N404UA

Part: FUEL CAP — MISSING (NA) · airframe 87,228 hrs · 33,599 cycles

PDA 2 FUELER REPORTED FUEL CAP MISSING WHEN THEY ARRIVED TO FUEL AIRCRAFT REFER TO LP 7720911 REFERENCE GMM 02-30-95. FURTHER DETAILS WAITED.

Part: NONE — FAILED (NLG BAY) · airframe 86,781 hrs · 33,404 cycles

FLIGHT CREW REPORTED VIA AIRINC L/G DOOR NOT CLOSED FAULT ON ECAM, FLIGHT CREW ATTEMPTED TO RECYCLE GEAR AS CALLED OUT FOR IN QRH FAULT REMAINED. NLG DOOR UPLOCK ACTUATOR LEAKING. REMOVED NOSE GAER UPLOCK ACTUATOR REF AMM 32-31-14-000-002-A. PULLED AND COLLARED CB C9, Q 34 AND Q35. REMOVED NLG UPLOCK ASSY. REF AMM32-31-12-000-001-A. FOUND UPPER REF L/P 7278287. REPLACED NLG DOOR UPLOCK ASSY REF AMM ATTACHED BOLT ITM 13, CORRODED, PARTS ON ORDER, M&E 32-31-14-400-001-A. NEED TO ACP FUNCTIONAL TEST PER AMM 17-3231-3-0001. 32-13-14-400-001-A ITEM 4K. ADD EMP:U110298 ACP LANDING GEAR DOOR TEST REF AMM 32-31-00-710-002-A, WITH FALSE TARGETS, OPS CHECKS GOOD. PUT AIRCRAFT BACK TO GROUND CONFIGURATION ADD EMP:U30999

Part: LINE — LEAKING (HYD SYSTEM) · airframe 86,122 hrs · 33,069 cycles

ECAM CAUTION MESSAGE - B RSVR LO LVL MESSAGE INOP - HYD HYD B SYS LO LVL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INVESTIGATE AND CONTACT TOMC 847-700-9980 UPDATED MAA CODE EFS USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INVESTIGATE AND CONTACT TOMC 847-700-9980 REPLACED WORN LINE IN HYDRAULIC BAY, M&E NUMBER 18-2912-3-0017. SERVICED HYDRAULICS AND HEAD PRESSURE PER AMM 12-12-29. BLED BLUE SYSTEM PER AMM 29-00-00-870-009-A. TOPPED ALL THREE RESEVOIRS. HYDRAULICS OPERATION AND LEAK CHECK, CHECKED OK.

Part: SKIN — CORRODED (LT WING) · airframe 85,078 hrs · 32,622 cycles

GEN BY: UA QC REQUEST: LT WING, UPPER SKIN SURFACE CORROSION OVERWING EMERGENCY EXIT PATH AREA, APPROXIMATELY AT RIB 2, AREA BETWEEN STRINGER 2 AND 4. REF BY PEMCO NR. 10321.0410. REPAIRED 10EA AREAS OF CORROSION ON LT WING UPPER SKIN BETWEEN RIBS 1-3 AND STR 15 TO FRONT SPAR, PER REF A320 SRM 57-21-11 -283-014. REPAIR CATEGORY A. NO SRI RE-INSPECTION.

Part: SKIN — CORRODED (LT WING) · airframe 85,078 hrs · 32,622 cycles

CORROSION AT LT WING UPPER SKIN AT RIB 2 BETWEEN STR 6 AND STR 9 EXCEEDS ALLOWABLE DAMAGE LIMITS, IAW AIRBUS A320 SRM 57-21-11-283 -013, FIG 001 SHEET 01. ACCOMPLISHED INTERIM REPAIR, PER ECRA 5721-01440 PART 1. ACCOMPLISH THE PERMANENT REPAIR AT LT WING TOP SKIN UPPER SURFACE BETWEEN STR 5 AND 9 AT RIB 2, PER PART 3 OF THE LATEST REVISION OF EC/RA 5721-01440 ON OR BEFORE 05JUL2021. PLANNING TO CONTACT ENGINEERING AFTER 01JUN2021, BUT BEFORE 15JUN2021 FOR PERMANENT REPAIR. OK TO CARRY INTERIM REPAIR. PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 05JUL2021. PLANNING TO CONTACT ENGINEERING AFTER 01JUN2021, BUT BEFORE 15JUN2021 FOR PERMANENT REPAIR. TOMC-APPROVAL FROM SC1ELBYC COMMENT Q/C REVIEWED. RECORDS UPDATE Q/C REVIEWED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 81,295 hrs · 30,953 cycles

EPSU BATTERY EMER L FAULT ON AAP WHEN EMERGENCY LIGHT OPS CHECK IS COMPLETED. REPLACED LEFT EMER PWR SUPPLY AND BATTERY PER AMM 33-51-38. TEST OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248304 SN OFF 8072 IPC REFERENCE # POWER SUPPLY, C OFF 31-3350-9-9001 8072 ON 31-3350-9-9001 8098.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 81,295 hrs · 30,953 cycles

EPSU BATTERY EMER L FAULT ON AAP WHEN EMERGENCY LIGHT OPS CHECK IS COMPLETED. REPLACED LEFT EMER PWR SUPPLY AND BATTERY PER AMM 33-51-38. TEST OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248304 SN OFF 8072 IPC REFERENCE # POWER SUPPLY, C OFF 31-3350-9-9001 8072 ON 31-3350-9-9001 8098.

Part: FEEDER CABLE — MELTED (NR 2 ENGINE) · airframe 79,511 hrs · 30,147 cycles

NR 2 ENGINE UPPER FWD PYLON ATTACH SHACKLE FEEDER WIRE ARRAY BUNDLE IN CONTACT WITH SHACKLE, MELTED THREE WIRES . REPAIRED IAW ECRA 57620-03014.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 79,306 hrs · 30,072 cycles

WHILE TROUBLESHOOTING THE R1 DOOR, FOUND THE SLIDE LOOSE IN THE BUSTLE . WHEN THE DOOR WAS OPENED, THE SLIDE FELL OUT. INSTALLED A NEW SLIDE IAW 25-62-44-400-803A, AND 52-10-00-860-001A. OPS CHECKED GOOD.

Part: INLET — DAMAGED (APU) · airframe 78,615 hrs · 29,786 cycles

SMOKE IN AFT CABIN. ELETRICAL ODOR. APU INJESTED PHENOLIC PIECE OF INLET DIVERTER DUCT CAUSING SMOKE AND ODOR IN CABIN. BORESCOPE COMPLETED WITHOUT SIGNS OF DAMAGE. BOTH CABIN RECIRCULATION FILTERS CHANGED.

Part: ADIRU — MALFUNCTIONED (NR 1) · airframe 78,437 hrs · 29,708 cycles

NAV IR 1 2 3 FAULT ECAM WARNING. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 ADIRU , OPS CHECKED GOOD IAW AMM 34-13-00, AND LAND TEST AFS PASSED. ACFT STATUS IS FULL CAPABILITY IAW AMM 22-97-00.

Part: BRAKE SYS — UNKNOWN (MLG) · airframe 78,437 hrs · 29,708 cycles

CREW REPORTS THAT BRAKES MALFUNCTIONED ON LANDING. UNUSUAL PEDAL TRAVEL. CREW REPORTS "INTERMITTENT BRAKE LOSS BELOW 27 KNOTS. OPS CHECKED BRAKES NUMEROUS TIMES AND WITNESSED ALL BRAKES OPERATIONAL. CHECKED BSCU THRU MCDU AND NO FAULTS. CREW TAXIED AIRCRAFT AND BRAKES OPS NORMAL.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 78,382 hrs · 29,684 cycles

F/CTL SLATS FAULT ECAM. EMERGENCY DECLARED. REPLACED NR 2 SLAT OTBD ACT REF AMM 27-84-49-000-001-A AND AMM 27-84-49-400-001-A.

Part: O-RING — LEAKING (PCU VALVE) · airframe 77,177 hrs · 29,130 cycles

GREEN SYSTEM LO PRESSECAM. NO FLUID IN RESERVOIR. EMERGENCY DECLARED. FOUND O-RING LEAK ON LEFT SLAT PCU VALVE BLOCK 25CV IPC 27-84-53 ITEM 60 . REPLACE O RING PER 27-84-53-400-003-A NOTE; GREEN SYSTEM CONTAINED 2 GALLONS OF HYD FLUID

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,928 hrs · 29,021 cycles

EMERGENCY LIGHTS TEST FAILED. EPSU AFT LEFT. REPLACED AFT LEFT EMERGENCY LIGHTS BATTERY PER MM 33-51-38. OPS CK GOOD.

Part: SHEAR TIE — BENT (FRAME 73) · airframe 75,301 hrs · 28,319 cycles

FRAME 73 SHEAR TIE BETWEEN STRINGERS 31-32R & 32-34R BENT. REPLACED IAW ECRA 5310-07001.

Part: FRAME — DAMAGED (FRM 74) · airframe 75,301 hrs · 28,319 cycles

FRAME 74 LOWER SECTION BENT & BUCKLED. REMOVED AND REPLACED FRAME IAW SRM 51-71-11 AND ECRA 5310-07001.

Part: FITTING — GOUGED (RT MLG) · airframe 75,301 hrs · 28,319 cycles

RT WING MLG RETRACT JACK FTG LWR FLANGE 5TH HOLE FROM IB HAS GOUGE. INTERIM REPAIR ACP IAW EC RA 5720-02838 PART1.

Part: CLEAT — BENT (FUSELAGE) · airframe 75,301 hrs · 28,319 cycles

FR73 CLEAT BETWEEN STRINGER 32L-34L IS BENT. REPLACED CLEAT AT FR73 BETWEEN STRINGER 32L-34L IAW SRM 51-42-11.

Part: FITTING — GOUGED (RT MLG) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

RT MLG RETRACTION JACK ANCHORAGE FITTING CORRODED. INTERIM RPR ACP IAW ECRA 5720-02838 PART1.

Part: SKIN — DAMAGED (RUDDER) · airframe 75,301 hrs · 28,319 cycles

LT RUDDER HAS MULTIPLE LIGHTNING STRIKES LOCATED APPROX 79" UP FROM BOTTOM AND 12.5" FWD OF TRAILING EDGE. PERMANENT REPAIR ACP IAW ECRA 5540-01464.

Part: FRAME — CORRODED (FRM 68) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

FRAME 68 ABOVE STR 23R CORRODED. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR FITTING IAW SRM 53-41-12 FIG 202 AND INSTALLED IAW SRM 53-41-12 FIG 202 PARA 5-B AND SRI 53-41-12-1-002-00 PARA 5.B 202

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

AFT CARGO STR 43LT CORRODED BETWEEN FR 54 - 55. STRINGER 43LT BETWEEN FR 54-55 REPAIRED IAW SRM 53-00-13 PARA 4 A (3) FIG 102.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

AFT CARGO PIT INNER DOOR SILL WEB HAS AREAS OF CORROSION FR52-FR56. REMOVED AND REPLACED AFT CARGO DOOR SILL WEB FR52-FR56 IAW SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

AFT PIT STRINGER 42L BETWEEN FR 58-59 HAS CORROSION. REMOVED & REPLACED STRINGER AND FACTORY SPLICE PLATES IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

FWD PIT FR 28-FR 33 STRINGER 40 RT HAS CORROSION. REMOVED & REPLACED STRINGER AND SPLICE PLATES IAW SRM 51-42-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,301 hrs · 28,319 cycles

FUSE EXTERIOR HAS DENT AT LT SIDE FR 30-31 STR 38. FOUND DENT TO BE OUT OF LIMITS, CUTOUT OUT DAMAGE AREA AND FAB REPAIR DOUBLER FORM 2024-T3-.063 SKIN THICKNESS IN THIS AREA IS .047 AND INSTALLED REPAIR IAW SRM 53-00-11 FIG220. THIS IS A CAT B REPAIR.

Part: STRINGER — CORRODED (FRAME 67) · corrosion level 2 · airframe 75,301 hrs · 28,319 cycles

CORROSION ON STRINGER 23L. AFT ENTRY DOOR SILL FRAME 67. REMOVED AND REPLACED DOOR SILL IAW A320 51-22-11

Part: CONTROL UNIT — MALFUNCTIONED (NLG STEERING) · airframe 72,649 hrs · 27,139 cycles

LOSS OF NOSE WHEEL STEERING ON LANDING, REQUIRED TOW INTO GATE. EMER DECLARED ON DESCENT. REPLACED STEERING CONTROL UNIT.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 70,466 hrs · 26,217 cycles

RIGHT ELEVATOR UPPER SKIN HAD 2 WATER FINDINGS FROM THERMOGRAPHY INSPECTION. 102.5 INCHES FROM INBD END & 4 INCHES FROM TE. 74 INCHES FROM INBD END & 4.5 INCHES FROM TE. BOTH AREAS REPAIRED IAW SRM 55-21-11 REPAIR PGS 234 - 236 FIG 205. REPAIR AREAS WERE BETWEEN 1.55 & 23.25 SQ INCHES. FOG 205 REFERS TO SRI 55-21-11-2-002-00 PARA 3B TABLE 203 TO REINSPECT AT 60000C OR 120000T FROM COMPONENT DELIVERY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,483 hrs · 25,432 cycles

NW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. CYCLED NOSE STEERING SWITCH ON FWD INSTRUMENT PANEL. ACCOMPLISHED BITE OF BSCU 1 & 2 TEST PASSED NO FAULTS DISPLAYED.

Part: BUSHING — WORN (L1 DOOR) · airframe 67,113 hrs · 24,906 cycles

DOOR 1L DIFFICULT TO OPEN & CLOSE. REPLACED UPPER DOOR HINGE ASSEMBLY WITH BUSHING. SEE PTT SEQ 1132021, ACCOMPLISHED IAW AMM 52-11-11-400-001-A.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 66,992 hrs · 24,857 cycles

COCKPIT AUDIO CONTROL PANEL 1 INOPERATIVE, CONSTANT HOT MIC. REPLACED CAPTAIN`S ACP, OPERATIONS CHECKED GOOD.

Part: SLEEVE — LOOSE (THRUST REVERSER) · airframe 66,601 hrs · 24,704 cycles

NR 1 ENG OTBD REVERSER SLEEVE INNER LINING 3 FOOT BY 4 FOOT SECTION OF WIRE MESH LINING LOOSE. IAW ECRA 7830-02698 SLEEVE MUST BE REPLACED WITHIN 25 HOURS OR BY PTT 66626, USING PART 115- 9105 & MUST BE CHECKED ONCE PER DAY. ** DL1694 CREATED TO MONITOR **

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 66,524 hrs · 24,681 cycles

PFR SHOWS "FLP LT PROX SNSR 2 39CV OR LGCIU 2" PREVIOUSLY BOTH PARTS ARE REPLACED.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 65,695 hrs · 24,363 cycles

ENG 1 SENSOR FAULT.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 65,374 hrs · 24,264 cycles

DUE TO FAN BLADE DAMAGE ON NR 2 ENGINE CAUSED BY BIRD STRIKE. ACCOMPLISHED INSPECTION OF THE FAN BLADES PER AMM TASK 72-31-11-200-010-B 13. FOUND ONE BLADE WITH ALLOWABLE DEFLECTION LIMIT & EVIDENCE OF AN AREA OF 'RUB ON THE ATTRITION LINER.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 65,490 hrs · 24,284 cycles

DURING EMERGENCY LIGHT TEST, EPSU INT LOAD EMERGENCY LIGHT FAILURE MESSAGE. REPLACED LT CABIN EMERGENCY EXIT POWER SUPPLY IAW MM, TESTS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 65,338 hrs · 24,229 cycles

EMERGENCY LIGHT TEST FAILED ON 2 SVC. REPLACED BATTERY IAW MM 33-51-38.

Part: BOOT — TORN (COCKPIT STICK) · airframe 65,214 hrs · 24,172 cycles

COPILOTS SIDE STICK BOOT TORN AFT INBD CORNER. SMALL TEAR INBD AFT SIDE OF JOY STICK. REPLACED COPILOTS JOYSTICK BOOT.

Part: SEAL — MISSING (RT TE FLAP) · airframe 65,114 hrs · 24,129 cycles

PILOTS REPORTED SOMETHING FLAPPING UNDER THE RT SIDE OTBD SPOILER. REMOVED DAMAGED PART OF SEAL. OTBD RT FLAP TRACK FAIRING INBD BLADE SEAL PARTIALLY MISSING. REPLACED SEALS ON RT OTBD FLAP FAIRING.

Part: SCREW — LOOSE (WING LE) · airframe 65,082 hrs · 24,118 cycles

LOOSE SCREW ON INBD LEADING EDGE JUST BELOW SLATS. TIGHTENED LOOSE SCREW.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 65,030 hrs · 24,099 cycles

EMERGENCY LIGHT TEST FAILED. MESSAGE 'EPSU INT LOAD FWD L'. REPLACED FWD EPSU & BATTERY, OPS CHECKED GOOD PER AMM.

Part: UNKNOWN — LEAKING (LAVATORY) · airframe 64,916 hrs · 24,061 cycles

CREW REPORT: F/A REPORTS AFT GALLEY CARPET SOAKED WITH WATER. POSSIBLY FROM FWD AFT LAV FOUND WATER LINE GOING TO FLUSH VALVE CRACKED AND LEAKING. INOP WATER TO TOILET WILL BE A DRY FLUSH. REF IPC 38-31-41-30C ITEM 80 2-012N602-70 ITEM 130 3-906E515-80 ITEM190 15800-192 PACKINGS AND SCREEN 38-12-04-30F ITEM 210 AE66363H0113 HOSE.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 63,685 hrs · 23,585 cycles

ECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD. CREW COMMENTS: HYD G RSVR LO LVL ECAM ON TAXI OUT WHILE IN RUN UP AREA GND CREW NOTED PUDDLE HYD FLUID. REPAIRED HYD LINE AND SERVICED G SYSTEM.

Part: COMPUTER — MALFUNCTIONED (NR 2) · airframe 62,644 hrs · 23,176 cycles

AILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: F-CTL AIL SERVO FAULT SAMC TEXT: CFDS FAULTING ELAC2. IF DF WILL NEED TO SWAP WITH ELAC 1 TO DF ELAC1. REMOVED AND REPLACED ELAC PER AMM.

Part: O-RING — LEAKING (BLUE HYD SYSTEM) · airframe 62,051 hrs · 22,951 cycles

LOST BLUE HYDRAULIC QTY, WENT TO ZERO. FLIGHT RETURNED. FOUND HYDRAULIC FITTING ON INBD SIDE OF BLUE HYD PUMP LEAKING. REPLACED O-RING AND RESECURED LINE. PRESSURIZED SYS, NO LEAKS.

Part: SCAVENGE PUMP — FAILED (NR 2 ENGINE) · airframe 61,618 hrs · 22,779 cycles

TOWER REPORTED SMOKE FROM NR 2 ENGINE. ACCOMPLISHED BOROSCOPE OF OIL FEED LINES PER MT72-022 NO COKING NOTED. ACCOMPLISHED INSPECTION OF NR 5 BEARING COMPARTMENT PER MT72-033, NO BLOCKAGE NOTED. REINSTALLED LINES AND COVERS. FOUND OIL PUDDLING AT BASE OF TURBINE BLADES ON THE #2 ENGINE SEVERAL TURBINE BLADES HAVE SIGNS OF OIL RESIDUE ON THEM AS VIEWED FROM THE ENGINE EXHAUST. REPLACED #2 ENG.OIL SCAVENGE PUMP

Part: ENGINE — STALLED (NR 1) · airframe 61,470 hrs · 22,724 cycles

NR 1 ENG STALL ECAM. ACCOMPLISHED FUNCTIONAL CHECKS OF THE HPC 7TH STAGE A, B & C SOLENOID VALVES PER AMM, HPC 7TH STAGE BLEED VALVES PER AMM. HPC 10TH STAGE SOLENOID VALVE PER AMM AND 10TH STAGE BLEED VALVE PER AMM. ACCOMPLISHED ALL TASKS IN TSM 71-00-00-810-808. ALL BLEED AND SOLENOID VALVES CHECKED OK. ACCOMPLISHED LUBE OF VSV AND 2.5 BLEED, CHECKED OK. ACCOMPLISHED POWER ASSURANCE RUN AT 1.39 EPR WITH NO FAULTS.

Part: GIRT BAR — INOPERATIVE (EVAC SLIDE) · airframe 61,368 hrs · 22,685 cycles

NR 1 RT DOOR OVERWATER SLIDE MR25613-020 CAME WITH INOPERABLE GIRT BAR. TELESCOPING END WOULD NOT RETRACT INTO BAR. REPLACED WITH SERVICABLE. GIRT BAR WAS REPLACED WITH SERVICABLE GIRT BAR ON SLIDE RAFT REPLACEMENT TASK CARD SEQ680 4S2592044.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 61,325 hrs · 22,672 cycles

CAP SEAT RECLINE INOP DEFECTIVE RATCHETS AND DIFFICULT TO ADJUST. REPLACED SEAT IN REF TO AMM, OPS CHECK NORMAL.

Part: CONNECTOR — BROKEN (NR CID) · airframe 60,214 hrs · 22,258 cycles

NR 1 CIDS BENCH PLUG BROKEN.

Part: SNUBBER — FAULTY (R1 DOOR) · airframe 60,104 hrs · 22,207 cycles

R1 DOOR HAS NO SNUBBING ACTION DURING LAST ONE THIRD TO ONE QUARTER OF DOOR TRAVEL IN THE CLOSED DIRECTION. SNUBBER ACTUATOR WAS REPLACED SEPT 12 . REPLACED SNUBBER PER MM. OPS CHECKED NORMAL.

Part: FAN BLADE — DAMAGED (NR 1 ENGINE) · airframe 59,343 hrs · 21,898 cycles

NR 1 ENG FAN BLADE AT 6 O`CLOCK POS HAS A NICK IN IT. DETERMINED DIMENSIONS OF NICK TO BE 1-32 INCH DEEP BY 1-16 INCH LONG IN AREA AT, 5 INCHES FROM BLADE TIP. DRESSED. REPAIRED NICK PER AMM TASK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,277 hrs · 21,868 cycles

CABIN EMERGENCY LIGHT TEST FAILED. MESSAGE: EXT LOADS FWD L 33-51-38. JUMPED BOTH LT AND RT SLIDES, NO HELP. HOOKED UP NEW BATTERY AND POWER SUPPLY, NO HELP. TROUBLE SHOT PER WD 33-51-04. FOUND NO GROUND AT FWD RT DOOR SLIDE CONNECTOR 2870VC PIN B TO GROUND. FOUND BROKEN WIRE WHERE WIRE PASSES THRU DOOR HINGE. SPLICED WIRE PER GNMM 2-15-00-001. CABIN LIGHTS NOW TEST OK.

Part: LIMITER — MALFUNCTIONED (LE SLAT) · airframe 58,511 hrs · 21,546 cycles

CREW REPORT: F-CTL SLATS FAULT. CREW REPORTED FLAPS-SLATS FAULT GOING TO FLAPS 1. CFDS SHOWED "27-80-00 SLT 1 SYS JAM - CHECK MECH DRIVE" AND "27-80-00 SLT 2 SYS JAM - CHECK MECHANICAL DRIVE. CREW USED CAPT EMERG AUTHORITY TO CYCLE CB'S B6+B7+Q21 FAULT CLEARED. SAMC TEXT: CONTACT SAMC, TROUBLESHOOT PER TSM "SLAT SYSTEM JAM". PER OPBLM NR 2 SLAT TORQUE LIMITER TRIP. T-S SLAT SYS JAM AND FOUND LT NR 2 SLAT TORQUE LIMITER TRIPPED. REPLACED LIMITER PER MM AND LUBED TRACK AREA, OPS CHECK NORMAL.

Part: LANYARD — UNSECURE (SLIDE RAFT) · airframe 58,047 hrs · 21,370 cycles

AFT RT SLIDE RAFT SURVIVAL KIT LANYARD AND RELEASE STRAP FOUND LOOSE. RE-INSTALLED LANYARDS. SLIDE RAFT RESTORED TO TOLERANCE.

Part: WHEEL — CRACKED (MLG) · airframe 57,923 hrs · 21,319 cycles

ON ARRIVAL FOUND NR 2 WHEEL ASSY CRACKED AND RUBBING ON BRAKE ASSY. NR 2 MLG BRAKE ASSY DAMAGED FROM BROKEN WHEEL ASSY. REMOVED NR 2 WHEEL ASSY. INTERIM INSTALLATION OF TIRE AND WHEEL ASSY FOR ACFT TOWING. REPLACED BRAKE ASSY. FOUND NR 2 MLG TACHOMETER FITTING DAMAGED FROM BROKEN WHEEL ASSY. REPLACED NR 2 MLG TACHOMETER 21GG AND HSG IAW MM. TESTED OK.

Part: PUMP — LEAKING (FUEL TANK PUMP) · airframe 57,673 hrs · 21,217 cycles

LEFT WING FUEL TANK PUMP HOUSING AREA IS WET WITH FUEL WIPED DOWN AREA AND 15 MINS LATER AREA IS WET AGAIN. FUEL STAINS APPEAR TO BE STREAMING AFT ALONG WIRE COVER AFT DURING FLIGHT. FOUND FUEL PUMP 25QA LEAKING. BEGAN REMOVAL IAW MM. CIRCUIT BREAKERS HAVE BEEN PULLED AND TAGGED IAW MM. SECOND FUEL LEAK FOUND AT LT WING LOWER SURFACE APPROX 2 FT AFT OF L/E AND 1 FOOT OTBD OF FUSELAGE. COMING FROM WEEP HOLE AND ACTIVELY STREAMING AT GATE ON UNDERSIDE OF WING. VERIFIED FUEL LEAK AT FRONT SPAR, APPROX AT RIB NR 2. SPECIFICALLY AT THE 2 ATTACH FASTENERS HOLDING WIRE BUNDLE. REPAIRED FUEL LEAK ON L/E SPAR APPROX AT RIB NR 2. ACCOMPLISHED LEAK CHECK OF FUEL PUMP, NONE FOUND AND COMPLETED TASK TO END.

Part: LANYARD — MISINSTALLED (L2 DOOR SLIDE) · airframe 57,636 hrs · 21,201 cycles

DOOR 2L SLIDE LANYARDS NOT INSTALLED CORRECTLY. WHITE LANYARD IS ROUTED THROUGH TRIGGER. YELLOW LANYARD IS NOT ROUTED THROUGH TRIGGER. OPENED GIRT AND ROUTED BOTH LANYARDS IAW FIG 410 OF MM. CLOSED GIRT, CHECKED ARM DISARM ACTION. VERIFIED CORRECT LANYARD ROUTINGS.

Part: HOOK — OUT OF ADJUST (R2 DOOR) · airframe 56,786 hrs · 20,825 cycles

DOOR 2 RT - INTERIOR HANDLE CAN BE MOVED TO THE CLOSED POSITION WITH DOOR STILL OPEN. SUSPECT HANDLE INTERLOCK MECHANISM NOT FUNCTIONING AS DESIGNED. REMOVED UPPER DOOR LINING. FOUND THE HOOKS HAVE SLIPPED ON THEIR ADJUSTMENT SERRATIONS. (THEY ARE MOUNTED ON GEARBOX ASSY & CONTROLLED BY THE LOWERING SHAFT). REPLACEMENTS ON AOM'S Z2575 & U2510. ADJUSTMENT IN AMM. ADJUSTED THE REPLACED HOOKS PER MM AND REINSTALLED UPPER DOOR LINER ON DOOR 2R. NOTE: THE SLIDE WAS NOT DISTURBED.

Part: PROXIMITY SWITCH — FAULTED (ESCAPE SLIDE) · airframe 56,393 hrs · 20,661 cycles

RT AFT SLIDE INDICATION INOP ON DOOR-OXY SYS ECAM PAGE - DOOR-OXY. SLIDE ARMED INDICATION INTERMITTENT. REPLACED 7WN2 PROX SW AND TESTED IAW MM. CHECKED GOOD ON TEST. ACCOMPLISHED RII INSP AS REQUIRED. OPS CHECK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,126 hrs · 20,535 cycles

STRINGER JUST BELOW THE CABIN OUTFLOW VALVE IS CORRODED. REPAIR IAW SRM 51-42-11,ON WU P7018X,AND SRM 51-75-12.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,980 hrs · 20,479 cycles

AFTER DMC 3 FAULT AT CRUISE CREW AND PAX EXP ACRID SMELL. ACCOMPLISHED TSM 24-00-00- 201 PAGES 25 AND 26. FOUND NO IRREGULARITES DURING OPS OR SNIFF CHECK TO DMC3. FOUND NO TRIPPED C-B'S, ECAM MESSAGES AND NO CIDS OR DEU PROBLEMS. CHECKED ALL E&E COMPARTMENTS AS WELL AS CARGO PITS WITH NO ODORS NOTED.

Part: VALVE — FAULTY (MLG DOOR) · airframe 55,506 hrs · 20,267 cycles

MLG DOOR IS STUCK IN THE DOWN POSITION LT SIDE. DOOR IS STUCK DUE TO FAULTY VALVE. REPLACED BYPASS VALVE AND OP CHECKS ARE OK.

Part: HANDLE — NOT SEATED (CARGO DOOR) · airframe 55,220 hrs · 20,135 cycles

DOOR FWD CARGO LT ILLUM, RTFL. FOUND FWD CARGO DOOR HANDLE JUST OFF DETENT POSITION, BUT DOOR STILL IN LOCKED POSITION. OPERATED DOOR HANDLE SEVERAL TIMES, LOCKS PROPERLY. CHECKS GOOD. NO HISTORY. ACFT OK FOR SVC.

Part: SMOKE DETECTOR — FALSE INDICATION (E/E BAY) · airframe 54,664 hrs · 19,907 cycles

AVIONICS SMOKE MSG, RTFL. CYCLED D5, D6, Y17, C06, T18. CHECKED PFR NO FAULTS ON SYS, CHECKED AVIONICS BAY NO SMOKE PRES ENT RAN CFDS TEST OF ECAM1 REF TSM 26-15-00-810-803. MSG CLEARE D AND NOT PRESENT AT THIS TIME SUSPECT HIGH HUMIDITY IN AVIONICS BAY. NO FURTHER ISSUES OBSERVED.

Part: BELLCRANK — FROZEN (DOOR 1L) · airframe 54,339 hrs · 19,774 cycles

DOOR 1L HARD TO ARM. LINER REMOVED. ISOLATED CABLE FROM SYSTEM. STILL HAVE SOME BINDING. FOUND FROZEN BELLCRANK AND SPACER FROZEN TO BOLT. (BELLCRANK ASSY AND ROD ASSY ARE DISCONNECTED AND GIVEN TO HNGR SMC.. WITH BELLCRANK DISCONNECTED DOOR ARMS NORMALLY). REPLACED BELLCRANK AND RECONNECTED ROD ASSY. REPLACED SLIDE DUE TO SLIDE GIRT FLAP NOT FOLDED CORRECTLY.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 54,130 hrs · 19,667 cycles

DOOR 1R LANYARD NOT VISIBLE ON SLIDE PACK. MAYBE MISSING OR DAMAGED BEYOND SVC LIMITS, A-C CANNOT OPERATE ON EXTENDED OVERWATER. FOUND LANYARD TWISTED AND OUT OF POSITION, REPOSITIONED AND SECURED MOORING LINE AND SURVIVAL KIT LANYARD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 54,130 hrs · 19,667 cycles

LANYARD MISSING FROM SLIDE PACK DOOR 2R: MAYBE MISSING OR DAMAGED BEYOND SVC LIMITS, A-C CANNOT OPERATED ON EXTENDED OVERWATER. FOUND LANYARD TWISTED AND OUT OF POSITION, REPOSITIONED AND ROUTED MOORING LINE AND SURVIVAL KIT LANYARD.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 53,156 hrs · 19,221 cycles

AFT MOST EEL FEEDER CABLE BROKEN AT SEAT TRACK. REPAIRED CABLE, OP CHECK EMERGENCY LIGHTS.

Part: SLIDE — FAULTY (DOOR 1L) · airframe 53,156 hrs · 19,221 cycles

L1 DOOR SLIDE LOWER SUPPORT BRACKET BROKEN. REPLACED & INSPECTED SLIDE. MANAGEMENT INSPECTED INSTALLATION AND CONFIRMED WITH AMT THAT PROPER PROCEDURES WERE FOLLOWED.

Part: ACTUATOR — WORN (AILERON) · airframe 51,774 hrs · 18,688 cycles

A/C FLIES WITH LT WING DOWN WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.

Part: ACTUATOR — OUT OF RIG (AILERON) · airframe 51,774 hrs · 18,688 cycles

A/C FLIES WITH LT WING DOWN, WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OUTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS OUT OF RIG. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

RT TRAY (AFT OF DOOR 2R) IS CRACKED AND MARKED. FABRICATED TRAY FROM 2024T3.063 THICK. INSTALLED TRAY.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

DOOR 2R SILL PLATE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED DOOR 2R SILL PLATE.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 50,915 hrs · 18,359 cycles

RT SHEAR TRAY HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. TRAY REPLACED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

RT BEAM LABELED - Y1292 HAS CORROSION AT FR66 AND IS MARKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED BEAM TO AIRCRAFT. NEEDS SUPPORTS BETWEEN FR64 - FR65 INSTALLED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

BEAM 205 HAS CORROSION AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 205 TO BEAM 200. READY TO INSTALL IN AC. INSTALLED BEAM.

Part: THRESHOLD — CORRODED (R2 DOOR) · airframe 50,915 hrs · 18,359 cycles

RT DOOR 2R THRESHOLD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED DOOR SILL AND STARTED TO MFG NEW SILL. INSTALLING FASTENERS. CONTINUED INSTALLING FASTENERS AND MFG NEW FWD SPLICE ANGLES. INSTALLING FASTENERS, STILL. COMPLETED INSTALLING NEW THRESHOLD PAN.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

RT AFT SHEAR PLATE SUPPORT HAS CORROSION ON BOTTOM SIDE. SUPPORT NEEDS REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE SUPPORT.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

RIGHT AFT SHEAR PLATE CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

BEAM 200 HAS CORROSION AT FRAME 67. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 200 TO BEAM 205. READY TO INSTALL IN ACFT. INSTALLED BEAM 200 TO ACFT.

Part: SHEAR PLATE — CRACKED (L2 DOOR) · airframe 50,915 hrs · 18,359 cycles

LT TRAY AFT OF DOOR 2L CRACKED AND MARKED. MAJOR REPAIR ACCOMPLISHED. FINISHED DRILLING NEW SHEAR PLATE AND STARTED INSTALLING. INSTALLED REMAINING FASTENERS LT TRAY AFT OF DOOR 2L. ACCOMPLISHED INSPECTION OF FASTENER INSTALLATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,915 hrs · 18,359 cycles

BEAM 235 HAS CORROSION AT AFT END OF FRAME 68. REMOVED FASTENERS BEAM STILL NEEDS REMOVED. REMOVED BEAM 235. NEW BEAM IS ON BENCH AND IS DRILLED OUT, MOUNTS ARE HELD IN PLACE. PLACED SEALANT AND HARDWARE BY BEAM. REPLACED BEAM.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 49,735 hrs · 17,927 cycles

LAVATORY DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND SMOKE DETECTOR MALFUNCTIONED. REPLACED SMOKE DETECTOR, SYS OPS CHECKED NORMALLY.

Part: CHARGER — FAULTY (CABIN) · airframe 49,552 hrs · 17,864 cycles

EMERG LIGHT TEST FAILED AFTER SLIDE CHANGE..."L EMERG BATT" FAULT. WEAK BATTERY, REPLACED LEFT OVERWING BATTERY & CHARGER. TEST OK.

Part: RELAY — FAILED (FIRE EXTING) · airframe 48,931 hrs · 17,632 cycles

APU FIRE EXTINGUISHING CIRCUIT CHECK FAILS. FOUND FLIGHT GROUND RELAY 43WF FAILING. FLIGHT GROUND RELAY 43WF REPLACED, OPS TESTED SYSTEM NORMAL.

Part: COMPUTER — FAULTED (NR 2 ELAC) · airframe 48,668 hrs · 17,538 cycles

F-CTL ELAC 2 FAULT ON UPPER ECAM. PERFORMED RESET AND RECURRED. ELAC INTERMITTANT, BAD MPS BOARD INTERNAL. REPLACED ELAC 2, ALL TESTS NORMAL.

Part: WINDOW FRAME — DENTED (FUSELAGE) · airframe 48,660 hrs · 17,535 cycles

DENT 12 INCH BELOW F/O WINDOW FRAME 5.5 INCH HIGH 4.5 INCH WIDTH 0.1 DEEP. 12 INCHES ABOVE CF9026. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED MAJOR REPAIR IN SFO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,145 hrs · 17,354 cycles

SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE LIGHT OUT AT SEAT 24C. REPLACED LIGHT ASSY.

Part: LIGHT — BROKEN (SEAT 17) · airframe 46,499 hrs · 16,762 cycles

AISLE EMERGENCY LIGHT PATH HAS LIGHT BROKEN AT SEAT 17. UNKNOWN DAMAGE TO LIGHT ASSY. REPLACED LIGHT ASSY AT SEAT 17.

Part: LIGHT — INOPERATIVE (ROW 18,) · airframe 46,499 hrs · 16,762 cycles

AISLE EMERGENCY LIGHT PATH HAS LIGHTS OUT AT ROW 18, 19, 21. FOUND LAMPS FAULTY. RELAMPED EMERGENCY LIGHTS AT ROW 18,19,21.

Part: WIRE — SHORTED (CABIN) · airframe 44,760 hrs · 16,136 cycles

CABIN EMERGENCY LIGHTING DOES NOT TEST OK. SEAT FOUND MOUNTED ON TOP OF POWER (RED) WIRE, CAUSING SHORT. RESPLICED ALL THREE SEATS TO POWER AND GROUND WIRE FROM WALL CONNECTOR. ROUTED PROPERLY AND SECURED. ALL LIGHTS TEST NORMAL. EMER LIGHT TEST AT ATTNDT PANEL OK.

Part: A/C PACK — OVERHEATED (NR 2) · airframe 44,425 hrs · 16,014 cycles

PACK 2 OVERHEAT DISPLAYED ON UPPER ECAM SCREEN. AIR CREW COMMENTS: FLIGHT ATTENDANT OBSERVED VERY FAINT SMOKE IN BACK AS WELL AS ODOR. [SUP 05-16-07] DETERMINED THAT AIR CYCLE MACHINE IN PACK 2 HAD SEIZED DUE TO FAILED BEARINGS.

Part: SLIDE — FAULTY (LT OVERWING) · airframe 44,395 hrs · 16,003 cycles

FOUND AT PTP PANEL TEST LEFT INTER EXTERNAL FAULTS. [SUP 05-16-07] REPLACED THE LT OVERWING SLIDE ASSEMBLY. AT OVERHAUL, DETERMINED THAT THE PACK BOARD WAS FAULTY.

Part: COVER — DISLODGED (L2 DOOR SLIDE) · airframe 43,547 hrs · 15,697 cycles

SLIDE COVER AT 2L COMES OFF. REPLACED 2 LEFT SLIDE RAFT.

Part: VALVE — UNSERVICEABLE (SLIDE) · airframe 43,251 hrs · 15,594 cycles

LOW BOTTLE PRESSURE. SHOP FINDINGS: LEAKING AROUND FILL VALVE O-RING. REPLACED FILTER VALVE AND FILL VALVE O-RING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,697 hrs · 14,696 cycles

PUNCTURE TO FUSELAGE SKIN FOUND ON LT SIDE BETWEEN BODY STATION 11100 TO 12167. APPROX FRAME 27 TO FR 29. DAMAGE ENCOMPASSES A 40 INCHES LONG HORIZONTAL INDENTATION, 21.5 INCH LONG X 15 PUNCTURE. DAMAGE IS ALONG SKIN LAP. MAJOR REPAIR DOUBLER INSTALLED IN ACCORDANCE WITH SRM 53-00-11, FIGURE 212 AND AIRBUS RAS 042528/006/2006 ISSUE A.

Part: LIGHT — INOPERATIVE (SEAT 13ABC) · airframe 39,839 hrs · 14,387 cycles

SEAT MOUNTED EEL LIGHT INOP AT SEAT 13ABC. REPLACED CABLE ASSY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,537 hrs · 14,275 cycles

FUSELAGE SKIN IN AREA AROUND DOOR 2L IS DAMAGED. REPAIRED AREA AROUND DOOR 2L WITH DOUBLER PER SRM 53-00-11 PR 313-314.

Part: DUCT — LOOSE (LT WING) · airframe 37,812 hrs · 13,698 cycles

LEFT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT LOOSE AT FIRST CLAMP AFT OF THE GROUND AIR CONNECTOR. REPOSITIONED DUCT AND RESECURED CLAMPS.

Part: DUCT — DISCONNECTED (BLEED AIR) · airframe 37,812 hrs · 13,698 cycles

LT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT DISCONNECTED AT GROUND BLEED AIR CONNECTOR. RECONNECTED DUCT.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 32,992 hrs · 12,066 cycles

LEFT ELEVATOR UPPER SKIN HAD ONE AREA OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205, SHEET 3.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 32,992 hrs · 12,066 cycles

RT ELEVATOR UPPER SKIN HAD 2 AREAS OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205 SHEET 3 & 4.

Part: BLADE — FRACTURED (COMPRESSOR) · airframe 30,643 hrs · 11,193 cycles

COMPRESSOR STALL NR 2 ENGINE. THROTTLED TO IDLE, ENGINE WAS NOT SHUTDOWN. ENGINE TEARDOWN REVEALED C6 BLADE FAILURE RESULTING FROM NICKED C6 VANE. BIRD INGESTION 17 DAYS PRIOR HAD BEEN BORESCOPED WITH NO FINDINGS IN FIRST THREE STAGES.

Part: OIL COOLER — LEAKING (APU) · airframe 30,567 hrs · 11,166 cycles

NOXIOUS ODOR IN CABIN AFTER TAKEOFF. SUBJECT APU OIL LEAK WAS CONFIRMED AT TEST. OIL COOLER WAS LEAKING SEVERELY (APPROX 1/2 QT. / MINUTE) FROM THE INLET SIDE OF THE PRESSURE REGULATOR. FURTHER DISASSEMBLY REVEALED SEVERAL DEEP VERTICAL SCRATCHES EVIDENT AT THE INSIDE DIAMETER THAT INTERFACES WITH THE REGULATOR CAP THAT IS SEALED WITH AN O-RING. THE DAMAGE APPEARS TO HAVE OCCURRED DURING ASSEMBLY OF THE REGULATOR VALVE, SPRING, AND CAP ASSEMBLY.

Part: IDG — OVERHEATED (LT ENGINE) · airframe 27,752 hrs · 10,032 cycles

NR 1 INTEGRATED DRIVE GENERATOR DISCONNECTED AND UNABLE TO START AUXILIARY POWER UNIT. REPLACED NR 1 ENGINE INTEGRATED DRIVE GENERATOR.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 26,618 hrs · 9,593 cycles

ON CLIMBOUT FELT STRONG VIBRATION IN RUDDER PEDALS. STRONG VIBRATION WAS FELT IN THE REAR OF THE CABIN. THE VIBRATION WAS REPORTED AS BEING A SIDE-TO-SIDE MOTION. FAC (FLIGHT AUGMENTATION COMPUTER) WAS REPLACED.

Part: TUBE — UNSERVICEABLE (SLIDE) · airframe 25,493 hrs · 9,506 cycles

SLIDE/RAFT D30665-105 TOP INFLATION TUBE RT SIDE SEAM FAILED DURING PROOF PRESSURE TEST. TOP TUBE HAS A 4 FOOT SEAM RIP ON RT SIDE ABOVE THE REDUCER BULKHEAD FROM THE FAILURE. UNIT IS BEING SENT TO THE VENDOR FOR REPAIR.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 23,823 hrs · 8,646 cycles

OUTER LAMINATE WINDOW R-3 PEELED OFF IN FLIGHT. SUPPLEMENTAL DATA UPDATE INITIAL FINDINGS SHOW STRONG PROBABILITY THAT THE FAILURE OCCURRED DUE TO SUBSTANDARD INTERLAYER BONDING DUE TO A BAD PRIMER USED DURING PRODUCTION. REPLACED WINDOW.

Part: SEAT PAN — CRACKED (CABIN)

DURING FIRST HEAVY MAINTENANCE VISIT FOR THIS AIRBUS, A-320-232, 100 PERCENT OF THE SEAT PANS WERE FOUND CRACKED ON THE RECARO MODEL 3410, 720 SERIES PASSENGER SEATS USED IN THE COACH CLASS CABIN. THESE SEAT PANS ARE CRACKED ADJACENT TO THE SCREW HOLES ON THE FORWARD EDGE OF THE PAN. THESE ARE THE HOLES USED TO ATTACH THE SEAT PAN TO THE SEAT FRAME.

Part: PUMP — FAILED (GREEN HYD SYST)

CREW REPORT, GREEN EDP LOW PRESSURE AND LOW GREEN SYSTEM PRESSURE. QUANTITY IS INDICATING ZERO AMBER ALERT. RETURNED TO DENVER. *S/D* GREEN SYSTEM HYD PUMP REPLACED.

Part: PROXIMITY SWITCH — DIRTY (CARGO DOOR)

CREW REPORTED, THAT THE FORWARD CARGO DOOR LIGHT CAME ON INTERMITTENTLY IN CRUISE AND THEN WENT OUT. FOUND DOOR PROXIMITY SWITCH DIRTY, CLEANED AND OPERATIONALLY CHECKED NORMAL.

Part: ENGINE — FLAME-OUT (NR 1)

NUMBER ONE ENGINE FLAMED-OUT IN FLIGHT.