N330NW

Part: OXYGEN BOX — OPEN (ZONE 200) · airframe 88,947 hrs · 41,536 cycles

SHIP 3230 DISC: O2 MASK COMPARTMENT ABOVE L1 FA JUMPSEAT OPENED, DROPPING BOTH O2 MASKS. C/A: RESECURED FWD FA MASK IAW A320 AMM 35-21-41. A/C OK SERVICE. (LP: 5980116)

Part: TACHOMETER — FAULTED (ZONE 700) · airframe 88,649 hrs · 41,384 cycles

SHIP 3230 DISC: ON FINAL APPROACH WHEN WE LOWERED THE LANDING GEAR WE RECEIVED " BRAKES AUTO BRAKE FAULT" CAUTION. DID A GO AROUND AND LANDED WITH MANUAL BRAKES. AFTER LANDING WE NOTICED THE #3 BRAKE WAS RELEASED. C/A: REMOVED AND REPLACED #3 MLG TACHOMETER PER A320 AMM 32-42. FUNCTIONAL CHECK OK. (LP: 6682062)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 88,234 hrs · 41,196 cycles

SHIP 3230 DISC: EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:22D. C/A: SECURED 22D EMERGENCY LITE ASSY OPS OK IAW AB320 AMM 33/51. (LP: 0586191)

Part: BOTTLE — LOW PRESSURE (EMERGENCY OPS) · airframe 88,106 hrs · 41,122 cycles

SHIP 3230 DISC: ON SVC CHK FOUND DOOR R1 EMER OPERATING ACCUMULATOR PRESSURE LOW. C/A: RE-CHARGED EMER OPERATING CYLINDER IAW A320 AMM 52-10. OK FOR SVC. (LP: 5127279)

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 88,106 hrs · 41,122 cycles

SHIP 3230 DISC: ON SVC CHK FOUND ALL FOUR OVERWING EXIT HATCH HANDLE ILLUMINATION EMER. LIGHTS INOP. C/A: FOUND PWR CONNECTOR DISCONNECTED FROM LH FWD LIGHT ASSY. RE-SECURED SAME AND RE-LAMPED BOTH RH LIGHT ASSY AND LH AFT LIGHT ASSY. OPS CHK ALL DOOR EMER LIGHT SYS IAW A320 AMM 33-51. OK FOR SVC. (LP: 5127280)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 87,818 hrs · 40,958 cycles

SHIP 3230 DISC: O2 MASK DROPPED ON T/O BY DOOR 2R IN R/H GALLEY. C/A: *** CONTRACT MAINTENANCE EVENT - OCM: 285615 *** STOWED O2 MASK AND SECURED DOOR TEMP CLOSED. PERFORMED MANUAL RELEASE OF O2 SYSTEM IAW A320 AMM 35-23. LATCH AT 2R WILL NOT STAY CLOSED WHEN IN THE LOCKED POSITION.DEFER AFT SWIVEL F/A SEAT O2 MASK PER MEL 35-21-01E. M-PROCEDURE C/W PLACARD INSTALLED. R/R CONTAINER PER A320 AMM 35-21, CKS GOOD. OK RO REMOVE MEL & PLACS. REV "M" PROCS C/W. OK FOR SVC. (LP: 6079254)

Part: ARMING LEVER — FAULTED (DOOR) · airframe 86,856 hrs · 40,414 cycles

SHIP 3230 DISC: FA REPORTS THAT AT DOOR 2R ARM/DISARMED WILL NOT WORK PROPERLY WITH PIN INSTALLED. C/A: FOUND SIMILAR PROBLEM ON DOOR 2L. 2L AND 2R ARE ABLE TO ARM WITH PIN INSTALLED. REPLACED SLIDING ARMING PINS NO HELP W.I.P 957193 REMOVED BOTH 2L AND 2R ARMING LEVERS PER A320 AMM 52-13 WIP 313880 OK TO INSTALL REPLACEMENT ARMING LEVERS ON 2LAND 2R DOORS QC 5363 REPLACED 2L AND 2R DOOR ARMING LEVERS RIG AND OPS CHECK CW REF A320 AMM 52-13 WIP CE827027 RII C/W QC536. (LP: 5403452)

Part: FUEL SYS — MALFUNCTIONED · airframe 86,785 hrs · 40,381 cycles

INBOUND WRITE UP- FUEL AUTO FEED FAULT IN FLIGHT. LEFT TANK LESS THAN 11,000 WITH MORE THAN 550 IN CENTER TANK, FUEL INBALLANCE APPROX 3,000 LBS. QRH 12.3 AND 12.9 COMPLIED WITH. OPS RETURNED TO NORMAL. REDISTRIBUTED FUEL AS NEEDED IAW A320 AMM 28-00-00 IN ORDER TO CLEAR FAULT.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 86,785 hrs · 40,381 cycles

SHIP 3230 DISC: 1R DOOR ASSIST BOTTLE BELOW SVC CHECK LIMITS. C/A: SERVICED 1R EMERGENCY OPERATING CYLINDER/ACCUMULATOR I.A.W. A320 AMM 52-10-00-610-801C1 NO LEAKS, OPS CHK GOOD, A/C OKAY OKAY FOR SVC. (LP: 5403409)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,553 hrs · 40,263 cycles

SHIP 3230 DISC: REWORK REQUIRED PER ER/A 605439-14 REV C. SEE SECTION II: REWORK FOR REWORK DETAILS. C/A: REWORK REQUIRED PER ER/A 605439-14 REV C. SEE SECTION II: REWORK FOR REWORK DETAILS. PREVIOUS REPAIR AT FR8 ABOVE STRINGER 31R. ASSOCIATED ER/A 14-605439 ADDED FOR AC 3230. (LP: 0222221)

Part: PACKING — DAMAGED (HYD CHK VALVE) · airframe 86,454 hrs · 40,203 cycles

SHIP 3230 - MISC/DE - DUE TO HYD Y RSVR LO LVL ECAM MESSAGE. ALL HYDRAULIC PRESSURES NORMAL. QUANTITY AT 0. CORRECTIVE ACTION: FOUND PACKING ON YELLOW SYSTEM HP MANIFOLD CHECK VALVE PLUG DAMAGED. REPLACED SAME. LEAK CHECK GOOD.

Part: NONE — NONE (NONE) · airframe 86,258 hrs · 40,097 cycles

SHIP 3230 DISC: PHOTO NEEDED FOR STAGE II AND III DAMAGE REQUIREMENTS. REFERENCE ERA 605439-14 FOR DAMAGE LOCATION. ASSOCIATED LOG 2720022. C/A: TAKE PHOTOS OF DAMAGE AREA INSIDE AND OUTSIDE. INSIDE PHOTOS NEED TO BE FRONT BACK AND SIDES OF REPAIR FOR AIRBUS REVIEW. EMAIL PHOTOS TO ENGINEERING @ ATL555, LIAISONENG. SENT EMAIL WITH PICTURES TO ATL 555 LIAISON ENG AS REQUESTED. (LP: 0166704)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,286 hrs · 39,039 cycles

SHIP 3230 MANY N/R'S NEEDED FOR ERA 604084-14 BIRDSTRIKE REPAIRS. CORRECTIVE ACTION: COMPLIED WITH ALL NON-ROUTINES. (2774342)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 #1 ENGINE FAILED FADEC MOTORING TEST DURING PREFLIGHT. CH 1B FAULT-LPTC VLV. CORRECTIVE ACTION: INSTALLED NEW LPTACC PER A320 AMM 75-22-10. (2770013)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 NEED TO REPLACE LHS LATERAL WINDOW FRAME. CORRECTIVE ACTION: REPLACED FRAME PER ERA 604084-14 REV ORIG. OK FOR SERVICE. MAJOR REPAIR. (2756043)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 BIRD STRIKE/LOWER FRAME 8/CRACK AND DEFORMATION. CORRECTIVE ACTION: REPAIRED DAMAGE ON NRC 156 AND ERA 605439-14 REV A. FOLLOW UP INSP REQUIRED WITHIN 12 MONTHS. (2725587)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 ER/A 605439-14 REV A TRACKING FOR AIRCRAFT 3230. BIRD STRIKE AIRCRAFT. CORRECTIVE ACTION: COMPLIED WITH ERA. (2720022)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 REPLACEMENT CROWN SKIN HAS A MIS-DRILLED FASTENER HOLE AT FR11, AND INTERIOR INTERCOSTAL (8" FROM RIGHT EDGE AND 10" FROM AFT EDGE OF SKIN). MARKED. CORRECTIVE ACTION: COMPLIED WITH ERA 607816-14 REV ORIGINAL. (2717575)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 REV ORIGINAL FRAME 12 PERM REPAIR NEEDED. CORRECTIVE ACTION: COMPLIED WITH ERA 606392-14 REV ORIGINAL. (2716456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FUSELAGE SKIN FR15-FR16 SPLICE REPAIR DUE TO BIRD STRIKE. CORRECTIVE ACTION: COMPLIED WITH ERA 605603-14 REV ORIG. (2716420)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 REMOVE AND REPLACE FR11 DAMAGED DURING BIRD STRIKE. CORRECTIVE ACTION: COMPLIED WITH ERA 606266-14 REV ORIGINAL. (2716461)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FUSELAGE / FRAMES / LHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT DUE TO BIRDSTRIKE. CORRECTIVE ACTION: COMPLIED WITH ERA 604084-14 SECTION I. (2714792)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FUSELAGE / FRAMES / LHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT DAMAGED FROM BIRSTRIKE. CORRECTIVE ACTION: COMPLIED WITH ERA 604084-14 REV ORIGINAL SECTION II. (2714717)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 ESTABLISHING DTE RESTRICTION FOR ER/A 604084-14. REPAIR APPROVAL IS LIMITED TO 30,000 FLIGHT CYCLES FROM DATE OF APPROVAL ONLY. CORRECTIVE ACTION: COMPLIED WITH, (2714806)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 SRM REPAIR FOLLOW-ON INSPECTION REQUIRED FOR BUSHING REPAIR OF FUSELAGE SKIN PER ER/A 607816-14 AT FR11, RHS, ABOVE W/S UPPER SILL. CORRECTIVE ACTION: COMPLIED WITH. (2713274)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FORWARD FUSELAGE UPPER FO BIRD STRIKE DAMAGE SITE #3 FR9. CORRECTIVE ACTION: COMPLIED WITH MAJOR REPAIR (2708839)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 NEED TO COMPLY WITH ERA 606550-14 REV ORIG FWD FUSELAGE LHS FRAME 3 PERMANENT REPAIR. CORRECTIVE ACTION: COMPLIED WITH. (2705193)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 ER/A 606392-14; ESTABLISHING 100,000 FLIGHT CYCLE RESTRICTION. CORRECTIVE ACTION: COMPLIED WITH. (2703869)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 NEED TO ACCOMPLISH ER/A 605354-14 REVISION ORIGINAL SECTION II BIRD STRIKE MAJOR REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA. (2695915)

Part: UNKNOWN — UNKNOWN · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FR15-FR16 / SPLICE REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 605603-14. (2674288)

Part: UNKNOWN — UNKNOWN · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 A320 / FUSELAGE / SKIN / FR15-FR16 / SPLICE REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 605603-14. (2674267)

Part: NONE — NONE · airframe 84,275 hrs · 39,033 cycles

SHIP 3230 FRAME 3 DAMAGED FROM BIRDSTRIKE. CORRECTIVE ACTION: REPAIRED PER MULTIPLE NON-ROUINES AND A320 SRM 51-40-02. OK FOR SERVICE. (2659702)

Part: FRAME — DAMAGED · airframe 84,272 hrs · 39,032 cycles

DAMAGE TO FRAMES 2,3,8,9,10,11, AND 12. PARTS WERE REQUIRED TO BE FABRICATED BY PMSG. REPAIR PART FABRICATION INSTRUCTIONS WERE PROVIDED BY ENGINEERING ON ERA 604142-14. CORRECTIVE ACTION: COMPLIED WITH ERA. (2571829)

Part: UNKNOWN — DAMAGED · airframe 84,272 hrs · 39,032 cycles

DAMAGE FOUND DURING GVI IN PILOT REPORT OF BIRD STRIKE. DAMAGE LOCATED ON L/H OF A/C FWD OF CAPTAINS WINDOW AND AFT OF RADOME 20'' ABOVE STATIC PORT. COMPLIED WITH ERA 603955-14 REV.ORIG TO PRI 603955-14 REVS 0 THRU 2.

Part: NONE — NONE (NONE) · airframe 84,272 hrs · 39,032 cycles

DAMAGE FOUND DURING GVI IN PILOT REPORT OF BIRD STRIKE. DAMAGE LOCATED ON R/H OF A/C ABOVE AND AFT OF FIRST OFFICERS WINDOW FWD OF FRAME 12. CORRECTIVE ACTION: COMPLIED WITH PRI 603956-14 REV 2. (2570664)

Part: FRAME — DENTED (FRM 10) · airframe 84,272 hrs · 39,032 cycles

DURING REPAIR OF DAMAGE ON FRAME 10 FOUND DENT ABOVE REPAIR AREA. COMPLIED WITH PRI 604384-14.

Part: NONE — NONE (NONE) · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 AFTER FRAME 9 REPAIR COMPLETED ON LOG PAGE: 2530575 ENGINEERING REDESIGNATED REPAIR AS TIME LIMITED. CORRECTIVE ACTION: COMPLIED WITH ERA 604384-14 REV. ORIG SECTION II. (2570767)

Part: NONE — NONE (NONE) · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 AFTER FRAME 10 REPAIR COMPLETED ON LOG PAGE: 2530550 ENGINEERING REDESIGNATED REPAIR AS TIME LIMITED (BIRD DAMAGE) CORRECTIVE ACTION: COMPLIED WITH ERA 604384-14 REV. ORIG SECTION III

Part: FRAME — CRACKED · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 DURING OPEN UP FOR DAMAGE ON N/R 6 FOUND FRAME 3 CRACKED. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S. (2570813)

Part: FRAME — CRACKED (FRM 11) · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 DURING OPEN UP FOR DAMAGE ON N/R 9 FOUND FRAME 11 CRACKED. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S. (2559193)

Part: FRAME — CRACKED (FRM 2) · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 DURING OPEN UP FOR DAMAGE ON N/R 6 FOUND FRAME 2 CRACKED. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S. (2559280)

Part: NONE — NONE (NONE) · airframe 84,272 hrs · 39,032 cycles

DAMAGE FOUND DURING GVI IN PILOT REPORT OF BIRD STRIKE. DAMAGE LOCATED BELOW LOWER SKIN LAP AFT OF RADOME FWD OF AVI BAY ACCESS DOOR. COMPLIED WITH MULTIPLE ERA'S. (2557902)

Part: FRAME — CRACKED (FRM 8) · airframe 84,272 hrs · 39,032 cycles

DURING OPEN UP FOR DAMAGE ON N/R 4, FOUND FRAME 8 CRACKED. COMPLIED WITH MULTIPLE ERA'S.

Part: FRAME — CRACKED (FRM 12) · airframe 84,272 hrs · 39,032 cycles

DURING OPEN UP FOR DAMAGE ON N/R 9 FOUND FRAME 12 CRACKED. COMPLIED WITH MULTIPLE ERA'S.

Part: FRAME — CRACKED · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 DURING OPEN UP FOR BIRD STRIKE DAMAGE ON N/R 9 FOUND FRAME 10 CRACKED. (DAMAGE 3). CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-11-12. (2530550)

Part: FRAME — CORRODED · airframe 84,272 hrs · 39,032 cycles

SHIP 3230 FOUND FRAME 9 CRACKED. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-11-12. (2530575)

Part: NONE — NONE · airframe 83,531 hrs · 38,605 cycles

SHIP 3230 -ATO- AT 50 KNOTS DUE TO SPOILER 3 AND 4 FAULT MESSAGE. CORRECTIVE ACTION: DEFERRED SPOILERS 3 AND 4 PER MEL. REMOVED AND REPLACED SPOILER ELEVATOR COMPUTER PER A320 AMM 27-64. OPS CHECK WAS GOOD. MEL/PLAC REMOVED. (9108744)

Part: NONE — NONE · airframe 83,292 hrs · 38,454 cycles

SHIP 3230 DOOR DAMPER ON R2 (842) FAILED OPERATIONAL TEST. CORRECTIVE ACTION: CURRENTLY DEFERRED. DAMPER TO BE REPLACED PER A320 AMM 52-15. (6758238)

Part: NONE — NONE · airframe 83,292 hrs · 38,454 cycles

SHIP 3230 R1 DOOR DAMPER WEAK. CORRECTIVE ACTION: CURRENTLY DEFERRED. DAMPER TO BE REPLACED PER A320 AMM 52-15. (6758241)

Part: NONE — NONE · airframe 83,292 hrs · 38,454 cycles

SHIP 3230 DOOR L2 DAMPER WEAK. CORRECTIVE ACTION: CURRENTLY DEFERRED. DAMPER TO BE REPLACED PER A320 AMM 52-15. (6758239)

Part: NONE — NONE · airframe 83,292 hrs · 38,454 cycles

SHIP 3230 L1 (831) DAMPENER FUNCTION WEAK. CORRECTIVE ACTION: CURRENTLY DEFERRED. DOOR DAMPER TO BE REPLACED PER A320 AMM 52-15. (6758240)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 INOP EPSU-EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU PER A320 AMM 33-51-38. OK FOR SERVICE. (2306183)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION FOUND IN RH FWD KEEL BEAM CONNECTING PLATE AT LOWER FASTENER HOLE AFT POSITION. CORRECTIVE ACTION: COMPLIED WITH ER/A 599728-14AD REV. ORIGINAL. (2303428)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION FOUND IN RH FWD KEEL BEAM HINGE FITTING AT LOWER FASTENER HOLE AFT FACE. CORRECTIVE ACTION: COMPLIED WITH ERA 599728-14AD REV. ORIGINAL. (2303433)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 832 DAMPER DOES NOT WORK CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-10-04. OK FOR SERVICE. (6758225)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION ON FRAME 16 LH SIDE IN INTERCOSTAL FITTING OPEN FASTENER HOLE 1 AT DOOR STOP 7 POSITION. CORRECTIVE ACTION: COMPLIED WITH ERA 599689-14AD REV. ORIGINAL. (2303586)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 842 DAMPER DOES NOT WORK CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-10-04. OK FOR SERVICE. (6758224)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION ON FRAME 16 RH SIDE IN INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION. CORRECTIVE ACTION: COMPLIED WITH ER/A 599688-14AD REV. A. (2303643)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 841 DOOR DAMPER CYLINDER AT FWD GALLEY AREA DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-10-04. OK FOR SERVICE (6758227)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION ON FRAME 16 LH SIDE IN INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION. CORRECTIVE ACTION: COMPLIED WITH ER/A 599689-14AD REV. ORIGINAL. (2303613)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION ON FRAME 16 RH SIDE IN INTERCOSTAL FITTING OPEN FASTENER HOLE 1 AT DOOR STOP 7 POSITION. CORRECTIVE ACTION: COMPLIED WITH ER/A 599688-14AD REV. A. (2303636)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 831 DOOR DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER PER A320 AMM 52-10-04. (6758226)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION FOUND IN RH FWD KEEL BEAM HINGE FITTING AT LOWER RADIUS FWD FACE. CORRECTIVE ACTION: COMPLIED WITH ER/A 599728-14AD REV. ORIGINAL. (2303434)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK INDICATION FOUND IN OPEN FASTENER HOLE OF THE INNER SIDE OF THE UPPER ATTACHMENT OF THE WINDSHIELD SIDE POST FRAME 4 L/H. CORRECTIVE ACTION: COMPLIED WITH ERA 599520-14AD REV. ORIGINAL. (2302315)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION RUDDER HINGE 6 BEARING ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED OF RUDDER HINGE BEARING PER A320 AMM 55-46-11. OK FOR SERVICE. (2301136)

Part: NONE — NONE · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACKS FOUND IN RHS FWD HINGE AND ACTUATOR FITTINGS AND CONNECTING PLATE. CORRECTIVE ACTION: COMPLIED WITH ERA 599728-14AD. OK FOR SERVICE. (2299121)

Part: BUSHING — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 831 UPPER AND LOWER CONNECTION LINK BONDED BUSHINGS WORN ON THE SUPPORT ARM AND INTERNAL DOOR CONNECTION LINK AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-11-21. (2289073)

Part: FRAME — COLD SOLDER JT · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 NEED TO COLDWORK HOLE 8 AND HOLE 9 IN ACCORDANCE WITH WORK CARD 5311-01171-03A. CORRECTIVE ACTION: COMPLIED WITH COLD WORKING. OK FOR SERVICE. (2289588)

Part: DOOR — OUT OF ADJUST · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 831 OUT OF ADJUSTMENT/HARD TO OPEN. CORRECTIVE ACTION: RIGGED DOOR PER DELTA WORKCARD AMDS 5210-7089-LF. OK FOR SERVICE. (2289585)

Part: DOOR — OUT OF ADJUST · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 831 HARD TO OPEN/OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF PASSENGER CREW DOOR 831 PER A320 FAM AMM 52-11-21. (2289578)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION STRINGER 26R LOC.BTW FR66 AND FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SECTION STRINGER, SPLICE AND FASTENERS PER A320 SRM 51-42-11 AND 51-72-11. (2288093)

Part: LINK — EXCESS PLAY · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 832 ON UPPER AND LOWER CONNECTION LINKS HAVE EXCESSIVE PLAY. CORRECTIVE ACTION: REPLACED LINKS PER A320 AMM 52-10-00. OK FOR SERVICE. (2287537)

Part: HINGE — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 WEAR ON RUDDER HINGE 5 IN VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED RUDDER HINGE 5 IN VERTICAL STABILIZER PER A320 SRM 51-42-11 AND 51-72-11. OK FOR SERVICE. (2287490)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION FLOORBEAM -Y765 LOC. FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-11. (2288092)

Part: ROLLER — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 831 ROLLERS UPPER AND LOWER FWD WORN. CORRECTIVE ACTION: REPLACED ROLLERS PER A320 AMM 52-11-31. OK FOR SERVICE. (2287559)

Part: ATTACH FITTING — CORRODED · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION ATTACH FITTING ELEVATOR ACTUATOR INBOARD FITTING INBOARD LUG ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED I/B ATTACH FITTING PER A320 SRM 55-26-47. (2287569)

Part: CROSSBEAM — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION INTERNAL STRUCTURE CROSSBEAM LOCATED FR58 AND BTW STR 38R TO STR 38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: INSTALLED NEWCROSS BEAM, BRACKETS (5EA) AND SUPPORT FITTING (1EA) PER A320 SRM 51-42-11 AND 51-72-11. (2286574)

Part: SUPPORT ANGLE — CRACKED · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CRACK SUPPORT ANGLE ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE ELEVATOR HINGE ARM PER 320 SRM 51-42-11 AND 51-72-11. (2286536)

Part: ROLLER — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 WEAR ON PASSENGER CREW DOOR 841 ROLLER LOWER FWD AND AFT POSITION AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED ROLLERS. OK FOR SERVICE. (2282054)

Part: DOOR — OUT OF ADJUST · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 842 OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-13-21. OK FOR SERVICE. (2280528)

Part: DOOR — EXCESS PLAY · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 EXCESSIVE PLAY IN PASSENGER CREW DOOR 842 UPPER AND LOWER CONNECTION LINKS. CORRECTIVE ACTION: REPLACED LINKS. OK FOR SERVICE. (2280530)

Part: ROLLER — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 832 LOWER FWD AND AFT POSITIONS ROLLERS WORN. CORRECTIVE ACTION: REPLACED ROLLERS. OPS CHECK GOOD. (2269447)

Part: ROLLER — WORN · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 PASSENGER CREW DOOR 842 LOWER AFT POSITION ROLLERS WORN. CORRECTIVE ACTION: REPLACED ROLLERS. OPS CHECK GOOD. (2269443)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION FLOORBEAM Y-1250 LOC FR66 TO FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-11. (2268106)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION FLOORBEAM -Y1162 LOC FR68 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-11. (2268092)

Part: STRUT — CORRODED · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: R/R INTERCONNECTING STRUT PER A320 AMM 27-51-44. OK FOR SERVICE. (2265539)

Part: STRUT — CORRODED · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION INTERCONNECTING STRUT OB FLAP ON RH WING . CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH PER DELTA WORKCARD AMDS CARD 2750-6010-RT. (2265543)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 CORROSION FLOORBEAM -Y765 LOC. FR66 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-11. (2258835)

Part: FRAME — DAMAGED · airframe 83,291 hrs · 38,453 cycles

SHIP 3230 NEED TO COLDWORK HOLE 8 AND HOLE 9 IN ACCORDANCE WITH WORK CARD 5311-01171-03B PRIOR TO FURTHER FLIGHT IS REQUIRED. AA 5311- 01171, SB A320-53-1264, AD-2018-06-04. FR35 RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ALL PREVIOUSLY MENTIONED REFERENCES. OK FOR SERVICE. (2256961)

Part: NONE — NONE (NONE) · airframe 83,007 hrs · 38,327 cycles

SHIP 3230 - ATB - DUE TO AFT CARGO SMOKE INDICATION. CARGO FIRE EXTINGUISHER DISCHARGED BY CREW. SUSPECT SMOKE WAS CAUSED BY USE OF GSE EQUIPMENT NEAR THE CARGO DOOR PRIOR TO FLIGHT THAT RESULTED IN ACCUMULATION OF FUMES IN THE COMPARTMENT. CORRECTIVE ACTION: REPLACED CARGO FIRE EXTINGUISHER AND RETURNED TO SERVICE.

Part: HOLDER — BROKEN (EMERGENCY LIGHT) · airframe 82,705 hrs · 38,179 cycles

EMERGENCY PATH LIGHT ASSEMBLY BROKEN, REPLACED LAMP HOLDER AT SEAT 25 DEF

Part: BOTTLE — DAMAGED (OVERWING EXIT) · airframe 78,567 hrs · 36,074 cycles

RIGHT SIDE OVER WING EXIT INFLATION RESERVOIR WIRE CONTROL ASSEMBLY IS BROKEN AT CABLE END. REPLACED RESERVOIR BOTTLE.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 80,546 hrs · 37,026 cycles

AFT CARGO DOOR DURING SHOP VISIT OVERSIZED FASTENERS WERE INSTALLED AT 9 LOCATIONS BETWEEN OUTER SKIN AND FRAME FORKS FR53, FR54, FR54A, FR55, AND FR55A. REPAIRED PER ERA 567713-14AD SECTION I.

Part: SKIN — UNKNOWN (FRAME 64) · airframe 76,988 hrs · 35,361 cycles

EXISTING RE-WORK EXTERNAL SKIN AT FR 64+2 AND STRG 41R ON LOWER FUSELAGE, PERFORMED PERMANENT REPAIR EXTERNAL SKIN AT FR 64+2" AND STR 41R ON LOWER FUSELAGE AS PER ER/A 563230-14AD REVISION ORIGINAL AND PRI 563230-14 REVISION 0.

Part: PIN — OUT OF POSITION (CABIN) · airframe 74,629 hrs · 34,193 cycles

EPSU COMM EMER L SHOWN AFTER TEST OF EMER LIGHTS. INSPECTED TB 7225VT AND FOUND PIN PULLED OUT OF 6G POSITION, RESECURED SAME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,510 hrs · 33,685 cycles

EMERGENCY LIGHT TEST FAILED ON LEFT SIDE AFT EMERGENCY EXIT. REPLACED THE POWER SUPPLY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,853 hrs · 33,341 cycles

CRACK INDICATION FOUND IN OPEN HOLE ON CROSSBEAM SPLICING ON FRAME 16 FIRST HOLE FROM OTBD EDGE IN LATERAL AVIONIC COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATION ON CROSSBEAM SPLICING ON FRAME 16 FIRST HOLE FROM OTBD EDGE IN LATERAL AVIONINC COMPARTMENT LT IAW ER/A 546735-14 AD.

Part: SKIN — GOUGED (RT WING SLAT) · airframe 74,285 hrs · 34,053 cycles

SLAT GOUGED AT 2 LOCATIONS ON LWER SKIN TRAILING EDGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN ON SLAT 3 BTW RIB 7 TO RIB 8 ON RH WING IAW PRELIMINARY REPAIR INSTRUCTION ER/A 547917-14 REVISION 0 AND ER/A 545659-14 REVISION A, TABLE 1, ITEM 28 PAGE 17 AND ER/A 547917-14 REVISION ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,834 hrs · 38,245 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOC BTW FR72 TO FR73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FR 72 TO FR 73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE AS PER SRM 53-00-11 PARAGRAPH 4.W STEP 7(A) FIGURE 238 589/590, AS PER ER/A NR .545659-14 REVISION A ITEM 12.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 72,071 hrs · 32,980 cycles

CORROSION DAMAGE, 2 AREAS, TO THE INTERNAL SIDE OF THE SKIN, JUST OTBD OF S-43L, BETWEEN FRAME 56 TO FRAME 57. REPAIR IAW ERA 543887-14, REV O.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 72,071 hrs · 32,980 cycles

EVIDENCE OF CORROSION ON STR S43L BETWEEN FRAMES 56-57. REMOVED STR 43L MIDDLE OF FRAME 55 TO MIDDLE OF FRAME 58, SRM 53-00-13, FIG 201 IAW ERA 543887-14, REV O.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 71,990 hrs · 32,941 cycles

EMERGENCY LIGHT CHECK FAILS, EMERGENCY RT UNIT. REPLACED RT EPSU, W/O BATTERY.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 67,181 hrs · 30,588 cycles

DURING M-CHECK, A CRACK FOUND ON THE UPPER ATTACHMENT OF THE RT SLIDING WINDOW FRAME, IN HOLE NR 3 IAW ALI 53-11-35-PB6.

Part: STRINGER — CORRODED (FRAMES 64-65) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORRODED STRINGER 31R BETWEEN FRAMES 64 - 65 IN AFT CARGO BAY. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION LOCATED AROUND OF FLOOR PANEL 231AF AT FWD GALLEY AREA. REPLACED FLOOR PANEL.

Part: CLEAT — CORRODED (FRAME 33) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT FR 33 BETWEEN S41-42R IAW SRM 51-72-11 AND DWG D53230514.

Part: CLEAT — CORRODED (FRAME 31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT IAW SRM 51-72-11, DWGS D53231568, AND D53230811.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-21) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 AND 21, Y-1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 844. REPLACED LT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER FITTING AFT POSITION LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED LOWER FITTING, TEE SECTION, LOCATED AT AFT POSITION ON EMERGENCY EXIT HATCHES NR 833 IAW SRM 51-72-11 AND DWG D52279010.

Part: STRINGER — CORRODED (FRAMES 32-33) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40R BETWEEN FRAMES 32 TO 33 IN FWD CARGO BAY. REPLACED STRINGER 40R IAW SRM 51-72-11 AND DWG D53231568.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LOAD TRASMITING PROFILE, RT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834. REPLACED TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LOAD TRANSMITTING PROFILE LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834 IAW SRM 51-72-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LOAD TRANSMITTING PROFILE RT OF EMERGENCY EXIT HATCH 843. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, RT SIDE OF EMERGENCY HATCH 843 IAW SRM 51-72-11 AND DWG D52279010.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-21) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 AND 21 Y-765 . REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53112812.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 844. REPLACED RT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LOAD TRANSMITING PROFILE RT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED TRANSMITING PROFILE, SEGMENT, RT SIDE LOCATED ON EMERGENCY EXIT HATCHES NR 833 IAW SRM A320 51-72-11 AND DWG D52279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LOAD TRANSMITING PROFILE LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED TRANSMITING PROFILE, SEGMENT, LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833 IAW SRM 51-72-11 AND DWG D52279010.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40R BETWEEN FRAMES 30 - 31 FWD CARGO BAY.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CRACK ON LT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 843. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, LT SIDE OF EMERGENCY EXIT HATCH 843 IAW SRM 51-72-11 AND DWG D52279010.

Part: PLATE — CORRODED (FRAMES 28-29) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, CORROSION ON PLATE LOCATED AT STRINGER 43L BETWEEN FRAMES 28- 29 IN FWD CARGO BAY. REPLACED PLATE IAW 51-72-11 AND DWG D53230861.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 39R BETWEEN FRAMES 30 & 31 INE FWD CARGO BAY. REPLACED STRINGER 39R IAW SRM 51-72-11 AND DWG D53231568.

Part: SKIN — GOUGED (FRAME 25) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND GOUGE ON FUSELAGE EXTERNAL SKIN FRAME 25+3 BETWEEN S41-42L. REPAIRED SKIN IAW SRM 53-00-11 PARA 4.W, FIG 238.

Part: FITTING — CORRODED (FRAMES 17-19) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FRAMES 17 - 19. REPLACED CENTER FITTING OF FWD PAX CABIN ENTRY DOOR IAW SRM 51-72-11 AND DWG D53112198.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FRAME 20. REPLACED AFT LOWER CORNER OF RT FWD PASSENGER/CREW DOOR CUT OUT IAW SRM 51-72-11 AND DWG D53112109.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y765 BETWEEN FRAMES 47, 51, AND 64. FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11, 53-41-15 FIG 202, PAG 215/216, DWG D534-7200, & D534-70080.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER OF FRAME 16. REPLACED FWD LOWER CORNER OF FRAME IAW SRM 51-72-11 AND DWG D53112109.

Part: DOOR SILL — CORRODED (FRAMES 16-20) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER R1 DOOR SILL. REPLACED DOOR SILL BETWEEN FRAMES 16 TO 20 IAW SRM 51-72-11 AND DWG D53110339.

Part: CLEAT — CORRODED (FRAME 32) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FRAME 32 BETWEEN S42 -43R IN FWD CARGO BAY . REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231212.

Part: CLEAT — CORRODED (FRAME 31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT ON FRAME 31 BETWEEN S43-44L IN FWD CARGO BAY. REPLACED THE CLEAT IAW SRM 51-72-11 AND DWG D53231212.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 47,51, AND 64 . FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 41) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 FRAME 41. FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 36 - 41 IAW SRM 51-72-11 AND DWG D53370500 .

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40L BETWEEN FRAMES 33-34 IN FWD CARGO BAY. REPAIRED STRINGER IAW SRM 53-00-13.

Part: CLEAT — CORRODED (FRAME 31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT ON FRAME 31 BETWEEN S41-42R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231582,

Part: CLEAT — CORRODED (FRAME 32) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 32 BETWEEN S40-41R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231582,

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292, BETWEEN FRAMES 64-66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472832.

Part: CLEAT — CORRODED (FRAME 33) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FRAME 33 BETWEEN S40-41R IN FWD CARGO BAY.

Part: CLEAT — CORRODED (FRAME 31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FRAME 31 BETWEEN S41-42R IN FWD CARGO BAY.

Part: FLOOR SUPPORT — CORRODED (BS 66-67) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472816.

Part: CLEAT — CORRODED (FRAME 32) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT ON FRAME 32 BETWEEN S41-42R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231582.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 BETWEEN FRAMEE 47, 51, & 64. FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40L BETWEEN FRAMES 33-34 IN FWD CARGO BAY. REPAIRED STRINGER IAW SRM 53-00-13. PARA 4A, STEP 7. FIGURE 201.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231212.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53472000.

Part: CLEAT — CORRODED (FRAME 33) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED ON FRAME 33 BETWEEN S40-41R IN FWD CARGO BAY. REPLACED CLEAT IAW DWG D53231582.

Part: SPLICE — CORRODED (FRAMES 30-31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE S41L BETWEEN FRAMES 30 - 31 IN FWD CARGO BAY. REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53231626.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765, FRAME 35+8 ON UPPER FLANGE. FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 35-36 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 41) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 AT FRAME 41 ON UPPER FLANGE. FOUND OUT LIMITS AND REPLACED THE SEAT TRACK BETWEEN FRAMES 36-41 IAW SRM 51-72-11 AND DWG D53370500.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5-67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15-69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: SEAT TRACK — CORRODED (FRAME 44) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765, AT FRAME 44+8 ON UPPER FLANGE. FOUND OUT LIMITS AND REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: SPLICE — CORRODED (FRAMES 30-31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE AT S43L BETWEEN FRAMES 30-31 IN FWD CARGO BAY. REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53231375.

Part: SPLICE — CORRODED (FRAMES 30-31) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE, BETWEEN FRAMES 30-31 IN FWD CARGO BAY. REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53231626.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y1292 FRAME 35+9 ON UPPER FLANGE. FOUND OUT LIMITS AND REPLACED SEAT TRACK BETWEEN FRAMES 35-36 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 FRAME 37 UPPER FLANGE. FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 36- 41 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 24- 35. FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53110920.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16 - 20, Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG 3D53112816 AND DWG D53110920.

Part: SEAT TRACK — CORRODED (FRAME 36) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 FRAME 36+2 LOWER SURFACE. FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 36-41 IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAME 45) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 FRAME 45+3 LOWER SURFACE. FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 41 - 47 IAW SRM 51-72-11 AND DWG D53370500.

Part: FITTING — CORRODED (LT NACELLE) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON LT UPPER PYLON SPIGOT RECEPTACLE FITTING BORE. REPLACED UPPER PYLON SPIGOT RECEPTACLE FITTING LT PYLON IAW SRM 54-51-12.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND ELONGATED HOLE ON FUEL TANK ACCESS PANEL 550BB AT LT WING. REPLACED FUEL ACCESS PANEL 550BB AT LT WING IAW AMM 57-27-11-400-002-A. THE INSTALLATION IS DOCUMENTED ON AMDS CARD 5730-6014 MAXIMUN DIAMETER ON HOLE IS 0.291" EVALUATED AND FOUND OUT LIMIT DUE TO MAXIMUN DIAMETER IS 0.0265" IAW SRM 57-27-11.

Part: SEAT TRACK — CORRODED (FRAME 46) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 FRAME 46+15 UPPER FLANGE AND FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 41-46 IAW SRM 51-72-11 AND DWG D533371000.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 47-64. FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53472000, & D53470080.

Part: SKIN — DENTED (FRAME 78) · airframe 67,151 hrs · 30,574 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN FRAME 78+12" AND BETWEEN S1-2L UPPER FUSELAGE TAIL CONE. REPAIRED IAW SRM A32053-51-11, FIG 203.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 67,151 hrs · 30,574 cycles

CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64-66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472832 AND D53472816.

Part: DUMMY RAIL — CORRODED (FRAME 16) · airframe 67,151 hrs · 30,574 cycles

CORROSION ON DUMMY RAIL FRAME 16, Y-81. REWORKED AREA AND FOUND WITHIN LIMITS IAW SRM 53-11-14, FIG 106, PAG 115, 116.

Part: FITTING — CORRODED (L1 DOOR FRAME) · airframe 67,151 hrs · 30,574 cycles

CORROSION ON AFT LOWER CORNER FITTING ON L1 DOOR, FRAME 20. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: COVER — CORRODED (FRAME 14) · airframe 67,151 hrs · 30,574 cycles

CORROSION ON JOINT COVER FRAME 14, Y-81. REPLACED JOINT COVER IAW SRM 51-72-11 AND DWG D53112620.

Part: DUMMY RAIL — CORRODED (FRAME 16) · airframe 67,151 hrs · 30,574 cycles

CORROSION ON DUMMY RAIL FRAME 16, Y503.2. REPLACED DUMMY RAIL IAW SRM 51-72-11, DWG NR D53112825 AND DWG D53110984.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,128 hrs · 30,102 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHTS TEST FAILED. MAINTENANCE REPLACED FWD LT EPSU BATTERY AND FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,299 hrs · 29,698 cycles

DURING EMERGENCY LIGHTS CHECK, FOUND AFT LT BATTERY PACK FAULT. REPLACED BATTERY AND FUNCTION WAS NORMAL.

Part: SKIN — DAMAGED · airframe 72,071 hrs · 32,980 cycles

BELOW CARGO DOOR OPENING AND SCRATCHES VISUALLY INSPECT AND NO CRACKS FOUND AFT DENT 1 X 1, .125" DEEP. FWD 1 X .5", .125" DEEP WITHIN LIMITS IAW SRM 53-11-11, PAR 125, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FRAME 25 TO FRAME 27 AND STR 39R TO STR 43R IAW ERA 526367-14.

Part: EPSU — FAILED (CABIN) · airframe 58,840 hrs · 26,517 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT FAILED FAP PANEL TEST AT L1. MAINTENANCE REPLACED THE L1 EPSU AND SYSTEM TEST WAS NORMAL. AIRCRAFT HAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,408 hrs · 24,949 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 22 INOPERATIVE. REPLACED FLOOR PATH LIGHT ASSY AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE. (2010-00441)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,753 hrs · 22,532 cycles

DURING TESTING OF THE EMERGENCY EGRESS LIGHTING, EPSU COMM EMER L ANNUNCIATED. REPLACED POWER SUPPLY 11WL, CHECKS GOOD. (A)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,995 hrs · 22,173 cycles

COM EMERGENCY LIGHT FWD FAULT ON CIDS. REPLACED FWD LEFT EPSU BATTERY, EMERGENCY LIGHTS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,162 hrs · 20,332 cycles

RIGHT AND LEFT AFT ENTRY DOOR EMERGENCY LIGHT EXIT SIGNS INOP. REPLACED AFT EPSU, CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

LEFT AND RIGHT AFT ENTRY DOOR EMERGENCY LIGHT EXIT SIGNS INOP. REPLACED AFT EPSU, CHECKS OK.

Part: EPSU — FAULTY (CABIN) · airframe 1,210 hrs

 EPSU, COM EMER L FAULT MESSAGE ON CIDS DEU. REPLACED POWER SUPPLY AND RECONNECTED CONNECTOR. OPERATIONAL CHECK OK.

Part: ACCUMULATOR — CRACKED (HYD SYSTEM) · airframe 44,187 hrs · 19,851 cycles

IN CRUISE, HYDRAULIC GREEN RESERVOIR LO LEVEL MESSAGE, WITH FLUID LEVEL INDICATED IN AMBER. FOLLOWED COM PROCEDURE. AIRCRAFT DIVERTED INTO IAD FOR ITS LONGER RUNWAY. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. MAINTENANCE FOUND GREEN HYDRAULIC SYSTEM ACCUMULATOR CRACKED, AND REMOVED AND REPLACED SAME.

Part: VALVE — LEAKING (NR 2 ENGINE) · airframe 42,798 hrs · 19,159 cycles

DURING CLIMB ENG NR 2 FIRE LOOP B MSG ENUNCIATED FOLLOWED BY ENGINE NR 2 FIRE WARNING AT 7000 FT. FLIGHT CREW SHUTDOWN ENGINE NR 2 AND RETURNED TO DEPARTURE AIRPORT. ENGINE FIRE BOTTLES WERE NOT DISCHARGED. MAINTENANCE FOUND HOT AIR LEAK AT THE HPTCC VALVE MOUNTING FLANGE.

Part: PRIORITY VALVE — LEAKING (PTU MANIFOLD) · airframe 37,758 hrs · 16,735 cycles

JUST PRIOR TO APPROACH, RECEIVED ECAM MESSAGE 'HYD Y RSVR LO LVL'. FOLLOWED COM AND LANDED UNEVENTFULLY. ECAM INDICATED NEAR TOTAL LOSS OF FLUID. FOUND PRIORITY VALVE AT PTU MANIFOLD LEAKING. REPLACED PRIORITY VALVE AND SERVICED YELLOW HYDRAULIC RESERVOIR. LEAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RESERVOIR — BROKEN (LEFT) · airframe 32,750 hrs · 14,457 cycles

DURING 'L' CHECK, FOUND THE LEFT ESCAPE SLIDE CYLINDER CONTROL CABLE BROKEN. REPLACED THE LEFT ESCAPE SLIDE CYLINDER CONTROL CABLE RESERVOIR. OPERATIONAL CHECK GOOD.\N\N\NMANUFACTURER: AIRBUS\NMODEL: A319114

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED BATTERIES AT THE FORWARD LEFT CABIN, 10WL. REPLACED BATTERY PACKS, OPS CHECK OK.

Part: SLIDE — MALFUNCTIONED (DOOR 4R)

AFTER THE AIRCRAFT ARRIVED AT THE GATE, THE FLIGHT ATTENDANT INADVERTENTLY DEPLOYED THE SLIDE AT DOOR 4R. THE SLIDE DID NOT FULLY INFLATE. MAINTENANCE REMOVED SLIDE AND SENT TO THE SHOP WHERE THE SLIDE WAS REPACKED. THIS SLIDE WILL BE INSTALLED ON AN AIRCRAFT AND RE-DEPLOYED FOR TROUBLESHOOTING PURPOSES AT A LATER DATE.

Part: IRU — FAILED (NR 1)

SHORTLY AFTER LEVEL OFF AT FL 310, AIRCRAFT WENT INTO ALTERNATE YAW. AIRCRAFT RETURNED TO MSP WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA IRU AND NR 2 SPOILER ELEVATOR COMPUTER, OPERATIONAL CHECK OK.