCARD AMDS CARD 2561-4002-RF. (1744146)

Part: SEAT TRACK — CORRODED (FWD GALLEY) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 CORROSION SEAT TRACK -Y765 AT LEVEL FR20 AT FWD GALLEY AREA. CORRECTVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11. (1741136)

Part: SKIN — CRACKED (FRAME 24) · airframe 79,611 hrs · 35,724 cycles

DURING ROUTINE MAINTENANCE FOUND A SKIN BULGE AND CRACK NEAR DRAIN PORT AT FS 24 AND STRINGER 44. CORRECTIVE ACTION: ACCOMPLISHED REPAIR, PER ER/A 588926-14.

Part: LIGHT — FAULTED (EXTERIOR) · airframe 77,152 hrs · 34,479 cycles

EPSU FAULT EXT LOAD EMER RT WING AFT EMERGENCY LIGHT ASSY, REPLACED 2EA BULBS.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 76,591 hrs · 34,213 cycles

AFT CARGO DOOR DURING SHOP VISIT INSTALLED OVERSIZED FASTENERS ON FR54 AND FR54A AT THE FORK ENDS AND REPLACED FRAME FORK F53, REPAIRED PER ER/A 574737-14AD SECTION I.

Part: FIRE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 76,243 hrs · 34,055 cycles

(LP# 5225164) FALSE AFT LAVATORY FIRE WARNING. NOBODY IN LAVATORY. NO FAULTS NOTED. OK FOR SERVICE.

Part: SKIN — DENTED (FRAMES 24-24A) · airframe 79,970 hrs · 35,913 cycles

SHIP 3235 FUSELAGE SKIN DENT/GOUGE DAMAGE AT FR24-24A/STR36R. CORRECTIVE ACTION: COMPLIED WITH ER/A 00-564547. (0364656)

Part: BOX BEAM — DAMAGED (RIGHT) · airframe 70,101 hrs · 31,204 cycles

RT SIDE BOX BEAM FLANGE CRACKED AT AFT HOLE. IAW AMDS 5310-01450-01, REPAIR WAS ACCOMPLISHED IAW AMDS 5310-01450-02.

Part: LIGHT — BROKEN (CABIN) · airframe 69,489 hrs · 30,875 cycles

EMERGENCY FLOOR LIGHTS ON SIDE OF SEAT 1C BROKEN. REPLACED EMERGENCY LIGHT ASSY 1C AND 3C.

Part: STRUCTURE — DAMAGED (LT FLAP TE) · airframe 79,611 hrs · 35,724 cycles

DURING WALK AROUND FOUND LT OUTBOARD UPPER FLAP TRAILING EDGE DAMAGED. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-53-00 PARA 8. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,669 hrs · 29,066 cycles

DURING NON ROUTINE CHECK, FOUND AFT CABIN EPSU 13WL IS INOPERATIVE. REPLACED EPSU 13WL AND OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,669 hrs · 29,066 cycles

DURING NON ROUTINE CHECK, FOUND EPSU 12WL IS INOPERATIVE. REPLACED EPSU 12WL AND OPS CHECK WAS NORMAL.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA, FR 20; FLOOR SUPPORT BEAM-Y254 HAS CORROSION. REMOVED & REINSTALLED FLOOR SUPPORT AT -Y254 IAW SRM 51-42-11, BLENDED AREA AT FR 20 -Y254, W=2.0", L=2.0", D=0.010" IAW SRM 51-74-00, TOOL TR 14559, ORIGINAL MATERIAL .149". COMPLIED WITH FINAL ER/A 531230-14, REV "O".

Part: SKIN — UNKNOWN (FRAMES 55-56) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND SKIN IN THE AFT CARGO COMPARTMENT BETWEEN FR 55 & FR56. ACCOMPLISHED REPAIR IAW SRM 53-00-11, FIG 222.

Part: TEE FITTING — CORRODED (EMERGENCY EXIT) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT LEFT SIDE LOWER TEE FITTING CORRODED. REPLACED THE TEE FITTING IAW SRM 51-42-11.

Part: TEE FITTING — CORRODED (EMERGENCY EXIT) · airframe 65,669 hrs · 29,066 cycles

DURIONG INSPECTION, FOUND LEFT AFT EMERGENCY EXIT TEE FITTING CORRODED. REPLACED THE TEE FITTING IAW SRM 51-42-11.

Part: TEE FITTING — CORRODED · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND LEFT FWD EMERGENCY EXIT LEFT LOWER TEE FITTING CORRODED. REPLACED THE TEE FITTING IAW SRM 51-42-11.

Part: WEB — CORRODED (FRAME 20) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA FR 20,FLOOR SUPPORT WEB -Y1732 HAS CORROSION. SSI 531189. BLENDED CORROSION IAW SRM 51-74-00, ORIGINAL MATERIAL 0.071", MATERIAL LOSS 0.024", REMAINING 0.047" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 101. REPLACED FLOOR SUPPORT BATCH 2144824, PART D5311278400301,

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD CARGO PANEL 131FF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 131FF ON VTMAE TRAVELER T15/1122401, DWG NW3B25-37705, INSTALLED ON W/C 2500-5018 FWD CARGO CLOSE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD CARGO PANEL 131HF HAS MULTIPLE PUNCTURES. FABRICATED FLOOR PANEL 131HF ON VTMAE TRAVELER T15/1122403 DWG NW3B25-37705, INSTALLED ON WC 2500-5018 FWD CARGO CLOSE VT MAE.

Part: DOOR SILL — CORRODED (R1 DOOR) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND R1 DOOR SILL HAS CORROSION UNDER GIRT BAR FITTING, FWD. REPLACED DOOR SILL, PN D5311219120306, BATCH 2013603 IAW SRM 51-42-11, AND SRM 51-44-11. BLENDED AREA IAW SRM 51-74-00.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD CARGO PANEL 131AF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 131AF ON VTMAE TRAVELER T15/1122402 DWG NW3B25-37705, INSTALLED ON W/C 2500-5018 FWD CARGO CLOSE VT MAE.

Part: INTERCOSTAL — CORRODED (FRAME 58) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND HIDDEN CORROSION ON LT SEALING PLATE BOTTOM SKIN ATTACHED INTERCOSTAL AT FRAME 58, LT SIDE. FABRICATED ON VT MAE TRAVELER T15/ 1126576 & IAW SRM 53-41-89. REMOVED AND INSTALLED INTERCOSTAL IAW SRM 51-42-11.

Part: FRAME — CORRODED (FRM 66) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND LT AFT UTILITY AREA FR 66 JUST ABOVE DOOR SILL HAS CORROSION, AROUND THE HOLE. REMOVED CORROSION IAW A320-53-41-12, FOUND TO BE OUT OF LIMITS, MATERIAL THICKNESS 0.098", MAT LOSS 0.020", REMAINING 0.078". INSTALLED DOUBLER IAW SRM 51-42-11.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 70,231 hrs · 31,278 cycles

CORROSION AROUND GIRT BAR MOUNT HOLES. REMOVED AND INSTALLED NEW DOOR SILL AND SPLICES IAW SRM.

Part: DOOR SILL — CORRODED (L2 DOORWAY) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND L2 DOOR SILL IS CORRODED. INSTALLED NEW DOOR SILL,STOP CORNER 7 ANGLE SPLICE IAW 51-42-11, 51-21-11, 51-75-12, 51-74-00, 100 MAT LOSS, 53-41-14, FIG 101 AND DWG 53480019.

Part: PANEL — CORRODED (FWD CARGO) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD CARGO ENTRY PANEL 132DF HAS CORROSION. REMOVED CORROSION IAW SRM 51-73-00, L= 4.00", W= 1.00", D= 0.043", TR83340. NO LIMITS FOUND IAW SRM NOTED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-69) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND AFT UTILITY AREA BETWEEN FRAME 66-69, FLOOR SUPPORT BEAM -Y1292 HAS CORROION, S5I 534147, BLENDED AREA AT FRAME 66 IAW TRM 53-41-15 AND SRM 51-74-00. AFTER REWORK: L=2.3",W=1", D=.036", OUT OF LIMIT IAW TRM 53-41-15 MAX DEPTH ALLOWED,.027". REPLACED FLOORBEAM AT FRAME 66-AND 51-42-11, PN=D53472172203.

Part: STRINGER SPLICE — CORRODED (FRAMES 26-27) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD CARGO COMPARTMENT STRINGER SPLICE CORRODED AT FRAME 26/FRAME 27 S-44-0. NO REPAIR LIMITS ON FACTORY STRINGER SPLICE. R & R STRINGER SPLICE IAW SRM 51-42-11. NEW STRINGER SPLICE FABBED ON VTMAE TRAVELER T15/1122311 IAW SRM 53-00-13 AND FILLER IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND LT AFT UTILITY AREA FR68 JUST ABOVE DOOR, DOOR SILL HAS CORROSION, AROUND THE HOLE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12, L=0.95", W=0.75" ORIGINAL MATERIAL 0.098". REMOVED 0.046", REPAIRED FRAME IAW SRM 53-41-12, FIG 201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND CABIN FLOOR PANEL 232 FF HAS A HOLE. FABRICATED A NEW FLOOR PANEL IAW DWG NW3025-37498 AND INSTALLED.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND CABIN FLOORBOARD 231CF HAS HOLE. FABRICATED A NEW FLOORBOARD IAW DWG NW3025-37498 AND INSTALLED ON CARD 2500-6601.

Part: FLOOR PANEL — DAMAGED · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FLOOR PANEL 231 QF HAS FACE SKIN DAMAGE. FABRICATED NEW FLOOR PANEL IAW NW3025-37498.

Part: FLOOR SUPPORT — CRACKED (FRAMES 11-12) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND COCKPIT AREA BETWEEN FRAMES 11 & 12 + Y765 FLOOR SUPPORT CRACKED. REMOVED & REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 20) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA FRAME 20, SEAT TRACK -Y 765 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REPLACED THE SEAT TRACK BETWEEN FRAMES 12-24 IAW SRM 51-42-11 AND TRM 53-21-01.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FRAME 20, FLOORBEAM -Y1292 CORRODED. BLENDED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-11-15, FIG 102. REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND AFT UTILITY AREA BETWEEN FRAMES 66 TO 70 FLOOR SUPPORT -Y765 HAS CORROSION. REMOVED CORROSION IAW SRM 51-22-00, FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED THE FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-21) · airframe 65,669 hrs · 29,066 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 20 - 21 -Y 189 CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 107.

Part: WIRE — LOOSE (CABIN) · airframe 58,474 hrs · 25,685 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY FLOOR PATH LIGHT AT ROW 24C INOPERATIVE. MAINTENANCE SECURED LOOSE WIRE AT ROW 24C AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,444 hrs · 25,670 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT 23C INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,444 hrs · 25,670 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY EXIT LIGHT HAS MANY BURNT LAMPS. MAINTENANCE REPLACED LAMPS AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,374 hrs · 25,639 cycles

DURING NON ROUTINE CHECK, EMERGENCY LIGHT AT 1C FAILED TEST. MAINTENANCE REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORNAL.

Part: FLOOR PANEL — ERODED (CARGO BAY) · airframe 54,237 hrs · 23,769 cycles

AFT CARGO COMPT FLOOR PANEL 161AF IS DELAMINATED AND ERODED AROUND CUT OUT. REMOVED PNL 151AF IAW AMM 53-42-17, PB401. PNL161AF FABRICATED ON TRAVELER T11/880745 IAW DWG 3025-3770; MAT ID: A402AB-60X144 BATCH: 1886727. INSTALLED 161AF IAW AMM 53-42-17, PB401.

Part: FLOOR SKIN — CRACKED (CABIN) · airframe 54,237 hrs · 23,769 cycles

AFT CARGO COMPT FLOOR PANEL 151GF HAS CRACKS AND MULTIPLE DENTS ON UPPER SKIN. REMOVED PNL 15GF IAW AMM 53-42-14, PB 401. FABRICATED NEW ON STAM TRAVELER T11/880729 IAW DWG 3025-3770, MAT ID A402AB-60X144, BATCH 1886727. INSTALLED 151GF IAW AMM 53-42-14PB401.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,533 hrs · 23,491 cycles

CORROSION AT SEAT TRACK FLANGE, RBL "60" INBD OF FRAME 20 RT CORROSION REMOVED & CONTAINED, CUTOUT DAMAGE, FABRICATED,REPAIR ANGLE FROM .080 7075-0 HEAT TREATED. DRILLED, TRIMMED & DEBURRED. TREATED & PRIMED & INSTALLED IAW 53-11-15. REQUIRED INSP COMPLETE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 2,522 hrs · 1,091 cycles

DURING EMERGENCY LIGHT TEST FOUND ROW 5C PATH LIGHT INOPERATIVE, REPLACED BROKEN CONNECTOR AND TESTS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 52,547 hrs · 23,049 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT ROW 22L AND 25L INOPERATIVE. MX REPLACED BLACK WIRE AT JIFFY AND PERFORMED SUCCESSFUL TEST. ACFT RETURNED TO SERVICE.

Part: EPSU — DISCHARGED (CABIN) · airframe 49,406 hrs · 21,781 cycles

EPSU TEST FAULTED THE OVERWING ESCAPE SLIDE LIGHT SW/EPSU. REPLACED EPSU AND TESTED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 44,131 hrs · 19,421 cycles

DURING GROUND OPERATIONS FUSELAGE SKIN WAS DENTED AND GOUGED BETWEEN STRINGER 34 TO 38 FRAMES 19 TO 24. REPAIRED PER EA 32-211270.

Part: SKIN — GOUGED (FUSELAGE) · airframe 44,131 hrs · 19,421 cycles

DURING GROUND OPERATIONS FUSELAGE SKIN WAS GOUGED ON FORWARD SIDE OF CARGO DOOR OPENING AT STA C24-C24A BETWEEN STRINGERS 36R-37R. REPAIRED PER EA 32-211163.

Part: FAN — FAILED (CABIN) · airframe 35,719 hrs · 15,537 cycles

DURING CRUISE, PILOTS EXPERIENCED SLIGHT SMOKE AND BURNING ODOR. DIVERTED TO DES MOINES AND LANDED UNEVENTFULLY. INSPECTED CABIN, AVIONICS BAY, AND CARGO BAYS AND FOUND NO DEFECTS. FOUND LEFT CABIN FAN SUPPLY CIRCUIT BREAKER POPPED AND LEFT FAN INDICATION IN THE COND PAGE. APPLIED MEL PROVISIONS FOR LEFT CABIN FAN. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN)

DURING TEST OF EMERGENCY LIGHTS, FOUND ESCAPE PATH LIGHTS INOPERATIVE ON LAST THREE SEAT ROWS. MAINTENANCE REPAIRED BROKEN WIRE AT SIDEWALL CONNECTOR. OPERATIONAL CHECK OK.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR)

DURING ROTATION, RECEIVED FORWARD CARGO DOOR OPEN AND MASTER CAUTION WARNING. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. DOOR INDICATION RETURNED TO NORMAL AFTER CLEARING RUNWAY. MAINTENANCE PERFORMED ADJUSTMENT OF THE FORWARD CARGO DOOR PROXIMITY SENSOR, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE CHECK, FOUND BOTH AFT DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED LEFT AFT EPSU. OPERATIONAL CHECK OK.

Part: FAN — SEIZED (AVIONICS BAY)

DURING APPROACH AT 7,000 FEET, CREW NOTED A BURNING SMELL IN COCKPIT FOLLOWED FIVE MINUTES LATER BY A VENT EXTRACT FAULT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AVIONICS COOLING EXTRACT FAN SEIZED. REPLACED SAME, OPERATIONAL CHECK OK.

Part: BSCU — MALFUNCTIONED (AVIONICS COMPT.)

DURING TAXI IN AT THE GATE, THE BRAKES DID NOT RESPOND. USED ENGINE THRUST REVERSE TO STOP AIRCRAFT SAFELY AT THE GATE. THE BRAKES GRABBED AS THE AIRCRAFT CAME TO A STOP. MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT. OPERATIONAL CHECK OK.