N423UA

Part: NONE — LOCKED (FLAPS) · airframe 87,329 hrs · 34,510 cycles

FLAPS STUCK AT LESS THAN 1F/CTL FLAPS/LOCKED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM GVI OF PERFORM GVI OF SLATS AND FLAPS AND CALL TOMC 847-700-9980 PERFORM GVI OF SLATS AND FLAPS AND CALL TOMC 847-700-9980 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM GVI OF SLATS AND FLAPS AND CALL TOMC 847-700-9980 SLATS AND FLAPS AND CALL TOMC 847-700-9980 ACP WTB RESET PER AMM TASK 27-50-00-869-006-A, T/S FLAP MECH 27-54-00-710-00-1-A. NO FAULTS TEST OK. DRIVE SYSTEM PER TSM 27-51-00-810-818-A , DUE TO BOTH SFCC1 AND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1903120 SN OFF 4054 SFCC2 FAULTING RH MECH DRIVE, REPLACED RH INTERCONNECTING STRUT PER AMM 27-51-44-400-001-A, PERFORMED SYSTEM OPS TEST PER AMM STRUT, CONNECTI OFF 31-2751-9-9001 4054 ON 31-2751-9-9001 4976

Part: NONE — FAILED (ENG #1) · airframe 86,775 hrs · 34,253 cycles

TOTAL LOSS OF GREEN HYD SYS, #1 ENGINE DRIVEN HYD PUMP REQUIRES REPLACEMENT. REPLACED HYD PUMP . STOPPED AT STEP CORRECTING M&E SN COMPLETED #1 EDP INSTALLATION. LEAK CHECK REQUIRED. REPLACED POWER TRANSFER UNIT, REQUIRES OPS D.3 ROTABLE PARTS CHANGE WAS INDICATED - SN OFF 0752 IPC REFERENCE # 29-11-51-01 UNIT, TRANSFER OFF 31-2920-9-0001 0752 ON 31-2920-9-0001 1585 SERVICED HYDRAULIC SYSTEMS AND PERFORMED BLEED PUMP, HYDRAULIC OFF 31-2914-9-9003 8683 ON 19-2910-9-0003 6395

Part: FUEL CAP — MISSING (NA) · airframe 84,936 hrs · 33,403 cycles

PDA 2 PDA LOG PAGE GENERATED FOR MISSING FUEL CAP REFERENCE LOG PAGE 746973 PER GMM 02-30-95 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V916121 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003027389 AND PRTR LUIBRAND, NATHAN (V916121) COMPLIED WITH DOCUMENTATION OF PDA CAT 2 FOR MISSING FUEL CAP AS PER GMM 02-30-95. VARGAS TOMC LUIBRAND, NATHAN (V916121) COMPLIED WITH DOCUMENTATION OF PDA CAT 2 FOR MISSING FUEL CAP AS PER GMM 02-30-95. VARGAS TOMC ADD EMP:V916121

Part: RIVET — DAMAGED (NR 1 ENG INLET) · airframe 84,099 hrs · 33,024 cycles

PDA 3 TOTAL OF 6EA RIVET HEADS BROKEN/MISSING AT OUTER LIP SKIN OF #1 ENG AIR INLET COWL -- SEE PHOTO CORRECTION - #2 ENG AIR INTAKE COWL REPLACED 6 EA RIVETS REF ECRA 7111-01387

Part: FRAME — CRACKED (FRM 35) · airframe 77,261 hrs · 29,980 cycles

A CRACK INDICATION DURING ROTO PROBE AT FRAME 35, STRINGER 30L, ACCOMPLISHED A PERMANENT REPAIR IAW ECRA 5331-02230, PART 3.

Part: SLIDE — DELAMINATED (LT OVERWING) · airframe 77,260 hrs · 29,980 cycles

LEFT OVERWING SLIDE HAS COMPOSITE DELAMINATION ON FWD EDGE. REMOVED AND REPLACED THE SLIDE.

Part: STRINGER — CORRODED (FRAMES 31-32) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON STRINGER BETWEEN FR 31-32. REPAIRED, HFEC,ROTOPROBE , UT AND RESTORED IAW SRM 21-74-00-001, AND SRM 53-21-13-300-002.

Part: LENS — MISSING (LAVATORY D) · airframe 77,260 hrs · 29,980 cycles

LAVATORY D, AFT EMERGENCY LIGHT LENS WAS MISSING, REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33 -51-19-000-002-A, AND 33-51-19-400-002-A. PERFORMED CHECK OF CABIN LIGHTS AND SIGNS IAW AMM 33-51-00-710-009-A. NO DEFECTS NOTED.

Part: CIRCUIT BREAKER — BROKEN (EMERGENCY LIGHTS) · airframe 77,260 hrs · 29,980 cycles

EMERGENCY LIGHT CIRCUIT BREAKER H5, WAS BROKEN. REPLACED THE CIRCUIT BREAKER IAW ESPM 20-46-10 IDT.

Part: STRINGER — CORRODED (FRAMES 32-33) · airframe 77,261 hrs · 29,980 cycles

CORROSION ALONG STRINGER 40R BETWEEN FRAMES 32 AND 33 IN THE FWD CARGO BILGE AREA. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-13-283-001. INSTALLED A REPAIR IAW SRM 53-21-13-300-004.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 77,260 hrs · 29,980 cycles

EEPL HARNESS BETWEEN SEAT ROW 29 TO 31 HAS DAMAGED INSULATION. REMOVED AND REPLACED EEPL HARNESS BETWEEN SEAT ROW 29 TO 31 IAW AMM 33-51-22-400-802C1. OPS TESTS TO BE PERFORMED.

Part: PLATE — CORRODED (FRAME 29) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43R, FRAME 29, IN THE FWD CARGO BILGE. REMOVED & REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, PERFORMED ROTO PROBE IAW NTM 51-10-0 1, NO DEFECTS FOUND. RESTORED PROTECTIVE FINISH IAW SRM 51-75 -12-911-002, 51-43-00-001, AND ER5100R01017 REV E.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE SHEAR TIE AT FRAME 31, BETWEEN STRINGERS 38R AND 39R, IN THE CARGO BILGE AREA. REMOVED, FABRICATED, AND INSTALLED A SHEAR TIE IAW SRM 51-75-12- 911-002, 51-72-11-911-001, 56-26-00, 51-21-11, 51-23-00, ER5100R0 1017, REV E, AND NTM 51-10-01.

Part: PLATE — CORRODED (FRAME 32) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43R, FRAME 32 IN THE CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-001, SRM 51-72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV E.

Part: PLATE — CORRODED (FRAME 34) · airframe 77,261 hrs · 29,980 cycles

CORROSION WAS FOUND ON THE FISH PLATE BETWEEN STRINGERS 41R AND 42R, FRAME 34 IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED FISH PLATE IAW SRM 51-72-11-9 11-001, NTM 51-10-01, AND ER 5100R01017, REV E.

Part: PLATE — CORRODED (FRAME 27) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42R AND 43R, FRAME 27, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV, E.

Part: PLATE — CORRODED (FRAME 31) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42R AND 43R, FRAME 31 IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51- 72-11-911-001, NTM 51-10-01, AND ER 5100R01017, REV E.

Part: DOOR FRAME — CORRODED (FR 68) · airframe 77,261 hrs · 29,980 cycles

CORROSION ON L2 DOOR AFT FRAME 68, BLENDED THE CORROSION IAW SRM 51-74-00-001. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12-283-001, FIGURE 10102, (SHEET 1). ACCOMPLISHED HFEC AND ROTOPROBE OF BLENDED AREA IAW NTM 51 -10-02,51-10-01. NE DEFECTS NOTED.

Part: PLATE — CORRODED (FRAME 32) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 43L AND 44L, FRAME 32 FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, AND ER5100R01017, REV E.

Part: PLATE — CORRODED (FRAME 32) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 39R AND 40R, FRAME 32, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE. PERFORMED A ROTO PROBE INSPECTION. NO CRACKS OR CORROSION NOTED.

Part: PLATE — CORRODED (FRAME 33) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41R AND 42R, FRAME 33, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED FISH PLATE IAW SRM 51-72-11-911-001, NTM 51-10-01, ER5100R01017, REV E.

Part: SKIN — DENTED (FRAMES 55-56) · airframe 77,261 hrs · 29,980 cycles

DENT FOUND IN THE LEFT LOWER FUSELAGE BETWEEN FRAMES 55 & 56 JUST ABOVE STRINGER 35L. CUT OUT THE DAMAGE & REPAIRED THE SKIN IAW SRM 53-00-11-300-042. ACCOMPLISHED HFEC OF CUTOUT & ROTO PROBE OF OPEN HOLES, NO CRACKS FOUND.

Part: STRINGER — CORRODED (FRAME 58) · airframe 77,261 hrs · 29,980 cycles

CORRODED STRINGER 41R, FRAME 58. FOUND TO BE OUT OF LIMITS, NO DEFECTS NOTED. CUTOUT THE DAMAGE SECTION OF THE STRINGER BETWEEN FRAMES 58 TO 59, AND INSTALLED A REPAIR.

Part: PLATE — CORRODED (FRAME 31) · airframe 77,261 hrs · 29,980 cycles

CORROSION ON FISH PLATE AT FRAME 31 BETWEEN STRINGERS 40 AND 41R, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001, AND N TM 51-10-01.

Part: PLATE — CORRODED (FRAME 33) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 43L TO 43R, FRAME 33, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-42-11-001, NTM 51-10-01, AND SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 34) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41 AND 42L, FRAME 34, IN THE FWD CARGO BAY AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-72-11-911-001. ACCOMPLISHED ROTO-PROBE OF OPEN HOLES, NO DEFECTS NOTED. REAMED UP FOUR FASTNERS HOLES TO .189 IAW IAW SRM 51-44-11-001.

Part: FRAME — DENTED (FRM 53) · airframe 77,261 hrs · 29,980 cycles

AFT CARGO FRAME 53, STRINGERS 39 - 40L THE FRAME WAS DENTED. REMOVED AND REPLACED THE FRAME IAW SRM 57-72-11-911-001.

Part: PLATE — CORRODED (EXHAUST VENT) · airframe 77,261 hrs · 29,980 cycles

LAVATORY EXHAUST VENT HAD CORROSION ON THE INSIDE REINFORCEMENT PLATE, ON THE SKIN IN THE AFT WET AREA. REMOVED AND REPLACED REINFORCEMENT PLATE IAW SRM 51-42-11-001.

Part: COVER — CORRODED (AFT CARGO) · airframe 77,261 hrs · 29,980 cycles

AFT CARGO TORSION BOX COVER HAS SEVERAL AREAS OF CORROSION, BLENDED OUT CORROSION, AND FOUND TO BE 100% MATERIAL LOSS. REMOVED AND REPLACED TORSION BOX COVER, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911-001.

Part: INTERCOSTAL — CRACKED (DOOR FRAME) · airframe 77,261 hrs · 29,980 cycles

ROTO PROBE SHOWED A CRACK INDICATION AT FRAME 16, NR 7 DOOR STOP, ON THE INTERCOSTAL ONLY, REMOVED AND REPLACED THE INTERCOSTAL IAW IAW SRM 51-72- 11-911-001.

Part: WIRE — DAMAGED (FRAME 63) · airframe 77,260 hrs · 29,980 cycles

TWO DAMAGED WIRES AT FRAME 63, STRINGER 14L, BETWEEN THE AFT 2 WINDOWS. REPAIRED THE WIRES 3351-1765 & 3351-1759 IAW ESPM 20-53-21-0201.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE STRINGER 41R SPLICE BETWEEN FRAMES 30 AND 31, IN THE FWD CARGO BILGE AREA. REMOVED & REPLACED THE STRINGER SPLICE IAW SRM 51-72-11-911-001, AND 51-42-11-001-2E

Part: DOOR SILL — CORRODED (R2) · airframe 77,261 hrs · 29,980 cycles

R2 DOOR SILL WAS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 30) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 41R AND 42R, FRAME 30, IN THE FWD CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW 51-72-11-911-001, ER 510 0R01017, AND SRM 51-75-12-001.

Part: PLATE — CORRODED (FRAME 24) · airframe 77,261 hrs · 29,980 cycles

CORROSION ON FISH PLATE BETWEEN STRINGERS 43 AND 44R, FRAME 27, IN THE CARGO BILGE AREA. REMOVED AND REPLACED THE FISH PLATE IAW SRM 51-42-1 1-001-2E, AND 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 30) · airframe 77,261 hrs · 29,980 cycles

FWD CARGO FISHPLATE HAD CORROSION FRAME 30 BETWEEN STRINGERS 43 AND 44L. REMOVED AND REPLACED THE FISHPLATE IAW SRM 51-72-11-911-001, 2 (A), (3) A, NTM 51-10-01, SRM 51-75 -12-001, AND ER 5100R01017.

Part: SPLICE — CORRODED (FRAME 68) · airframe 77,261 hrs · 29,980 cycles

AFTER REMOVAL OF THE R2 DOOR SILL, FOUND THE CROSSBEAM TO FRAME CONNECTION SPLICE CORRODED AT FRAME 68. REMOVED AND REPLACED FRAME TO CROSSBEAM SPLICE IAW SRM 51-72-11-911-001.

Part: STRINGER — CORRODED (FRAME 66) · airframe 77,261 hrs · 29,980 cycles

FRAME 66, STRINGER 25R HAS AN AREA OF CORROSION ON THE STRINGER UNDER THE R2 DOOR SILL. REMOVED AND REPLACED THE STRINGER FROM FRAMES 64 TO 67 IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 29) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 43L AND 43R AT FRAME 29, REMOVED AND REPLACED THE PLATE IAW SRM 51-72-11-91 1-001.

Part: PLATE — CORRODED (FRAME 31) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGER 41 AND 42R, AT FRAME 31. REMOVED & REPLACED THE PLATE IAW SRM 51-72-11-911-001.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 77,260 hrs · 29,980 cycles

WIRE 3351-1240 FOUND DAMAGED FOR THE EMERGENCY LIGHT CONNECTOR. REPAIRED IAW ESPM 20-53-21-0201, AND 20-48-14-0101. NO DEFECTS NOTED.

Part: PLATE — CORRODED (FRAME 27) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 39 AND 40 AT FRAME 27. REMOVED AND REPLACED THE PLATE IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 28) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43L, FRAME 28. REMOVED AND REPLACED THE PLATE, ACCOMPLISHED A ROTO-PROBE, NO DEFECTS NOTED IAW SRM 51-72-11-001.

Part: PLATE — CORRODED (FRAME 32) · airframe 77,261 hrs · 29,980 cycles

CORROSION ON FISH PLATE BETWEEN STRINGERS 40 AND 41R, AT FRAME 32. REMOVED AND REPLACED THE PLATE IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 32) · airframe 77,261 hrs · 29,980 cycles

CORROSION FOUND ON THE FISH PLATE BETWEEN STRINGERS 42 AND 43 LEFT AT FRAME 32. REMOVED AND REPLACED THE PLATE IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 28) · airframe 77,261 hrs · 29,980 cycles

FISHPLATE HAS CORROSION AT FRAME 28 BETWEEN STRINGERS 42R AND 43R. REMOVED AND REPLACED THE PLATE IAW SRM 51-72-11-911-001.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 77,079 hrs · 29,904 cycles

FWD EMERGENCY LIGHT POWER SUPPLY FAILED A TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-38-40 0-002-A. TESTED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,569 hrs · 28,730 cycles

ELECTRICAL ODOR AFT GALLEY RAN OVENS, CHILLERS AND COFFEEMAKERS ALSO ALL LIGHTS ON FOR 25 MINUTES, COULD NOT DUPLICATE THE ODOR.

Part: ENGINE — OVERTEMP (NR 2) · airframe 73,588 hrs · 28,308 cycles

CREW REPORTS ON APPROACH ENG 2 SPIKED TO 890 DEGREES. SHUTDOWN ENGINE PER QRH. PULLED THROTTLE BACK, EGT STAYED AT 890. COMMENCE ENGINE SHUTDOWN PER QRH REMOVED AND RPL THE FWD AND AFT EGT HARNESS AND 4 EACH THERMOCOUPLE EGT PROBES REF AMM-TASK 77-21-43-00-010B AND AMM 77-21-43. FUNCTIONAL TEST REF 77-21-43-700-010-A TEST PASSED. REMOVED AND REPLACED NR 2 ENG REF MT71- 017 REV S.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

LIGHT OVER EMERGENCY EXIT WILL NOT SHUT OFF WITH REST OF LIGHTS. SECURED LOOSE CONNECTOR ON RT SIDE BALLAST, OPS OK

Part: FEEDER CABLE — UNSECURE (CABIN) · airframe 71,000 hrs · 27,092 cycles

LEFT AFT EMER BATTERY IS INOPERATIVE. SECURED POWER FEEDER. OPERATIONS GOOD.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 71,000 hrs · 27,092 cycles

ON TWO SERVICE FOUND LT AFT 3 EMER EXIT LIGHTS INOPERATIVE. NO VOLTAGE AT 36 ABC EMER EXIT LIGHT HARNESS. REPAIRED WIRE AT CONNECTOR, WDM 33-51-04. EMER EXIT LIGHTS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 69,513 hrs · 26,450 cycles

MULTIPLE FAULTS ON APP B14, CB TRIPPED. F-LOCKED BUT FLAPS OPERATES NORMAL, DUCT OVHT & PACK OVHT, SUCCESSFUL WTB RESET. CYCLED FLAPS NO FAULTS. RAN BOTH ENGS. VOLTS & FREQS ALL NORMAL. AC & DC BUSSES ALL POWERED NORMALLY. PACK TEMPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 69,513 hrs · 26,450 cycles

MULTIPLE FAULTS ON APP B14, CB TRIPPED. F-LOCKED BUT FLAPS OPERATES NORMAL, DUCT OVHT. PACK OVHT SUCCESSFUL WTB RESET. CYCLED FLAPS, NO FAULTS. RAN BOTH ENGS VOLTS & FREQS, ALL NORMAL. AC & DC BUSSES ALL POWERED NORMALLY. PACK TEMPS NORMAL.

Part: STRUT — DEFECTIVE (LANDING GEAR) · airframe 68,331 hrs · 25,969 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. FAULTS WITH PROXIMITY SENSORS 21GA & 23GA. STRUT IS SHOWING A 250 PSI DIFFERENCE BETWEEN UPPER & LOWER CHAMBERS, 25 PSI IS GENERAL DIFFERENCE LIMIT. ADJUSTED PROXIMITY SENSOR. PERFORMED FULL STRUT SERVICE & GEAR SWING 32-31-00-720-002.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,316 hrs · 25,961 cycles

STRINGER 31R AT FRAME 65 BELOW OUTFLOW VLV IS CORRODED. REPLACED FACTORY SECTION OF STRINGER IAW SRM 51-72-11.

Part: SELECTOR VALVE — LEAKING (NLG STEERING) · airframe 66,880 hrs · 25,378 cycles

FLUID COMING OUT AROUND NOSE STRUT. R & R LEAKING NLG STEERING SWIVEL SELECTOR VLV.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 66,291 hrs · 25,155 cycles

COND AFT CARGO HEAT FAULT DISPLAYED. UPDATE CREW ABORTED TO LESS THAN 60 KTS DUE TO ECAM DISPLAYED ON ROLL.

Part: BOLT — LOOSE (FUSELAGE) · airframe 64,833 hrs · 24,566 cycles

BOLT HANGING DOWN ON PACK COVER JUST FWD OF RAT.

Part: TRANSCEIVER — FAULTY (VHF COMM) · airframe 64,370 hrs · 24,390 cycles

VHF 2 TRANSMIT GARBLED. REPLACED VHF 2 TRANSCEIVER IAW MM.

Part: BARREL NUT — DAMAGED (FUSELAGE) · airframe 64,347 hrs · 24,380 cycles

CREW REPORTS FASTENER LOOSE & HANGING FROM BELLY PANEL 192KB. REPLACED DAMAGED BARREL NUTS & REINSTALLED PANEL IAW AMM 53-35-13-400-002-A.

Part: EXCITER — FAULTY (APU) · airframe 64,100 hrs · 24,289 cycles

AUXILIARY POWER UNIT WILL NOT START. R & R AUXILIARY POWER UNIT IGNITER BOX. R & R AUXILIARY POWER UNIT PLUGS. R & R AUXILIARY POWER UNIT IGNITER PLUG LEADS, OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 64,098 hrs · 24,288 cycles

FORWARD CARGO DOOR EXTERIOR SKIN LOWER AREA HAS LIGHTNING STRIKE. REPAIRED LIGHTING STRIKE ON FWD CARGO DOOR SKIN FASTENER IAW SRM 52-00-00 FIG 213. REPAIR WORK PERFORMED PER FIG 213 SHEET 2C IIR 52-00-00-2-003-00 & PAGES 211 212 TABLE 204. AT TIME OF 1ST INSPECTION, RE-CHECKED SRI & APPLY APPLICABLE LIMITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,098 hrs · 24,288 cycles

FWD RT FUSELAGE SKIN FASTENERS HAVE SEVEN EACH LIGHTING STRIKES BETWEEN FRAME 09-24 & STR 37-39. REPAIRED SEVEN EACH LIGHTING STRIKES FWD LOWER RT FUSELAGE SKIN FM 9-24 STR 37-39 IAW SRM 53-11 -11 FIG 211.

Part: COMPUTER — FAILED (NR 2 ELAC) · airframe 63,887 hrs · 24,196 cycles

ELAC 2 FAULTED. DUE TO REPETITIVE ELAC 2 FAULTS WITH NO CFDS FAULT ACTIVITY, AND MULTIPLE SUCCESSFUL RESETS, ACCOMPLISHED TSM TASK 27-93-00-810-947. ELAC 2 FAILED AND WAS SWAPPED WITH ELAC 1, OP CHECKED GOOD.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 63,716 hrs · 24,128 cycles

RT WING FUEL PANEL 640QB, SCRE HOLE FOUND MIS-DRILLED. REPAIRED 1 EA MISDRILLED HOLE RT WING PANEL 640QB LANDING IAW ECRA 5720-02416.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 63,716 hrs · 24,128 cycles

LT FUEL PANEL 540LB BETWEEN RIBS 16-17 HAS SEVEN ELONGATED HOLES IN TANK LANDINGS. REPAIRED FOUR HOLES IAW SRM 57-21-11, REPAIRED THREE HOLES IAW ECRA 5720-02415 REV A.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 31 DEF) · airframe 63,453 hrs · 24,026 cycles

OXYGEN MASKS DEPLOYED 31DEF. STOWED MASKS AT 31DEF IAW MT 35-003 AMM. INSPECTED BOX AND LATCH ALL OPS CHECKED GOOD. ACCOMPLISHED MANUAL MASK DROP TEST IAW MM 35-23-00-710-001-A. TESTED, OPS NORMAL. NO DEFECTS NOTED.

Part: CONTROL UNIT — FAILED (MLG) · airframe 63,392 hrs · 23,998 cycles

LG CIU 2 HIT TWICE ON LAST FLIGHT-FIRST TIME WAS ON THE GROUND. CREW PERFORMED FM RESET SYS, RESTORED TO NORMAL. SECOND TIME WAS ON ROLLOUT, CREW HAD TO CYCLE NWS SWITCH TO REGAIN STEERING AND FAULT CLEARED, HAS HISTORY. INSPECTED & OHMED WIRING CLEANED CP AT 4029VC. TAXIED AC ALL INDICATIONS NORMAL. R & R LG CIU 2 IAW 32-31-71 AS PRECAUTION. TESTED NOSEWHEEL STEERING IAW 32-46-00 & TAXI ALL CHECKED NORMAL. CLOSED & SECURED ALL DOORS.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 63,388 hrs · 23,996 cycles

LGCIU 2 INOPERATIVE ON PUSH BACK. LAST LEG REPORT SHOWS PROXIMITY SENSOR 17GA -L LG DOWNLOCK. VERIFIED LGCIU NR 2 CORRECT IAW EA 3260-01136, REV A. REPLACED PROXIMITY SENSOR 17GA IAW AMM, TARGET CLEARANCE OK IAW AMM.

Part: EXHAUST DUCT — CRACKED (NR 2 ENGINE) · airframe 61,371 hrs · 23,194 cycles

TWO INCH CRACK IN SHEETMETAL IN ENG NR 2 AT 12.30 POSITION IN EXHAUST END. STOPPED DRILLED PER MT78-00. CRACK BEYOND ALLOWABLE MM LIMITS. REPLACED CNA MM 78-11-11.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 60,422 hrs · 22,789 cycles

OXYGEN MASKS FELL IN ROW 31DEF ON TAKEOFF. STOWED MASKS.

Part: OIL COOLER — FAILED (NR 1 ENGINE) · airframe 59,497 hrs · 22,411 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND FUEL ON OIL SIDE OF FCOC, REPLACED FUEL CONTROL OIL COOLER PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,457 hrs · 22,398 cycles

JIC 49795401C DURING HMV 3 VISIT REQUIRES LT AIRPHONE ANTENNA REMOVED AND SKIN DOUBLER INSTALLED. MAJOR REPAIR ACCOMPLISHED: INSTALLED SKIN DOUBLER PER SRM. SRI REQUIREMENTS REF SRI 53-00-11-TABLE 219. INSTALLED SKIN DOUBLER.

Part: DOUBLER — FAULTY (FUSELAGE) · airframe 59,457 hrs · 22,398 cycles

EXISTING SKIN DOUBLER AT FR 73- 74, STR 31R-33R.33R. REMOVED EXISTING RPR AND INSTALLED NEW DOUBLER RPR PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,457 hrs · 22,398 cycles

PER JIC 49795401C REQUIRES REMOVAL OF RT AIRPHONE ANTENNA AND SKIN DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED AIRPHONE ANTENNA & INSTALLED SKIN DOUBLER. THIS ITEM ACCOMP COA 40795C.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 59,457 hrs · 22,398 cycles

EMERGENCY LIGHTS IN CABIN ARE VERY DIM AND EPSU WILL NOT SELF TEST. RMVD & RPLD EPSU, OP CHECKS GOOD IAW A320 MM ON N-R V9255I.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,457 hrs · 22,398 cycles

STR 43L AT FRAME 63 HAS CORROSION. MAJOR REPAIR. INSTALLED STRINGER REPAIR PER SRM.

Part: SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 59,457 hrs · 22,398 cycles

MAJOR REPAIR. R2 DOOR SILL HAS CORROSION. DOOR SILL REPLACED IAW SRM 51-42-11.

Part: RAM AIR TURB — DAMAGED (HYDRAULIC SYS) · airframe 59,188 hrs · 22,282 cycles

REF EQ3075, FOUND BOTH RAM AIR TURBINE BLADES WITH WEAR MARKS IN LEADING EDGES, 3IN FROM HUB. WEAR IS 1-8\ DIA X .002' DEEP, NO RELIEF. WEAR HAS BEEN CAUSED BY CROSS MEMBER IN RAM AIR TURBINE STORAGE WELL, WEAR DAMAGE ON CROSS MEMBER IS APPROX 3-16\W X 1-8\D. RMV'D RAM AIR TURBINE. REPLACED RAT ASSEMBLY, CKS GOOD. ALSO NEED TO REPLACE EJECTOR JACK FOR RAT RPLC'D EJECTION JACK.

Part: FASTENER — LOOSE (RT WING) · airframe 58,976 hrs · 22,195 cycles

CREW REPORT: FUEL SEEPAGE ON RIGHT WING BY ACCESS PANEL JUST OTBD OF FUELING PANE. SAMC TEXT: FUEL ACCESS PLATE. TORQUED FASTENERS FOR PANEL 640NB, NO LEAKS NOTED.

Part: MOTOR — FAULTY (WINDSHIELD WIPER) · airframe 58,747 hrs · 22,079 cycles

LEFT WINDSHIELD WIPER INOP - ANTI-ICE. CREW COMMENTS: CAPT WIPER NOT MOVING THRU FULL ARC. MOTION IS VERY ERRATIC. DOES NOT CLEAR WINDSHIELD. REPLACED MOTOR ASSY.

Part: PANEL — LOOSE (RT WING) · airframe 57,840 hrs · 21,656 cycles

RETORQUED FUEL PANEL 640NB ON RT WING. FUEL SEEPING APPROX 6 INCHES INBD FROM FLAP FAIRING ON AFT EDGE. TORQUED PANEL IN ACCORDANCE WITH MM.

Part: STRUCTURE — LEAKING (WING) · airframe 57,657 hrs · 21,577 cycles

UNWANTED FUEL XFER INTO CENTER TANK. TROUBLESHOT PER TSM. CONTINUED SUMPING & PREP FOR CTR TNK ENTRY - NEED TO CHECK AIR INLET VLV & FLOAT VENT VLV. LT WING FUEL LEAKING OUT OF DRY BAY DRAIN HOLES. LT WING HAD MAX LEVEL FUEL FOR TROUBLESHOOTING PURPOSE. LEAKS FOUND AND MARKED WITH RED GREASE PEN. APPLIED A HALF SEALANT INSIDE AND OUTSIDE DRY BAY UPPER CORNER AND ALONG INBD RIB AND INBD SIDE OF DRY BAY PANEL. NEEDS LEAK CHECK. STATIC CHECK FAILED. STATIC CHECKED 6 HRS. CHECKS GOOD. NO LEAKS NOTED. RT WING FUEL LEAKING OUT OF DRY BAY DRAIN HOLES. FUEL LEVEL WAS AT MAX LEVEL FOR TROUBLESHOOTING.

Part: STRUT — UNDERSERVICED (MLG) · airframe 56,340 hrs · 21,021 cycles

TOOK 3 TRIES TO GET THE LANDING GEAR HANDLE TO MOVE TO GET THE GEAR TO RETRACT. FOUND BOTH MAIN GEAR STRUT UPPER CHAMBERS LOW. ACP FULL SVC ON MAIN GEAR. ACP GEAR SWING 3 TIMES, OPS GOOD.

Part: PUMP — ACTIVATED (RAT) · airframe 56,228 hrs · 20,967 cycles

RAT TEST FAILED. GREEN LIGHT DID NOT ILLUMINATE, RAT DID NOT COME UP TO SPEED. REPLACED RAT HYDRAULIC PUMP AND RAT GROUND CHECK MODULE. RAT FAILED TEST. RAT WILL NOT COME UP TO REQUIRED SPEED AND GREEN LIGHT WILL NOT ILLUMINATE.

Part: FIRE LOOP — FAULTY (LT MLG WW) · airframe 55,217 hrs · 20,511 cycles

FOUND FIRE LOOP IN LEFT WHEEL WELL MAKING CONTACT WITH SHIELDING AND BURNED. REPLACED SECTION OF APU BLEED AIR DUCTING IN LEFT WHEEL WELL.

Part: CONNECTOR — MALFUNCTIONED (RAT) · airframe 54,702 hrs · 20,255 cycles

2 HOURS AFTER TAKEOFF GOT A -RAT OUT- MEMO ON ECAM WITH A RAT OPERATING ICON ON HYD STATUS. NO ADDITIONAL NOISE NOTED IN CRUISE, JUST ECAM INDICATIONS. TROUBLESHOT IAW TSM, FAULT ISOLATION STEP 4B (1). RAT DID NOT DEPLOY, BUT AMBER "RAT HYD FAULT" AND "RAT OUT" WERE OBSERVED. ACCOMPLISHED STEPS IAW MM, DISCONNECTED CONNECTOR AND RAT FAULT MESSAGE EXTINGUISHED. . REPLACED RAT EJECTION JACK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 54,456 hrs · 20,150 cycles

CREW REPORTED BURNING ELECTRICAL ODOR UPON ENTERING COCKPIT, AVIONICS HORN ON. BLOWER EXTRACT FAULT. ODOR DISSIPATED WHEN ACFT PACKS WERE TURNED ON PER MEL. NO ECAM FAULTS. ACFT POWERED UP WITHOUT REGARD TO MEL PROCEDURE, BY OPS. POST FLIGHT REPORT SHOWS NO OTHER FAULTS.

Part: SLIDE — NO TEST (R2 DOOR) · airframe 54,281 hrs · 20,066 cycles

R2 DOOR SLIDE FAILED TO DEPLOY DURING ROUTINE DEPLOYMENT. SLIDE DID FULLY DEPLOY AFTER DOOR WAS MANUALLY PUSHED TO FULL OPEN POSITION. SLIDE REPLACED PER JIC AND INSPECTED BY LC81. SFOEG AND FLIGHT SAFETY NOTIFIED. NEED TO REPLACE R2 DOOR ASSIST BOTTLE ASSY PER SFOEG AND FLIGHT SAFETY. REPLACED ASSIST BOTTLE ASSY.

Part: BOTTLE — DAMAGED (EVAC SLIDE) · airframe 54,281 hrs · 20,066 cycles

RT OVERWING EMERGENCY EXIT SLIDE BOTTLE HAS BROKEN CABLE END. REMOVED & REPLACED RT OFFWING SLIDE BOTTLE. OPS TEST OF INFLATION RESV GOOD.

Part: CABLE — BROKEN (OVERWING SLIDE) · airframe 54,281 hrs · 20,066 cycles

RT OVERWING EMERGENCY EXIT SLIDE BOTTLE HAS BROKEN CABLE END.

Part: HYDRAULIC SYSTEM — LEAKING (GREEN) · airframe 53,842 hrs · 19,876 cycles

GREEN HYD ECAM, FLIGHT DIVERTED. FREEFALL EXTENTION OF GEAR WAS UTILIZED. CREW REPORTED THAT THEY FOLLOWED ECAM PROCEDURE AND SHUTOFF GREEN PUMP AND PTU. FOUND FLUID LOSS TO GREEN SYS. SERVICED GREEN SYS & ACCOMPLISHED MANUAL EXTENSION RESET.

Part: ENGINE — POWER LOSS (NR 1) · airframe 53,487 hrs · 19,727 cycles

NR 1 ENG MOMENTARY EPR-EGT DROP. IAW CREW THE DROP OCCURS AT FL270 275 KNOTS SAT -45. ENG PARAMETERS ARE NOW STABLE IN CRUISE. CREW CONFIRMS A SLIGHT MOMENTARY YAW WHILE ENGINE RECOVERED. A-T ON, A-P 2 ON. ACFT EXPERIENCING MODERATE TURBULENCE AT THE TIME. DROP WAS MOMENTARY AND RECOVERED IMMEDIATELY. FLEW ON AP1 & AP2 AUTOTHROTTLE ON & OFF, EPR IN NUMEROUS POSITIONS NO LOSS OF POWER. TRIED DIFFERENT SPEEDS AND ANGLES OF FLT. NO FAULTS NOTED.

Part: ATTACH FITTING — WORN (LT MLG DOOR ACT) · airframe 53,417 hrs · 19,687 cycles

LT MLG DOOR ACTUATOR ATTACH FITTING FWD LUG FWD FACE WAS FOUND WORN 0.0150" AT 5 O'CLOCK POS AND THE AFT LUG AFT FACE WAS FOUND WORN 0.0085" AT 1 O'CLOCK POS. REMOVED BUSH AT DOOR HINGE FWD LUG & SPOT FACED IAW STAM EA 320-5336-13-A1947. BLENDED AFT LUG. R & R BUSH & INSTALLED FILLER WASHERS & RESTORED SURFACE PROTECTION. THIS EVA HAS RECEIVED STAGE ONE APPROVAL (FOR STATIC STRENGTH) IAW PENDING DAMAGE TOLERANCE ANALYSIS. MFG MUST ISSUE NEW RAS WITH DTA FINDINGS ON OR BEFORE 19OCT 2010 OR ACFT MUST BE REMOVED FROM SERVICE.

Part: FITTING — WORN (R MLG DOOR ACT) · airframe 53,417 hrs · 19,687 cycles

RT MLG DOOR ACTUATOR ATTACH FITTING FWD LUG FWD FACE WAS FOUND WORN 0.0065" AT 12 O'CLOCK POS. REMOVED BUSH AT FWD LUG AND PERFORMED SPOT FACING. INSTALLED BUSH & FILLER WASHER & RESTORED SURFACE FINISH IAW EA THIS REPAIR HAS RECEIVED STAGE (1) APPROVAL (FOR STATIC STRENGTH) IAW UAL EVA PENDING DAMAGE TOLERANCE ANALYSIS (DTA). MFG MUST ISSUE A NEW RAS WITH DTA FINDINGS ON OR BEFORE 19OCT 2010 OR ACFT MUST BE REMOVED FROM SERVICE.

Part: COMPUTER — FAILED (FLT MANAGEMENT) · airframe 52,022 hrs · 18,983 cycles

FMGC NR 1 FAILURE, RTFL. RESET SYSTEM, CHECKS GOOD. ACCOMPLISHED AFS & AUTOLAND CHECK. OPS CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,491 hrs · 18,720 cycles

BURNING ODOR AROUND ROW 18. ALSO NOTICED BY PAX. CHECKED AREA OPEN STOW BINS FOUND NO DAMAGE OR PROBLEMS.

Part: BATTERY — FAULTY (CABIN) · airframe 50,738 hrs · 18,386 cycles

CIDS PANEL HAS EPSU FWD L MESSAGE. REPLACED BATTERY, TESTS OKAY.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 50,197 hrs · 18,176 cycles

ELECTRIC ODOR IN PAX CABIN. SUSPECT PAX ENTERTAINMENT SYSTEM. UNDER SEAT SBB PCN 582-0051 ODOR IS LIKE ELECTRICAL. CABLE RDAM6852-4 (565-1415) HAS MALE PIN STUCK IN HARNESS CONNECTOR. REQUIRES SEB AND HARNESS. PERFORMED OP TEST ON PTP PANEL. ALL SYS WORKING NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,147 hrs · 18,155 cycles

EXTERIOR EMERGENCY LEFT MESSAGE ON EMERGENCY LIGHT TEST. RELAMPED LT EXT OVERWING ILLUM LIGHTS, RE-RAN EMERGENCY LIGHT OPS TEST, OPS NORMAL.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 49,703 hrs · 17,974 cycles

GREEN HYD SYSTEM LOSS GREEN RESERVOIR. HYDRAULIC LEAK FOUND ABOVE NR 1 ENGINE. LEAK IS HYD PRESSURE LINE AT FIREWALL DISCONNECT. SWEDGE FITTING AT BULKHEAD IS LEAKING. FOUND PRESSURE LINE TO REV CONTROL MODULE LEAKING. ACCOMPLISHED PERMA SWEDGE REPAIR. LEAK CHECK OK.

Part: FILTER — DIRTY (E&E BAY) · airframe 48,851 hrs · 17,585 cycles

ELECTRICAL BURNING ODOR IN COCKPIT. RTFL. AFTER CONFER WITH CAPT, REMOVED CAPTS SIDE PFD & ND, CHECKED AREA FOR ELECT BURN ODOR & DAMAGE, NONE FOUND, EQUIPT COOLING NORMAL. REPLACED AND TESTED CRTS, CKS GOOD. FOUND AVIONICS COOLING FILTER HEAVILY SOILED. REPLACE AVIONICS COOL INLET FILTER. AEVC CFDS TESTS CKS PASSED. PRECAUTIONARY REPLACED BOTH THE LT & RT RECIRC FILTERS. CHECKED RECIRC SYSTEM, BOTH FANS OPERATE & NO ODORS PRESENT. ACP'D CABIN PRESS TO 5.3 DP FOR 57 MIN DURATION PRECAUTIONARY, NO ABNORMALITIES NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,850 hrs · 17,584 cycles

APPROX STA 1325 FRAME 74 + 5 INCHES, 10 INCHES TO THE RIGHT OF THE BELLY CENTER LINE IS DENTED. DRESSED OUT DENT, NDT INSP FOR FURTHER DAMAGE INSIDE AND OUTSIDE OF SKIN, NO CRACKS DETECTED. PAINT TO MATCH REWORK AREA.

Part: CONTROLLER — MALFUNCTIONED (CABIN) · airframe 48,374 hrs · 17,391 cycles

EMERGENCY LIGHT TEST FAILS 3 SERVICE TEST AT FLIGHT ATTENDANT PANEL. FAULT INDICATES "INT LOAD EMER L AFT" PRESENT. RESET EXIT LIGHT CONTROLLER. EMERGENCY LIGHTS TEST OKAY.

Part: ATTACH BRACKET — BROKEN (NR 3 FLAP TRACK) · airframe 48,843 hrs · 17,363 cycles

LEFT NR 3 FLAP TRACK AFT END STAY ASSY ATTACH BRACKET I/B LUG BROKEN.

Part: UNKNOWN — ODOR (UNKNOWN) · airframe 47,420 hrs · 17,070 cycles

F/A REPORTS VERY STRONG ODOR POSSIBLE CHEMICAL. STEAM CLEANED TWICE WITH CITRA SAFE, RINSED WITH WATER AND DRIED FWD OF BILGE. FINAL FIX?

Part: UNKNOWN — ODOR (CABIN) · airframe 47,420 hrs · 17,070 cycles

F/A REPORTS VERY STRONG ODOR POSSIBLE CHEMICAL.

Part: SWITCH — ILLUMINATED (OXYGEN SYSTEM) · airframe 46,588 hrs · 16,799 cycles

ECAM MSG O2 REG LOW PRESS WITH SWITCH ON. FOUND LOW OXYGEN PRESSURE SWITCH FAILED. REPLACED LOW OXYGEN LOW PRESSURE SWITCH.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 45,480 hrs · 16,366 cycles

NR 2 ENGINE COMPRESSOR STALL REPORTED. IFSD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,120 hrs · 16,234 cycles

EPSU FWD L MESSAGE, BATTERY PACK FAILS TEST. REPLACED BATTERY PACK. FUNCTIONS FINE FOR FURTHER FLIGHT.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 45,111 hrs · 16,229 cycles

EMERGENCY ESCAPE PATH LIGHTING AT SEAT 25C IS INOP. REPAIRED WIRE ON LIGHT CONNECTOR, OPS NORMAL.

Part: CYLINDER — READS LOW (CREW OXYGEN) · airframe 44,622 hrs · 16,057 cycles

CREW O2 CYLINDER NEEDS SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,837 hrs · 15,763 cycles

AT C-CHECK FOUND RIGHT BELLY FAIRING SUPPORT BRACKET Y127 UPPER ANGLE IS CRACKED AT FRAME 46 JUST BELOW KEELBEAM. REPLACED BRACKET Y127 AT C CHECK.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,837 hrs · 15,763 cycles

LEFT BELLY FAIRING SUPPORT BRACKET Y127 IS CRACKED AT FRAME 46 JUST BELOW KEEL BEAM. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.

Part: SWITCH — FAULTY (CABIN) · airframe 43,061 hrs · 15,486 cycles

EMERGENCY EXIT LIGHT SWITCH EXTREMELY DIFFICULT TO MOVE. [SUP 4-24-07] REPLACED SWITCH. OPS NORMAL AT THIS TIME.

Part: LIGHT — DAMAGED (CABIN) · airframe 42,948 hrs · 15,442 cycles

EMERGENCY FLOOR PATH LIGHT DAMAGED AT SEAT 23ABC. REPLACED LIGHT ASSY, EMERGENCY LIGHTS OP CHECK GOOD.

Part: SMOKE WARNING — ACTIVATED (COCKPIT) · airframe 42,430 hrs · 15,242 cycles

WHILE STARTING NR 1 ENGINE GOT SMOKE AFT CARGO SMOKE ECAM. DISCHARGED FWD AND AFT BOTTLES. MOMENTARILY GOT AN AFT SQUIB FAULT AND AFT BOTTLE DISCHARGE LIGHT NEVER ILLUMINATED. INSPECTED CARGO COMPARTMENTS AND DID NOT FIND ANY DEFECTS WITH SMOKE DETECTION SYSTEM OR EVIDENCE OF FIRE. REPLACED BOTH FWD AND AFT BOTTLES. SUSPECT THAT MOMENTARY SQUIB FAULT AND DISCHARGE LIGHT NOT ILLUMINATING WAS DUE TO A DELAY IN THE SQUIB FIRING. NO SPECIFIC PART/COMPONENT IS RESPONSIBLE FOR THIS PARTICULAR EVENT SINCE THE CAUSE OF THE INITIAL SMOKE INDICATION IS STILL UNKNOWN.

Part: GIRT BAR — FAULTY (R2 DOOR) · airframe 42,175 hrs · 15,158 cycles

DOOR 2R HARD TO ARM-DISARM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 41,130 hrs · 14,809 cycles

EMERGENCY LIGHT TEST FAILED. COM L - INT LOADS - BATTERY. RESET SYSTEM, AND SECURED CONNECTOR AT POWER UNIT.

Part: BATTERY — FAULTY (CABIN) · airframe 40,397 hrs · 14,530 cycles

WHILE PERFORMING EMERGENCY SYSTEM TEST FOR SLIDE CHANGE BY-BACK, MESSAGE (BATTERY AFT LEFT ATA 33-51-48) CAME INTO VIEW ON CIDS PANEL. REPLACED EPSU BATTERY 13WL AFT LEFT. OPS CHECKS NORMAL.

Part: DUCT — CHAFED (LT WING) · airframe 35,162 hrs · 12,595 cycles

LEFT WING BLEED LEAK MESSAGE AFTER TAKEOFF. A SMALL HOLE WAS FOUND IN A WING-ANTI ICE DUCT FLANGE. THE HOLE WAS CAUSED BY A CLAMP CHAFING THE DUCT FLANGE. THE DEFECTIVE DUCT WAS REPLACED AND A NEW CLAMP INSTALLED.

Part: PIPE · airframe 27,940 hrs · 9,883 cycles

FLIGHT DIVERTED DUE TO GREEN HYDRAULIC SYSTEM LOW. SUPPLEMENTAL DATA UPDATE FOUND LINE FROM HYD PRESSURE MODULE #1 ENG LEAKING AT FITTING. THE LINE WAS REPLACED. THE ENGINE PUMP CASE DRAIN AND HYDRAULIC CONTROL UNIT FILTERS WERE ALSO REPLACED PRECAUTIONARY.

Part: PUMP — INTERMITTENT (FUEL SYSTEM) · airframe 21,987 hrs · 7,605 cycles

WING BOOST PUMP FAILURE. *S/D* THE NR 2 FUEL BOOST PUMP WAS GROUND CHECKED WITH NO FAULTS FOUND. THE PUMP HAS NO HISTORY OF BEING INOPERATIVE AND HAS FLOWN 2 FLIGHTS SINCE IT WAS CHECKED AS NORMAL.

Part: SKIN — DAMAGED (TAIL) · airframe 19,024 hrs · 6,623 cycles

TAIL OF AIRCRAFT STRUCK UPON FLARE AND LANDING AT SNA. SIX FOOT LONG SCRAPE ON BOTTOM OF AIRCRAFT FUSELAGE WITH NUMEROUS BREAKS IN SKIN LOCATED IN AREA AFT OF DRAIN MAST. *S/D* EXCESSIVE FLARE DURING LANDING. ISSUED EVA MOC1-8111 TO INSTALL TEMPORARY REPAIR PATCH FOR FERRY FLIGHT TO REPAIR STATION AS APPROVED PER AIRBUS TELEX 942-009205/011/2000. FINAL REPAIR WAS ACCOMPLISHED PER AIRBUS A320 STRUCTURAL REPAIR MANUAL (SRM) 53-00-11 FIG 207 & 218.

Part: SWITCH — FAILED (GREEN HYD SYST)

GREEN HYDRAULIC SYSTEM LOW-PRESSURE/LOW VOLUME. LANDED AMBER ALERT. *S/D* FOUND HYDRAULIC LEAK AT GREEN HYDRAULIC PRESSURE SWITCH ON NR 1 ENGINE. LEAK COMING FROM PACKING. REPLACED PRESSURE SWITCH, OPS CHECK GOOD.

Part: FIRE TEST — FAILED (CARGO COMPT)

WHEN CREW DOES FIRE TEST OF BOTH CARGO PITS, SYSTEM IS NOT TESTING PROPERLY, RECEIVES 'LAV AND CARGO SMOKE FAULT'. *S/D* MECHANIC CHECKED PINS ON SMOKE DETECTOR CONTROL UNIT, CHECKED OK. RECYCLED POWER, OP CHECKS OK.

Part: CONTROL UNIT — MALFUNCTIONED (RT MLG)

RIGHT LANDING GEAR DID NOT DISPLAY GREEN ON GEAR EXTENSION. CYCLED GEAR AND RIGHT GEAR DOOR ECAM DISPLAYED MOMENTARLY FOLLOWED WITH NORMAL 3 GREENS. *S/D* REPLACED LGCIU AND OPERATIONALLY CHECKED NORMAL.