N347NW

Part: FILTER — DIRTY (ZONE 100) · airframe 95,852 hrs · 44,751 cycles

APPROXIMATELY 30 SECONDS AFTER CLEARING THE RUNWAY, SMOKE AND HAZE ENTERED THE COCKPIT. SMOKE WAS REPORTED BY THE FAS IN THE CABIN (FAS SAY IT WAS MOSTLY REAR CABIN.) PILOTS USED OXYGEN MASKS. SMOKE DISAPETED W/IN 2 MIN. INSPECTED ENGS FOUND EXCESSIVE SAND AND DIRT ON BOTH ENG T/RS AND INLETS FROM RUNWAY AND TAXIWAY. NO LEAKS OR DAMAGE FOUND. PER MCC C/W LEVEL A DECON PER W/C 2100-2007 AND C/W W/C 0550- 2002. R & R RECIRC AND AVIONICS FILTERS IAW AMM 21-26. RAN BOTH ENGS/APU MULTIPLE TIMES NO SMOKE, SMELL OR HAZE. CREW O2 WITHIN LIMITS. (LP: 8158152)

Part: OIL SYSTEM — LEAKING (ZONE 100) · airframe 95,465 hrs · 44,542 cycles

DURING PREFLIGHT CREW NOTICED FUMES/OILY SMELL WHEN APU BLEED AIR WAS ACTIVATED . SMELL ESPECIALLY STRONG AROUND ROW 26. C/W W/C 0550-2002 CLASSIFED AS TYPE 1 APU LEAK. C/W W/C 4900- 2001 PLACED APU ON MEL REF LOG 7967753 . C/W LEVEL B DECONTAMINATION OF THE ECS AND DUCTS PER A320 AMM 21-00-00 AND AMM 36-10-00 . CONTACTED MCC NO 1261830.NO ODORS PRESENT. OK FOR SVC REF. MDLOG 1261830. (LP: 7967752)

Part: WIRE HARNESS — DAMAGED (ZONE 200) · airframe 95,085 hrs · 44,353 cycles

DURING MASK MANUAL DROP TEST FOUND ROW 27 ABC MASKS NOT DROPPING. FOUND WIRE HARNESS F224270-507 DAMAGED. R & R WIRE HARNESS F224270 -507 AT 27ABC REF AMM 25-25 AND CMM 25-25, AND AWM 23- 73. OPS TEST GOOD. DROP TEST GOOD IAW AMM 35-23-00. (LP: 7403315)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 900) · airframe 95,085 hrs · 44,353 cycles

AFT LAV OXYGEN MASK FELL DOWN. LAVATORY OXYGEN MODULE. REMOVED AND REPLACED PASSENGER OXYGEN CONTAINER IAW AMM 35 -21. OPS CK GOOD. (LP: 7403310)

Part: SLAT SYSTEM — LOCKED · airframe 94,949 hrs · 44,278 cycles

SHIP 3247 - ATB - DUE TO THE SLATS BEING LOCKED AT FULL EXTENSION WITH A SLATS MECHANICAL OVERSPEED MESSAGE. CORRECTIVE ACTION: NO TROUBLE FOUND. RESET WING-TIP BRAKES AND LUBRICATED SLAT SYSTEM. AIRCRAFT RTS. (LP: 7455658)

Part: A/C PACK — FAULTED (NR 2) · airframe 94,310 hrs · 43,931 cycles

SHIP 3247 - MISC/DE - DUE TO BLEED AND PACK ISSUES LEADING TO EXCESSIVE CABIN ALTITUDE AND LOW CABIN DIFFERENTIAL PRESSURE MESSAGES. PAX MASKS DEPLOYED. PACK 2 WAS ALREADY ON MEL. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS. (LP: 7530094)

Part: WIRE HARNESS — DAMAGED (ZONE 700) · airframe 93,488 hrs · 43,495 cycles

SHIP 3247 - LG - DECLARED EMERGENCY DUE TO LH MAIN LANDING GEAR UNSAFE/GEAR DISAGREE MESSAGE. CORRECTIVE ACTION: FOUND LH MLG HARNESS DAMAGED AT LH MAIN GEAR 15GA DOWNCLOCK SENSOR CONNECTOR. REPLACED LH GEAR 1M HARNESS. (LP: 65880506)

Part: SCREEN — CONTAMINATED (APU) · airframe 92,537 hrs · 42,976 cycles

SHIP 3247 DISC: ON LANDING AND TAXI IN, BACK OF AIRCRAFT REPORTS A DIRTY SOCK ODOR. C/A: ACCOMPLISHED W/C 0550-2002. ISOLATED TO APU. FOUND INLET, INLET SCREEN & IGV'S OIL SOAKED. FOUND OIL IN AIR/OIL HX TUBE & OIL IN FAN ON GEARBOX. NEEDS APU. ACCOMPLISHED ECS DECONTAMINATION W/C 2100-2005. INSPECTED ENGINES. NO LEAKS OR WETTING AT SPINNERS - NO SMELL DURING ENGINE RUNS. NO SMELLS AFTER DECONTAMINATION. RECIRC FILTERS REPLACED. WILL NEED W/C 4916-2001 & 4900-2001 COMPLETED AFTER APU REPLACEMENT. W/C 0550-9001-A320FAM ACCOMPLISHED. (LP: 5380582)

Part: INLET — CONTAMINATED (APU) · airframe 92,505 hrs · 42,961 cycles

SHIP 3247 DISC: DIRTY SOCKS SMELL IN COKPIT AND CABIN FROM 10000 TO 20000 ON CLIMBOUT. EVENTUALLY DISSIPATED. FA REPORTED SMELLING IT IN THE DESCENT FROM REAR JUMPSEAT. STRONG IN ROWS 28,29. C/A: FOUND NO APU OIL USAGE ON LAST 10 DAYS. FOUND NO HYDRAULIC SERVICING IN LAST 30 DAYS (BT 707431) PREV SHIFT FOUND OIL SOAKED CHEESE CLOTH STUCK TO APU INLET SCREEN. FOD REMOVED. NO APU COMPARTMENT LEAKS NOTED. INSPECTED APU OUTLET DUCT WITH BLACK LIGHT. NTF. C/W WORKCARDS 7900-2001, 2100-2003, 0550- 2001, AND 0550-2002 IN ENTIRETY. ENGINES BORESCOPED WITH NO FINDINGS. NO SPINNER WETTING. C/W REVERSE DUCT BURNOUT AND ECS DECONTAMINATION REF W/C 2100-2003. NO SMELLS NOTED AFTER DECONTAMINATION. RECIRC FILTERS REPLACED. C/W ALL ODI PREV STEPS REF LOG 0535603 INCLUDING ODI CAPTURE WORKCARD 0550-9001- A320FAM. (LP: 5380576)

Part: OIL SYSTEM — LOW PRESSURE (LEFT ENGINE) · airframe 91,672 hrs · 42,514 cycles

SHIP 3247 -DIV/IFSD-DIVERTED TO IAH DUE TO LEFT ENGINE OIL LOSS. FLIGHT CREW COMMANDED SHUTDOWN ON DESCENT DUE TO OIL PRESSURE DECREASING TO 6 PSI. CORRECTIVE ACTION: ENGINE CHANGE REQUIRED DUE TO ENGINE OIL PRESSURE OPERATING BELOW LIMITS. (LP: 5355770)

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 2CD) · airframe 91,149 hrs · 42,232 cycles

SHIP 3247 DISC: ROW 2 CD O2 MASK DROPPED IN FLIGHT. C/A: SECURED O2 MOD DOOR AT ROW 2CD PER A320AMM 35-21-00. OK FOR SERVICE. (LP: 4866494)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,801 hrs · 41,542 cycles

SHIP 3247 - MISC/DE - DUE TO F/CTL FLAPS LOCKED ECAM MESSAGE AND F/CTL CLASS II MESSAGE. CORRECTIVE ACTION: FOUND RIGHT #4 ROTARY ACTUATOR (6283CM) LEAKED GREASE. REPLENISHED #4 ROTARY ACTUATOR OFFSET GEARBOX WITH SEMI-FLUID. OPS CHECK GOOD. OK FOR SERVICE. (4543760)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,747 hrs · 41,517 cycles

SHIP 3247 FOUND EVIDENCE OF PREVIOUS REPAIR AT FR68 LH. CORRECTIVE ACTION: COMPLIED WITH PRI 611837-14 REV 0, PRI 611837-14 REV 1, AND ERA 611837-14AD REV A SECTION I. (2954891)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,747 hrs · 41,517 cycles

SHIP 3247 (DTE) DAMAGE TOLERANCE EVALUATION DUE WITHIN 6 MONTHS PER ER/A 611837-14. CORRECTIVE ACTION: COMPLIED WITH ERA 611837-14 REV A. (2954674)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,257 hrs · 41,262 cycles

SHIP 3247 EXIT SIGNS FLASHING ON/OFF UNTIL GEAR RETRACTED AND DID NOT COME ON WITH GEAR EXTENSION CAME ON AT TOUCHDOWN. CORRECTIVE ACTION: REPLACED RELAY 8WL. OPS CK GOOD. (4962986)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,703 hrs · 40,902 cycles

SHIP 3247 -ATB- FLIGHT RETURNED TO MCI DUE TO RIGHT ENGINE HIGH VIBES INDICATION. CORRECTIVE ACTION: INSPECTED BLADES FOUND TWO FAN BLADES SHINGLED AT MIDSPAN. UN-SHINGLED OVERLAPPED BLADES AND PERFORMED VIBE RUN. NO ABNORMAL VIBES DETECTED. (9983152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,639 hrs · 40,858 cycles

SHIP 3247 - ATB - DUE TO LEFT WING FUEL PUMPS INOPERATIVE, WITH NO FAULT INDICATIONS CAUSING FUEL IMBALANCE. CORRECTIVE ACTION: FOUND RIGHT FORWARD INNER TRANSFER VALVE (29QM) ACTUATOR (10QP) FAULTING. REPLACED RIGHT INTERCELL TRANSFER VALVE (10QT) NO FURTHER FAULTS. OK FOR SERVICE. (4070399)

Part: NONE — NONE · airframe 88,267 hrs · 40,678 cycles

SHIP 3247 "SMOKE AFT CARGO SMOKE MESSAGE" AT GATE IN MSP. RAN ECAM. AGENT DISCHARGED. AARF INSPECTED COMPARTMENT NO EVIDENCE OF FIRE. CORRECTIVE ACTION: REPLACED SMOKE DETECTORS AND FIRE BOTTLES. OPS CHECK GOOD. (9492088)

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 87,966 hrs · 40,524 cycles

HYD/MISC/DE - DUE TO GREEN SYSTEM HYDRAULIC LOSS. FOUND #1 ENGINE EDP OUTLET LINE LEAKING AT CLAMP, REPLACED SAME. DURING LEAK CHECK FOUND TUBE PRESSURE SWITCH LEAKING FROM THE B-NUT. R/R PRESSURE SWITCH LINE. OPS CHECK GOOD.

Part: ENGINE — MAKING METAL (NR 1) · airframe 87,835 hrs · 40,455 cycles

RETURNED TO GRR DUE TO #1 ENGINE FAIL, COMPRESSOR STALL, AND UN-COMMANDED SHUTDOWN. MAINTENANCE FOUND METAL IN THE TAIL PIPE. R & R ENGINE PER WORK-CARD 7100-9901-LT. OK FOR SERVICE.

Part: PANEL — CORRODED (NLG WW) · airframe 87,419 hrs · 40,225 cycles

CORROSION ON INBD FACE OF NLG LATERAL PANEL AROUND L/H BUSHING FOR NLG. COMPLIED WITH PRI 603249-14 REV 1.

Part: BATTERY PACK — INOPERATIVE · airframe 86,593 hrs · 39,723 cycles

SHIP 3247 EMER LIGHT TEST ON FAP FAILED. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERIES PER A320 AMM 33-51. ALL TEST NOW PASS. OK FOR SERVICE. (8997426)

Part: NONE — NONE · airframe 86,240 hrs · 39,528 cycles

SHIP 3247 EMERGENCY EXIT SIGNS DID NOT ILLUMINATE ON GEAR EXTENSION. AFTER THE TOUCHDOWN LIGHTS BLINKED AND WORKED NORMAL. CORRECTIVE ACTION: TROUBLESHOT SYSTEM WITH NO TROUBLE FOUND. (8651724)

Part: NONE — NONE · airframe 85,822 hrs · 39,280 cycles

SHIP 3247 - ATB - DUE TO F/A AND PAX REPORT OF LH UPPER AILERON HINGE CLOSEOUT PANEL DEPARTING THE AIRCRAFT. CORRECTIVE ACTION: FOUND ACCESS PANEL 575AT PARTIALLY MISSING. INBOARD MOUNT BRACKET CRACKED AND PARTIALLY GONE. INBOARD FORWARD SCREWS APPEAR TO BE MISSING. REPLACED SUPPORT BRACKET AND ANGLE AND REPLACED PANEL. AILERON WAS ALSO DAMAGED AND WAS REPLACED AND RIGGED. OK FOR SERVICE. (8772572)

Part: NONE — NONE · airframe 85,818 hrs · 39,278 cycles

SHIP 3247 - ATB - DUE TO F/A AND PAX REPORT OF LH UPPER AILERON HINGE CLOSEOUT PANEL DEPARTING THE AIRCRAFT. CORRECTIVE ACTION: FOUND ACCESS PANEL 575AT PARTIALLY MISSING. INBOARD MOUNT BRACKET CRACKED AND PARTIALLY GONE. INBOARD FORWARD SCREWS APPEAR TO BE MISSING.

Part: NONE — NONE · corrosion level 2 · airframe 85,685 hrs · 39,204 cycles

SHIP 3247 CORROSION TANK 1 UPPER SURFACE OF THE UPPER SKIN LOC BTW FR 41/ 42 AND BTW Y1292AND Y 1732 IN CENTER FUEL TANK. CORRECTIVE ACTION: COMPLIED WITH ERA 596503-14AD REV. ORIGINAL. (2125609)

Part: NONE — NONE · corrosion level 2 · airframe 85,685 hrs · 39,204 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED FR56 AND STR41L TO STR42L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER A320 SRM 51-72-11 AND 51-42-11. (2125027)

Part: NONE — NONE · corrosion level 2 · airframe 85,685 hrs · 39,204 cycles

SHIP 3247 CORROSION STRINGER 43L LOCATED BTW FR 33 TO FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-00-13. (2125040)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK DOOR LOWER CORNER FITTING AFT POSITION IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOOR LOWER CORNER FITTING AFT POSITION IN FWD CARGO COMPARTMENT PER A320 SRM 51-72-11. (2124141)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 596545-14. (2123858)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR 33 BTW STR. 42L TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2123956)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION BONDING PLATE FLAP TRACK FAIRING 633CB ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 596545-14. (2123080)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 68 RH SIDE ON OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-12. OK FOR SERVICE. (2123070)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 WEAR ON ACCESS PANEL 194AB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH 596506-14 REVISION ORIGINAL. (2120579)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 REPAIR PASSENGER DOORS PER ERA. CORRECTIVE ACTION: COMPLIED WITH ERA 596958-14 REV ORIGINAL. DVI OF EXISTING REPAIR. (2120578)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DELAMINATED C-DUCT INTERNAL AREA LOC. UPPER AFT POSITION OUTBOARD THRUST REVERSER ON ENGINE 1. CORRECTIVE ACTION: COMPLIED WITH ER/A 597118-14. (2119976)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION INTERNAL STRUCTURE WEB LOCATED FR62 TO FR63 AND STR38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11 AND 51-72-11. (2118643)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION BRACKET FLOOR STRUCTURE LOCATED FR 48 TO FR 49 AND STR 36R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED BRACKET AND STRINGER PER A320 SRM 51-42-11. (2118649)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK ANGLE SUPPORT BELLY FAIRING LOC. KEEL BEAM BTW FR46 TO FR47 R/H SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-35-11. (2117374)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 41L LOCATED BTW FR33 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2117370)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK SUPPORT ANGLE LOCATED BETWEEN FR64 TO FR65 AT LEVEL STR44 AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE PER A320 SRM 51-42-11 AND 51-72-11. (2117338)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 ELONGATED HOLE CENTER FITTING LOCATED BTW FR16 TO FR20 STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING PER A320 SRM 51-72-11. (2117565)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INTERNAL STRUCTURE LOCATED FR52 AT LEVEL STR44 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE PER A320 SRM 51-42-11 AND 51-72-11. (2117600)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER PRI #596350-14AD REV.0, REV.1 AND ER/A #596350-14 AD REV ORIGINAL. (2117405)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR32 BTW STR 42R TO STR 43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2115135)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: REPLACED BELLCRANK ASSY AND ADJUSTED DOOR PER A320 FAM AMM 52-11-22. OK FOR SERVICE. (2114948)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 ELONGATED HOLE LOWER SILL FR66 AT LEVEL STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-14. (2115177)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK BRACKET ON FR 20 AT LEVEL OF INTERCOSTAL FITTING 7 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED BRACKET PER A320 SRM 51-72-11. (2114863)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SUPPORT ANGLE LOCATED FR66 AND STR 25R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11 AND 51-72-11. (2115148)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR32 BTW STR 40R TO STR 41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2115139)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR32 BTW STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2115159)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION INTERNAL STRUCTURE WEB LOCATED FR50 TO FR51 AT LEVEL STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11. (2115162)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTON: REPAIRED PER PRI #596350-14AD REV.0, REV.1 AND ER/A #596350-14 AD REV.ORIGINAL. (2115204)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION INTERNAL STRUCTURE ANGLE CLIP LOCATED FR65 AND STR 26R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED ANGLE CLIP AND FASTENERS PER A320 SRM 51-42-11 AND 51-72-11. (2114088)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 26R LOCATED FR66 TO FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER SECTION PER A320 SRM 51-44-11 AND 51-72-11. (2113808)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR33 BTW STR 40R TO STR 41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11. (2113736)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION RIVET HEAD FLOOR STRUCTURE LOCATED FR65 TO FR70 STR 23L/R LOWER AREA AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED RIVET FLOOR STRUCTURE PER A320 SRM 51-42-11. (2113796)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR32 BTW STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2113780)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR STRUCTURE CONNECTING LOCATED FR67 AND STR 31R IN AFT CARGO COMPARTMENT. CORRECTVE ACTION: REPLACED FLOOR STRUCTURE PER A320 SRM 51-72-11. (2113812)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION INTERNAL STRUCTURE RIVETS HEAD LOCATED BTW FR24 TO FR28 AND STR 38L TO STR 38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REMOVED AND REPLACED FASTENERS PER A320 SRM 51-42-11. (2113733)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR32 BTW STR 42L TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2113791)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK BRACKET LOCATED FR20 AT LEVEL OF INTERCOSTAL FITTING 7 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED BRACKET PER A320 SRM 51-72-11. (2113798)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR 33 BTW STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER A320 SRM 51-42-11. (2112918)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOC. AT FRAME 73 BTW STR 23L AND 24L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596722-14 REV 0 AND ER/A 596722-14 REV ORIGINAL. (2112934)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER PRI 596350-14AD REV.0, REV.1 AND ERA 596350-14AD REV. ORIGINAL. (2112908)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOC.AT FRAME 74 BTW STR 19 AND STR 20 ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596720-14REV.0 AND ERA 596720-14 REV. ORIGINAL. (2112888)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 35, STR 30 LH HOLE 6 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 596379-14AD, REV. ORIGINAL. (2112937)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER PRI 596350-14AD REV.0, REV.1 AND ERA 596350-14AD REV. ORIGINAL. (2112928)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER PRI 596350-14AD REV.0, REV.1 AND ERA 596350-14AD REV. ORIGINAL. (2112932)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR 33 BTW STR 43L TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER A320 SRM 51-42-11. (2112913)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 AD RELATED 5340-01075-03A TO UPDATE CARD 1/730 MIGRATED ATTACHMENT FITTINGS MLG ACTUATOR BUSHING FWD LUG AT LH MAIN LANDING GEAR ACCORDING ER/A 596650-14D. CORRECTIVE ACTION: COMPLIED WITH ERA. (2112905)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FRAME 68 AT LEVEL STR 23L FORWARD FACE AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 596753-14 REV. ORIGINAL. (2112936)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOCATED FR4 AT LEVEL -Y675 ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ERA 596749-14 REV, ORIGINAL. (2112891)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR 33 BTW STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER A320 SRM 51-42-11. (2112910)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FRAME 68 AT LEVEL STR 23RH FWD FACE AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH PRI 596752-14 REV.0. (2112900)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENTS ON EXTERNAL SKIN LOC. AT FRAME 71 R/H BTW STR 14R AND STR 16R ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596721-14 REV.0 AND ERA 596721-14 REV. ORIGINAL. (2112907)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 3 POSITION. CORRECTIVE ACTION: COMPLIED WITH SRI 53-41-12-205-009. CONTINUE ON MON. (2110790)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 A CORROSION SPOT FOUND ON FWD FACE OF FR 68 WEB AT LEVEL OF STR 23LH. CORRECTIVE ACTION: COMPLIED WITH 596753-14. (2107800)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 43R LOCATED BTW FR33 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER PER A320 SRM 53-00-13. (2106837)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION ON FRAME 68 LH SIDE ON OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (2106781)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION WAS FOUND ON WEB OF FR68 AT STRGR 23R ON FWD FACE OF FRAME. CORRECTIVE ACTION: COMPLIED WITH ER/A 32-596752. CONTINUE ON MON. (2107020)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SHEAR TIE LOCATED AT FR34 BTW STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2106819)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK FLOOR STRUCTURE WEB BTWFR 68/69 AND BTW Y1162.5/1353.01 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB PER A320 SRM 51-72-11 AND 51-42-11. (2106016)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 831 OUT OF ADJUSTMENT/HARD TO OPEN. CORRECTIVE ACTION: R/R BUSHINGS AND ADJUSTED DOOR PER AMM. OK FOR SERVICE. (2106012)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 44 LOCATED BTW FR 33 TO FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED STRINGER PER A320 SRM 53-00-13. (2105422)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INTERNAL STRUCTURE WEB LOCATED BTW FR 68 TO FR 69 AT LEVEL STR 2 3R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-72-11 AND 51-42-11. (2105458)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 43L LOCATED BTW FR 32 TO FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED STRINGER PER A320 SRM 53-00-13. (2105449)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 WHILE PERFORMING INSPECTIONS PER 5312-01183 (A320-53-1372) A CRACK WAS FOUND IN FASTENER HOLE #6. CORRECTIVE ACTION: COMPLIED WITH ERA 596379-14AD. (2105488)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 ELONGATED HOLE LOWER SILL CORNER FITTING LOCATED FR 16 STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CORNER FITTING PER A320 SRM 51-72-11. (2105461)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION STRINGER 42R LOCATED BTW FR 32 TO FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER PER A320 SRM 53-00-13. (2105435)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 EVIDENCE OF REWORK EXTERNAL SKIN AT 18 INCHES BELOW OF RH SIDE STRINGER AND 6 INCHES FWD OF FR24 STATIC PORT AREA AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 596473-14, REV ORIGINAL. (2103422)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK STRINGER 23R AT LEVEL FR69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2103426)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK SUPPORT WEB BELLY FAIRING LOCATED FR47 AT LEVEL STR 40LH AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERM REPAIR PER ERA 596429-14. (2103448)

Part: NONE — NONE · airframe 85,876 hrs · 39,311 cycles

SHIP 3247 CRACKS FOUND IN Y-765 HOLE#2, Y-254 HOLE#1, Y254 HOLE#1, AND Y765 HOLE#2, ALL IN FLOOR BEAM LAYER. CORRECTIVE ACTION: PUT ON A MONITOR INSPECTION. OK FOR CONTINUED SERVICE. (2102639)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK ACCESS PANEL 191KB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI #596507-14 VALIDATED ER/A #596507-14. (2099901)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 831 IS OUT OF ADJUSTMENT/HARD TO OPEN. CORRECTIVE ACTION: COMPLIED WITH DELTA WORKCARD AMDS 5210-7089-LF. OK FOR SERVICE. (2100329)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CRACK INDICATION FOUND IN OPEN HOLE 3, ON FRAME 20 RH, AND DOOR STOP FITTING 1. CORRECTIVE ACTION: COMPLIED WITH PRI 596547-14AD. OK FOR SERVICE. (2097756)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR BEAM +Y1292 BTW FR 18/20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2093965)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SEAT TRACK -Y765 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, SPLICE AND NEW FASTENERS PER A320 SRM 51-72-11. (2093989)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION SEAT TRACK -Y1292 AT LEVEL FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 51-72-11. (2093984)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR BEAM -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2090534)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION WEB LOCATED BTW FR 20 TO FR 21 AND STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-72-11. (2090563)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 HOLE RAIL DUMMY -Y189 AT LEVEL FR 23 AT FWD GALLEY AREA. (CORROSION) CORRECTIVE ACTION: REPLACED RAIL DUMMY PER A320 SRM 51-72-11. (2090560)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 ELONGATED HOLE FLOOR BEAM +Y1162.5 AT LEVEL OF FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2090545)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2088377)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: RIGGED DOOR PER A320 AMM 52-11-21. OK FOR SERVICE. (2087493)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 841 DOOR DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-11-14. OK FOR SERVICE. (2083266)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR BEAM -Y1589 LOCATED BTW FR 65 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2083975)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 832 OUT OF ADJUSTMENT. HARD TO ARM. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF THE COMPENSATION MECHANISM (H) IN THE UP POSITION AT AFT GALLEY AREA AS PER A320 FAM AMM 52-13-21. (2082709)

Part: NONE — NONE · corrosion level 2 · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 CORROSION FLOOR BEAM -Y 464.8 AND FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2082676)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOCATED FROM FR19 TO FR20 AND 11 INCHES ABOVE LOWER STRINGER RH AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 51-73-11 AND FOUND DENT TO BE WITHIN LIMITS. (2082868)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 832 OUT OF ADJUSTMENT HARD TO ARM. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF THE COMPENSATION MECHANISM (K) AT AFT GALLEY AREA AS PER A320 AMM 52-13-21. (2082705)

Part: SKIN — DENTED (FRM 62 S40-41R) · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOCATED AT FR 62 AND BTW STR 40R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 53-41-11. OK FOR CONTINUED SERVICE. CONTINUE ON MON. (2081596)

Part: SKIN — DENTED (FRM 63 S40-41R) · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 DENT EXTERNAL SKIN LOCATED AT FR 63 BTW STR 40R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 53-41-11. OK FOR CONTINUED SERVICE. CONTINUE ON MON. (2081599)

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 SLIDE RAFT AT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA DEFORMED. CORRECTIVE ACTION: R/R SLIDE PER DELTA WORKCARD AMDS CARD 2561-4002-RF. OK FOR SERVICE. (2081785)

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 SLIDE RAFT AT PASSENGER CREW DOOR 842 AT AFT GALLEY AREA DEFORMED. CORRECTIVE ACTION: R/R SLIDE PER DELTA WORKCARD AMDS 2561-4002-RA. (2078385)

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 SLIDE RAFT AT PASSENGER CREW DOOR 831 AT FWD GALLEY AREA IS DEFORMED. CORRECTIVE ACTION: R/R SLIDE PER DELTA WORKCARD AMDS CARD 2561-4001-LF. OK FOR SERVICE. (2078381)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 PASSENGER CREW DOOR 831 DOOR DAMPER DID NOT PASS TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER PER A320 AMM 52-15. OK FOR SERVICE. (2077681)

Part: NONE — NONE · airframe 85,684 hrs · 39,203 cycles

SHIP 3247 HISTORY OF EMERGENCY LIGHTS FLICKERING. CORRECTIVE ACTION: REPLACED CIDS2 (102RH) SERVICEABLE CONDITION AS PER A320 FAM AMM 23-73 AND PERFORMED OPERATIONAL TEST. TEST GOOD. (2058897)

Part: NONE — NONE · airframe 85,608 hrs · 39,159 cycles

SHIP 3247 EMERGENCY EXIT LIGHTS FLICKER. CORRECTIVE ACTION: CLEANED CONNECTION. OK FOR SERVICE. (8061071)

Part: PROXIMITY SWITCH — FAULTED (LT AFT DOOR) · airframe 84,361 hrs · 38,428 cycles

SHIP 3247 DOOR L AFT EMER EXIT DOOR L AFT EMER EXIT FAULT" ON ECAM FOR SEVERAL FLIGHTS DURING CRUISE. CORRECTIVE ACTION: REMOVED & REPLACED L/H AFT OVERWING EMERGENCY DOOR PROX SWITCH (21WV1) IAW A320 AMM 52-71. OPS CK GOOD. (1842738)

Part: WARNING MESSAGE — FALSE INDICATION (EMERGENCY EXIT) · airframe 84,299 hrs · 38,390 cycles

SHIP 3247 AT ALTITUDE ECAM MSG L FWD EMER EXIT MESSAGE ILLUMINATED. HAD NUISANCE REOCCURANCES FOR DURATION OF FLIGHT. CORRECTIVE ACTION: REMOVED AND REINSTALLED COVER FLAP LH FWD EMG EXIT HATCH PER A320 TSM 52-21. OPS CK GOOD. (7605809)

Part: STRUT — FAULTED (MLG) · airframe 84,304 hrs · 38,393 cycles

SHIP 3247 - DIV - TO MSY DUE TO LANDING GEAR SHOCK ABSORBER FAULT AND OTHER ASSOCIATED AIR/GROUND SHIFT FAILURE MESSAGES. CORRECTIVE ACTION: FOUND NLG PROXIMITY SENSOR 24/25GA TARGET ARM WITH EXCESSIVE PLAY. INSTALLED NEW BUSHINGS AND RIGGED PROX SENSORS.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 84,275 hrs · 38,375 cycles

SHIP 3247 CRACK ON ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 591949-14 REV. ORIGINAL AND SRM 55-32-11. (1833845)

Part: SKIN — DAMAGED (LT NR 2 SLAT) · airframe 84,275 hrs · 38,375 cycles

SHIP 3247 MISSING MATERIAL EXTERNAL SKIN LOCATED FWD EDGE OF SLAT #2 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 591923-14 REV.0 AND ER/A 591923-14 REV. ORIGINAL. (1832939)

Part: ACCESS PANEL — DAMAGED (RT NACELLE) · airframe 84,275 hrs · 38,375 cycles

SHIP 3247 ELONGATED HOLE ACCESS PANEL 424CR ON RH PYLON. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 591929-14 REV.0 AND ER/A 591929-14 REV.ORIGINAL. (1832910)

Part: NONE — NONE · corrosion level 2 · airframe 85,331 hrs · 38,978 cycles

SHIP 3247 CORROSION AFT MOVABLE FAIRING WEB ON RH PYLON. CORRECTIVE ACTION: REPLACED AFT MOVABLE FAIRING WEB PER SRM A320 51-72-11. (1825789)

Part: STRINGER — CORRODED (FRM 66 S42L) · corrosion level 2 · airframe 84,275 hrs · 38,375 cycles

SHIP 3247 CORROSION INTERNAL STRUCTURE ON STRINGER 42L AND STRINGER 43L BTW FR56 TO FR57 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER 320 SRM 51-72-11. (1823610)

Part: FRAME — CRACKED (FRM 16) · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 CRACK INDICATIONS IN RH FRAME 16, STOP #7, HOLES #1, #2. CORRECTIVE ACTION: COMPLIED WITH ERA 590536-14AD REV O. (1755488)

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 CRACK INDICATION AT DOOR STOP #7, FR 16-, LH SIDE, HOLE #2 IN THE INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ERA 590536-14AD REV O. (1755490)

Part: FRAME — CRACKED (FRM 20) · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 CRACK INDICATIONS IN RH FRAME 20, STOP #7, HOLES #1 FRAME AND #2 FRAME. CORRECTIVE ACTION: COMPLIED WITH ERA 590536-14AD REV O. (1755487)

Part: STOP FITTING — CRACKED (FRM 20) · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 CRACK INDICATION AT DOOR STOP #7, FR 20-, LH SIDE, HOLES 3 AND 4 IN THE INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ERA 590536-14AD REV O. OK FOR SERVICE. (1755489)

Part: DOOR FRAME — CRACKED · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 HOLES 1 AND 4 OF DOOR STOP FITTING #1 CRACK INDICATIONS IN INTERCOSTAL. CORRECTIVE ACTION: COMP LIED WITH ERA 590536-14AD REV O. OK FOR SERVICE. (1755491)

Part: DOOR FRAME — CRACKED · airframe 83,748 hrs · 38,149 cycles

SHIP 3247 CRACK INDICATION AT DOOR STOP #1, FR 16-, LH SIDE, HOLES #1 AND #3 IN THE FRAME, AND HOLE #2 IN THE INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ERA 590536-14AD REV O. (1755492)

Part: PANEL — NO TEST (PSU SEAT 25DEF) · airframe 83,732 hrs · 38,142 cycles

SHIP 3247 DURING TEST FOUND PSU OXY PANEL AT SEAT 25DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7432258)

Part: PANEL — NO TEST (PSU SEAT 13ABC) · airframe 83,732 hrs · 38,142 cycles

SHIP 3247 DURING TEST FOUND PSU OXY PANEL AT SEAT 13ABC DID NOT OPEN. CORECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7432259)

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 80,055 hrs · 36,207 cycles

DURING INSPECTION OF LH PRESSURE FLOOR PANEL FASTENER HOLES AT FRAME 36, CRACK FOUND AT HOLE "A" ( INBOARD LOCATION), REPAIR IN ACCORDANCE WITH WORK CARD 5311- 01171-04A PRIOR TO FURTHER FLIGHT. "AA 5311-01171" "SB A320- 53-1264" "AD-2018-06-04"

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 80,055 hrs · 36,207 cycles

DURING INSPECTION OF RT PRESSURE FLOOR PANEL FASTENER HOLES AT FRAME 36, CRACK FOUND AT HOLE "B" ( OUTBOARD LOCATION), REPAIR IN ACCORDANCE WITH WORK CARD 5311- 01171-04B PRIOR TO FURTHER FLIGHT. "AA 5311-01171" "SB A320-53- 1264" "AD-2018-06-04"

Part: FRAME — DAMAGED (FRM 68) · airframe 80,024 hrs · 36,194 cycles

FRAME 68 LH SIDE STR.16, TOP HOLE FOUND DAMAGED IN FRAME 68 WHERE GUSSET WAS REMOVED ON NR 162 AND GUSSET ATTACH HOLES OF FRAME 68 INNER CAP, STR 16 LT: LOWEST HOLE IS MISDRILLED, NEXT TWO HOLES ABOVE LOWEST HOLE INTERIORS HAVE DEEP SCORES, REPAIRED PER PRI-579137-14 REV 0, REV 1, REV 2, REV 3, REV 4 AND ERA 579137-14AD REV ORIGINAL

Part: STRUCTURE — DAMAGED (R1 DOOR) · airframe 78,311 hrs · 35,336 cycles

(LP 0804023) TRANSFERRED FROM LOGBOOK 5149566. DAMAGE REPORTED BY CATERING ON R1 DOOR APPROXIMATELY 1/2 INCH NEAR BOTTOM AFT CORNER OF DOOR. REMOVED DAMAGE, EDDY CURRENT, DAMAGE EXCEEDS ALLOWABLE LIMITS. INCREASED SIZE OF CUTOUT, EDDY CURRENT, FABRICATED AND INSTALLED REPAIR IAW SRM 52-10-00-300-003.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 78,311 hrs · 35,336 cycles

(LP 0804282) R1 MAIN CABIN DOOR SLIDE NOT EFFECTIVE IPC. REMOVED AND REPLACED IAW 2561-4002.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 76,654 hrs · 34,524 cycles

AFT EPSU UNIT FAILED ON SERVICE CHECK, REPLACED AFT EPSU.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,831 hrs · 33,198 cycles

DURING SVC CK FOUND EMERGENCY LIGHTS OUT AT ROWS 8,13,AND 17. RELAMPED.

Part: BOX BEAM — CRACKED · airframe 72,895 hrs · 32,779 cycles

LT SIDE BOX BEAM FLANGE AFT AND CTR BOLT HOLE CRACKED. REPAIRED IAW AMDS 5310-01450-02.

Part: BOX BEAM — CRACKED · airframe 72,895 hrs · 32,779 cycles

RT SIDE BOX BEAM FLANGE AFT BOLT HOLE CRACKED, REPAIRED IAW AMDS 5310-01450-02.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 71,132 hrs · 31,914 cycles

FOUND FWD LT EPSU FAULT, REPLACED EPSU.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 70,377 hrs · 31,604 cycles

TESTED EMERGENCY LIGHTS THEY FAULTED FOR RT BATTERY PACK. REPLACED THE BATTERY PACK.

Part: GROUND WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 70,256 hrs · 31,555 cycles

18A EMERGENCY LIGHT INOPERATIVE, GROUND WIRE DISCONNECTED AT OUTBOARD SEAT LEG. RECONNECTED GROUND WIRE.

Part: POWER SUPPLY — FAILED (EMERGENCY LGIHTS) · airframe 69,999 hrs · 31,433 cycles

DURING S/C FOUND FWD EMERGENCY POWER SUPPLY UNIT FAULTING FIN10WL, REPLACED EPSU, W/O BATTERY 10WL.

Part: SKIN — DAMAGED (FRAMES 24-25) · airframe 68,952 hrs · 30,886 cycles

ELONGATED HOLES ON EXTERNAL SKIN AND LOWER FLANGER AT STR 36LT AND ELONGATED HOLES ON VERTICAL FLANGE OF THE STR 35 LT BETWEEN FRAME 24 TO FRAME 25 AT LOWER FUSELAGE. PERFORM PERMANENT REPAIR STRINGER 35 LT AND 36LT IAW SRM 53-00-13 PARA 4.A FIGURE 201. THE REPAIR ON EXTERNAL SKIN OF ELONGATED HOLES IS DOCUMENTED ON ERA 537648-14.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON STRINGER 31R BETWEEN FRAMES 65 AND 66. REPLACED STRINGER 31R BETWEEN FRAME 65 AND FRAME 66 AND FASTENERS IAW SRM 51-72-11 AND DWGS D53480505 AND D53480016.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,952 hrs · 30,886 cycles

CRACK ON EMERGENCY EXIT DOOR FRAME, BETWEEN BEAM 1 AND BEAM 3. REPLACED THE DOOR FRAME IAW SRM 51-72-11 AND DWG D52279010.

Part: STRINGER — CORRODED (FRAMES 31-32) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON STRINGER 41L, FRAMES 31 TO 32. REPAIRED THE STRINGER IAW ER/A.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,952 hrs · 30,886 cycles

A CRACK WAS FOUND ON THE EMERGENCY EXIT DOOR FRAME. REPLACED THE FRAME IAW SRM 51-72-11, DWG D52279040, AND D52279010.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,952 hrs · 30,886 cycles

CRACK WAS FOUND ON THE EMERGENCY DOOR FRAME. REPLACED THE FRAME IAW SRM 51-72-11, DWG D52279040, AND D52279010.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,952 hrs · 30,886 cycles

A CRACK WAS FOUND ON THE EMERGENCY DOOR FRAME. REPLACED THE FRAME IAW SRM 51-72-11, DWG D52279040, AND D52279010.

Part: RAIL — CRACKED (SLIDING WINDOW) · airframe 68,952 hrs · 30,886 cycles

CRACK ON SLIDING WINDOW RAIL. REPAIRED THE RAIL IAW SRM 53-11-12, PARA 5C.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,952 hrs · 30,886 cycles

A CRACK WAS FOUND ON THE EMERGENCY EXIT DOOR FRAME. REPLACED THE FRAME IAW SRM 51-72-11, DWG D52279040, AND D52279010.

Part: RAIL — CRACKED (SLIDING WINDOW) · airframe 68,952 hrs · 30,886 cycles

A CRACK WAS FOUND ON THE SLIDING WINDOW UPPER RAIL. REPAIRED THE RAIL IAW SRM 53-11-12, PARA 5C, 2.

Part: STRINGER — CORRODED (FRAME 32) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON STRINGER 41R ON FRAME 32+9 IN FWD CARGO BAY. REPLACED THE STRINGER IAW SRM 51-42-11, 51-72-11, AND DWG D53231626.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-20) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON FLOOR SUPPORT -Y254 AT FRAMES 18 TO 20. REPLACED THE FLOOR SUPPORT IAW ER/A 536263.

Part: PLATE — CORRODED (FRAME 58) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON PLATE AT FRAME 58, STRINGER 44 IN AFT CARGO COMPARTMENT. REPLACED THE PLATE IAW SRM 51-72-11 AND DWG D53974836.

Part: STRUCTURE — CORRODED (FRAME 67) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON INTERNAL STRUCTURE SECTION CONNECTION AT FRAME 67 AND STR 26L. REPLACED IAW ER/A 537625-14.

Part: STRUCTURE — CORRODED (FRAME 67) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON INTERNAL STRUCTURE SECTION CONNECTION AT FRAME 67 AND STRINGER 28L. REPLACED SECTION CONNECTION IAW ER/A.

Part: WEB — CRACKED (FRAMES 8-11) · airframe 68,952 hrs · 30,886 cycles

CRACK ON WEB-Y765 BETWEEN FRAME 8 TO FRAME 11 FLOOR STRUCTURE IN COCKPIT. REPLACED WEB -Y765 BETWEEN FRAME 8 TO FRAME 11 FLOOR STRUCTURE IN COCKPIT IAW SRM 51-72-11 AND DWG D53113219.

Part: WEB — CRACKED (FRAMES 8-11) · airframe 68,952 hrs · 30,886 cycles

CRACK ON WEB +Y765 BETWEEN FRAME 8 TO FRAME 11 FLOOR STRUCTURE IN COCKPIT. REPLACED WEB -Y765 BETWEEB FRAME 8 TO FRAME 11 FLOOR STRUCTURE IN COCKPIT IAW SRM 51-72-11 AND DWG D53113219.

Part: DOOR SILL — CORRODED (FRAME 16) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON LOWER DOOR SILL FRAME 16 AND STRINGER 23R. REPLACED IAW SRM 51-72-11 AND DWG D53110339.

Part: WEB — CORRODED (FRAMES 58-59) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SUPPORT WEB BETWEEM FRAMES 58 - 59, STR 38L. REPLACED THE SUPPORT WEB IAW SRM 51-72-11 AND DWG D53470320.

Part: FLOOR SUPPORT — CORRODED (FRAMES 21-22) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT -Y1292 FRAMES 21 - 22. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53112812 AND D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-21) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT -Y189 FRAMES 20 - 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: FRAME SPLICE — DAMAGED (FRAME 24) · airframe 68,952 hrs · 30,886 cycles

ELONGATED HOLES ON SPLICE LOCATED AT FRAME 24 -Y254. REPLACED SPLICE LOCATED AT FRAME 24 -Y254 INBD AND OTBD IN PASSENGER CABIN 2 EA IAW SRM 51-72-11 AND DWG D53110920.

Part: FITTING — CORRODED (FRAME 66) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON CORNER FITTING FRAME 66. REPLACED THE FITTING IAW SRM 51-72-11, DWG D53480019 AND D53480505.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON LOWER DOOR SILL BETWEEN FRAMES 66 - 68. REPLACED DOOR SILL IAW SRM 51-72-11, DWG D53480019, D53474250 AND D53480076.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON LOWER DOOR SILL LOCATED FRAMES 66 - 68. REPLACED THE DOOR SILL IAW SRM 51-72-11, DWG D53480019, D53474250, AND D53480076.

Part: FITTING — CORRODED (FRAMES 66-68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON CENTER FITTING BETWEEN FRAME 66 - 68. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: FITTING — CORRODED (FRAME 68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON CORNER FITTING FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11, DWG D53480019 AND D53880505.

Part: FITTING — CORRODED (FRAMES 66-67) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON CENTER FITTING FRAME 66+5 - 67+16. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: CROSSBEAM — DAMAGED (FRAME 68) · airframe 68,952 hrs · 30,886 cycles

ELONGATED HOLE ON CROSSBEAM SECTION IN PASSENGER CABIN ON FRAME 68 AND -Y1162. REPLACED CROSSBEAM SECTION IN PASSENGER CABIN ON FRAME 68 AND - Y1162 IAW SRM 51-72-11 AND DWG D53474250.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT -Y1162 LOCATED BETWEEN FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040.

Part: FRAME — CORRODED (FRAME 68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FRAME 68 AT STR 23L. REPAIRED THE FRAME IAW SRM 53-41-12, TABLE 202, PARA 5.A, FIGURE 201, PAGE 202 TO PAGE 208.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK -Y1292 FRAMES 41 TO 47. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D533 71112.

Part: FITTING — CORRODED (FRAME 68) · airframe 68,952 hrs · 30,886 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT +Y512 BETWEEN FRAMES 64 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472040.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 68,952 hrs · 30,886 cycles

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

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK +Y765 FROM FRAMES 12 - 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG D53110920, DWG D53110984.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK +Y1292 FROM FRAMES 12 - 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG D53110920 AND DWG D53110984.

Part: WEB — CORRODED (FRAME 20) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON WEB, FRAME 20, STRINGER 23R. REPLACED THE WEB IAW SRM 51-72-11, DWG D53114392, AND D53112784.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-22) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT -Y765, FRAMES 20 - 22. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG NR D53110920, D53110984, AND D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT +Y1225 BETWEEN FRAMES 66 - 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT Y1292 LOCATED BETWEEN FRAMES 64 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON FLOOR SUPPORT +Y1162 BETWEEN FRAMES 68 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,952 hrs · 30,886 cycles

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

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK, +Y765, FRAME 36 - 41 IN PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130147.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK +Y1292, FRAME 41 TO 47 IN THE CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D533-7112.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 68,952 hrs · 30,886 cycles

CORROSION FOUND ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 TO 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472035 AND D53472229

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 68,952 hrs · 30,886 cycles

CORROSION ON SEAT TRACK +Y1292, FRAME 36 - 41 IN PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D533-71112.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON INSERT OF FLOOR PANEL 262AB. REPLACED THE FLOOR PANEL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · airframe 68,952 hrs · 30,886 cycles

CORROSION FOUND ON THE FLOOR SUPPORT +Y160 BETWEEN FRAMES 68 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040 AND D53474250.

Part: FLOOR SUPPORT — CORRODED (FRAMES 14-16) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON FLOOR SUPPORT Y503.2, FRAMES 14 TO 16. REPLACED THE FLOOR SUPPORT.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON INSERT OF FLOOR PANEL 261PF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT GALLEY) · airframe 72,865 hrs · 32,764 cycles

CORROSION ON INSERT OF FLOOR PANEL 261AB IN THE AFT GALLEY AREA. REPLACED INSERT ON THE FLOOR PANEL.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 68,867 hrs · 30,850 cycles

EMERGENCY LIGHT TEST FAILED EPSU, IAW AMM 33-51-00. REPLACED EPSU 11WL AND FUNCTIONAL CHECK WAS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,755 hrs · 30,801 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 21 INOPERATIVE. REPAIRED ROW 21 EMERGENCY LIGHT WIRING IAW ESPM 20-25-21.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,755 hrs · 30,801 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 6 INOPERATIVE. REPAIRED ROW 6 EMERGENCY LIGHT WIRING IAW ESPM 20-25-21.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 68,083 hrs · 30,486 cycles

LEFT INBD FLAP BOTTOM SKIN DAMAGED. REPAIRED IAW SRM 57-52-00.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 72,865 hrs · 32,764 cycles

EVIDENCE OF CORROSION ON SKIN AT STRINGER 42L BETWEEN FRAMES 56 AND 57. REPAIRED IAW SRM AND ER/A.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 72,865 hrs · 32,764 cycles

EVIDENCE OF CORROSION ON SKIN AT STRINGER 43L BETWEEN FRAMES 56 AND 57. REPAIRED THE SKIN.

Part: LIGHT — INOPERATIVE (ROW 19) · airframe 67,482 hrs · 30,214 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROW 19 ABC INOPERATIVE. INSTALLED A NEW LIGHT ASSY AND FUNCTIONAL CHECKED NORMAL.

Part: LIGHT — DAMAGED (SEAT 21) · airframe 64,957 hrs · 29,053 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHT DAMAGED OR INOPERATIVE AT SEAT 21. MAINTENANCE REPLACED DAMAGED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,431 hrs · 28,292 cycles

DURING NON-ROUTINE CHECK, FOUND EVACUATION LIGHTS AT ROWS 1, 2, 3, 5, 6, 7 INOPERATIVE WHEN ACFT IS NOT POWERED. REPLACED FORWARD EPSU BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,240 hrs · 28,194 cycles

DURING NON ROUTINE CHECK, FOUND FWD LT EPSU SHOWS INTERNAL LOAD FAULT. MX RESET FWD LT EPSU AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 61,910 hrs · 27,540 cycles

DURING NON ROUTINE CHECK, FOUND 1R DOOR EMERGENCY LIGHT BROKEN. MX REPLACED THE LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,025 hrs · 23,408 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 13WL AFT CABIN INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LGIHTS) · airframe 52,233 hrs · 23,116 cycles

TEST OF EMERGENCY LIGHTS FOUND SEAT 16 PATH LIGHT INOP, REPAIRED BROKEN CONNECTOR AT SEAT TRACK AND CHECKS OK.

Part: LIGHT — FAILED (ESCAPE SLIDE) · airframe 50,175 hrs · 22,273 cycles

SLIDE EPSU FAILED EMERGENCY LIGHT SYSTEM CHECK, REPLACED SLIDE AND TESTED GOOD.

Part: BUTTSTRAP — DENTED (FUSELAGE) · airframe 48,186 hrs · 21,379 cycles

DURING GROUND OPS FR 24 BUTT SPLICE STRAP WAS DENTED AT S35L. REPAIRED PER EA 32-213810.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,494 hrs · 19,632 cycles

EMERGENCY ESCAPE LIGHTING, EPSU 13WL INOP. REPLACED EPSU 13WL AND BATTERY, CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,114 hrs · 19,438 cycles

RT EMERGENCY POWER SUPPLY UNIT BATTERY PACK READS ZERO VOLTS. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OP CHECKS GOOD.

Part: CONTROLLER — FAILED (OVEN) · airframe 38,898 hrs · 17,074 cycles

DURING CLIMB, A BURNING ODOR WAS NOTED IN THE COCKPIT AND SMOKE/HAZE REPORTED IN CABIN. DECLARED YELLOW EMERGENCY AND RETURNED TO MEM AND LANDED UNEVENTFULLY. FOUND ROW 25 LEFT OVERHEAD FLUORESCENT LAMP INOP. FOUND NO EVIDENCE OF BURNED PINS. RELAMPED AND CHECKED OK. NOTED BURNED CONNECTOR PIN ON NR 1 OVEN CONTROLLER. REPLACED NR 1 OVEN CONTROLLER AND CHECKED GOOD. REPLACED AVIONICS VENTILATION FILTER. PRESSURIZED AIRCRAFT, RAN ALL ELECTRICS AND LIGHTS, CHECKED OK. AIRCRAFT RETURNED TO SERVICE.

Part: CHECK VALVE — INOPERATIVE (RT PACK BAY) · airframe 35,912 hrs · 15,683 cycles

WITH NR 1 PACK ON MEL, PASSING ABOUT 15,000 FT MSL, CREW NOTED A RUMBLE IN THE AC DUCT SYSTEM. CABIN CLIMB RATE WAS ABOUT 650-700 FPM. AT FL240, CREW NOTED A STRONG RUMBLE AND VIBRATION AND INCREASE IN CABIN CLIMB RATE. THE 10,000 FT CABIN ALTITUDE WARNING SOUNDED AND THE CREW DONNED OXYGEN MASKS AND BEGAN EMERGENCY DESCENT UNTIL CABIN ALTITUDE STABILIZED BELOW 10,000 FT. CONTINUED TO DTW AND LANDED UNEVENTFULLY. REPLACED NR 2 PACK DOWNSTREAM CHECK VALVE AND SLEEVE/SEALS BETWEEN THE NR 2 PACK HEAT EXCHANGER AND ACM. BOTH PACKS LEAK AND OPERATIONAL CHECK GOOD. CLEARED NR 1 PACK MEL. AIRCRAFT RETURNED TO SERVICE.

Part: RESERVOIR — LACK OF LUBE (HYD SYSTEM) · airframe 26,729 hrs · 11,601 cycles

DURING APPROACH, RECEIVED HYD G RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURE, GRAVITY EXTENDED LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESERVICED THE GREEN HYDRAULIC SYSTEM. LEAK AND OPERATIONAL CHECK NORMAL.

Part: SERVO — LEAKING (LT ELEVATOR)

DURING CRUISE, RECEIVED HYD B SYS LOW PR MESSAGE. LOW SYSTEM QUANTITY AND LOW SYSTEM PRESSURE WAS CONFIRMED. SHUT OFF BLUE SYSTEM HYDRAULIC PUMP, CONTINUED TO DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT OUTBOARD ELEVATOR SERVO. LEAK AND OPERATIONAL CHECK OK.

Part: ENGINE — FAILED (NR 1)

DURING DESCENT WITH POWER AT FLIGHT IDLE, ENG 1 FAIL ECAM MESSAGE ANNUNCIATED AND NR 1 ENGINE AUTO SHUT DOWN. ONE SUCCESSFUL RELIGHT WAS ATTEMPTED. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND NR 1 ENGINE FUEL FILTER CONTAMINATED WITH BRONZE. REPLACED THE NR 1 ENGINE.

Part: SENSOR — FAILED (LT MLG)

ON APPROACH AFTER LANDING GEAR SELECTED DOWN, THE LEFT MAIN GEAR UNLOCKED INDICATION MESSAGE WAS DISPLAYED. CREW RECYCLED LANDING GEAR. DECLARED AN EMERGENCY AND PERFORMED A GRAVITY EXTENSION RESULTING IN ALL THREE GEAR INDICATING DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN DOWNLOCK SENSOR 15GA, OPERATIONAL CHECK OK.

Part: RESERVOIR — LOW LEVEL (YELLOW HYD SYST)

DURING POWER APPLICATION FOR TAKEOFF, HYD Y RSVR LO LVL MESSAGE ILLUMINATED. TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLENISHED THE FLUID IN THE YELLOW HYDRAULIC SYSTEM.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB)

DURING CLIMBOUT AT APPROXIMATELY 600 FEET AGL, RECEIVED 'F/CTL ELAC 2 PITCH FAULT' ACCOMPANIED BY UNCOMMANDED 2 TO 3 DEGREE PITCH DOWN INPUTS AND SLUGGISH PITCH RESPONSE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR, OPERATIONAL CHECK OK.

Part: UNLOCK ASSY — MALFUNCTIONED (LT MLG DOOR)

DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G DOORS NOT CLOSED MESSAGE. LEFT MAIN LANDING GEAR DOOR INDICATED OPEN. CYCLED LANDING GEAR HANDLE WITH NO CHANGE IN INDICATION. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR UPLOCK ASSEMBLY, OPERATIONAL CHECK OK.

Part: INDICATION — MALFUNCTIONED (LDG GEAR DOOR)

DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G DOORS NOT CLOSED MESSAGE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCY.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE WHILE PERFORMING THE EMERGENCY LIGHTS SYSTEM TEST, THE FORWARD LEFT BATTERY FAULTED. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: TARGET BOLT — FAILED (LT MLG DOOR)

DURING CLIMBOUT, RECEIVED L/G DOORS NOT CLOSED MESSAGE ON ECAM. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR UPLOCK TARGET BOLT. OPERATIONAL CHECK OK.

Part: PROXIMITY SENSOR — FAILED (LT MLG)

DURING LANDING GEAR RETRACTION AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE CLOSED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR (27GA), OPERATIONAL CHECK OK.

Part: PROXIMITY SW — DIRTY (LT MLG DOOR)

BOS - DURING APPROACH, AFTER THE LANDING GEAR WAS EXTENDED RECEIVED L/G DOORS NOT CLOSED MESSAGE. THE LEFT MAIN LANDING GEAR DOOR INDICATED PARTIALLY OPEN ON ECAM. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CYCLED LANDING GEAR HANDLE. ALL INDICATIONS NORMAL AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE CANNON PLUGS ON BOTH MAIN LANDING GEAR DOOR PROXIMITY SWITCHES AND OPERATIONAL CHECK OK.

Part: HANDLE — NOT STOWED (AFT CARGO DOOR)

DURING TAKEOFF ROLL, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE NOT FAIRED. STOWED HANDLE AND ALL INDICATIONS WERE NORMAL.