N414UA

Part: NONE — INOPERATIVE (TCAS COMPUTER) · airframe 87,478 hrs · 35,495 cycles

CHRONIC TCAS INOP. PLEASE FOLLOW TSM 34-43-00-810-832A FOR TROUBLESHOOTING. NEED TO NOTE AHM REPORTS CFDIU NO COMMUNICATING WITH PROCESSOR SO SUSPECT BAD TCAS COMPUTER. IF FAULT CANNOT BE DUPLICATED REPLACE COMPUTER. THANKS LARRY THOMSON DENMM CARRIED BY ELB PERFORMED TSM 34-43-00-810-832A, FAULT NO DUPLICATED. REMOVED/REPLACED TCAS COMPUTER PER AMM 34-43-34, PERFORMED BITE AND FUCTIONAL TEST WITH TCAS RAMP TEST SET TR220. TEST OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1866956 SN OFF 8787 COMPUTER, TRAFF OFF 31-3445-9-0001 8787 ON 31-3445-9-0001 7106

Part: FRAME — CORRODED (FRAME 67L) · airframe 87,346 hrs · 35,424 cycles

COROSSION FOUND ON FRAME 67L CORRECTION , FRAME 70 ,SIX OCLOCK POSITION CORRECT LOCATION OF CORROSION IS FRAME 67- STRINGER 44 PER SRM DAMAGE IS AT STR 44 FR 67 53-41-12-75-A FIGURE C REMOVED 60 FASTNERS COMON TO F,S 67L IN THE 6 OCLOCK POSITION AND L-ANGLE UPDATE TO CAPTURE SDR AND MAJOR REPAIR.

Part: STRINGER — CORRODED (FRAME 67-STRINGE) · airframe 87,346 hrs · 35,424 cycles

CORROSION FOUND ON STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70. CORROSION LOCATION IS FRAME 67-STRINGER 27 PER SRM ENGINEERING UPDATE, IT IS STRG 26R 53-41-13-50-A. REMOVED STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70.AND ASSOCIATED FASTNER FWD OF F.S 70 STR 26R PER SRM 51-42-11/001 UPDATE TO CAPTURE SDR AND MAJOR REPAIR. LOCATED AND DRILLED SPLICE ANGLE D5348004621301 AS PER SRM REMOVED STR 26R PN# D5348004720200 AT F.S 67 AND FWD TO F.S 64 51-44-11/001 PER SRM 51-42-11. POSITION AND DRILLED FULL SIZE NEW STR 26R PN# D5348004720200 / PER SRM 51-42-11.

Part: FRAME — CORRODED (STR 26R) · airframe 87,346 hrs · 35,424 cycles

FOUND CORROSION AT STR 26R END FITTING AT FRAME FR70. SEE ATTACHED PICTURES. PICS ADDED DAMAGE IS 9 INCHES LONG PROTEUDIMG FORWARD FROM FRAME 70 ON CORROSION LOCATION IS ON FRAME 67-STRINGER 27 SRM ENGINEERING UPDATE, IT IS STR 26R STRINGER 26 R/H 53-41-13-50-A. FIGURE B UPDATE TO CAPTURE SDR AND MAJOR REPAIR. REMOVED FRAME SECTION F.S 67, 25 INCH LONG BETWEEN STR 24R THRU 30R , ALSO REMOVED FRAME SPLICE F.S 67 AT STR 30R. PER SRM 51-42-11. REMOVED RII, NOT A MAJOR REPAIR PREPARED AND INSTALLED 25INCH LONG FRAME SECTION AND ALSO FRAME SPLICE STR 24R-STR 30R SPLICE STR 30R, INSTALLED 75% FASTNERS COMMON TO THE FRAME AND SPLICE. AND SKIN / PER SRM 51-42-11.

Part: NONE — NONE (FR 56-67/STR 36R) · airframe 87,346 hrs · 35,424 cycles

*THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 08/22/2022* AFT PIT BY LAV TANK FOUND TO HAVE OLD WASTE. LAV SPILL CLEAN UP PERFORMED BTW FRMS 56-67, STR 36R-36L IAW ECRA2011-01000, CORRECTIVE MEASURES B. IN-DEPTH CLEANUP, ALL STEPS UPTO AND INCLUDING (1) THRU (13); COMPLIED WITH ALL STEPS IN ECRA 2011-01000 STEP 2 B

Part: NONE — MISSING (RH WING) · airframe 86,609 hrs · 35,078 cycles

PDA 3 FUELER REPORTS FUEL CAP LANYARD IS MISSNG WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSNG PER CDL DISPATCH DESK: 25 NAME: JG DATE: 17-MAY-22- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V081328 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. APPLY CDL 28A MAC RELATED WORK ORDER 000000003044419 AND PRTR WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSNG PER CDL REPLACED CABLE ASSY REF IPC 28-25-41-02B ITEM #90.

Part: CONDENSER — CRACKED (LH PACK) · airframe 86,409 hrs · 34,982 cycles

FLT DECK DIRTY SOCK -LIKE PACK ISSUE REMOVED LEFT HAND PACK ACCESS PANEL TO FOM FOUND LEFT PACK CONDENSER CRACKED AT WELD SEAM. REMOVED AND REPLACED LFT PACK CONDENSER IAW AMM 21-15-12. OPS CHECKS NORMAL ROTABLE PARTS CHANGE WAS INDICATED - TT # 1096657 SN OFF 1274 CONDENSER, AIR OFF 31-2152-9-9002 1274 ON 31-2152-9-9002 4053

Part: STRINGER — CORRODED (FRAME 59) · airframe 81,707 hrs · 32,827 cycles

AFT CARGO COMP LOWER BILGE AREA HAS CORRODED STRINGER 43L AT FR 59 ON HAECO LCQ REF 9298369 SPEC A3NB-05-3-6023. REMOVED DAMAGED SECTION OF STRINGER 43L FROM FR58+16" TO FR59+13 " AND INSTALLED SPLICE REPAIR IAW SRM 53-00-13-001. SUPPLEMENTAL INSP REQUIRED IAW SRI 53-00-13-205-001 BEGINNING AT 60000 FLIGHT CYCLES OR 120000 FLIGHT HOURS FROM REPAIR EMBODIMENT WITH SUBSEQUENT INSP INTERVALS AND METHOD TBD. OKAY TO DIP REPAIR ON STRINGER 43L PER SRM 53-00-13-300-001. REF SRI 53-00-13-205-001, MUST ACCOMPLISH REINSPECTION OF REPAIR WITHIN 60,000 FLIGHT CYCLES-120,000 FLIGHT HOURS FROM REPAIR EMBODIMENT. AT TIME OF FIRST INSPECTION, REVIEW SRI AND APPLY APPLICABLE RECHECK LIMITS. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED

Part: PROXIMITY SWITCH — FAULT MESSAGE (CARGO DOOR) · airframe 81,598 hrs · 32,779 cycles

AIR RETURN CREW REPORT ECAM MSG AFT CARGO DOOR ON AT 4000 FT FWD TO MEL VERIFIED AFT CARGO DOOR LOCKED NOC DESK: 320 NAME: SH DATE: 28-OCT-19- APPROVED MEL 5270D C/W DDP DOOR CLOSED PERFORMED LGCIU1 BITE FOUND AFT CARGO DOOR PROX SWITCH 34WV FAULT REF AMM 32-69-00-740-001-A. REPLACED AFT CARGO DOOR PROX SWITCH 34WV REF AMM 52-71-12 OPS CHECK GOOD

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 78,486 hrs · 31,410 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST, GOT AFT L EPSU FAULT MESSAGE REMOVED AND REPLACED AFT L EPSU AND BATTERY PACK, REF AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. ADD EMP:U098939 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248220 SN OFF 8117 IPC REFERENCE # 33-51-38-01 POWER SUPPLY, C OFF 31-3350-9-9001 8117 ON 31-3350-9-9001 1039 ACP''D IDT INSP REF GMM 09-10-05 REFERENCE UPDATE FOR WORK PERFORMED

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 78,357 hrs · 31,346 cycles

BOTH TRANSFER VALVES STUCK IN CLOSED POSITION REPORTED BY CREW. TOMC BROADSTONE. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN VERIFY TRANSFER VALVES OPEN REF MEL 2815R. CONTACT TOMC 847-700- 9980. ACCOMPLISHED CHECK OF REFUEL POWER SWITCH UPON LANDING, SWITCH WAS IN THE NORMAL POSITION. AFTER REFUELING ACFT, ACP'D THE MAINTENANCE PROCEDURE OF MEL 2815B AND DEACTIVATED THE INTERCELL TRANSFER VALVES OPEN. VERIFIED VALVES OPEN ON ECAM PAGE. MAC RELATED WORK ORDER 000000001592907 AND PRTR MAC METER INITIATED FOR WITH VENDOR ACCOMPLISHED CHECK OF REFUEL POWER SWITCH UPON LANDING, SWITCH WAS IN THE NORMAL POSITION. AFTER REFUELING ACFT, ACP'D THE MAINTENANCE PROCEDURE OF MEL 2815B AND DEACTIVATED THE INTERCEL TRANSFER VALVES OPEN. VERIFIED VALVES OPEN ON ECAM PAGE.

Part: COVER — LOOSE (FLOOR) · airframe 75,664 hrs · 30,112 cycles

L OVERWING EMER EXIT DISPLAYED-SLIDE IN WHITE. FOUND DOOR TRIM COVER PLATE CAME OFF. REINSTALLED AND INDICATION NOW NORMAL. OK FOR SERVICE.

Part: BRACKET — BENT (EMERGENCY EXIT) · airframe 75,608 hrs · 30,083 cycles

LEFT FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR LEFT FWD EMERGENCY EXIT DISPLAYED ON ECAM, NO ABNORMAL CABIN V/SNOTED STRAIGHTENED BRACKET AND ADJUSTED COVER SWITCH

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 75,587 hrs · 30,074 cycles

EMERGENCY EXIT LENS AT SEAT 20A FELL OFF. REPLACED THE LENS. OK AT THIS TIME

Part: COVER — LOOSE (DOOR HANDLE) · airframe 75,572 hrs · 30,068 cycles

LEFT DOOR FWD EMERGENCY EXIT ECAM ILLUMINATED DURING LANDING. F/A SAID HANDLE COVER POPPED OFF. REINSTALLED THE DOOR HANDLE COVER. COVER SECURE. DOOR INDICATION OUT IN THE COCKPIT.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 75,529 hrs · 30,050 cycles

OVERWING EMERGENCY LIGHT POWER SUPPLY 11WL FAILED AN OPS CHECK. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY 11WL IAW AMM 33-51-38-000-001-A, AND 33-51-38-400-001-A. PERFORMED AN OPS CHECK, NO DEFECTS NOTED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 75,529 hrs · 30,050 cycles

OVERWING EMERGENCY LIGHT POWER SUPPLY 12WL FAILED AN OPS CHECK. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-38-000-001-A, AND 33-51-38-400-001-A, NO DEFECTS NOTED.

Part: SKIN — CORRODED (RT WING) · airframe 75,529 hrs · 30,050 cycles

RIGHT WING UPPER SURFACE TRAILING EDGE HAS CORROSION. BLENDED THE AREAS OF CORROSION, ACCOMPLISHED ROTO PROBE, HFEC, AND UT. NO CRACKS OR CORROSION FOUND. FOUND TO BE WITHIN LIMITS. FLAP PEEN REPAIRED.

Part: STRUT — LOW PRESSURE (NLG) · airframe 75,508 hrs · 30,041 cycles

MLG SHOCK ABSORBER FAULT, MLG NOT UPLOCKED, MLG DOORS NOT CLOSED, ECAM WARNINGS WITH CORRELATED FAILURE MESSAGES NLG SHOCK ABSORBER 2526GM AND NLG EXT PROXIMITY SENSOR 25GA TGT POS. EMERGENCY DECLARED. CHECKED NLG SHOCK ABSORBER CHARGE PRESSURE IAW AMM 12-14-32-614-004. FOUND STRUT LOW, SERVICED THE STRUT IAW AMM AND BITE CHECK OF LGCIU TESTS GOOD. OK TO DIP RECHECK IAW AMM 12-14-32-614-004, CHECKED THE NLG SHOCK PRESSURE BETWEEN 4 AND 7 DAYS AFTER THE FIRST SUBSEQUENT FLIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,508 hrs · 29,128 cycles

EMERGENCY EXIT LIGHT BATTERY POSITION L FWD 10WL FAILED CAPACITY TEST PER A CHECK CARD. REPLACED FWD LEFT EMERGENCY EXIT LIGHT BATTERY REF AMM 33-51-00 -710-003. OPS TEST PASSED.

Part: WARNING LIGHT — FALSE ACTIVATION (FWD CARGO DOOR) · airframe 73,204 hrs · 28,984 cycles

ABORT TAKEOFF AT 90 KNOTS FOR CARGO DOOR LIGHT COMING ON. INSPECTED FWD CARGO DOOR ON ARRIVAL AT GATE. FOUND FWD CARGO DOOR HANDLE NOT PROPERLY SECURED CAUSING DOOR HANDLE TO OPEN DURING TAKEOFF. FWD CARGO DOOR HANDLE AND DOOR OPERATION IAW AMM 52-31-00-0710-001-A.. CARGO DOOR OPERATES NORMAL. ACFT OK FOR SERVICE

Part: DOOR FRAME — CRACKED (FRM 68) · airframe 68,328 hrs · 26,810 cycles

L2 DOOR CUTOUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION AT 6 O'CLOCK AND 12 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5.E. FIG 204.

Part: TAIL CONE — CRACKED (NR 1 ENGINE) · airframe 72,932 hrs · 28,853 cycles

WHILE WORKING FCD 7811-01330 FOUND NR 1 ENG TAIL CONE WITH WELDS AND CRACKS AT 11:00 AND 5:00 POSITION. REPLACED TAIL CONE PER MM 78-30-00.

Part: TAIL CONE — CRACKED (NR 2 ENGINE) · airframe 72,932 hrs · 28,853 cycles

WHILE ACCOMPLISHING FCD 7811-01330, FOUND TWO .5 CRACKS IN THE NR 2 ENGINE TAIL CONE. REPLACED TAIL CONE PER MM 78-11-12-000-010-A 13.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,918 hrs · 27,929 cycles

LAVATORY SERVICE PANEL, INTERIOR DOUBLER HAS CORROSION. EVALUATED CORROSION, FOUND TO BE OUT OF LIMITS. R & R INTERIOR DOUBLER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,328 hrs · 26,810 cycles

L2 DOOR CUT OUT FRAME 66 LOWER STOP LOWER INBD HOLE HAS A CRACK. ACCOMPLISHED REPAIR IAW REO-L18732 & ECRA 5340-01644. HOLE WAS REAMED & FREEZE PLUG INSTALLED. INTERIM APPROVED IAW RDAS 80025005-003-2015 ISSUE A FOR 50C. NEW RDAS PROVIDING PERM APPROVAL MUST BE RECEIVED BEFORE 26860C. IF NEW RDAS NOT RECEIVED ACFT WILL BECOME UN AIRWORTHY.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,328 hrs · 26,810 cycles

R2 DOOR CUT OUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION IN FRAME AT 6 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,328 hrs · 26,810 cycles

L2 DOOR CUT OUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION IN FRAME AT 6 O'CLOCK & 12 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 68,328 hrs · 26,810 cycles

R2 DOOR CUT OUT FRAME 68 SECOND FROM LOWER STOP, OTBD UPPER HOLE HAS AN ELONGATION INDICATION OUT OF LIMITS IN FRAME. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 66,023 hrs · 25,864 cycles

EMERGENCY LIGHTS TEST FAULTS. RESEATED CONNECTORS ON 30 0RH, CIDS TEST & EMERGENCY LIGHTS TESTED OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,021 hrs · 25,863 cycles

AFT FUSELAGE BELLY SKIN DENTED APPROX 8 INCHES FWD OF APU INLET. EVALUATED THE ARCHIVED ITEM & FOUND A PERMANENT DOUBLER REPAIR INSTALLED IAW SRM 53- 00-11 PG 567-568 FIG 238. THIS REPAIR REFERS TO SRI INSPECTION IAW SRI 53-00-11-2-017-00 PARA 3L TABLE 224. FIRST INSPECTION 60000 FC & 75000 FH. QC LC-80 CURRENT PTC IS 25863 & CURRENT PTT IS 66021. CF ITEM CREATED TO ACCOMPLISH SRI INSPECTIONS.

Part: STRIKER — FAULTY (COCKPIT DOOR) · airframe 65,043 hrs · 25,482 cycles

FLT DECK DOOR MID STRIKE FAULT, OK TO DEFER IAW MEL 5250P, MID STRIKE DEACTIVATED IAW MEL. REPLACED MID STRIKE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 65,043 hrs · 25,482 cycles

LT WINDOW DISPLAYED ON UPPER ECAM SCREEN. WHC TEST FAULTING LT SLIDING WINDOW SENSOR. CB RESET NO HELP. WHC R & R 12-10-13. WINDOW SENSOR FAULTING LT SLIDING WINDOW ASSEMBLY PCN 110- 3203, IAW IPC 56-12-11-01B ITEM NR 50.

Part: RUB STRIP — DAMAGED (NR 2 ENGINE) · airframe 65,008 hrs · 25,463 cycles

ENG 2 FAN BLADE RUB STRIP IS DAMAGED AT 5 O'CLOCK. REPAIRED DAMAGED AREA IAW MT72-017 REV E. DAMAGED LOCATED AT 7 - 8 O'CLOCK POSITION LOOKING FWD.

Part: APU — SHUTDOWN (APU BAY) · airframe 65,008 hrs · 25,463 cycles

FUEL APU LP VLV FAULT ECAM ON LANDING WHILE STARTING APU. APU AUTO SHUTDOWN.

Part: ACOUSTIC LINER — DETERIORATED (NR 2 ENGINE) · airframe 64,719 hrs · 25,355 cycles

ACOUSTIC PANEL REPAIR ENG 2 HAS DETERIORATION. PLACED NR 2 ENG ATTRITION LINER AT 8 O'CLOCK POSITION ON CF873, NO LOOSE MATERIAL & GRC LAYER NOT PUNCTURED, IAW MT 72-017.

Part: ACOUSTIC LINER — DAMAGED (NR 2 ENGINE) · airframe 64,729 hrs · 25,358 cycles

ACOUSTIC LINER NEEDS TO BE REEXAMINED FOR INTEGRITY. MORE DAMAGE NOTED AT 1 O'CLOCK POSITION. PREVIOUS REPAIRS AT 2:00 POSITION & 7:00 POSITION. NR 2 ENG INLET ATTRITION GRC LAYER REQUIRE PERM REPAIR IAW A320 MT 72-017. DAMAGE LESS THAN 20 PERCENT, PLACED ON CF0874.

Part: LINER — MISSING (NR 2 ENGINE) · airframe 64,424 hrs · 25,252 cycles

NR 2 ENG INTAKE INSULATION AT 2 O'CLOCK POSITION HAS COME OFF. ACTUAL IS ATTRITION LINER MISSING 1X1 SECTION AT THE 11 O'CLOCK POSITION. MUST BE REPAIRED IAW MT 72-017 WITHIN 20 CYCLES. REPAIRED ATTRITION LINER IAW MT 72-017.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 64,295 hrs · 25,207 cycles

FIRST OFFICER`S ND IS TOO DIM, CANNOT SEE SYMBOLS IN BRIGHT SUNLIGHT. R & R FIRST OFFICER`S ND. OPERATIONS CHECKED GOOD.

Part: HANDLE — UNLATCHED (CARGO DOOR) · airframe 64,139 hrs · 25,151 cycles

FWD CARGO DISPLAYED ON UPPER ECAM SCREEN. FWD CARGO OPEN INDICATION ECAM. PRESS DIFF-ALL INDICATIONS NORMAL. FOUND DOOR HANDLE HANGING IN UNLATCHED POSITION DOWN IN AIRSTREAM & VENT DOOR SLIGHTLY AJAR. ALL DOOR LOCKED INDICATORS SHOWING LOCKED. INSPECTED DOOR & HANDLE LATCHING MECHANISM ALL APPEAR OK UNABLE TO FALSE LATCH HANDLE WILL RECHECK AT DEPARTURE.

Part: THRUST REVERSER — DELAMINATED (LT ENGINE) · airframe 63,963 hrs · 25,078 cycles

LT ENGINE RT THRUST REV HALF HAS APPROXIMATELY 35 SQ IN OF DELAMINATION ON ACOUSTIC SCREEN AT 3-OCLOCK. CLEANED & APPLIED SPEED TAPE. REF MT78-010.

Part: RUB STRIP — LOOSE (L2 DOOR) · airframe 63,873 hrs · 25,046 cycles

L2 DOOR MAKES RATTLING ODD NOISES. FOUND MED 2L DOOR COVER PLATE RUB STRIPS LOOSE. REMOVED RUB STRIPS FROM DOOR FRAME AREA, DOOR FUNCTIONS NORMAL FLAP IS FLUSH WITH AIRFRAME. ACFT OK FOR SERVICE.

Part: LINER — DAMAGED (ENGINE) · airframe 63,802 hrs · 25,022 cycles

SMALL PIECES OF ATTRITION LINER MISSING AT 4, 5, 10, 11 O'CLOCK POSITIONS, LOOKING FROM REAR OF ENGINE. MISSING LINER LESS THAN 20 PERCENT OF LINER SEGMENTS.

Part: SOLENOID — FAULTED (EGT) · airframe 63,747 hrs · 24,997 cycles

NR 1 ENG EGT OVERTEMP, RTFL AT 685 DEGREES DURING TAKEOFF. ENG EGT MAX READING 644 DEGREES RECORDED, INSPECTED AND LUBED ALL NORMAL, PERFORMED BLEED SOLENOID CHECK IAW JIC 4-2275, FOUND 10 STAGE SOLENOID FAULT. REPLACED SOLENOID. PERFORMED HIGH POWER ASSURANCE TEST, INDICATIONS NORMAL.

Part: LATCH — BROKEN (SMOKE HOOD) · airframe 63,611 hrs · 24,942 cycles

COCKPIT SMOKE HOOD DOOR LATCH AND LID BROKEN. COMPLIED WITH ECRA 251401 109 MUST REPAIR BY 2 FLIGHT CYCLE PCN (110-1915).

Part: LINER — DAMAGED (NR 2 NACELLE) · airframe 63,280 hrs · 24,816 cycles

NR 2 ENGINE HAS DAMAGE TO ACCOUSTICAL MATERIAL AT THE 5:30 POSITION NEAR NACELLE LIP.

Part: DUCT — CRACKED (NR 1 ENGINE) · airframe 62,918 hrs · 24,673 cycles

NR 1 ENGINE PRECOOLER 'Y' DUCT IS CRACKED. REPLACED PRECOOLER 'Y' DUCT.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 62,790 hrs · 24,620 cycles

CREW REPORTS RIGHT WATER SUMP DRAIN HAS FUEL DRIP. SAMC TEXT: OPERATE SUMP DRAIN. REPLACED SUMP OUTER VALVE PER AMM. NO LEAKS.

Part: STRUCTURE — DAMAGED (ENGINE) · airframe 62,665 hrs · 24,564 cycles

PUDDY ON HONEYCOMB RIGHT SIDE HAS PIECE MISSING. DAMAGE IS AT 8 O'CLOCK POS O F NR 2 ENG FWD LOOKING AFT MEASURES 2.72 INCH BY 1 INCH. REPAIRED ATTRITION LINER IAW MT 72-017.

Part: UNKNOWN — ODOR (AFT GALLEY) · airframe 62,329 hrs · 24,424 cycles

FLIGHT ATTENDANT REPORT, BURNING ODOR IN AFT GALLEY BY COFFEEMAKERS. REMOVED BOTH COFFEEMAKERS TO LOOK FOR ANY DISCREPANCIES BEHIND COFFEEMAKERS, NONE NOTED. REPLACED BOTH COFFEEMAKERS.

Part: LINER — MISSING (NR 2 ENGINE) · airframe 62,315 hrs · 24,418 cycles

NR 2 ENGINE, LOOKING FORWARD AT THE 8 O`CLOCK FAN POSITION IS A MISSING SECTION OF ATTRITION LINING. THIS MEASURED SECTION MISSING IS 1.5 X 2 IN. REPAIRED AND APPLIED ADHESIVE IAW MT72-017.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 62,304 hrs · 24,412 cycles

EMERGENCY LIGHTS BATTERY FAULTING ON TEST AND LIGHTS NOT WORKING. BATTERY UNIT ALSO FAULTING. REPLACED BATTERY, TESTED AND CHECKED OK.

Part: FITTING — LOOSE (HYD SYSTEM) · airframe 62,146 hrs · 24,352 cycles

ON WALKAROUND, FOUND FLUID ON AIRPLANE AT NOSEGEAR AND DRIPS ON GROUND AROUND NOSEGEAR. CLEANED NOSE WHEEL WELL AREA. WRENCHED CHECKED LINES. PRESSURE LINE FITTING TO NLG ACTUATOR LOOSE. TIGHTENED FITTING.

Part: COMPUTER — FAULTED (SLAT SYSTEM) · airframe 62,137 hrs · 24,346 cycles

SLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. PFR FAULTED COMMAND SENSOR UNIT. REPLACED CSU AND NR 2 SFCC. ALL TESTED OK CAT 3 TEST ACCOMPLISHED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,827 hrs · 23,774 cycles

INTERNAL DOUBLER AT AFT WASTE DRAIN PANEL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: FABRICATED DOUBLER PER RFTS 60004 ON NR F3376L. REMOVED AND REPLACED DOUBLER PER SRM 51-42-11 ON NR F3268L. INSTALLED LAV SVC PAN-DOOR PER SRM 51-42-11 AND DWG 53480016, PART MARKED DOUBLER PER GNMM 1-0-1-07 AND 1-0-1-023, FILLET SEALED PER SRM 51-24-00 ON NR F3543L.

Part: BATTERY — FAULTY (NR 2) · airframe 60,825 hrs · 23,773 cycles

BCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC REPLACED CONTACTOR AND NR 2 BATTERY PER MM, OPS CHECKED NORMAL

Part: STARTER — SPARKS (NR 1 ENGINE) · airframe 60,393 hrs · 23,599 cycles

NR 1 ENGINE START FAULT. RAMP SAW SPARKS FROM BOTTOM OF ENGINE AND FLAMES OUT TAILPIPE. REPLACED STARTER PER AMM. NO OTHER DAMAGE NOTED. SERVICED STARTER PER AMM. RAN ENGINE AND OPS CHECKED NORMAL.

Part: MODULE — LEAKING (HYDRAULIC SYS) · airframe 60,285 hrs · 23,550 cycles

GREEN HYD LOW, DOWN 2.25 GALLONS FOUND 1146GM GROUND LEAKAGE MEASUREMENT SEL VAL G LEAKING WHEEL WELL. REPLACED SEAL ITEM 100 REF IPC 29-19-41 NO HELP, THE MODULE ITSELF IS LEAKING FROM A PORT ON THE I/B SIDE THAT IS NOT SHOWN IN THE IPC, IT NEEDS A NEW MODULE P/N 644-1005, ON AOG R3548. RPL'D GREEN SYSTEM HYD MANIFOLD (1146GM) PER MM, OPS CK GOOD

Part: DIRECTOR — MALFUNCTIONED (CIDS) · airframe 59,118 hrs · 23,037 cycles

CIDS MAINT TEXT: CREW REPORTED EVAC WARNING SOUNDING AND COULD NOT RESET. REPLACED CIDS DIRECTORS NR 1 AND NR 2. BOTH CIDS DIRECTORS PASSED. CONFERRED WITH TOMC.

Part: COMPUTER — FAULTY (SPOILER SYS) · airframe 58,566 hrs · 22,820 cycles

GROUND SPOILER FAULT, FLT DIVERTED. CFDS SHOWS "GND SPLR 3X4 FAULT". NO OTHER FLT CONTROL PAGE FAULTS NOTED. SAMC TEXT: CONTACT TOMC BEFORE SIGN OFF. OPBLM - CREW REPORTS SPOILERS DID NOT WORK ON LANDING: BEFORE NEXT FLT PERFORM TSM 27-60-00-810-806, REPLACED SEC 1 PER MM. ACCOMP EFCS GRD SCAN AND SEC TEST PER MM, ALL TESTS GOOD.

Part: BATTERY — DISCHARGED (NR 1) · airframe 58,466 hrs · 22,771 cycles

BATTERY 1 LOW VOLTAGE AND FAILS PREFLIGHT AMPERAGE CHECK. REPLACED NR 1 BATTERY & NR 1 BATTERY CHARGE LIMITER.

Part: SERVO VALVE — MALFUNCTIONED (NLG STEERING) · airframe 57,547 hrs · 22,399 cycles

NW STRNG FAULT DISPLAYED-NOSE WHEEL STEERING INOP. ATTEMPTED RESET OF NWS SWITCH AND BOTH BSCU 1&2, NO HELP. MAINT TEXT: BOTH BSCU 1 & 2 FAULT STEERING ELECTRO HYDRAULIC MODULE 6GC. REPLACED NOSE WHEEL STEERING SERVO VALVE.

Part: COMPUTER — FAULTY (NR 1) · airframe 57,200 hrs · 22,264 cycles

SIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL CREW COMMENTS: AT SHUTDOWN. REPLACED ELAC NR 1. ACCOMPLISHED SFCS GROUND SCAN REF MM AND ACCOMPLISHED LAND CAT III. ALL TESTS PASS.

Part: UNKNOWN — DAMAGED · airframe 57,189 hrs · 22,258 cycles

A-C SUSTAINED HAIL STORM AT GATE. NEED TO PERFORM HAIL DAMAGE INSP.

Part: MASTER CYLINDER — FAULTY (BRAKE SYS) · airframe 57,164 hrs · 22,246 cycles

CAPT LEFT TOE BRAKE SLOW TO RETURN TO NORMAL POSITION AFTER BRAKE APPLICATION. REPLACED LT BRAKE CONTROL MASTER CYLINDER, OPS CHECK NORMAL.

Part: RAM AIR TURB — FAULTY (HYD SYSTEM) · airframe 56,243 hrs · 21,862 cycles

RAT FAILS TEST. GREEN LIGHT WON'T COME ON AND STAY ON. FIRST TEST FAILED. REPLACED HYD PUMP ASSY RAT HYD PUMP ASSY OP CHECKS GOOD, NO LEAKS.

Part: STRINGER — DENTED (FUSELAGE) · airframe 55,686 hrs · 21,635 cycles

FOUND STRINGER 41 DENTED BETWEEN FRAME 61 AND 62 AT SKIN LAP. NO CRACK NOTED. ACCOMPLISHED DAMAGE AREA INSPECTION IAW SRM. NO CRACK NOTED. FOUND STR 40 DAMAGE BETWEEN FRAME 61 AND 62. REMOVED DAMAGE. NO DAMAGE TO STRINGERS FOUND AFTER SKIN REMOVAL. HFEC NOT ACCOMPLISHED YET. "REMOVED DAMAGE" ABOVE REFERS TO DAMAGED SKIN ONLY BEING REMOVED. NO STRINGERS WERE REMOVED. FILLER COMPLETE WORKING ON DOUBLER THEN SHOOT RIVETS. COMPLETED REPAIR REF EVA 80508.

Part: STRINGER — CORRODED (S43L) · airframe 55,534 hrs · 21,572 cycles

STRINGER 43L AT FRAME 54-58 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED STRINGER SECTION. REPLACED STRINGER SECTION BETWEEN FR 54-58 AND FABRICATED AND INSTALLED SPLICE REPAIRS.

Part: STRINGER — CORRODED (S42L) · airframe 55,534 hrs · 21,572 cycles

STRINGER 42L BETWEEN FR 58 AND 59 IS CORRODED. REMOVED CORRODED STRINGER SECTION. REPLACED STRINGER SECTION BETWEEN FR 57-60 AND FABRICATED AND INSTALLED SPLICE REPAIRS.

Part: STRINGER — CORRODED (S40L) · airframe 55,534 hrs · 21,572 cycles

STRINGER 40L AT FRAME 63 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED STRINGER SECTION. REPLACED STRINGER SECTION BETWEEN FR 62-64 AND FABRICATED AND INSTALLED SPLICE REPAIRS. PER SRM THIS REPAIR IS VALID UNTIL 31 DEC 2013.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,534 hrs · 21,572 cycles

CORROSION AT STRINGER 31R AT FRAME 65 NEAR OUTFLOW VALVE. MAJOR REPAIR. REPLACED STRINGER SECTION.

Part: FLOORBOARD — DELAMINATED (ROW 18) · airframe 54,938 hrs · 21,301 cycles

AT ROW 18 THE CABIN FLOOR IS SPONGY AND HAS A DIP IN IT. REMOVED FLOORBOARD 251FF ROW 16 THRU 19. BOARD REPORTED SPONGY AT ROW 18. FOUND FLOORBOARD DELAMINATED. REPLACED FLOORBOARD. FOUND FLOORBOARD SUPPORT BRACKET BROKEN ROW 18. REPLACED SUPPORT BRACKET.

Part: LATCH — BROKEN (ESCAPE ROPE) · airframe 54,215 hrs · 20,982 cycles

LATCH FOR RIGHT OVERWING ESCAPE ROPE IS BROKEN. REPLACED LATCH.

Part: RIB — DELAMINATED (TE FLAP) · airframe 53,865 hrs · 20,841 cycles

CLOSURE RIB 1 ON LT OUTBOARD FLAP IS DAMAGED. THE DAMAGE IS AN AREA OF DELAMINATION OF APPROXIMATELY 1.5 INCH IN DIAMETER. MAJOR REPAIR ACP'D. DAMAGED AREA WAS CUTOUT AND REPAIRED PER SRM AND UA-EVA-73902 REV B. REPAIR AND RII INSP WAS ACP'D ON SMB N-R K5016D.

Part: STRUCTURE — DENTED (NR 2 SLAT) · airframe 53,865 hrs · 20,841 cycles

DENT ON LEADING EDGE NR 2 SLAT APPROX 1 FT OUT FROM INBOARD EDGE MEASURES 6-32 DEEP. TEMPORARY REPAIR INSTALLED. MUST INSTALL STRUCTURAL INSERT REPAIR WITHIN 4500 FC, OR 6000 FH OR 20 MONTHS OR CHECK WHICHEVER OCCURS FIRST. REPLACED SLAT ON WUP K4341F.

Part: FIRE DETECTOR — FAULTY · airframe 53,608 hrs · 20,732 cycles

FIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN. -ENG 2. FIRE LOOP B CAME ON AFTER FIRST POWER REDUCTION REPEAT. CHRONIC PROBLEM AND SUSPECT LOOP ISSUE, WORK WITH SW1746. PREVIOUS HAND-OVER-HAND CK OF FAN LOOP INDICATED POSSIBLE HIGH RES AT HYD FILTER AREA. REPLACED 450VT2 PER TSM AND WDM. ACP CALJIC SW1746. TESTED OKAY.

Part: FIRE LOOP — FALSE INDICATION (NR 2 NACELLE) · airframe 53,225 hrs · 20,568 cycles

ENG 2 FIRE LOOP 'B' FAULT ECAM DISPLAYED. COMPLIED WITH MEL. SUGGEST TROUBLESHOOT. REF TSM26-12-00-810-806 NR 2 ENG B LOOP. CHECKED B LOOP RESISTANCE FROM NR 2 FDU PINS J&K,HAD 1 502 OHMS. OK IAW TSM, CKD LOOPS FOR DAMAGE, NONE FOUND. SUGGEST CHANGING ONE LOOP ON NR 2 ENG. DUE TO PREV LEGS SHOWS FAULT EVERYDAY. CHECKED HARNESS FOR DAMAGE NO DAMAGE FOUND. REPLACED FDU. OPS CHECK NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 53,077 hrs · 20,509 cycles

CRACK IN FO'S FIXED SIDE WINDOW. REPLACED WINDOW. SEALED WITH FAST CURE SEALANT APPLIED AT 03:30.

Part: MICROPHONE — INOPERATIVE (O2 MASK) · airframe 52,732 hrs · 20,348 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. CREW COMMENTS: CAPT SWAPPED MASK WITH 1 OBS MASK--NO CHANGE PROBLEM IN LOWER BOX. SWAPPED FIRST OBSERVERS MASK BOX ASSY WITH CAPTS MASK BOX ASSY. OPS CHECK OF CAPT'S OXY MASK MIC GOOD. FIRST OBSERVERS SEAT DEFERRED.

Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 52,625 hrs · 20,309 cycles

GREEN HYD SYS LOW. SERVICED SYS TO FULL.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 51,850 hrs · 19,960 cycles

F/O O2 MASK MIC INOPERATIVE. REPLACED BOX, MASK AND AMU, OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (DOOR 2R) · airframe 49,946 hrs · 19,125 cycles

DOOR 2 RT DOES NOT SHOW SLIDE ARMED IN FLT. CREW REPORTS WHEN PUSHING DOWN ON ARMING HANDLE SLIDE INDICATION IS NORMAL, ONCE PRESSURE IS OFF, SLIDE SHOWS DISARMED ON ECAM AGAIN. DOOR 2R SLIDE REMOVED FOR ACCESS. ADJUSTED AFT GIRT BAR FOOT DOOR ARMING SYSTEM. OPERATES CORRECTLY.REINSTALLED ORIGINAL SLIDE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,600 hrs · 18,976 cycles

LWR AFT FUSELAGE LEFT AND RIGHT ANTENNA CUTOUTS. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW DOUBLERS.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 49,248 hrs · 18,821 cycles

THE LANDING GEAR LOCK-STAY ACTUATOR ON THE LEFT MAIN GEAR LEAK REF CF371 IS OUT OF LIMITS. REPLACE THE LOCK STAY ACTUATOR DUE TO WEAR.

Part: WIRE — DAMAGED (CABIN) · airframe 48,434 hrs · 18,415 cycles

SEAT EEL LIGHTS AT SEATS 1C ,3C, 11C INOP. DAMAGE (UNKNOWN) TO EEL WIRING. REPAIRED WIRING AT SEATS, TESTS OKAY.

Part: OXYGEN SYSTEM — FAULTY (CREW) · airframe 45,411 hrs · 17,023 cycles

CREW 02 SYSTEM NEEDS SERVICING. *S/D* SERVICED CREW O2 SYSTEM.

Part: UNKNOWN — WARNING LIGHT (CARGO DOOR) · airframe 45,217 hrs · 16,935 cycles

RTFL DUE TO AFT CARGO DOOR INDICATION. DUE TO HISTORY OF THIS DOOR, REPLACED DOOR HANDLE SPRING, INSPECTED AFT CARGO DOOR LATCHING MECHANISM AND PROX SENSORS, NO DEFECTS NOTED. CHECKED PROX SENSOR 34WV FOR CONDITION AND CLEANED SENSOR. OPERATED DOOR AND LATCHING MECH POSITION CORRESPONDS WITH ECAM INDICATION. DISCREPANCY HAS NOT REPEATED SINCE SEPT 4.

Part: DOOR — UNKNOWN (CARGO) · airframe 45,115 hrs · 16,888 cycles

CARGO DOOR OPEN WARNING. MESSAGE RECURRED ON 'SOME' FOLLOWING FLIGHTS. REPLACED FLAP HANDLE SPRING, CLEANED PROX SENSORS AND READJUSTED HANDLE FLAP LINKAGE. THIS ITEM HAS NOT REAPPEARED OR REPEATED SINCE AUG 21.

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 42,532 hrs · 15,739 cycles

AIRFRAME VIBRATION ON CLB AT FL250-340 .78 MACH. LIGHT VERTICAL VIBRATION FELT THRU THE FLOOR, NOSE TO TAIL AT 327 KNOTS, 78 MACH ON CLIMB FROM FL 250 -340. NO ENGINE VIBRATION. CONTROL INPUT DID NOT STOP VIBRATION. FOUND 10" PIECE OF WING TO BODY FAIRING SEAL ON LT SIDE JUST FORWARD OF FLAP FLAPPING IN THE WIND. TRIMMED WING TO BODY SEAL AND TAPED OVER AREA WITH SPEED TAPE. NEED FURTHER CREW COMMENTS ABOUT VIBRATIONS. DROPPED FLAPS AND SLATS, NO OTHER DEFECTS NOTED. DL5435 CREATED TO MONITOR.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 42,384 hrs · 15,680 cycles

AFT LT EPSU FAILED. REPLACED EPSU.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 41,944 hrs · 15,474 cycles

EMERGENCY LIGHT FAIL TO TURN AT AFT GALLEY SWITCH, AND ONLY HALF TURN ON FROM COCKPIT. REPLACED AFT ATTENDANT CONTROL MODULE AND LEFT SIDE EMERGENCY BATTERY. ALL SYSTEM NOW CHECK OK.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 40,955 hrs · 15,027 cycles

SEAT 11C EMERGENCY LIGHT BROKEN. REPLACED LAMP OPS GOOD.

Part: SENSOR — DIRTY (CARGO DOOR) · airframe 39,175 hrs · 14,217 cycles

RETURN TO FIELD DUE TO CARGO DOOR INDICATION. CLEANED SENSOR. OPERATED DOOR SEVERAL TIMES WITH NO FAULTS.

Part: PROBE — FAILED (TAT NR 1) · airframe 37,377 hrs · 13,584 cycles

LOST BOTH FAC'S, WENT INTO ALTERNATE LAW. INDICATION DUE TO PROBE TAT 1 FAILURE, TAT 2 REPLACED PRECAUTIONARY. TAT 1 AND TAT 2 PROBES REPLACED.

Part: COMPRESSOR — STALLED (LT & RT ENGINE) · airframe 37,155 hrs · 13,499 cycles

CREW HAD MOMENTARY ENGINE STALL ECAM FOR BOTH ENGINES. EVENT LASTED 2 SECONDS AND SUBSEQUENT PARAMETERS WERE NORMAL. CAUSED BY A COMBINATION OF UNIQUE FLIGHT CONTROL INPUT , AND ENVIRONMENTAL FACTORS , AND SPECIFIC ENGINE CONDITIONS . THE FIX FOR THIS PROBLEM WAS AN ENGINE CHANGE. RISK ANALYSIS BY AIRBUS AND IAE SHOW RISK OF RE-OCCURRENCE OF THIS EVENT AS EXCEEDINGLY LOW. HOWEVER, TO FURTHER REDUCE RISK DOWN TO ZERO, ENGINE CONTROL SOFTWARE UPGRADES FROM ENGINE OEM IS DUE IN 2006.

Part: PROXIMITY SENSOR — MALFUNCTIONED (CARGO DOOR) · airframe 36,166 hrs · 13,136 cycles

AFT CARGO DOOR WARNING LIGHT ILLUMINATED. REPLACED THE AFT CARGO DOOR PROXIMITY SENSOR 32WV AND CONNECTOR.

Part: LINE — OUT OF POSITION (ESCAPE SLIDE)

MOORING LINE LOOP UNDER LOWER LACING COVER. SLIDE REPACKED WITH MOORING LINE LOOP INSTALLED ON TOP OF LACING.

Part: UPLOCK — DAMAGED (LT MLG) · airframe 33,068 hrs · 12,024 cycles

RETURN TO FIELD DUE TO LEFT MAIN GEAR NOT LOCKED INDICATION. REPLACED MLG UPLOCK ASSEMBLY AND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR.

Part: ENGINE — POWER LOSS (NR 1) · airframe 27,612 hrs · 9,900 cycles

ABORTED TAKEOFF AT 90-100 KNOTS DUE TO NR 1 ENGINE NOT PRODUCING ENOUGH THRUST.

Part: LIGHT — SMOKE (CABIN) · airframe 25,218 hrs · 8,894 cycles

SMOKE FROM FORWARD ENTRY LIGHTS. CIRCUIT BREAKER PULLED AND SMOKE APPEARS TO BE DISSIPATING.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,877 hrs · 8,415 cycles

CABIN PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA UPDATE FOUND RED CAPS INSTALLED ON STATIC PORTS ON BOTH PRESSURE CONTROLLERS. REMOVED CAPS, AND PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING SYSTEM. TESTED GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 22,565 hrs · 7,977 cycles

EMERGENCY POWER SUPPLY OVER LEFT WING EXIT FAILED. REPLACED POWER SUPPLY.

Part: ACTUATOR — FAILED (YAW DAMPER)

HYDRAULIC FLUID LEAKING LT EMPENNAGE SECTION, APPEARS TO BE COMING FROM RUDDER. *S/D* YAW DAMPER SERVO ACTUATOR LEAKING. ACTUATOR WAS REPLACED BY IMC ON 4/26/99 AND CORRECTED THE PROBLEM.

Part: RETRACT MECH — MALFUNCTIONED (NLG)

COULD NOT RETRACT NOSE GEAR. ALSO, LGCIU 1 AND 2 SHOWED FAILED. CONNECTED TO UNI.

Part: HYD SYST — REQD SERVICE (BLUE HYD SYST)

DIVERTED TO DEN DUE TO BLUE SYSTEM HYDRAULIC PRESSURE/VOLUME LOW.

Part: STARTER — MALFUNCTIONED (NR 1 ENGINE)

SPARKS UNDER NR 1 ENGINE UPON START-UP NOTED BY PUSHBACK MECHANIC. SHUTDOWN ENGINE. *S/D* REPLACED STARTER AND START VALVE PER MM 80-13-41. OPERATIONAL CHECK TESTED GOOD.

Part: ACTUATOR — MALFUNCTIONED (NLG DOOR)

SHORTLY AFTER GEAR EXTENTION ON APPROACH FOR LANDING, ECAM INDICATED LGCIU 1 AND 2 FAULT. GEAR INDICATION WAS DOWN AND LOCKED. LANDING UNEVENTFUL. *S/D* CFDS REPORTED BOTH NOSE GEAR DOOR CLOSED SENSOR TARGETS (30GA AND 31GA) OUT OF POSITION. REPLACED NOSE GEAR DOOR UPLOCK AND ACTUATOR. DOOR ACTUATOR TESTED OK IN SHOP. NOSE GEAR DOOR UPLOCK IS STILL AT THE VENDOR UNDERGOING EXAMINATION AND REPAIR.