N348NW

Part: UNKNOWN — ODOR (CABIN) · airframe 94,631 hrs · 44,243 cycles

FLT ATTENDANTS REPORTED A DIRTY SOCK SMELL COMING FROM THE CABIN VENTS WITH APU BLEED ON. ACCOMPLISHED ON LOG #1291912. (LP: 7845300)

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 94,104 hrs · 43,937 cycles

EMERGENCY LIGHTS FLICKERING IN THE CABIN DURING FLIGHT WITH SWITCH IN THE ARMED POSITION. PERFORMED BITE TEST IAW AMM 23-73, NO FAULTS NOTED. PERFORMED OPS TEST IAW AMM 33-51. NO FAULTS NOTED. NO 60 DAY HISTORY OK FOR SVC. (LP: 7615641)

Part: UNKNOWN — ODOR (CABIN) · airframe 92,983 hrs · 43,357 cycles

SHIP 3248 DISC: FUMES EVENT AT FL370 ONLY APPARENT BETWEEN ROWS 28-31 RAN QRH PACK 1 OFF THENON W/ NO CHANGE PACK 2 OFF & FA REPORTED IMPROVEMENT TO FUME SMELL. C/A: PERFORMED TYPE 9 INSPECTION PER JIC 0550-2002, REF SMOKE AND FUME SURVEY. INSPECTED OVERHEAD BINS AND LIGHTS, PSU'S + IFE EQUIP. NO TROUBLE FOUND. PER FLIGHT CREW REPORT MOST LIKELY CAUSE IS CARRY ON BAGGAGE. MCC NOTIFIED. A/C OK FOR SVC. (LP: 6988519)

Part: A/C PACK — FAULTED (ZONE 100) · airframe 92,323 hrs · 43,028 cycles

SHIP 3248 DISC: @ FL360 ECAM MSG A/THR OFF -WE TURN IT OFF,PACK 1+2 FAULT ECAM MSG WITH CABIN ALT GOING UP,EMER DESCENT INITIATED O2 MASK AND USED PACK1+2 LIGHTS FLASH ON OVERHEAD PANEL,PACK1 RESET IT DID NOT HELP,BETWEEN FL280-240 WHOLE SYSTEM RESET ITSELF,AND STARTED TO WORK ,WE LEVEL OFF AT FL200AFTER TALKING TO MCC,OCC WE CONTINUED TO OMA AND CLIMB TO FL300,THE REST OF THE FLIGHT WAS NORMAL,AT THE GATE IN OMA WE HAD ENG2 FADEC MX MSG II CAT MSG. C/A: T/S PER TSM 73-25.R/R`D EIU-2 PER AMM 73-25-34,AND RELAY 16HB PERFORMED 1+2 ENGINE RUN ALL NORMAL,O2 MASK STOWED AND AT 1300 , C/W MD LOG 08111222,MCC NOTIFIED OK FOR SVC. (LP: 6102908)

Part: ECU — FAULTED (NR 2 ENGINE) · airframe 92,316 hrs · 43,025 cycles

SHIP 3248 - DIV - TO ORD DUE TO ENG 2 EIU FAULT AND AIR BLEED ECAM MESSAGE, FOLLOWED BY CAB PR EXCESS CAB ALT AND AIR PACK 1 FAULT AND AIR PACK 2 FAULT. CORRECTIVE ACTION: REPLACED #2 ENGINE ECU. OK FOR SERVICE. (LP 6821996)

Part: CABIN PRESSURE — ABNORMAL (ZONE 200) · airframe 92,323 hrs · 43,028 cycles

SHIP 3248 DISC: DIVERSION LOSS CABIN PRESSURE AND PACK 1/2 FAULTS LEADS TO TSM 73-20-00-810-848-A PLEASE ACCOMPLISH THIS TSM AND PACK 1/2 OPERATIONAL TEST OF PACK 1/2 FLOW CONTROL VALVES REF AMM 21-51-00-710-002-A. C/A: FAULTS 732534. R/R #2 ENG ECU. REF A320 AMM 73-21. CHECKS GOOD. PERFORMED FLOW CONTROL AND IND SYS OPS TEST. REF A320 AMM 21- 51. CHECKS GOOD. C/W ODI W/C 0550-9001-A320FAM. PERFORMED BMC1/2 BITE. REF A320 AMM 36-11. TESTS PASSED. PERFORMED EIU1/2 OPS TEST. REF A320 AMM 73-25. NO FAULTS. A/C OK FOR SVC. (LP: 0808938)

Part: SELECTOR VALVE — FAULTED (ZONE 700) · airframe 92,305 hrs · 43,017 cycles

SHIP 3248 - GEAR/DE - DUE TO LANDING GEAR NOT DOWN AND LOCKED MESSAGE WHEN GEAR EXTENDED FOR APPROACH. MANUAL GEAR EXTENSION PERFORMED. CORRECTIVE ACTION: PREFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR. OPERATIONAL GOOD PER A320 AMM 32-31. REPLACED LANDING GEAR SELECTOR VALVE 40GA AND 62GA. (LP 6821980, 0805678)

Part: SHOCK ABSORBER — DISCHARGED (ZONE 700) · airframe 92,291 hrs · 43,008 cycles

SHIP 3248 - GEAR/ATB - DUE TO A L/G SHOCK ABSORBER FAULT THAT PREVENTED GEAR RETRACTION. CORRECTIVE ACTION: ACCOMPLISHED A FULL SERVICE OF THE NLG SHOCK STRUT. NLG 24GA AND 25GA PROXIMITY SENSORS REPLACED AS A PRECAUTION. (LP: 6821962)

Part: ACTUATOR — EXCESS PLAY (ZONE 300) · airframe 92,291 hrs · 43,008 cycles

SHIP 3248 DISC: DO NOT PASS FREE PLAY CHECK ON I/B ACTUATOR ELEVATOR RH SIDE ( THE DIMENSION BETWEEN BOTH POINTS FOUND OUT OF LIMITS. C/A: PERFORMED INSPECTION CHECK, FOUND WITHIN LIMITS OF I/B SERVO CONTROL P/N:31075-840 S/N:7229 RH ELEVATOR AND INSTALL, DEFLECTIONCHECK AS PER AA CARD 2734-01003-07 AND A320 FAM AMM 27 -34-51-200-001 , DEFLECTION CHECK FOUND OK DEFLECTION VALUE IS: 0.2188 IN(5.5 MM) TOOL USED: CHECK TOOL PN: M7316-5 SN: 98D2730300301 DUE DATE: 05-MAY-25, FORGE GAUGE PN: LG-100 SN: R18248 DUE DATE:16-DEC-25, DEPTH GAUGE PN:8645A12 DUE DATE 16- APR-25 RII INSPECTION COMPLETE 1715948 (AE403QC) JOB COMPLETE. (LP: 0796509)

Part: DAMPER — MALFUNCTIONED (ZONE 800) · airframe 92,290 hrs · 43,007 cycles

SHIP 3248 DISC: DONT WORK CORRECTLY DAMPER AT PASSENGER CREW DOOR 831. C/A: REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FROM PASSENGER CREW DOOR 831 ON UNSERVICEABLE CONDITION. REPLACED DAMPER PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52- 11-14-000-001-A AND A320 FAM AMM 52-11-14-400-001-A. LEAK CHECK GOOD. RII INSP C/W. JOB COMPLETE. (LP: 0783148)

Part: DAMPENER — INOPERATIVE (ZONE 800) · airframe 92,290 hrs · 43,007 cycles

SHIP 3248 DISC: DONT WORK CORRECTLY DAMPER PASSENGER CREW DOOR 832 (REFERENCE RII AMDS CARD 5210-7089-LA) AT AFT GALLEY AREA. C/A: REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FROM PASSENGER CREW DOOR 832 ON UNSERVICEABLE CONDITION PN: FE174-004 ,SN: 499 AS PER A320 FAM AMM 52-13-14-000-001-A STEP 3 C,D,AND 4A. (LP: 0781351)

Part: UPLOCK — FAULTED (ZONE 700) · airframe 91,127 hrs · 42,371 cycles

SHIP 3248 - ATB - DUE TO A KNOCKING NOISE FROM THE NOSE GEAR AREA. CORRECTIVE ACTION: R/R NLG UPLOCK ASSEMBLY (2530GM). OPS CHECK GOOD.(LP: 5137432)

Part: DOOR — LOOSE (NLG) · airframe 91,127 hrs · 42,370 cycles

SHIP 3248 - ATB - DUE TO VIBRATIONS IN THE NOSE AREA. CORRECTIVE ACTION: FOUND BOTH AFT NLG DOOR ASSEMBLIES LOOSE AT FITTINGS. R/R NLG AFT DOORS GIMBAL ASSEMBLY JOINTS. OPS CHECK GOOD.

Part: MANIFOLD — FAULTED (YELLOW HYD SYS) · airframe 90,997 hrs · 42,293 cycles

HYD Y RSRV OVERHEAT MESSAGE ON CLIMB OUT. T/S PER A320 TSM 29-3-00-810-802-A. LT Y SYS E PUMP RUNNING FOR 20 MINS. RCVD Y SYS OVHT FAULT. FOUND Y SYS OVERSERVICED BY 1 GALLON. DRAINED ALL FLUID AND R/R TEMP TRANSM SWITCH 3381GR. OPS TEST FAILED. INSTALLED IS BORROWED UNIT. CONT T/S PER TSM 29-13-00-810-802-A. REMOVED CHECK VALVE AND INSPECTED W/ NTF REINSTALLED SAME. REMOVED LP FILTER. INSPECCTED. W/ NTF REPLACED SAME AS PERCAUTION. REMOVED HP FILTER. FOUND FILTER W/ HEAVY DEBRIS. IAW AMM 29-13 L FILTER WILL REQ LEAK CHK. REMOVED AND REPLACED YELLOW HYD SYS HP MANIFOLD IAW AMM 29-13. WILL REQ LEAK CHK. C/W LEAK CHK OF HP MANIFOLD YELLOW SYS. NO LEAKS NOTED PER A320 AMM 29-13.

Part: SKIN — DAMAGED (RUDDER) · airframe 90,255 hrs · 41,914 cycles

SHIP 3248 DISC: RUDDER T/E AND I/B FLAP LOWER SURFACE DAMAGE BY LIGHTNING STRIKE. C/A: ACCOMPLISHED ER/A 617122-14 REV O SECTION I: TIME LIMITED REPAIR. (LP: 5346634)

Part: SKIN — DAMAGED (FRM 3) · airframe 90,199 hrs · 41,884 cycles

SHIP 3248 DISC: BURN MARK AT FR 3 LH FUSELAGE. C/A: REMOVED FASTENER REF A320 SRM 51-42-11(473292). PERFORMED BHEC ON REMOVED FASTENER HOLE. NO DEFECTS NOTED. REF A320 NTM 51-10- 01.(QC5350). INSTALLED PERMANENT REPAIR REF A320 SRM 53-11-11. (LP: 0276181)

Part: RADOME — DELAMINATED (NOSE) · airframe 90,199 hrs · 41,884 cycles

SHIP 3248 DISC: DURING LIGHTNING STRIKE INSPECTION FOUND DELAMINATION ON RADOME. C/A: MEASURED DELAMINATED AREA TO BE 2.2" IN ZONE A OF RADOME. PERFORMED TEMPORARY REPAIR WITH POLYURETHANE TAPE PER A320 AMM 53-15-11. PLACED RADOME REPLACEMENT ON MON FOR 600FH FROM FLT 1393 ON 02APR24 IN ORD. (LP: 5346633)

Part: SKIN — DAMAGED (FRM 6) · airframe 90,199 hrs · 41,884 cycles

SHIP 3248 DISC: BURN MARK JUST FWD OF FR 6 LH FUSELAGE C/A: 473292 W REPAIRED BURN MARK JUST FWD OF FR 6 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICHEVER COMES FIRST. CATEGORY C REPAIR. (LP: 0276199)

Part: SKIN — DAMAGED (FRM 5) · airframe 90,199 hrs · 41,884 cycles

SHIP 3248 DISC: BURN MARK JUST AFT OF FR 5 LH FUSELAGE. C/A: REMOVED FASTENER REF A320 SRM 51-42-11(43292). C/A: REMOVED FASTENER REF A320 SRM 51-42-11(473292). PERFORMED BHEC ON REMOVED FASTENER HOLE. NO DEFECTS NOTED. REF A320 NTM 51-10- 01.(QC5350). INSTALLED PERMANENT REPAIR REF A320 SRM 53-11-11. (LP: 0276192)

Part: SKIN — DAMAGED (FRM 5) · airframe 90,199 hrs · 41,884 cycles

SHIP 3248 DISC: BURN MARK JUST FWD OF FR 5 LH FUSELAGE. C/A: REPAIRED BURN MARK JUST FWD OF FR 5 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICH EVER COMES FIRST. CATAGORY C REPAIR. (LP: 0276183)

Part: SKIN — DAMAGED (FRM 6) · airframe 90,198 hrs · 41,883 cycles

SHIP 3248 DISC: BURN MARK JUST AFT OF FR 6 LH FUSELAGE. C/A: REPAIRED BURN MARK JUST AFT OF FR 6 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICHEVER COMES FIRST. CATEGORY C REPAIR. (LP: 0276206)

Part: DOOR FRAME — DAMAGED (R2) · airframe 89,608 hrs · 41,562 cycles

SHIP 3248 DISC: AD RELATED (AA5311-01216) R2 DOOR STOP #3 AT FR66 2EA. HOLE EXCEEDING LIMIT. HOLE #1&2. C/A: FR66 R/H DOOR STOP FITTING NO 3, 4 EA FASTENER HOLES COLD WORKED AND OVERSIZED TO 0.281" IAW A320 SRM 53-41-12-300-008, 53-41-12 -300-009, NTM 51-10-01, 51-10-08. FINAL REPAIR ACCOMPLISHED ON NR 14845.0132, 14845.0133, 14845.0134, PER ERA 615149-14AD REV O JOB COMPLETE. (LP: 0160635)

Part: DOOR FRAME — DAMAGED · airframe 89,608 hrs · 41,562 cycles

SHIP 3248 DISC: AD. RELATED (AA5311-01216) R2 DOOR STOP #1 AT FR66 4 EA. HOLE EXCEEDING LIMIT. C/A: FR 66 R/H STOP FITTING #1 4EA HOLES COID WORKED AND OVERSIZED TOM.281 IAW A320 SRM 53-41-12-300-009, 53-41-12-300-008, 51-48- 00-801, NTM 51-10-01, 51-10-08 REPAIR CAT B, REQUIRES INSPECTION WITH A THRESHOLD FROM ADL/REPAIR EMBODIMENT OF 56600 FC (FH NOT RELEVANT) WITH SUBSEQUENT INSPECTION AT INTERVALS OF 18600 FC ( FH NOT RELEVANT) PER SRM 53-41-12-205-00/8 JOB COMPLETED. (LP: 0160794)

Part: DOOR FRAME — DAMAGED (L2) · airframe 89,608 hrs · 41,562 cycles

SHIP 3248 DISC: AD RELATED(AA5311-01216) L2 DOOR STOP #3 AT FR66 4EA HOLE EXCEEDING LIMIT. C/A: FR 66 L/H DOOR STOP #3 4EA HOLES COLD WORKED AND OVERSIZED TO .281 IAW A320 SRM 53-41-12-300-009, 53-41-12-300-008, 51-48-00- 801 NTM 51-10-01, 51-10-08. FNAL ERA ACCOMPLISHED ON N/R: 14845- 0100, 14845.0099, 14845.0099, 14845.0098, 14845.0097. PER ERA 615149-14AD JOB COMPLETED. (LP: 0160726)

Part: DOOR FRAME — DAMAGED (R2) · airframe 89,608 hrs · 41,562 cycles

SHIP 3248 DISC: AD RELATED (AA 5311-01216) R2 DOOR STOP #6 AT FR66 2 EA HOLE EXCEEDING LIMIT. HOLE #1 & 3. C/A: FR 66 DOOR STOP FITTING NO. 6, 4EA FASTENER HOLES COLD WORKED AND OVERSIZED TO 0.281" IAW A320 SRM 53-41-12-300-008, 53-41-12- 300-009, NTM 51-10-01, 51-10-08. FINAL REPAIR ACCOMPLISHED ON N/ R 148456-0117, 14845-0118 PER ER/A 615149-14AD REV ORG. JOB COMPLETE. (LP: 0160669)

Part: STOP FITTING — OUT OF LIMITS (L2 DOOR) · airframe 89,621 hrs · 41,570 cycles

SHIP 3248 DISC: AD. RELATED (AA5311-01216) L2 DOOR STOP #1 AT FR66 4 EA. HOLE EXCEEDING LIMIT. C/A: FR 66 L/H DOOR STOP #1 4EA HOLE COID WORKED AND OVERSIZED TO .281 IAW A320 SRM 53-41-12-300-008, 53,41-12-300-009, 51-48-00- 801, NTM 51-10-01-51-10-08 SRM 53-41-12-205-008 REPAIR CAT B REQ INSOECTION WITH A THRESHOLD FROM ADL/REPAIR EMBODIMENT OF 56600 FC (FH NOT RELEVANT) WITH SUBSEQUENT INSPECTION AT INTERVAL OF 18600 FC (FH NOT RELEVANT) PER A320 SRM 53-41-12-205-008 JOB COMPLETED. (LP: 0160597)

Part: DOOR FRAME — DAMAGED (R2) · airframe 89,608 hrs · 41,562 cycles

SHIP 3248 DISC: AD. RELATED (AA5311-01216) R2 DOOR STOP #5 AT FR66 1 EA. HOLE EXCEEDING LIMIT. HOLE#2. C/A: FR66 R/H DOOR STOP FITTING NO.5, 4E A FASTENER HOLES COLD WORKED AND OVERSIZED TO 0.281 IAW A320 SRM 53-41-12-300-0 08, 53-41-12-300-009, NTM 51-10-01, 51-10-08. FINAL REPAIR ACCOMPLISHED ON N/R: 14845.0139, 14845.0138 PER ERA 615149-14AD REV ORG, JOB COMPLETE. (LP: 0160625)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,111 hrs · 41,315 cycles

SHIP 3248: ROW 29 DEF OXYGEN MASK DOOR OPENED IN FLIGHT DROPPING MASKS. CORRECTIVE ACTION: REPACKED PER A320 AMM 35-23. (LP 4864600)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,208 hrs · 40,833 cycles

SHIP 3248 FR 68, RHS/FRAME FLANGE CRACK, NEAR DOOR STOP #1. CORRECTIVE ACTION: COMPLIED WITH ERA 605147-14AD REV A SECTION II. (2865043)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,208 hrs · 40,833 cycles

SHIP 3248 NEED TO COMPLY WITH ERA 605147-14AD REV A SECTION V (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA 605147-14AD REV A SECTION V. (2865061)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,208 hrs · 40,833 cycles

SHIP 3248 NEED TO COMPLY WITH ERA 605147-14AD REV A SECTION IV. (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA 605147-14AD REV A SECTION IV. (2865058)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,208 hrs · 40,833 cycles

SHIP 3248 NEED TO COMPLY WITH ER/A 605147-14AD REV A SECTION III. (CRACK). CORRECTIVE ACTION: COMPLIED WITH ER/A 605147AD REV A SECTION III. (2865054)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,147 hrs · 40,801 cycles

SHIP 3248 A320/WINGS/LH ANCHORAGE FTG/LUG CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 605165-14AD REV A. (2852490)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,657 hrs · 40,527 cycles

SHIP 3248 - ATO - AT 40 KTS DUE TO PARK BRK ECAM MESSAGE. CORRECTIVE ACTION: R/R PARKING BRAKE ELECTRICAL CONTROL VALVE (72GG) AND SDAC-1 (1WV1). OPS CHECK GOOD. (9642584)

Part: FRAME — CRACKED (FRM 68 S22R) · airframe 86,736 hrs · 40,029 cycles

CRACK ON RH FR68, BELOW STR22 HORIZONTAL FLANGE RADII. COMPLIED WITH PRI 605147-14AD REV 0, REV 1, AND ERA 605147-14AD REV 0.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 86,745 hrs · 40,033 cycles

FWD LEFT EPSU FAULTING "EPSU INT LOAD FWD L. REMOVED AND REPLACED FWD L EPSU 10WL PER A320 AMM 33-51-38, OP'S CHECK GOOD.

Part: TRUNNION — CORRODED (NLG) · airframe 86,736 hrs · 40,029 cycles

PITTING ON RH NLG TRUNNION FITTING, INBD FACE. REPAIRED PER PRI 605148-14 REV 0, AND REV 1. ER/A 605148 REV ORIGINAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,208 hrs · 40,833 cycles

SHIP 3248 NEED TO ACCOMPLISH ERA 605147-14AD SECTION I (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA 605147-14AD SECTION 1. (2583816)

Part: TRUNNION — CORRODED (NLG) · airframe 86,736 hrs · 40,029 cycles

NLG AFT TRUNNION BUSHINGS ARE PITTED. REPAIRED PER A320 SRM 51-72-12. OK FOR SERVICE.

Part: TRUNNION — CORRODED (NLG) · airframe 86,736 hrs · 40,029 cycles

PITTING ON LH NLG TRUNNION FITTING, INBD FACE. COMPLIED WITH PRI 605145-14 REV 0, AND REV 1, AND ERA 605145-14 REV 0.

Part: NONE — NONE · airframe 85,335 hrs · 39,199 cycles

SHIP 3248 DAMAGE AT FR35 BULKHEAD AND STR - 30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595693-14AD. OK FOR CONTINUED SERVICE. (2269653)

Part: NONE — NONE · airframe 85,325 hrs · 39,195 cycles

SHIP 3248 ER/A 595693-14AD WAS ISSUED FOR DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA. (2269659)

Part: NONE — NONE · airframe 85,325 hrs · 39,195 cycles

SHIP 3248 ER/A 595693-14AD WAS ISSUED FOR DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA. (2269667)

Part: NONE — NONE · airframe 84,459 hrs · 38,649 cycles

SHIP 3248 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: REPLACED LENS COVER. OK FOR SERVICE. (2142391)

Part: NONE — NONE · airframe 84,459 hrs · 38,649 cycles

SHIP 3248 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: REPLACED LENS COVER. OK FOR SERVICE. (2142392)

Part: NONE — NONE · airframe 84,459 hrs · 38,649 cycles

SHIP 3248 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: REPLACED LENS COVER. OK FOR SERVICE. (2142390)

Part: COVER — UNSECURE (DOOR SLIDE) · airframe 84,028 hrs · 38,407 cycles

SHIP 3248 ON DESCENT INTO ATL RIGHT FWD EMER EXIT ILLUMINATED. CORRECTIVE ACTION: SECURED SLIDE ACCESS COVER INDICATION NORMAL PER TSM 5221. OK FOR SERVICE. (8237528)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 WEAR ON FITTING KEEL BEAM FWD ATTACHMENT DOOR FWD LUG FWD FACE RH SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH PRI 595828-14AD REV 0. (2075428)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INBOARD THRUST REVERSER LOC. AT 3 OCLOCK PIVOT FITTING UPPER FLAGE ON ENGINE 1. CORRECTIVE ACTION: COMPLIED WITH CMM REPAIR 87 78-32-35 AND ER/A 596072-14AD REV. ORIGINAL. (2075278)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 WEAR ON FITTING KEEL BEAM ACTUATOR ATTACHMENT FWD LUG FWD FACE IN MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH PRI 595828-14AD REV 0. (2075418)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 43R LOC. BTW FR 31 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073931)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK PROFILE LOCATED BTW FR 50 TO FR 54 LEVEL STR 35L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A #559065-14MA REV. ORIGINAL (2073939)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 43L BTW FR32 AND FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073932)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE STRAP LOCATED AT FR 67 BTW STR 27L TO STR 28L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596106-14AD REV ORIGINAL. (2074183)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FRAME 67 SUPPORT ANGLE LOCATED BTW STR42R TO STR42L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE PER A320 SRM 51-72-11. (2074120)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 35 LH SIDE AT OPEN FASTENER HOLE COMMON TO BULKHEAD AND MILLED COUPLING H6. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074200)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER SPLICE LOCATED STR26R AT LEVEL FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER SPLICE PER A320 SRM 51-72-11. (2074229)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 38R BTW FR 32 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: FOUND AREA WITHIN LIMITS. CONTINUE ON MON. (2073933)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 35 BULKHEAD TO SKIN ATTACHMENT AREA LH SIDE AT OPEN FASTENER HOLE H16. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074203)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 41R LOC.BTW FR 32 AND FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2072435)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE SUPPORT ANGLE LOCATED BTW FR 56 TO FR 57 AND STR 42L TO STR 43L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: R/R INTERNAL STRUCTURE SUPPORT ANGLE PER A320 SRM 51-72-11. (2072880)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 WEAR ON UPPER SPAR WEB RH SIDE CANTILEVER ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 596055-14 REV ORIGINAL. (2073069)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 68 LH DOOR STOP FITTING HOLE 1. CORRECTIVE ACTION: REPAIRED PER ER/A 596000-14AD REV. ORIGINAL. (2072462)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR STRUCTURE WEB BTW FR 56/57, STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: R/R PER ERA 596303-14 PRI REV.0 AND ER/A 596303-14 REV. ORIGINAL. (2073056)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 NEED TO PERFORM DTA MONITOR CRACK INSPECTION ER/A 596106-14. CORRECTIVE ACTION: COMPLIED WITH ERA. OK TO CONTINUE ON MON. (2072344)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION FOUND ON HOLE #8 LOC. REAR EMERGENCY EXIT DOOR CUTOUT EXTERNAL FUSELAGE LH STR20 BTW FR40 AND FR41. CORRECTIVE ACTION: COMPLIED WITH PRI 595702-14AD. (2070925)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DENT EXTERNAL SKIN ON DOUBLER REPAIR LOCATED AT FR74 AND BTW STR 30R TO STR 31R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A #496943-14 REV.B. (2070969)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION FOUND IN OPEN HOLE (H2) ON CROSSBEAM SPLICING AREA AT FRAME 16 LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 595688-14AD REV ORIGINAL. (2070932)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069667)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 41L BTW FR 27 AND FR 31 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2069966)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV. ORIGINAL. (2069674)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 WEAR ON LOWER SKIN SLAT 3 ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A #599222-14 REV.ORIGINAL. (2069578)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV. ORIGINAL. (2069702)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK FOUND IN OPEN FASTENER HOLE #13 FRAME 20 RH SIDE DOOR STOP #1 LOWER CORNER. CORRECTIVE ACTION: REPAIRED PER ER/A #595607-14AD REV. ORIGINAL. (2069788)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 16 LH DOUBLE JOGGLE AREA HOLE C IN COCKPIT. CORRECTIVE ACTION: REPAIRED PER ER/A #595611-14AD REV.ORIGINAL. (2070176)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV.ORIGINAL. (2069638)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069663)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069659)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069651)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK EMERGENCY EXIT DOOR 833 ON LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LH SEGMENT ANGLE AND FASTENERS PER A320 SRM 51-42-11, AND 51-72-11. (2070205)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

REAR FUSELAGE / FRAME - FR 68LH - DOOR STOP FITTING #1 - HOLE 4 - CRACK. ACCOMPLISH ER/A 596000-14 SECTION II INSPECTION WITHIN EVERY 19700 CYCLES AFTER ACCOMPLISHMENT OF THE SECTION I REPAIR. ASSOCIATED ER/A 00-596000 ADDED FOR AC 3248. (LP# 2068997)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 NEED TO COMPLY WITH ERA INSPECTION ER/A 595693-14. CORRECTIVE ACTION: COMPLIED WITH ERA (CRACK INSPECTION) OK TO CONTINUE. (2072092)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

DTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION IV REQUIRES DTA APPROVAL WITHIN 60000 CYCLES AFTER SECTION I. CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 60000 CYCLES AFTER SECT I PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-596000 ADDED FOR AC 3248. (LP# 2069007)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

DTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION III REQUIRES DTA APPROVAL WITHIN 37900 CYCLES AFTER SECTION I REPAIR CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 37900 CYCLES AFTER SECT I PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-596000 ADDED FOR AC 3248. (LP# 2069001)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION FLOOR BEAM +Y765 LOC. FR64 TO FR66 AT AFT GALLEY AREA (1EA)(SSI 534147). REPLACED SEAT TRACK Y765 LOC BTW FR64 TO FR66 AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG 10N01474. RII INSPECTION COM- PLETE 0113782 (AE262QC) JOB COMPLETE. (LP# 2067298)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

BENT FITTING DOOR LOWER CORNER AFT POSITION IN FWD CARGO COMPARTMENT. INSTALLED NEW CORNER AFT POSITION IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11, 51-71-11 AND DWG D532371810, ISSUE W, RELEASE DATE:16-JUN-20. RII INSPECTION COMPLETE 0294551 (AE166QC) JOB COMPLETE. (LP# 2067294)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION SEAT TRACK -Y765 LOC FR46+8 INCHES IN PASSENGER CABIN (MEASUREMENT ARE L=4.364 INCHES, W=0.380 INCHES, D=0.040). REPLACED SEAT TRACK -Y765 LOC FR41 TO FR47 IN PASSENGER CABIN AS PER A320 SRM 51-42-11, 51-72-11 AND DWG D53370500, RELEASE DATE:11-JAN-01, ISSUE AQ. RII INSPECTION COMPLETE 0313085 (AE205QC) JOB COMPLETE. (LP# 2067397)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION STRINGER 40L BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTION LOC. ON STRINGER 40L LOC AT FR33 AND FR34 IN FWD CARGO COMPARTMENT AS PER SRM A320 53-00-13- 300-001 PARAGRAGH 2, FIG 001. MEASUREMENT OF REWORK ARE P1 L= 2.861 INCHES, W=0.760. TOOL USED DIGITAL CALIPER P/N:700-113- 10, S/N:0031753, DUE DATE:06-NOV-22. NOMINAL THICKNESS IS 0.039 INCHES AS PER SRM A320 53-21-13-02A, FIG 02. PERFORMED ROTO TEST INSPECTION ON OPEN FASTENERS HOLFE AS PER NTM 51-10- 01. CRACK INDICATION NOT FOUND. TOOL USED EDDY CURRENT EQUIP- MENT P/N:NORTEC 600D, S/N:210138203, DUE DATE:05-MAR-22. RE- CHECK IS NOT REQUIRED DUE TO THIS REPAIR IS CLASSIFIED AS CATE- GORY A. RII INSPECTION COMPLETE 2431397 (AE14QC) JOB COMPLETE. (LP# 2067434)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION DOOR AFT CORNER LOCKING HOOK AREA IN AFT CARGO COMPARTMENT (SSI 523113). REPLACED CORNER LOCKING HOOK AREA LOC. AT AFT CARGO COMPARTMENT AS PER A320 SRM 51-42-11, 51-72-11 AND DWG 52371700 ISSUE G, RE- LEASE DATE:26-JUL-21. RII INSPECTION COMPLETE 1656995 (AE154QC) JOB COMPLETE. (LP# 2067287)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION STRINGER 39R LOC AT FR33 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTIONS LOC ON STRINGER 39R LOC AT FR32 PLUS 13.750 INCH TO FRAME 35 LESS 3 INCHES IN FWD CARGO COMP- ARTMENT AS PER SRM A320 53-00-13-300-001 PARAGRAPH 2, FIG 00. MEASUREMENT OF REWORKED AREA ARE P1 L=2.644 INCHES, W=0.759. TOOL USED DIGITAL CALIPER P/N:700-113-10, S/N:0031753, DUE DATE:06-NOV-22, NOMINAL THICKNESS IS 0.063 INCHES AS PER SRM A320 53-21-13-03A FIG 03. PERFORMED ROTO TEST INSPECTION ON OPEN FASTENERS HOLE AS PER NTM 51-10-01. CRACK INDICATION NOT FOUND, TOOL USED EDDY CURRENT EQUIPMENT P/N:NORTEC 600D, S/N: 210138203, DUE DATE:05-MAR-22. RECHECK IS NOT REQUIRED DUE TO THIS REPAIR IS CATEGORY A. RII INSPECTION COMPLETE 2431397. (LP# 2067427)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION SEAT TRACK +Y765 FR20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y765 AND FASTENERS LOC BTW FR12 TO FR24 FWD PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWGS #D53112812, ISSUE E00, RELEASE DATE:22-MAR-06, DWG D53110900, ISSUE L00, RELEASE DATE:22-MAR-06 AND DWG D53110984, ISSUE C00 AND RELEASE DATE:25-MAR-06. RII INSPECTION COMPLETE 2431397 (AE14QC) JOB COMPLETE. (LP# 2067401)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

CORROSION STRINGER 42L BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTIONS LOC ON STRINGER 42L LOC AT FR33 AND FR34 IN FWD CARGO COMPARTMENTS AS PER SRM A320 53-00-13- 300-001 PARAGRAPH 2, FIG 001. MEASUREMENT OF REWORK ARE P1 L= 1.853 INCHES, W=0.699, TOOL USED DIGITAL CALIPER P/N:700-113- 10, S/N:0031753, DUE DATE:06-NOV-22. NOMINAL THICKNESS IS 0.086 INCHES AS PER SRM A320 53-21-13-02A FIG 02. PERFORMED ROTO TEST INSPECTION ON OPEN FASTENERS HOLES AS PER NTM 51-10- 01. CRACK INDICATION NOT FOUND, TOOL USED EDDY CURRENT EQUIPM- ENT P/N:NORTEC 600D, S/N:210138203, DUE DATE:05-MAR-22. RE CHECK IS NOT REQUIRED DUE TO THIS REPAIR IS CLASSIFIED AS CATE- GORY A. RII INSPECTION COMPLETE 2431397 (AE14QC) JOB COMPLETE. (LP# 2067414)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB AT STR 38R BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11, AND 51-72-11. (2063728)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BELOW FRAME 73, BETWEEN 73, BETWEEN STRINGERS 31L AND 30L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060597)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y1292 LOC FR64 TO FR66 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060556)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON SKIN CLIPS/FRAME, FORWARD SIDE OF FRAME 72, BETWEEN STRINGERS 32R AND 34R. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060581)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, AFT OF FRAME 73, BETWEEN STRINGERS 30R AND 31R. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060583)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CRACK SUPPORT ANGLE LOCATED BTW FR64 TO FR65 AND LEVEL STR 44 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE PER A320 SRM 51-72-11 AND 51-42-11. (2060546)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BETWEEN FRAMES 73 AND 74, BETWEEN STRINGERS 34 AND 33L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060599)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y1292 LOC FR66 TO FR68 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060133)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM -Y1162.5 LOC. FR 68 TO FR 69 R/H IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060576)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS (5EA) BELOW FRAME 75 BTW STR 39L AND STR 39R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060588)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM -Y1292 LOC FR64 TO FR66 R/H IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060559)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y1162.5 LOC FR68 TO FR69 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060552)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS BELOW FRAME 74 BTW STR 30L 29L AND STR 30R AND 29R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060595)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y-464.8 LOC FR68 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2060541)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y-160.5 FR68 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2060542)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y-1292 LOC FR66 TO FR68 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2060136)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 GOUGE INTERNAL STRUCTURE SPLICE LOCATED FR30 AND BTW STR 34L TO STR 36L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SPLICE PER A320 SRM 51-72-11. (2058947)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB LOC BTW FR 62/63, STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER SRM A320 51-72-11. (2058959)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB BTW FR58/59, STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER SRM A320 51-72-11. (2058966)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 ER/A 592211-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH CORROSION ERA. (2058901)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 ER/A 592211-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH CORROSION ERA. (2058903)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 GOUGE INTERNAL STRUCTURE SPLICE OF FR 29 LOCATED BTW STR 34L TO STR 36L IN FWD CARGO COMPARTMENT. CORECTIVE ACTION: REPLACED SPLICE PER A320 SRM 51-72-11. (2057791)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 GOUGE FLOOR BEAM Y 512.5 LOC. BTW FR 64 TO FR 70 L/H IN PASSENGER CABIN. CORRECTIVE ACTION: R/R FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2057796)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM -Y254 BTW FR16/20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER SRM A320 51-72-11. (2056740)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 WEAR ON OFFWING SCAPE SLIDE BELLY FAIRING CHANNEL RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED OFFWING SCAPE SLIDE PER SRM A320 51-72-11. (2056746)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 BENT INTERNAL STRUCTURE WEB AT FR33 BTW STR 43L AND 43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER SRM A320 51-72-11. (2056782)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 ELONGATED HOLE OFFWING ESCAPE SLIDE BELLY FAIRING CHANNEL LEFT SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED OFFWING SCAPE SLIDE BELLY FAIRING CHANNEL PER SRM A320 51-72-11. (2056752)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM -Y765 BTW FR18/21 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2055563)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM -Y1292 BTW FR 16/21 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2054640)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION SEAT TRACK +Y765 LOC FR 46 AND 6 INCHES IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11. (2053670)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 BENT INTERNAL STRUCTURE SUPPORT AT FR 32 BTW STR 43L AND STR 43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB INTERNAL STRUCTURE SUPPORT (1 E/A) AND FASTENERS PER A320 SRM 51-72-11. (2054231)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB LOCATED BTW FR58 TO FR59 LEVEL STR 38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11, AND 51-72-11. (2053304)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB BTW FR60/61 AT LEVEL STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11, AND 51-72-11. (2053302)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB BTW FR51/52, STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB BTW FR51/52, STR 38R IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-42-11, AND 51-72-11. (2053410)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB BTW FR62/63, STR 38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRUCTURE WEB AND FASTENERS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (2052277)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION STRINGER 43L LOCATED BTW FR56 TO FR57 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AND CONTINUE ON MON. (2047862)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR STRUCTURE WEB AT LEVEL FR20, Y1732 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE PER A320 SRM 51-72-11. OK FOR SERVICE. (2046122)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR STRUCTURE ANGLE -Y1732, FR 16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-72-11. (2046128)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 GOUGE FRAME 30 AT LEVEL STR 36R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIR PER A320 SRM 51-42-11. OK FOR SERVICE. (2045542)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION INTERNAL STRUCTURE WEB AT STR 38L BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER SRM A320 51-42-11. (2045548)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DETERIORATED BUSHINGS ON PASSENGER CREW DOOR 831 UPPER AND LOWER LINK BTW SUPPORT ARM AND DOOR AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-11-21. OK FOR SERVICE. (2045537)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION LOWER SILL CORNER FITTING LOCATED AT FR16 STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CORNER FITTING PER A320 SRM 51-72-11. (2043974)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y765.0 LOC FR66 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2043981)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FRAME WEB LOCATED BTW FR69 TO FR70 LEVEL STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FRAME WEB AND FASTENERS PER A320 SRM 51-72-11. (2042747)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FRAME WEB LOCATED BTW FR69 TO FR70 LEVEL STR 23L AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FRAME WEB AND FASTENERS PER A320 SRM 51-72-11. (2042741)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION FLOOR BEAM Y-765 LOC. FR66 TO FR70 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2040567)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION BRACKET LOCATED ON WEB FR20 AT LEVEL STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BRACKET A320 SRM 51-42-11 AND 51-72-11. (2040560)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 PASSENGER CREW DOOR 832 DAMPER WEAK. CORRECTIVE ACTION: R/R DOOR DAMPER PER A320 AMM 52-13-01. OK FOR SERVICE. (2040457)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION WEB LOCATED AT FR20 AT LEVEL STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-42-11 AND 51-72-11. (2040553)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION LOWER SILL AT FR20 STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: INSPECTED PER SRI 53-11-14. CONTINUE ON MON. (2039145)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 PASSENGER CREW DOOR 842 DAMPER IS WEAK. CORRECTIVE ACTION: R/R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FROM DOOR 842 PER A320 AMM 52-13-14. (2036166)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 PASSENGER CREW DOOR 831 DOES NOT PASS DAMPER TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER PER A320 AMM 52-13-14. OPS TEST GOOD. (2036171)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 PASSENGER CREW DOOR 842 DIFFICULT TO OPEN/OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-13-21. OK FOR SERVICE. (2036744)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION LOWER SILL LOC FR66 TO FR68 L/H IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. BTW FR66 TO FR68 LH IN PASSENGER CABIN AS PER A320 SRM 53-41-14. (2035811)

Part: NONE — NONE · corrosion level 2 · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 CORROSION LOWER SILL LOC FR66 TO FR68 R/H IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A320 SRM 53-41-14. (2035828)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 PASSENGER CREW DOOR 831 AT FWD GALLEY AREA OUT OF ADJUSTMENT. CORRECTIVE ACTION. RIGGED DOOR PER A320 AMM 52-11-21. (2035784)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DETERIORATED PASSENGER CREW DOOR 841 ROLLER LOWER SIDE AT FWD AND AFT POSITION. CORRECTIVE ACTION: REPLACED ROLLERS PER A320 FAM AMM 52-11-31. (2035792)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DETERIORATED PASSENGER CREW DOOR 831 ROLLER FWD AND AFT POSITION AT LOWER SIDE OF THE DOOR AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PER A320 AMM 52-11-31. (2035795)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DENT ON DOOR INTERNAL AREA IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: EVALUATED DENT LOC. ON DOOR INTERNAL AREA IN FWD CARGO COMPARTMENT AND FOUND WITHIN LIMITS AS PER A320 SRM 51-73-11. (2034516)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 ROLLERS WORN ON PASSENGER CREW DOOR 842 FWD AND AFT POSITION AT LOWER SIDE. CORRECTIVE ACTION: REPLACED ROLLERS PER A320 AMM 52-13-31. OK FOR SERVICE. (2032169)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 ROLLERS WORN ON PASSENGER CREW DOOR 832 LOWER SIDE AT FWD AND AFT POSITION AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED ROLLERS PER A320 AMM 52-13-31. OK FOR SERVICE. (2032170)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 UPPER AND LOWER BUSHINGS ON CREW DOOR 832 WORN. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-13-21. OK FOR SERVICE. (2030364)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 UPPPER AND LOWER BUSHING WORN ON PASSENGER CREW DOOR 842. CORRECTIVE ACTION: R/R BUSHINGS PER A320 AMM 52-13-21. OK FOR SERVICE. (2030369)

Part: NONE — NONE · airframe 83,998 hrs · 38,392 cycles

SHIP 3248 DENT EXTERNAL SKIN LOCATED AT FR15 LEVEL STR 30L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-11-11. (2029283)

Part: NONE — NONE · airframe 83,794 hrs · 38,249 cycles

SHIP 3248 CRACK INDICATION AT STOP 7 FRAME 20 RH HOLE #4 IN INTERCOSTAL LAYER ONLY. CORRECTIVE ACTION: COMPLIED WITH ERA 594717-14 REV 0. (1982936)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 FUSELAGE / FR 20 / R-1 DOOR OPENING / STOP FITTING #7 / CRACK INDICATION AT HOLE #4. CORRECTIVE ACTION: COMPLIED WITH ER/A 00-594717. CONTINUE ON MON. (1981824)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 CRACK INDICATION IN FRAME AND INTERCOSTAL LAYER AT DOOR STOP #1, FRAME 16 LH HOLE NUMBER 3. CORRECTIVE ACTION: COMPLIED WITH ERA 594717-14 REV O. (1982184)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 FUSELAGE / FR 16 / L-1 DOOR OPENING / STOP FITTING #1 / CRACK INDICATION AT HOLE #3. CORRECTIVE ACTION: COMPLIED WITH ERA 594717-14AD. CONTINUE ON MON. (1981828)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 STOP FITTING #1 FRAME 20 RH. HOLE #1 IS OUT OF ROUND AND HOLES 2, 3, 4 ARE ALSO OUT OF ROUND. CORRECTIVE ACTION: COMPLIED WITH ERA 594751-14 REV O. (1982168)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 CRACK INDICATION IN INTERCOSTAL LAYER ONLY DOOR STOP #7, FRAME 16 LH AT HOLE NUMBER 3. CORRECTIVE ACTION: COMPLIED WITH ERA 594717-14 REV O. (1982180)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 CRACK AT STOP #7 FRAME 20 LH HOLE #2 IN INTERCOSTAL LAYER ONLY. CORRECTIVE ACTION: COMPLIED WITH ERA 594717-14 REV O. (1982186)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 A320 / FUSELAGE / FR-20 / R-1 DOOR OPENING / STOP FITTING #1 / INSPECTION AT HOLES #3 AND #4. CORRECTIVE ACTION: COMPLIED WITH ERA 594751-14AD REV ORIG. (1981217)

Part: NONE — NONE · airframe 83,771 hrs · 38,235 cycles

SHIP 3248 A320 / FUSELAGE / FR-20 / R-1 DOOR OPENING / STOP FITTING #1 / CRACK INDICATIONS AT HOLES #1 AND #4. CORRECTIVE ACTION: COMPLIED WITH ERA 14-594751. (1981206)

Part: NONE — NONE · airframe 83,680 hrs · 38,180 cycles

SHIP 3248 WHEN PERFORMING O2 DROP TEST PER DELTA W/C 2527-01041-02 THE FOLLOWING MASKS DID NOT DROP 1DC 2,3,4AB 11,17,18,20,21,23,28 AND 32ABC 14,19,20,25,26,27,29DEF. CORRECTIVE ACTION: REPACKED MASKS AND ALL PASSED TEST. OK FOR SERVICE. (7811232)

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 83,074 hrs · 37,807 cycles

SHIP 3248 CORROSION FRONT SPAR SKIN LOCATED UPPER SURFACE BETWEEN RIB11 TO RIB13 ON LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER PRI 592211-14 REV.0 AND ER/A 592211-14 REV. ORIGINAL. (1850844)

Part: SKIN — CORRODED (LT WING) · airframe 83,170 hrs · 37,867 cycles

SHIP 3248 WHILE ACCOMPLISHING JIC 5720-3951-LT, CORROSION SPOTS (2) FOUND ON EXTERNAL FUSELAGE SKIN PANEL 1, UPPER SURFACE ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 32-592211. (1850571)

Part: STRUCTURE — BROKEN (NR 2 SLAT TE) · airframe 83,074 hrs · 37,807 cycles

SHIP 3248 BROKEN TRAILING EDGE SLAT 2 LOCATED IB SIDE ON LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER SRM 57-43. (1838552)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,859 hrs · 37,701 cycles

SHIP 3248 - FOUND LAST 2 SEAT MOUNTED ESCAPE PATH EM. LIGHTS INOP AND THE RED EMERG LIGHT ON AFT LH DIVIDER WALL INOP. CORRECTIVE ACTION: REPAIRED IAW A320 AWL 33-51-08 AND ESPM 20-43. EMERGENCY LIGHTS TEST OK. (7283625)

Part: FILTER — DIRTY (PASS CABIN) · airframe 82,702 hrs · 37,623 cycles

SHIP 3248 PAC 1 & 2 DO NOT COOL AIRCRAFT WITH APU OR WITH ENGINES OAT 82 AT PBI (INSIDE TEMP 86/80/76) PACS HAVE DIRTY SOCKS SMELL CYCLED HOT AIR VALVE - IT WAS OPEN HOT AIR TO OFF FOR 5 MINS THAT HELPED COOL A/C. CORRECTIVE ACTION: REPLACED AIR ACTUATOR AND CABIN FILTERS. RAN PACKS PER A320 AMM 21-52. CABIN TEMP CORRECT. DIRTY SOCK SMELL GONE. (7590752)

Part: PSU — NO TEST (SEAT 31DEF) · airframe 82,130 hrs · 37,356 cycles

DURING TEST FOUND PSU OXYGEN PANEL AT 31DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 1CD) · airframe 82,130 hrs · 37,356 cycles

DURING TEST FOUND PSU OXYGEN PANEL AT 1CD DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 3AB) · airframe 82,130 hrs · 37,356 cycles

DURING TEST FOUND PSU OXYGEN PANEL AT 3AB DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,530 hrs · 37,041 cycles

FA REPORTED THE EMERGENCY LIGHTS FLASHED ON AND OFF THE ENTIRE FLIGHT. CORRECTIVE ACTION: R/R L AFT EPSU AND BATTERY PER A320 AMM 33-52, L AFT EPSU BATT FAULT CLEARED, EMERGENCY LTS OPS NML. FOUND INOP BULB IN RIGHT WING AFT OVERWING EXIT LIGHT HOUSING. RELAMPED BULB AND RAN OPS CHECK PER A320 AMM 33-51. OPS CHECK GOOD. FAULT NO LONGER EXIST.

Part: LEVER — BINDING (L1 DOOR) · airframe 81,505 hrs · 37,023 cycles

ON ARRIVAL, FLT ATTNDT NOTIFIED CREW THAT THE DISARMING LEVER AT 1L WAS VERY DIFFICULT TO MOVE AND MADE LOUD NOISE WHEN REACHING DISARM POSITION. CORRECTIVE ACTION: CLOSED 1L DOOR AND OPERATED DISARMING LEVER SEVERAL TIMES. ARMING LEVER OPERATES NML AT THIS TIME. REF A320 AMM 52-11

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 81,440 hrs · 36,986 cycles

EXTERIOR OVERWING EMERGENCY LIGHT FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU AND BATTERY OF EPSU, PER A320 AMM 33-51 -38. FAULT CLEARED. OPS CHECK GOOD.

Part: VENT — CORRODED (LAVATORY) · airframe 80,183 hrs · 36,362 cycles

AFT LAV VENT HAS CORROSION AROUND VENT, REMOVED EXISTING FASTENERS IN REPAIR AREA REMOVED CONNECTION PLATE AND CUTOUT DAMAGE SKIN AREA AND DEBURR THE EDGES, STEP 2A 1 THRU 6. NDT OPEN HOLE ROTARY INSP PER A320 NDTM 51-10-01 PBG PROCEDURE AND SURFACE SCAN FOR CRACKS CONTAINMENT PER A320 NTM 51-10-08 PBG PROCEDURE B NO CRACKS NOTED QC 1988.COMPLETED STEPS 7 THRU 16 OF A320 SRM 53-41-11-300-004 THIS IS PERMANENT REPAIR

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 79,369 hrs · 35,927 cycles

A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH. HOLE #14.AA5311-01171SB A320-53-1263AD-2018-06-04. COMPLIED WITH PRI 579496-14AD REV O, REV 1, REV 2, REV 3 AND REV 4, ALSO ER/A 579496-14AD REV O.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 79,369 hrs · 35,927 cycles

A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. HOLE # 26. AA 5311-01171SB A320-53-1263AD-2018-06-04. COMPLIED WITH PRI 579496-14AD REV O, REV 1, REV 2, REV 3 AND REV 4, ALSO ER/A 579496-14AD REV O.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 79,369 hrs · 35,927 cycles

A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35RH AND FR36RH. HOLE # 4. -M- AA5311-01171 SB A320-53-1263 AD -2018-06-04. REPAIRED PER PRI 579495-14AD REV 0 AND 1 AND ER/A 579495-14AD REV 0.

Part: MECHANISM — BENT (EMERGENCY EXIT) · airframe 79,369 hrs · 35,927 cycles

FWD RT EMERGENCY EXIT DOOR HANDLE LOCKING MECHANISM HAS A BENT PIN AND ARM. REMOVED AND REPLACED LATCH HANDLE MECHANISM REF CMM 52-21.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 79,369 hrs · 35,927 cycles

A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH. HOLE #3.AA5311-01171SB A320-53-1263AD-2018-06-04. COMPLIED WITH PRI 579496-14AD REV O, REV 1, REV 2, REV 3 AND REV 4, ALSO ER/A 579496-14AD REV O.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 79,369 hrs · 35,927 cycles

CAPTS WINDSHIELD HAS LOWER EDGE CRACK IN PANE. REMOVED AND REPLACED CAPTS WINDSHIELD REF AMM 56- 11-11 WINDOW.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,369 hrs · 35,927 cycles

EXFOLIATION CORROSION AFT OF AFT CARGO COMPT - GANG BOND/GROUND STRIP ANGLE ON STR 34 LT, BETWEEN FRAMES 65, SEE NR FOR ADDITIONAL INFORMATION 001-0057:5340-3001/001 00062 REPLACED GANG GROUND ANGLE REF SRM 51-72-11.

Part: BUSHING — SCORED (DOOR HINGE) · airframe 79,369 hrs · 35,927 cycles

FWD CARGO DOOR HINGE- ALL BUSHINGS ARE SCORED. AND #40 LUG FROM FWD IS MIGRATED. SEE NR FOR ADDITIONAL INFORMATION 000-0001:5231-4001/002 00228 FWD CARGO DOOR BEING REPLACED ON AMDS 5231-4001.

Part: DOOR FRAME — CRACKED (FWD CARGO) · airframe 80,568 hrs · 36,551 cycles

FWD CARGO DOOR FRAME FORKS FOUND CRACKED AND HAD OVERSIZED HOLES. REPAIRED IAW WITH ER/A 581907-14AD, REV ORIGINAL. ALL OTHER WORK ACCOMPLISHED ON SHOP ORDER PS4865.

Part: BATTERY — DISCHARGED (CABIN) · airframe 77,775 hrs · 35,155 cycles

EPSU BATTERY EMER R FAULT ON FAP. REMOVED AND REPLACED EPSU BATTERY FOR EMERGENCY RIGHT OVERWING EXIT DOOR. FAP SYSTEM CHECKS OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 77,007 hrs · 34,773 cycles

ROW 11 AND 18 AISLE ILLUMINATION EMERGENCY LIGHTS BROKEN/MISSING (BELOW SEATS). REPLACED.

Part: FITTING — FAULTY (DOOR) · airframe 76,441 hrs · 34,510 cycles

AFT LT DOOR ARMING PIN WILL NOT KEEP FROM ARMING DOOR. PIN PUSHES OUT WHEN LEVER IS PUSHED DOWN. INSTALLED DOOR PIN FITTING. OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ROW 25) · airframe 75,329 hrs · 34,001 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 25, REPLACED THE LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 74,242 hrs · 33,458 cycles

SEAT 11D MOUNTED EMERGENCY LIGHT BROKEN, REATTACHED LIGHT MOUNT TO SEAT.

Part: SLIDE — FAILED (CABIN) · airframe 72,568 hrs · 32,699 cycles

WHILE PERFORMING SLIDE DEPLOYMENT TEST REF FORECAST NR 32-0525-8-0188. SLIDE FAILED TO DEPLOY FULLY, REPLACED RT AFT SLIDE PER WORK CARD 2561-4002-RA REF LOG 2871251

Part: BOX BEAM — CRACKED · airframe 72,111 hrs · 32,515 cycles

RT SIDE BOX BEAM IS CRACKED AT FWD HOLE AT PRESSURE PLATE, MID HOLE AT BEAM FLANGE, AND AFT HOLE AT BEAM FLANGE. REMOVED AND REPLACED PRESSURE PLATE AND REPAIRED THE BOX BEAM IAW AMDS 5310-01450-02

Part: BOX BEAM — CRACKED · airframe 72,111 hrs · 32,515 cycles

LT SIDE BOX BEAM IS CRACKED AT AFT HOLE AT PRESSURE PLATE, AFT HOLE AT BEAM FLANGE AND MID HOLE AT BEAM FLANGE. REMOVED AND REPLACED PRESSURE PLATE AND REPAIRED BEAM IAW AMDS 5310-01450-02.

Part: STRUCTURE — CRACKED · airframe 69,213 hrs · 31,106 cycles

DURING ER/A 496764-14, SECT II INSPECTION, A CRACK IS FOUND IN ER/A FIG 3 AREA C, HOLE DURING OPEN HOLE HFEC INSPECTION. CONFIGURED ACFT ON JACKING CONDITION IAW ERA NR 496764-14AD REVISION "E" AND "F" SECTION VII PART "A", AND AMM 07-11-00-581-001A. REPLACED FR20 RT SIDE AND FASTENERS, KITS PN SR5312-90A10500, SR 5312-90H10201.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 69,629 hrs · 31,299 cycles

A CRACK WAS FOUND ON UPPER ATTACHMENT OF RT SLIDING WINDOW FRAME IN HOLE NR 3. PERFORMED TIME LIMITED REPAIR ON WINDSHIELD SIDE PAST AT FRAME 4 UPPER ATTACHMNET IN COCKPIT RT POSITION IAW PRI 536252-14AD, REV 0, 1, 2, 3, 4 AND ER/A 536252-14AD, REV ORIGINAL.

Part: FRAME — CORRODED (FRM 16) · airframe 72,029 hrs · 32,471 cycles

CORROSION ON FRAME 16 AFT FACE AT STRINGER 23R. REMOVED CORROSION, FOUND OUT OF LIMITS, TREATED AND PAINTED AREA.

Part: SKIN — CORRODED (RT WING) · airframe 72,029 hrs · 32,471 cycles

CORROSION ON UPPER SURFACE TOP SKIN AROUND FASTENERS HEAD AT RIB 1 BETWEEN STRINGERS 1 AND 2, RT WING. REPAIRED THE SKIN IAW ER/A 537612.

Part: SPAR — CORRODED (RT PYLON) · airframe 72,029 hrs · 32,471 cycles

CORROSION ON UPPER SPAR AT PS 648 RIB.09 RT PYLON. REPAIRED THE SPAR IAW ER/A.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 47.5 - 64 FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53476950.

Part: STRUCTURE — CORRODED (FRAME 67) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON INTERNAL STRUCTURE AT FRAME 67+6 STRINGER 25L. REPLACED THE STRUCTURE IAW SRM 51-72-11, PRI 537613-14, REV O AND ER/A 537613-14 .

Part: STRUCTURE — CORRODED (FRAME 67) · airframe 72,029 hrs · 32,471 cycles

CORROSION ON STRUCTURE, FRAME 67+6, STRINGER 27L. REPLACED IAW ER/A. LP#2068728

Part: STRINGER — CORRODED (FRAME 65) · airframe 68,196 hrs · 30,560 cycles

CORROSION FOUND ON STRINGER 26R FRAME 65. REPLACED THE STRINGER IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 68,196 hrs · 30,560 cycles

CORROSION FOUND ON SEAT TRACK +Y1292, FRAMES 35 - 36, FOUND TO BE OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371024.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y765, FRAMES 35 - 36. FOUND TO BE OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371024.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 68,196 hrs · 30,560 cycles

CORROSION FOUND ON SEAT TRACK -Y1292, FRAMES 35 - 36. FOUND TO BE OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371034.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 72,029 hrs · 32,471 cycles

CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 TO 24. REPAIRED FLOOR SUPPORT IAW ER/A.

Part: KEELBEAM — NOT REPORTED (FRAME 46) · airframe 68,196 hrs · 30,560 cycles

POSSIBLE FCS REPAIR ON FRAME 46 KEELBEAM LT AND RT SIDE AT LOWER FUSELAGE. REPLACED ANGLE CONNECT, LT SIDE, ANGLE CONNECT AND PLATE, RT SIDE, LOCATED FRAME 46 KEELBEAM, SRM 51-72-11 AND DWG D53371827, D53371817, D53371804.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,196 hrs · 30,560 cycles

CRACK ON EMERGENCY EXIT DOOR FRAME. REPLACED THE DOOR FRAME IAW SRM 51-72-11 AND DWG D52279010006.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON LOWER SILL AT LEVEL STR 23R AT AFT GALLEY AREA BETWEEN DOOR FRAME 66 TO DOOR FRAME. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480043.

Part: FITTING — CORRODED (FRAME 68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON CORNER FITTING FRAME 68 AT STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480019.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y1292 FRAMES 41 - 47. REPLACED THE SEAT TRACK IAW SRM 51-75-11 AND DWG 53370500.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON FLOOR SUPPORT, -Y1225 BETWEEN FRAMES 66 - 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON FLOOR SUPPORT, -Y1162 BETWEEN FRAMES 68 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON THE FLOOR SUPPORT AT +Y1225 BETWEEN FRAMES 66 - 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040.

Part: STRUCTURE — CORRODED (FRAMES 66-68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON LOWER SILL AT STRINGER 23L FRAMES 66 FRAME 68. REPLACED THE SILL IAW SRM 51-72-11 AND DWG D53780019.

Part: FITTING — CORRODED (FRAME 68) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON THE CORNER FITTING AT FRAME 68 STR 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480019.

Part: FITTING — CORRODED (FRAME 66) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON A CORNER FITTING AT FRAME 66 STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480042.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON THE FLOOR SUPPORT AT +Y1162 BETWEEN FRAMES 68 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y1292, FRAMES 36 - 41 AND FOUND OUT LIMITS. REPLACED THE SEAT TRACKS IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y765, FRAMES 36 - 41 AND FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y765, FRAME 41 TO 47 EVALUATE AND FOUND OUT LIMITS ON ON JOB CARD N2500-2031. REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FRAME 41 TO FRAME 42 IAW SRM 51-72-11 AND DWG D53370500.

Part: WEB — CORRODED (FRAMES 20-24) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON WEB -Y1732 BETWEEN FRAMES 20 TO 24 . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53112783.

Part: STRINGER — CORRODED (FRAMES 30-35) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON STRINGER 41L BETWEEN FRAMES 30+15 TO 35. REPLACED THE STRINGER IAW SRM 51-72-11, DWG D53231626 AND D53372507.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 47.5 - 64. FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472030.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66 - 70 . REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 12 - 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG NR D53110984 AND D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON FLOOR SUPPORT -Y1732 BETWEEN FRAMES 65 - 66 IN AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470150.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y1292 BETWEEN FRAMES 47.5 - 64. FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53476950.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y765, FRAMES 36 - 41. FOUND TO BE OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y765, FRAMES 41 - 47. FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK, +Y1292, FRAMES 36 - 41. FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG D57130146, AND D53370500.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y765, FRAMES 35 - 36. FOUND TO BE OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370382.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y1292, FRAMES 41 - 47 . FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON SEAT TRACK +Y765 BETWEEN FRAMES 47.5 TO 64 . FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472030.

Part: FLOOR SUPPORT — CORRODED (FRAMES 21-23) · airframe 68,196 hrs · 30,560 cycles

CORROSION ON FLOOR SUPPORT -Y189 BETWEEN FRAMES 21 TO 23. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53112834.

Part: HINGE — WORN (LT ELEVATOR) · airframe 67,026 hrs · 30,022 cycles

LT ELEVATOR HINGE OTBD BORE FITTING WORN, REPAIRED IAW SRM 55-26-41.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,315 hrs · 29,698 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT BATTERY PACKS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,604 hrs · 29,355 cycles

SEAT 22C EMERGENCY LIGHT INOPERATIVE, FOUND BROKEN WIRE ON LAMP HOLDER. NEEDS LIGHT ASSY STK NR 32-3300-3-0481. CAPPED BROKEN WIRE. FWD TO MEL AND PLACARD IAW MEL 33-50-03A. OK FOR SERVICE. INSTALLED NEW LIGHT ASSY IAW AMM 33-51 ALL OPS NORMAL.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,188 hrs · 28,689 cycles

DURING INSPECTION, FOUND ESCAPE PATH LIGHT MODULE MISSING. MAINTENANCE REPLACED ESCAPE PATH LIGHT MODULE AND FUNCTIONAL CHECKED NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 64,014 hrs · 28,608 cycles

DURING A NON ROUTINE CHECK, FOUND ROW 19 SEATS ABC EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BROKEN CONNECTOR AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,805 hrs · 28,016 cycles

DURING NON ROUTINE CHECK, FOUND INTERIOR EMERGENCY LIGHT FAILED CIDS TEST. REPLACED EPSU AND FUNCTIONAL CHECK WAS NORMAL.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,289 hrs · 27,254 cycles

DURING INSPECTION, FOUND ALL FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MX REPLACED EPSU AND OPS CHECK WAS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 60,655 hrs · 26,962 cycles

DURING SERVICE CHECK, FOUND ESCAPE PATH LIGHT AT SEAT 13C, INOPERATIVE. FOUND BAD CONNECTOR AT FLOOR. SECURED AND FUNCTIONAL CHECK WAS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 4,813 hrs · 2,066 cycles

SKIN DAMAGED FROM FRAME 71 TO FRAME 76 AND FROM STR 30 RT TO30 LT. REMOVED DAMAGED SECTION OF SKIN AND DRILLED UP REPAIR SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER AIRBUS DWG R53570010, 882888. ACCOMPLISHED REPAIR PER ERA 496943-14.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 4,813 hrs · 2,066 cycles

DURING CHECK, FOUND FUSELAGE SKIN, JACK PAD, STRINGERS AND FRAME DAMAGED BETWEEN FRAMES 73 AND 74 DUE TO CONTACT WITH STABILIZER JACK. MAINTENANCE INSTALLED REPAIR PER ER/A 496943-14.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 4,813 hrs · 2,066 cycles

FUSELAGE FRAME FR 75 AT STA 35719 IS BUCKLED BETWEEN STR 27 AND 28 LT AND AT STR 28 AND 29 RT REF NRC 178/179. REMOVED DAMAGED SECTION. DRILLED NEW SECTION, DRILLED REPAIR SLPICES PER A320 SRM 53-00-12 FIG 204. ACCOMPLISHED REPAIR IAW A320 SRM 53-00-12.

Part: FRAME — BUCKLED (FRAME 75) · airframe 4,813 hrs · 2,066 cycles

FRAME 75, BUCKLED, BETWEEN S 27-28L, S28-29R, REPAIRED IAW SRM 53-00-12.

Part: WIRE — DAMAGED (CABIN) · airframe 55,725 hrs · 24,624 cycles

DURING EMERGENCY LIGHT TEST FOUND AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED A WIRE ON THE LIGHT ASSEMBLY AND TESTS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,142 hrs · 22,737 cycles

AIRCRAFT HAS INTOLERABLE ODOR COMING OUT OF AIR CONDITIONING SYSTEM. ODOR IS SO TOXIC SMELLING IT IS UNBEARABLE ON THE GROUND WITH APU AND PACKS ON AND EXTREMELY STRONG AT LOW ALTITUDE, SHUT OFF APU BLEED AND LANDING WAS UNEVENTFUL. NO FLUIDS FOUND IN APU AND PACK INLETS, DID APU AND ENGINE RUN PACK BURN OUT AND NO ODOR NOTED.

Part: SKIN PANEL — DAMAGED (FUELAGE) · airframe 49,698 hrs · 22,140 cycles

DURING LINE CHECK FOUND DAMAGE TO LT FUSELAGE SKIN PANEL AT FR 69 BETWEEN S22L AND S23L. REPAIRED PER EA 32-215889 SECT I FOR 50 CYCLES PENDING ADDITIONAL MANUFACTURER REVIEW FOR REQUIRED REPETITIVE INSPECTIONS PER SECT II OF EA 32-215889.

Part: MODULE — SHORTED (CABIN) · airframe 41,349 hrs · 18,191 cycles

ROWS 12, 13, 14, 18, 19, 20, 24, 25, 26 EVACUATION LIGHTS INOP. REPLACED SHORTED OVERWING EXIT LAMP MODULE AND OVERWING POWER SUPPLY. SYSTEM CHECKS GOOD. Â

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 40,769 hrs · 17,917 cycles

DURING A-CHECK, THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT TEST FAILED, REPLACED BATTERY PACK.

Part: STRUT — FAILED (MLG) · airframe 33,248 hrs · 14,532 cycles

GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM MSP. RECEIVED SHOCK ABSORBER FAULT MESSAGE. COMPLIED WITH COM, BURNED DOWN FUEL, AND LANDED UNEVENTFULLY AT MSP. CHECKED RIGHT MLG STRUT PRESSURE AND FOUND 1250 PSI WITH 3-3/32 INCHES OF EXTENSION. JACKED AIRCRAFT AND STRUT WOULD NOT EXTEND. REMOVED RIGHT MLG STRUT, REPLACED SEALS, REASSEMBLED STRUT, AND SERVICED PER AMM. GEAR SWING CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,146 hrs · 14,486 cycles

DURING L CHECK FOUND CORROSION ON SEAT TRACKS Y-765 AND Y-1292 BETWEEN FRAMES 16-24. REPAIRED IAW EA 32-195649.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,146 hrs · 14,486 cycles

DURING "L" CHECK FOUND CORROSION ON RT FLOOR SUPPORT WEB AT FRAME 20. REPAIRED IAW EA 32-195961.

Part: SEAL — LEAKING (HMU) · airframe 31,642 hrs · 13,825 cycles

DURING CRUISE FLGHT ENGINE NR 2 N1 DETERIORATED TO 72 PERCENT N1 AND TEN MINUTES LATER ENGINE NR 2 FLAMED OUT. RELIGHT UNSUCCESSFUL. FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING AT DESTINATION AIRPORT. MAINTENANCE FOUND A FUEL LEAK AT THE HMU. MAINTENANCE REPLACED THE SEAL PLATE AT HMU TO FUEL FLOW TRANSMITTER.

Part: BUSHING — LOOSE (PAX DOOR)

AFTER ARRIVING AT THE GATE AND DEPLANING PASSENGERS. CATERING CREW FOUND THAT THEY WERE UNABLE TO OPEN DOOR 2L. MAINTENANCE FOUND THE DOOR UPPER SAFETY PIN GUIDE BUSHINGS HAD MIGRATED OUT OF THE FITTING NOT ALLOWING FOR FULL RETRACTION OF THE SAFETY PIN REQUIRED FOR DOOR OPENING. BUSHINGS WERE CEMENTED IN PROPER POSITION AND DOOR OPERATIONALLY CHECK NORMAL.

Part: BULBS — FAILED (CABIN)

DURING EMERGENCY LIGHT TEST, FOUND BOTH RIGHT OVERWING EXIT HANDLE ILLUMINATION LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS. OPERATIONAL CHECK OK.

Part: SKIN VALVE WARN — ACTIVATED (COCKPIT)

DURING TAKEOFF ROLL, RECEIVED VENT SKIN VALVE FAULT MESSAGE. ABORTED TAKEOFF AT 50 KTS. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.

Part: BATTERY — DISCHARGED (CABIN)

DURING EMERGENCY LIGHT TEST, RECEIVED FAULTS INT LOADS EMER R AND COMM EMER R. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK.

Part: BRACKET — LOOSE (NLG)

AFTER TAKEOFF, CREW SELECTED GEAR UP. NOTED NOSE GEAR DID NOT RETRACT AND RECEIVED MESSAGE: L/G SHOCK ABSORBER FAULT. CREW SELECTED GEAR DOWN, LANDING GEAR INDICATED DOWN AND LOCKED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED LOOSE BRACKET FOR NOSE GEAR AIR/GROUND SENSING PROXIMITY SWITCH TARGET AND FUNCTIONALLY CHECKED LANDING GEAR SYSTEM. OPERATIONAL CHECK OK.

Part: LIMITER — FAULTED (E/E COMPT)

AS POWER WAS BEING APPLIED FOR TAKEOFF, RECEIVED ELEC BCL 1 FAULT MESSAGE. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 BATTERY CHARGE LIMITER, OPERATIONAL CHECK OK.

Part: PROX SENSOR — MALFUNCTIONED (NLG)

DURING CLIMBOUT WHILE RETRACTING THE LANDING GEAR, THE NOSE LANDING GEAR WOULD NOT RETRACT. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR PROXIMITY SENSORS 24GA AND 25GA, OPERATIONAL CHECK OK.

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, THE LANDING GEAR DID NOT INDICATE UP LOCKED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NOSE LANDING SENSORS, OPERATIONAL CHECK OK.

Part: VBV — FAILED (NR 2 ENGINE)

DURING TAKEOFF ROLL, THE NR 2 ENGINE COMPRESSOR VANE MESSAGE ILLUMINATED. ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE VBV ASSEMBLY AND 4 VBV DOORS, ENGINE OPERATIONAL CHECK GOOD.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

DURING APPROACH INTO MSP, THE EMERGENCY EXIT SIGNS ABOVE THE AFT GALLEY DOORS DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK.

Part: DOOR LIGHT — ILLUMINATED (LT MLG)

DURING APPROACH INTO SFO AFTER THE LANDING GEAR WAS EXTENDED, THE LEFT MAIN LANDING GEAR DOOR WARNING LIGHT ILLUMINATED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TEST OF NR 1 AND NR 2 LANDING GEAR CONTROL INTERFACE UNITS REVEALED NO FAULTS. CLEANED ASSOCIATED GEAR DOOR INDICATION SWITCHES. OPERATIONAL CHECK OK.