N816UA

Part: FUEL CAP — MISSING (UNDERWING) · airframe 80,385 hrs · 34,943 cycles

REFUEL CAP MISSING ON ARRIVAL. REPLACED MISSING REFUEL/DEFUEL CAP IRW AMM 28-25-41-400-005-A.

Part: FUEL CAP — MISSING (UNDERWING) · airframe 79,915 hrs · 34,692 cycles

PDA 2 FUELERS REPORTED FUEL CAP MISSING. NOTIFIED TOMC CONTROLLER JAY NEWMAN APPROVED CDL FOR FUEL CAP MISSING.REF LOG PAGE 4650533. INSTALLED UNDERWING FUEL CAP REF AMM 28-25-41-400-005

Part: OVEN — FIRE (ZONE 900) · airframe 79,466 hrs · 34,444 cycles

OVEN 105 R11 IN FWD GALLEY HAD SMALL FLAME AND POSSIBLE DAMAGE TO INSIDE. REMOVED THE OVEN AT POSITION R11. INSPECTED THE OVEN EXTERNALLY AND ALSO THE COMPARTMENT FOR THE OVEN. VERIFY NO EVIDENCE OF HEAT DAMAGE IS PRESENT. THE FLAME WAS A PIECE OF FOOD INSIDE THE OVEN. FLAME WAS EXTINGUISHED WITH BOTTLED WATER. REF AMM 25-35-19. INOP STICKER INSTALLED. REPLACED R11 OVEN REF AMM 25-35-19 OPS CHECK GOOD.

Part: OXYGEN GEN — NO DISCREPANCY (ZONE 200) · airframe 79,165 hrs · 34,280 cycles

REF LP3459199 ENCOUNTERED SEVERE TURBULENCE ON DECENT AT AROUND 5-6K WITH AGGRESSIVE VERTICAL SHIFT OF THE AIRCRAFT THAT DEPLOYED ALL THE O2 MASKS. SMOOTH LANDING WITH AN EMERGENCY DECLARED. FA'S NOTICED A HOT SMELL IN THE CABIN THAT THE FIRE DEPARTMENT SUSPECTS IS COMING FROM THE OXYGEN GENERATORS BEING ACTIVATED DUE PRESENCE OF HEAT. INSPECTION OF THE AIRCRAFT AFTER A CREW REPORT OF EXCESSIVE TURBULENCE WITH NO EXTERIOR STRUCTURAL DEFECTS NOTED.FOUND O2 GENERATOR USED AT SEATS 1AB, 1EF, 2EF, 3EF, AND 1L JUMPSEAT. REPORTED BY LOCAL MAINTENANCE, INSPECTED ALL POSTIONS WHERE MASKS DROPPED REF AMM 35-21-00. CONFIRMED O2 GENERATORS USED AT THE LISTED LOCATIONS WITH THE EXCEPTION BEING 2EF. THE PIN REMAINS INTACT AND OK FOR CONTINUED SERVICE. REPLACED O2 GENERATOR AT 1L JUMPSEAT REF AMM 35-21-42. REPLACED O2 GENERATOR AT 1AB AND 3EF REF AMM 35-21-42. VERIFIED REMOVAL OF THE SHIPPING PIN AND PROPER INSTALLATION OF THE OXYGEN GENERATOR REPLACED O2 GENERATOR ASSEMBLY AND CONTAINER AT 1EF AND 2EF REF AMM 35-21-41. OPERATIONAL TEST OF EMERGENCY OXYGEN SYSTEM REF AMM 35-23-00-710-001-A .

Part: BATTERY — NO TEST (ZONE 200) · airframe 79,036 hrs · 34,205 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK. FOUND FWD BATTERY PACK 10WL, FAILED RED LIGHT. REPLACED EPSU BATTERY PACK, IAW 33-51-38-400-002-A0, OPS TEST GOOD.

Part: FUEL CAP — MISSING (WING) · airframe 78,859 hrs · 34,114 cycles

PDA 2 FUEL CAP REPORTED MISSING ON ARRIVAL. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V123456 MAC RELATED WORK ORDER 000000003122843 AND PRTR VERIFIED NO LEAKS FROM COUPLING. INSTALLED AN INOP STICKER ADJACENT TO THE REGISTRATION NUMBER ON THE FORWARD INSTRUMENT PANEL. CDL 28A APPLIED. COUPLING VERIFIED NOT LEAKING BY ON CALL TECH ROBERT SCOTT V899913. WORK ORDER 3122843. UPDATED SDR INFORMATION. VERIFIED NO LEAKS FROM COUPLING. INSTALLED AN INOP STICKER ADJACENT TO THE REGISTRATION NUMBER ON THE FORWARD INSTRUMENT PANEL. CDL 28A APPLIED. DISPATCH DESK: 16 NAME: JM DATE: 21-NOV-24- DEFERRED DIRECTLY BY TOMC . INSTALLED FUEL CAP IAW AMM 28-25-41 NO LEAKS THIS ACTION CLEARS CLD 28A PLACARD REMOVED PARTS TRANSACTION ADDED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1339668 SN OFF 0643 CAP, COUPLING R OFF 31-2825-9-0001 0643 ON 31-2825-9-0001 0299 CAP, COUPLING R OFF 31-2825-9-0001 0643 ON 0000

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 78,231 hrs · 33,753 cycles

HYD Y SYSTEM LO PR ECAM MESSAGE WITH THE ASSOCIATED HYD Y RSVR LO LVL AND ENGINE 2 PUMP LO PR MESSAGES..... UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CONTACT TOMC 847-700-9980 UPON A WALKAROUND INSPECTION FOUND HYD FLUID ACCUMULATION AT PANEL 196BB, AND THROUGH FURTHER INVESTIGATION FOUND FLUID SAMPLING VALVE LEAKING. REMOVED AND REPLACED O RING AT FLUID SAMPLING VALVE REFERENCE AMM TASK 29-13-34-400-001-A. OPS CHK GOOD, LEAK CHK GOOD. OK FOR SERVICE.PARTS USED: 00-0585-3-0326,QTY :1

Part: SKIN — CRACKED (FR35 STR30) · airframe 75,959 hrs · 32,597 cycles

ACCOMPLISH PERMANENT REPAIR AT LH FR35 STR30 HOLE 2 AND HOLES A, B, AND C PER PART 3 OF THE LATEST REVISION OF ECRA 5331-03055 ON OR BEFORE 29MAR2024. OR BEFORE 29MAR2024. ACCOMPLISH PERMANENT REPAIR AT LH FR35 STR30 HOLE 2 AND HOLES A, B, AND C PER PART 3 OF THE LATEST REVISION OF ECRA 5331-03055 ON ACCOMPLISH PERMANENT REPAIR AT LH FR35 STR30 HOLE 2 AND HOLES TOMC-APPROVAL FROM SC1ELBYC COMMENT A, B, AND C PER PART 3 OF THE LATEST REVISION OF ECRA 5331-03055 ON OR BEFORE 29MAR2024. Q/C REVIEWED. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — CRACKED (FR35 STR30) · airframe 75,959 hrs · 32,597 cycles

FOR THE REPAIR ACCOMPLISHED AT LH FR35 STR30 HOLES, PLANNING TO CONTACT ENGINEERING AFTER 29FEB2024 BUT BEFORE 15MAR2024, FOR THE EC 5331-03055 PART 3 PERMANENT REPAIR REQUIREMENTS. REF LP 5966875. THE EC 5331-03055 PART 3 PERMANENT REPAIR REQUIREMENTS. REF LP 5966875. FOR THE REPAIR ACCOMPLISHED AT LH FR35 STR30 HOLES, PLANNING TO CONTACT ENGINEERING AFTER 29FEB2024 BUT BEFORE 15MAR2024, FOR FOR THE REPAIR ACCOMPLISHED AT LH FR35 STR30 HOLES, PLANNING TO TOMC-APPROVAL FROM SC1ELBYC COMMENT CONTACT ENGINEERING AFTER 29FEB2024 BUT BEFORE 15MAR2024 PER ECRA 5331-03305 Q/C REVIEWED. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FITTING — CRACKED (RH MLG DOOR) · airframe 75,959 hrs · 32,597 cycles

RMLG DOOR ACTUATOR FITTING KEEL BEAM HOLE R16 AN R20 PRODUCED CRACK INDICATIONS IN THE 3 POSITION DURING LFEC INSPECTION FWD LUG . ACCOMPLISH A PERMANENT REPAIR FOR HOLES R1, R2, R12, R16, R18, PART 3B OF THE LATEST REVISION OF ECRA 5330-05721 ON OR BEFORE R20, & S2 ON THE KEEL BEAM AND MLG DOOR SUPPORT STRUCTURE PER 14-SEP-2024. INTERIM REPAIR PERFORMED PER PART 1B STEP 1 OF ECRA 5330-05721 TO RH MLG DOOR AND ACTUATOR FITTING HOLES. PER PART 1B STEP 2

Part: PANEL — CORRODED (AFT CARGO) · airframe 75,959 hrs · 32,597 cycles

AFT CARGO DRAIN MAST EXHAUST VENT INNER RETAINING PLATE HAS CORROSION BETWEEN RH STRG 38 AND 35 BETWEEN FRM 68 AND 69. RMV AND RPL AFT CARGO DRAIN MAST EXHAUST VEN INNER RETAINING PLATE REINFORCEMENT BETWEEN STRG 38R-STGR 35R AND BETWEEN FR68 AND FR69 IAW A319 SRM 51-72-11-911-001 AND SRM 51-72-11-911-002.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 75,959 hrs · 32,597 cycles

R2 PAX DOOR SILL AFT CORNER FITTING CORRODED GEN ON H AECO LCQ NR 9290566/40566 REMOVED AND REPLACED AFT CORNER FITTING ON FR 68 RT IAW A319 SRM 51-72-11.

Part: DOOR SILL — CORRODED (R2) · airframe 75,959 hrs · 32,597 cycles

R2 PAX DOOR SILL HAS MULTIPLE SPOTS OF CORROSION, ON HAECO LCQ NR 9290565/40565 REMOVED AND REPLACED R2 DOOR SILL FR 66-68 IAW A319 SRM 51-72-11 P 1&2- INSTALLED ATTACHING PARTS IAW A319 SRM 51-72-11.

Part: FRAME — CRACKED (R2 DOOR) · airframe 75,959 hrs · 32,597 cycles

UPON REMOVAL OF R2 DOOR SILL FR 67 FRAME SEGMENT (STRAP) WAS FOUND TO HAVE CRACK ON UPPER I/B REDIUS. GEN BY V061616 ON HAECO LC Q NR 9290815/40815 REMOVED AND REPLACED FRAME SEGMENT STRAP AT FRAME 67 IAW A319 SR M 51-72-11 P 1&2 ACMP BY V052030 INSP BY V079881

Part: GUSSET — CRACKED (R/H FR68) · airframe 75,959 hrs · 32,597 cycles

R/H FR68 GUSSET #3, HOLE #3 AND #4 HAS A CRACK INDICATION AT THE 12 O''CLOCK POSITION IN FRAME LAYER (A3NB-53-4-6355) GENERATED BY MECH V061632 GENERATED AT HAECO LCQ PER NR 9290457 (40457) REPAIRED RH FR68 GUSSET HOLE #3 HOLE #4 IAW ECRA 5311-02470 AS D IRECTED BY RFTS 60012 ACMP BY MECH V061616 INSP BY V899260

Part: GUSSET — CRACKED (R/H FR68) · airframe 75,959 hrs · 32,597 cycles

R/H FR68 GUSSET #3 HOLE #3 HAS A INDICATION AT THE 12 O CLOCK PO SITION IN FRAME LAYER GEN BY V061632 ON NR 9290457/ 40457 REPAIRED RH FR68 GUSSET #3 HOLE #3 IAW ECRA 5311-02470 AS DIRECTED BY RFTS 60012.

Part: SHEAR PLATE — CRACKED (AFT WET AREA) · airframe 75,959 hrs · 32,597 cycles

AFT WET AREA AFT RH SHEAR PLATE CRACKED (A3NB-53-3-6357) PER HAE CO LCQ NON ROUTINE 9290567/40567 GENERATED BY V937268 REMOVED AND REPLACED RH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 AND 7. ACMP BY MECH V944156 INSP BY V061771

Part: SHEAR PLATE — GOUGED (AFT WET AREA) · airframe 75,959 hrs · 32,597 cycles

AFT WET AREA AFT L/H SHEAR PLATE MULTIPLE HOLES ARE ELONGATED AND GOUGE (A3NB-53-3-6357) PER HAECO LCQ NON ROUTINE 9290574/40574 GENERATED BY V937268. REMOVED AND REPLACED LH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 ACMP BY MECH V944156 INSP BY V061771

Part: ANGLE — CRACKED (RH EMER DR) · airframe 75,959 hrs · 32,597 cycles

RH OVERWING EMERGENCY HATCH HAS SUSPECTED CRACK AT AFT VERTICAL SUPPORT @ RIVET POINTS (A3NB-05-3-6170) PER HAECO LCQ NON ROUTIN E 9290527/40527 GENERATED BY V899260 REMOVED FOR CRACK 2EA ANGLE SEGMENT FWD FR38 & AFT FR39 FROM R/H EMERGENCY DOOR & INSTALLED 2EA NEW ANGLE SEGMENT FWD FR38 & AFT FR39 IAW A319 SRM 51-42-11 PER MECH V913400 INSP V061771

Part: ANGLE — CRACKED (LH EMER DR) · airframe 75,959 hrs · 32,597 cycles

LH OVERWING EMERGENCY EXIT HAS SUSPECTED CRACKS AT FWD AND AFT VERTICAL SUPPORTS @ RIVET POINTS (A3NB-05-3-6171) PER HAECO LCQ NON ROUTINE 9290526/40526 GENERATED BY V899260 REMOVED CRACKED 2EA ANGLE SEGMENT AND INSTALLED NEW 2EA ANGLES SEGMENT FROM LH EMERGENCY DOOR FR38 FWD AND FR39 AFT IAW A319 SRM 51-42-11 ACMP BY MECH V052050 INSP BY V913126

Part: FUEL CAP — MISSING (FUEL PANEL) · airframe 72,748 hrs · 30,977 cycles

PDA 3 FUEL CAP MISSING REPLACED MISSING FUEL CAP PART CHANGE UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1613986 SN OFF 2830 CAP, COUPLING R OFF 31-2825-9-0001 2830 ON 31-2825-9-0001 0457

Part: CLAMP — BROKEN (ABOVE WATER SERV) · airframe 72,123 hrs · 30,670 cycles

REFERENCE 8020643, NEED TO ACCOMPLISH ECRA 2011-01000 DUE TO POTABLE WATER LEAK. NEED DEEP CLEANING FROM STA 19761FR47 TO STA 26695 FR64 DID INITIAL CLEAN UP ,NEED FURTHER CLEAN FROM STA19761FR47 TO STA26895FR64 WATER LEAK WAS CONFINED TO BELOW THE FLOOR FROM WATER SERVICE TOMC-APPROVAL FROM SC1ELBYC COMMENT PANEL FWD TO FRAME 47 APPROXIMATELY STRINGER 42R TO 42L. APPROVED DIP FOR IN DEPTH CLEANUP TO BE ACCOMPLISHED WITHIN 7 DAYS, PER EC/RA 2011-01000 CARGO COMPARTMENT SPILL, SECTION 2.B. DIP 38-DIP PLEASE INDICATE THAT THE INITIAL CLEANUP HAS BEEN ACCOMPLISHED PER ECRA 2011-01000. ACCOMPLISHED INITIAL CLEANUP NEED DEPH CLEAN UP FROM TOMC APPROVED

Part: BOLT — BROKEN (NR 1 MLG WHEEL) · airframe 70,571 hrs · 29,893 cycles

#1 MLG TIRE TIE BOLT BROKEN.. FOUND SHEAR TIE BOLT BROKEN AND MISSING FROM FAIRLY NEW TIRE UPDATING SDR REPLACED NUMBER 1 MAIN GEAR TIRE REF AMM32-41-11 WHEEL ASSYMBLY SERIAL NUMBER REMOVED 9336P INSTALLED SERIAL NUMBER 7106P. TIRE REMOVED WAS JUST INSTALLED YESTERDAY AND SHEAR TIE BOLT SHEARED AND FELL OUT, CHECKED BRAKE FOR DAMAGE NONE NOTED

Part: INTERCOSTAL — CRACKED (R1 DOOR FRAME) · airframe 69,001 hrs · 29,119 cycles

R1 DOOR FRAME 16 STOP FITTING NR 7 LOWER INBOARD HOLE IS CRACKED IN THE WEB AT 1 O'CLOCK AND IN THE INTERCOASTAL AT 7 O'CLOCK REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEERING FOR APPROVED REPAIR INSTRUCTIONS ON HAECO LCQ, REF 9298093 GEN BY V061633. REMOVED AND REPLACED R1 DOOR FRAME 16 STEP FITTING NR 7 INTEROSTAL, IAW A319 SRM 51-42-11-801 AND 51-72-11-911-001. PERFORMED BY MECH V079529 INSP BY N078625 AT HAECO LCQ.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 69,001 hrs · 29,119 cycles

EMERGENCY BATTERY 13WL FAILS TEST.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 68,586 hrs · 28,936 cycles

ECAM AFTER TAKEOFFHYD B LO PRESS REMOVED AND REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC POMP PER

Part: SEAL — DAMAGED (NR 2 ENGINE) · airframe 66,180 hrs · 27,788 cycles

PDA 2 ENGINE 2 INBOARD FLEX SEAL SEGMENT IS BENT, BROKEN, CRACKED, WITH PIECE MISSING.

Part: BUSHING — DAMAGED (LT MLG) · airframe 64,167 hrs · 26,770 cycles

LEFT MLG SIDE STAY UPPER INBD CARDAN BUSHING WAS DAMAGED IN THE INBD FACE. REMOVED TWO INBD SIDE STAY BUSHINGS AND OVERSIZED INBD LUG BORE TO 3.2515 FINAL SIZE. INSTALLED NEW BUSHINGS & HONED TO FINAL DIMENTIONS. SEALED BUSHING FLANGES. INSTALLED NEW GREASE NIPPLES. ALL WORK ACCOMPLISHED IAW SRM 57-26-13-300-023.

Part: FITTING — CORRODED (LT MLG) · airframe 64,167 hrs · 26,770 cycles

LEFT MLG SIDESTAY UPPER CARDAN OTBD BUSHING ROTATING. REMOVED THE BUSHING. THE BORE AND SPOTFACED INBD & OTBD FACES TO REMOVE ALL CORROSION. ACCOMPLISHED ISSURANCE CUTS TO ALL REWORKED AREAS AND RESTORED CHAMFERS. INSTALLED A NEW BUSHING. HONED TO FINAL DIM. INSTALLED NEW TAB WASHER, SPECIAL NUT, SEALED NEW FLANGES & INSTALLED NEW GREASE NIPPLES. ALL WORK ACCOMPLISHED IAW SRM 57-26-13-300-023.

Part: VALVE — LEAKING (HYD SYSTEM) · airframe 62,526 hrs · 25,957 cycles

RESERVOIR LOW DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND SAFETY VALVE 49GA LEAKING AT SWITCH ASSY. REPLACED LANDING GEAR SAFETY VALVE IAW AMM 32-31-17-000-001, LEAK CHECKED GOOD. COMPLETED MM 32-31-17, TESTED SAFETY VALVE IAW MM 32 -31-00. CHECKED GOOD.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 62,474 hrs · 25,933 cycles

GEAR WOULD NOT EXTEND NORMALLY AFTER CYCLING HANDLE 2 TIMES. HAD TO PERFORM MANUAL EXTENSION. EMERGENCY DECLARED. REMOVED AND REPLACED LDG SELECTOR VALVE REF AMM 32-31-12, EXTENSION & RETRACTION TESTS CHECK NORMAL. REMOVED AND REPLACED LDG SAFETY VALVE REF AMM 32-31-17, REQUIRES OPS CK TASK 32-31-00-710-005-A01. EXTENSION AND RETRACTION OF LANDING GEAR TEST. E AND L/G SAFETY VALVE PER AMM 32-31-12 AND 32-31-17. VERIFIED VERIFIED P/NS WITH IPC, VERIFIED INSTALLATION OF L/G SELECT VALVE REF ECRA 3231-01172 FOR LDG GEAR SELECTOR VALVE INSTALL. PERFORMED TASK 32-31-00-710-005-A01 , ALL OPS CKS NORMAL. ALL OPS CKS FOR NORMAL GEAR RETRACTION & EXTENSION NORMAL REF AMM TASK 32-31-00-720-002-A FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION VERIFIED GEAR EXTENSION AND RETRACTION, ALL OPS AND FUNCTIONAL C CHECKS PER AMM 32-31-00-710-005-A01 ALL OPS CKS FOR NORMAL GEAR RETRACTION & EXTENSION NORMAL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 60,337 hrs · 24,840 cycles

CREW REPORTED AT 6000 FT, CABIN PRESSURE LIGHT ON ECAM. AT 8000 FT, CREW RECEIVED A MASTER CABIN PRESSURE LIGHT. UNABL E TO CONTROL THE PRESSURIZATION AS CABIN CLIMBED. NEVER ASSENDED ABOVE 10000 FEET. TROUBLESHOT IAW TSM 21-31-00-810-831-A, AND FOUND A CPC1 FAULTING. REPLACED CPC1 IAW AMM 21-31-34-400-001-A. OPS TESTED IAW AMM 21-31-00-710-002 -A, BOTH SYSTEMS 1 AND 2 CHECKED OK. SYSTEM OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 59,170 hrs · 24,189 cycles

HORIZONTAL STAB THSA NO BACK YOKE AFT INNER YOKE FLANGE IS CONTACTING THE BASE OF ROD SPHERE WITH DAMAGE TO FLANGE AND ROD SPHERE (AT THE PRIMER COLORED RINGS ON THE ROD SPHERE). THSA REQUIRES REPLACEMENT IAW EA 2744-01056 REV C OP 002 STEP 5.3. REF AMM27-44-51-400-001-A . REMOVED AND REPLACED THS ACTUATOR

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 58,621 hrs · 23,920 cycles

DURING EG 1384, KEELBEAM, INSP 8 HOLES WERE FOUND TO BE DISCREPANT. ALL HOLES REPAIRED IAW ECRA 5330-05721.

Part: ACTUATOR — FAILED (BLEED SYS) · airframe 65,795 hrs · 7,673 cycles

NR 1 ENGINE EGT OVERLIMIT DURING TAKEOFF. FAULTED 2.5 BLEED ACTUATOR. EXCEEDANCE RECORDED WAS 640 FOR 8 SECONDS. REPLACED 2.5 BLEED ACTUATOR IAW AMM 75-31-42-400-010-B13

Part: FLIGHT RECORDER — FAULTED (COCKPIT) · airframe 52,925 hrs · 21,184 cycles

DFDR FAULT DISPLAYED ON UPPER ECAM. SYS FAULT ECAM AT PARKING INTERMITTENT. NO PREVIOUS HISTORY LAST LEG & PLR NO FAULTS. OPERATIONS CHECKED GOOD IAW AMM 31-33-00-710-007.

Part: OIL SYSTEM — OVERSERVICED (NR 2 ENGINE) · airframe 52,532 hrs · 21,021 cycles

ENG 2 OIL QTY GAUGE SHOWING AMBER XX. LATER OIL QTY INDICATOR BECAME NORMAL, SHOWING 26Q TS. REMOVED 2.5 QTS OF OIL IAW AMM 12-13-79, 5 MIN IDLE RUN QTY WITHIN ACCEPTABLE LIMITS & PRESENT IN ECAM AFTER ENG RUN, NO FURTHER SERVICE NEEDED.

Part: PUMP — LEAKING (FUEL SYSTEM) · airframe 51,956 hrs · 20,788 cycles

FLUID SEEP ON WALK AROUND. FOUND PUMP 37-QA LEAKING. REMOVED PUMP IAW AMM 28-21-51-000-002-A & INSTALLED PUMP IAW AMM 28-21-51-400-002-1 THRU STEP B 8. INSTALL PROC COMPLETED SEE SEQ 9562004.

Part: PUMP — LEAKING (FUEL SYSTEM) · airframe 51,884 hrs · 20,755 cycles

NR 1 CTR FUEL PUMP LEAKING. REMOVED NR 1 CTR FUEL PUMP REPLACE O-RING SEALS & PUMP, LEAK CHECKED GOOD IAW MM.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 51,328 hrs · 20,505 cycles

O2 MASKS FELL IN ROW 8 DEF. REPACKED & ACCOMPLISHED TEST MT35-00.

Part: SEAT BACK — LOOSE (CABIN) · airframe 51,172 hrs · 20,435 cycles

SEAT BACK LOOSE & ROCKING AT 11E. SWAPPED A NUT FROM SEAT 32F, SEAT 11E WORKS NORMALLY. DEFER 32F IAW MEL, LOCKED UPRIGHT. INSTALLED LOCK NUT ON 32F SEAT STILL LOCKED UPRIGHT.

Part: WIRE — SEVERED (FIRE BOTTLE) · airframe 50,970 hrs · 20,344 cycles

NR 1 ENGINE PYLON FWD FIRE EXT BOTTLE WIRES, SEVERED 8 INCHES FROM CONNECTOR 5WE1-A. REPLACED WIRE 2621-19-DL20 2621-20-CF20 AND CONDUIT IAW AWM 26-21-01.

Part: SEAL — UNSECURE (FUSELAGE) · airframe 50,577 hrs · 20,172 cycles

AIRFRAME VIBRATION FROM T/O THROUGH 17K FT. SUSPECT LOWER F/O NOSE AREA. ENGINE PARAMETERS NORMAL, FOUND SEAL AT PANEL 191BT AND 191DT SPLIT AND PROTRUDING OUT OF THE GAP. TAPED OVER DAMAGED AREA IAW AMM MT 53-004. COMPLETED VIBRATION SHEET AND TROUBLESHOOTING IAW MT 53-005. DL1493 CREATED TO MONITOR . SEAL WITH AERODYNAMIC SEALANT. SEAL INTACT AND SECURE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 50,546 hrs · 20,159 cycles

CABIN EMERGENCY LIGHTING MESSAGE "EPSU BATTERY AFT LIGHT". REPLACED POWER SUPPLY IAW AMM EST PASSED,

Part: TRUNNION — WORN (TE FLAPS) · airframe 50,345 hrs · 20,071 cycles

LEFT INBD FLAP TRUNNION WORN AT AREA D. BLENDED OUT DAMAGED AREA.

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 50,005 hrs · 19,927 cycles

ON WALK AROUND, FOUND SMALL HYDRAULIC LEAK FROM GREEN SYSTEM. VERIFIED LOW QTY ON COCKPIT GAUGES. FOUND BRAKE RETURN LINE UNION O-RING BAD. REPLACED O-RING, LEAK CHECKS GOOD.

Part: SEAT — BROKEN (CABIN JUMP SEAT) · airframe 49,836 hrs · 19,856 cycles

FORWARD CABIN F/A INBRD JUMP SEAT BROKEN BY 1L. UNTANGLED SEAT-BELTS.

Part: MICROPHONE — FAILED (OXYGEN MASK) · airframe 49,835 hrs · 19,855 cycles

CAPTAIN'S OXYGEN MASK FAILED TEST, NO TRANSMIT OF MICROPHONE. REPLACED OXYGEN MASK. CHECKED GOOD.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 49,613 hrs · 19,755 cycles

MULTIPLE WARNINGS, FLT DIVERTED. REPLACED BOTH FLIGHT WARNING COMPUTERS. PRECAUTIONARY WITH TOMC SUPPORT.

Part: CONNECTOR — FOULED (IGNITOR) · airframe 49,284 hrs · 19,611 cycles

ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN - APU. APU AUTO SHUTDOWN DURING START ON TAXI IN. :"RE-SET" "OPS CHECK OK" HAS MADE THIS ITEM-C. APU ASD W.O. BITE MSG REF: TSM 490000-810-992-A (POSSIBLE WATER INGRESS IN PANEL 121AL). REMOVED IGNITER PLUGS AND FOUND FOULED. REPLACED PLUGS IAW AMM 49-41-41, OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (SMOKE DETECTION) · airframe 49,145 hrs · 19,557 cycles

SMOKE DETECTOR FAULT DISPLAYED ON UPPER ECAM. REPLACED AFT PIT SMOKE DETECTOR 6WH. NO HELP, BOTH CHANNELS FAILING DIFFERENT SMOKE DETECTORS EACH TIME TESTED. SLAVED IN KNOWN GOOD DETECTOR NO HELP. TRIED NEW SDCU NO HELP. RE-INSTALLED ORIGINAL SDCU. REF TSM 26-16-0 0-810-819-A AND 26-17-00-810-803-A SDCU DOUBLE CHANNEL FAULT.

Part: LOCK RING — DEFECTIVE (CABIN SEAT) · airframe 48,878 hrs · 19,459 cycles

ROW 11ABC THE SEATS ARE LOOSE. REPLACED LOCK RINGS & SECURED SEATS PER AMM. ACCOMPLISHED IDT INSPECTION PER GMM- 09-10-05 AND MM25-21-41.

Part: CONTROL UNIT — FAULTY (SMOKE DETECTOR) · airframe 48,796 hrs · 19,430 cycles

SMOKE DETECTOR MESSAGE ECAM. REPLACED SDCU PER MM, NO HELP. RESET, CHECK OK PER TASK 26-17-00-810-803A. MSG CLEARED.

Part: THRUST REVERSER — DAMAGED (NR 1 ENGINE) · airframe 48,111 hrs · 19,135 cycles

NR 1 ENGINE INBOARD REVERSER AT THE 0100 POS (LOOKING AFT) HAS A 4X6 PIECE OF PREVIOUS REPAIR DEGRADING AND STICKING UP INTO THE AIRSTREAM. REPLACED INBOARD REVERSER PER MM. OPS CHECK PER MM AND OPS CHECK OKAY.

Part: PANEL — LOOSE (CEILING) · airframe 48,060 hrs · 19,114 cycles

OVERHEAD PANEL ABOVE SEAT 2F IS LOOSE. AFT END OF PANEL IS SECURE WITH TAPE. PSU AND VIDEO MONITOR ARE NOT OBSTRUCTED, OK FOR SERVICE. REPLACED PANEL COVE LIGHT ASSEMBLY AT 2EF.

Part: GIRT BAR — LACK OF LUBE (R2 DOOR GIRT BAR) · airframe 47,500 hrs · 18,883 cycles

DOOR 2R WILL NOT ARM. LUBED GIRT BAR FITTINGS AND ROLLERS ON DOOR FRAME. ARM DISARM FUNCTIONS OKAY.

Part: LIFE VEST — MISSING (COCKPIT) · airframe 47,401 hrs · 18,838 cycles

FIRST OBSERVER LIFE PRESERVER MISSING FROM FLT DECK. REPLACED LIFE VEST.

Part: LEVER — MISSING (COCKPIT SEAT) · airframe 46,392 hrs · 18,406 cycles

CAPT SEAT SHOULDER HARNESS LOCK-UNLOCK LEVER MISSING. SAMC TEXT: REF IPC 25-11-51-01M: REPLACE SEAT ASSY. PCN 021-9017. REPLACED CAPTAIN'S SEAT PER MM, OPS CHECKS GOOD.

Part: SLIDING WINDOW — OUT OF TOLERANCE (COCKPIT) · airframe 45,810 hrs · 18,169 cycles

RT SLIDING WINDOW REPLACEMENT. REPLACEMENT OF THE RT SLIDING WINDOW WAS ACCOMPLISHED PER TASK CARD 4S5686108.

Part: PUMP — FAULTED (NR 1 HYD SYSTEM) · airframe 45,529 hrs · 18,042 cycles

GREEN HYDRAULIC SYS OVERHEAT ILLUMINATED, FLIGHT DIVERTED. REPLACED OVERHEAT SWITCH 1381 GR, CHECKED CASE DRAIN FILTER NO DEFECTS. ACCOMPLISHED INTERNAL LEAK CHECK. NO DEFECTS. ACCOMPLISHED TSM 29-11- 00-810-802, ALL CHECKED GOOD. RAN ENGINE FOR 20 MINUTES NO OVERHEAT MESSAGE. REPLACED THE NR 1 ENGINE GREEN HYD PUMP 1030GK.

Part: BOTTLE — DISCHARGED (R1 DOOR ASSIST) · airframe 43,660 hrs · 17,208 cycles

DOOR 1R ASSIST BOTTLE PRESSURE LOW. SERVICED ASSIST BOTTLE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 41,427 hrs · 16,229 cycles

ON 3SV FAILED EMERGENCY LIGHT TEST BTSU INT LOAD AFT LT. REPLACED BATTERY FOR EPSU 13WL. EMER LIGHT TEST OK.

Part: CONNECTOR — MISSING (EMERGENCY LIGHTS) · airframe 41,427 hrs · 16,229 cycles

BACKSHELL FOR CONNECTOR ON EPSU 13WL, IS MISSING. ALSO STRAIN RELIEF IS CRACKED. REPLACED BACKSHELL-STRAIN RELIEF ON CONNECTOR 13WLA. EMERGENCY LIGHTS TEST PASSES.

Part: COMPUTER — MALFUNCTIONED (HYD SERVO) · airframe 40,452 hrs · 15,740 cycles

ON FLT CONTROL CHECK L-R AILERON HAVE HYD NOISE-VIBRATION HEARD AND FELT IN COCKPIT. ISOLATED RT AILERON HYD SYSTEMS, RT AILERON FLUTTERS WITH ONLY GREEN HYD SYSTEM ON. ATTEMPTED ELAC 1 AND 2 RESET, NO HELP. SUSPECT RT GREEN AILERON SERVO ISSUE. THERE WERE NO AILERON FLUTTER ISSUES WTH BLUE HYD SYS SELECTED, ONLY GREEN SYS. REPLACED RT GREEN AILERON SERVO CONTROL UNIT, OPS CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,679 hrs · 15,385 cycles

FRAME 73 STRINGER 31L & 32L SHEAR TIE DAMAGED. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,679 hrs · 15,385 cycles

FRAME 74 STRINGER 31L & 32L CRACKED AND DAMAGED. FRAME 74 STRINGER 31 LEFT AND 32 LEFT, SHEAR TIE CRACKED AND DAMAGED. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,679 hrs · 15,385 cycles

FRAME 74 STRINGER 32L & 33L CHECKED AND DAMAGED. FRAME 74, STRINGER 32L AND 33L SHEAR TIE IS CRACKED AND DAMAGED. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED TIE.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 39,679 hrs · 15,385 cycles

DOOR 1R SLIDE FAILED TO DEPLOY. SLIDE STILL IN PLACE ON ACFT WITH DOOR CLOSED AND UNARMED. UNABLE TO RECORD MR NR AND DASH DUE TO POSITION OF SLIDE. REPLACED SLIDE PACK.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 39,679 hrs · 15,385 cycles

RT MLG FAILED TO EXTEND. RAT DEPLOYED. VALVE FOUND FAULTY. REPLACED CUTOUT VALVE L-G FREE FALL 2515GM. OPS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM - Y765 HAS CORROSION FWD OF FR68. MAJOR REPAIR ACCOMPLISHED. BEAMS REMOVED AND BRACKETS TRANSFERRED (BEAM 95 AND 150) BEAMS NEED TO BE SPLICED TOGETHER AND INSTALLED. SPLICE INSTALLED AND BEAMS 95 AND 150 INSTALLED.

Part: STIFFENER — CRACKED (NLG WW) · airframe 35,277 hrs · 13,431 cycles

STIFFENER IN NOSE WHEEL WELL LEFT SIDE IS CRACKED ON THE RISER. REPAIRED STIFFENER PER SRM 57-11-16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM Y254 HAS CORROSION BETWEEN FR65 AND FR66 (MARKED). REPLACED BEAM 160. REPLACED FLOORBEAM 160.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM -Y1292 HAS CORROSION JUST AFT OF FR66. MAJOR REPAIR ACCOMPLISHED. REPLACED BEAM & SECURED WITH FASTENERS. ACP BEAM INSTALLATION FOR Y1292 FWD OF BEAM 140.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 145 HAS LOOSE RIVET(MARKED). MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FOUND CORRODED BEAM REPLACED. ACP INSP OF BEAM 145.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 185 HAS CORROSION AT FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. BEAM OUT AND ON BENCH WORKING. STARTED INSTALLATION OF BRACKETS. RIVETING OF STANDOFF BRACKETS IS WHAT IS LEFT. DRILLED AND INSTALLED NEW BEAM 185. ALL BRACKETS RE-INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

THE 2R DOOR SILL CORRODED AT FWD SPLICE OUTBOARD SIDE, AT NUT CLIP HOLE. MAJOR REPAIR ACCOMPLISHED. STARTED TO REMOVE FASTENERS, INBOARD AND OUTBOARD ANGLES, NEW ANGLES FOR REPAIR IN WORK AREA. ACCOMPLISHED REPAIR PER MT 53-025. INSPECTED REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

AFT RT SHEAR TIE CORRODED BETWEEN FRAME 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE. INSTALLED SHEAR PLATE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 190 HAS CORROSION AFT OF FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. BEAM REMOVED. STARTED INSTALLATION OF BEAMS 190 AND 195. SECURED NUT PLATES FOR FLOORBOARD. INSTALLATION IS COMPLETE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 195 HAS CORROSION ALONG LENGTH (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED SEVERAL FASTENERS FROM BEAM 190 TO REMOVE BEAM 195. BEAM REMOVED. INSTALLED 8 NUT PLATES ON BEAM 195 FOR PNL 261FF. SECURED NUT PLATES FOR FLOORBOARD HOLES. INSTALLATION IS COMPLETE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 175 HAS CORROSION ALONG LENGTH BETWEEN FR68 AND FR70. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. INSTALLED LAV AND GALLEY MOUNT FITTINGS TO NEW FLOORBEAM. DRILLED AND INSTALLED BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,277 hrs · 13,431 cycles

FLOORBEAM 140 HAS CORROSION ON ENTIRE LENGTH. MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FAB'D SPLICES FOR BEAMS FORE AND AFT PRIMED, SEALED & INSTALLED AFT END TO BEAM 145, FWD READY TO INSTALL. INSTALLED SPLICE TO BEAM 80. REPLACED BEAM AND COMPLETED WITH FASTENERS.

Part: LIGHT — NO TEST (CABIN) · airframe 35,009 hrs · 13,320 cycles

CABIN EMERGENCY LIGHTS WILL NOT TEST.

Part: BATTERY — FAULTY (CABIN) · airframe 34,582 hrs · 13,139 cycles

ON EMERGENCY LIGHT TEST, FAULT KEEPS COMING UP EPSU BATT AFT L.

Part: CONTROL UNIT — FAULTY (LT ELEVATOR) · airframe 34,426 hrs · 13,080 cycles

ELAC 2 FAULT INDICATIONS. SERVO 34CE1 FAILING CAUSING ELAC 2 TO FAULT CHRONICALLY. REPLACED LT INBOARD ELEVATOR SERVO CONTROL UNIT 34CE1, ADJUSTED AND OPS TESTED OK.

Part: SLIDE — DISLODGED (DOOR 1L) · airframe 34,058 hrs · 12,926 cycles

DOOR 1L SIDE FELL OUT OF PACK. REPLACED SLIDE WITH SERVICEABLE UNIT.

Part: SHEAR PIN — SHEARED (L1 DOOR SLIDE) · airframe 34,058 hrs · 12,926 cycles

FOUND DOOR 1 LEFT DOOR BOTTLE LOW AND SHEAR PIN, SHEARED IN REF TO SLIDE PACK ON JET WAY. REPLACED DIAPHRAGM AND SHEAR PIN AND SERVICED BOTTLE PER MM. ALSO REPLACED WITH SERVICABLE SLIDE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 34,025 hrs · 12,909 cycles

EMERGENCY LIGHTS TEST FAILED. FOUND EPSU FAILED. REPLACED EPSU 13WL, TEST PASSES.

Part: EPSU — FAILED (CABIN) · airframe 32,982 hrs · 12,510 cycles

EMERGENCY LIGHT SYSTEM FAIL TO TEST. EPSU FAILURE. REPLACED EPSU 13WL. OPS CHECKED NORMALLY.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 32,012 hrs · 12,112 cycles

FWD EMERGENCY LIGHT POWER SUPPLY FAIL TEST PER 3 SVC.

Part: ACCUMULATOR — READS LOW (R2 DOOR) · airframe 31,943 hrs · 12,076 cycles

DOOR 2R EMERGENCY CYLINDER ACCUMULATOR PRESSURE LOW.

Part: COMPUTER — MALFUNCTIONED (FLT CONTROLS) · airframe 31,793 hrs · 12,013 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, - F-CTL. AIRCRAFT STARTED UNCOMMANDED FLIGHT MOVEMENT IN A DOWN PITCH BEFORE ECAM AND AFTER FAULT NO FURTHER UNCOMMANDED MOVEMENT. RESET ELAC2 AND PERFORMED GROUND SCAN- NO PROBLEMS NOTED, NO REPEATS SINCE ORIGINAL

Part: OIL SYSTEM — LEAKING (APU) · airframe 31,277 hrs · 11,818 cycles

CREW REPORT, 280 MILES FROM DESTINATION GOT BURNED AIR COND DUCT OR OVERHEAT ODOR FROM ROW 10 TO COCKPIT. APU OIL LEAKING INTO BLEED AIR SYSTEM. APU REMOVED AND REPLACED.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 31,005 hrs · 11,694 cycles

CABIN EMERGENCY LIGHT TEST FAILED. EPSU 115 VAC EMER L.

Part: SENSOR — MALFUNCTIONED (MLG STEERING) · airframe 30,520 hrs · 11,517 cycles

NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN WHILE ENROUTE. NEEDED TOW TO GATE. ON SUBSEQUENT FLIGHT HAD LOW LEVEL GREEN HYD INDICATION. TOW TO GATE ALSO NEEDED. [06-22-07] FAULT TRACING FOUND A WANDERING SIGNAL VOLTAGE FROM 4GC NOSE WHEEL STEERING FEEDBACK SENSOR. REPLACED FAULTY FEEDBACK SENSOR AND REPLACED 6GC NOSE WHEEL STEERING SERVO AS A PRECAUTION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,380 hrs · 10,405 cycles

FOUND EMERGENCY LIGHTS FAILED. REPLACED BATTERY AT LEFT OVERWING EXIT TEST OK PER 33-51-00.

Part: CONTROL BOX — FAILED (CABIN) · airframe 27,146 hrs · 10,326 cycles

DIVERTED FLIGHT DUE TO ELECTRICAL ODOR IN CABIN. FOUND SEAT ELECTRONICS BOX (SEB) AT SEAT 13 DEF BURNED UP ALONG WITH SEAT TO SEAT CABLE 13DEF TO 14 DEF.REPLACED CABLE AND SEB.ALSO FOUND SEB'S BAD AT 15DEF,16DEF,16ABC. PULLED 3 CB'S ON 2000VU PANEL FOR PES CENTER, RIGHT, & LEFT. COLLARED. PA WORKS FOR SAFETY VIDEO. IN REF TO LOG 1 FOUND SEB AT SEAT 13DEF BURNED UP. REPLACED SEB AT 13 DEF AND SEAT TO SEAT CABLE 13DEF TO 14DEF ALSO REPLACED WALL DISCONNECT BOX. OP CHKS OK.

Part: CONNECTOR — LOOSE (DOOR WARNING) · airframe 26,774 hrs · 10,169 cycles

AFT CARGO DOOR LIGHT DISPLAYED ON CLIMB-OUT. CHECKED THAT NO BAGGAGE LOOSE IN COMPARTMNT. LGCIU STANDARD 4D INSTALLED. CHECKED AFT CARGO DOOR CLOSED AND ALL LOCKS ENGAGED. FOUND AFT CARGO DOOR CONNECTOR LOOSE, SECURED AND OPTS NORMAL.

Part: EPSU — FAULTY (AFT LEFT) · airframe 26,216 hrs · 9,963 cycles

AFTER REPLACING BATTERY IN REAR EPSU, PTP TEST DISPLAYS *EPSU AFT L*. REPLACED POWER SUPPLY. TESTED THROUGH PTP AND GOT GREEN OK LIGHT AND TEST OK MESSAGE.

Part: BATTERY — FAULTY (EMERGNECY LIGHT) · airframe 25,145 hrs · 9,570 cycles

EMERGENCY LIGHT TEST FAULTS LEFT FWD BATTERY. REPLACED BATTERY.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 17,170 hrs · 6,534 cycles

AFT PIT FRAME 54L DAMAGED AT STR 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: VALVE — DEFECTIVE (R2 DOOR) · airframe 13,200 hrs · 4,819 cycles

DOOR 2R DOOR ASSIST BOTTLE PRESSURE OVER LIMIT AT 2100 PSI. FOUND SCHRADER SERVICE VALVE BAD. REPLACED VALVE AND SEAL. SERVICED AND CHECKED OK.

Part: HYDRAULIC SYSTEM — FAILED (YELLOW SYS) · airframe 10,841 hrs · 3,876 cycles

LANDED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 10,203 hrs · 3,622 cycles

OVERHEAD EMERGENCY LIGHTS REMAIN ON. REPLACED RT OVERWING POWER SUPPLY.

Part: WINDSHIELD — CRACKED (RT COCKPIT)

CRACKED RIGHT WINDSHIELD. *S/D* CAUSE OF CRACKED RIGHT WINDSHIELD WAS FOD AS THERE WAS NUMEROUS HITS ALONG LOWER EDGE.

Part: FMGC — MALFUNCTIONED (E & E COMPT)

AUTOPILOT DISENGAGED ON APPROACH ALONG WITH THE MAP NOT AVAIL FLAG ON THE CAPTAIN SIDE NAV DISPLAY. PFR SHOWS FAILURE MESSAGES FMGC2 AND FAC2. *S/D* THE POSTFLIGHT REPORT IDENTIFIED THE FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC) NR 2 AND FLIGHT AUGMENTATION COMPUTER (FAC) NR 2 AS THE POSSIBLE FAULTS. THE FMGC 1 AND 2 WERE RERACKED AND SWAPPED BETWEEN POSITIONS. NO FURTHER FAILURES HAVE OCCURED. THIS MAY BE RELATED TO THE SOFTWARE ANOMALIES IDENTIFIED BY SEXTANT, AIRBUS AND AD 97-21-10. AIRBUS HAS BEEN NOTIFIED OF THIS EVENT. ADDITIONALLY COA 403350/1 HAS BEEN GENERATED TO TERMINATE AD 97-21-10.

Part: DOOR — MISINSTALLED (EMER EXIT)

OVERWING EMERGENCY EXIT DOOR AIR LEAK. SEATS 9BC AND 10ABC NOT TO BE OCCUPIED DURING FLIGHT UNTIL REPAIRS ARE COMPLETE. FOUND DOOR INSTALLED INCORRECTLY WITH SEAL STUCK IN THE GAP BETWEEN THE DOOR AND FUSELAGE. DOOR WAS REINSTALLED CORRECTLY.