N463UA

Part: FUEL CAP — MISSING (WING) · airframe 76,394 hrs · 31,235 cycles

PDA 2 UNDERWING REFUEL CAP MISSING REPLACED REFUEL CAP PER AMM. 28-25-41PARTS USED: 31-2825-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1356663 SN OFF 2456 IPC REFERENCE # 28-25-41-02B

Part: IDG — LOW (NR 1) · airframe 75,302 hrs · 30,724 cycles

IDG 1 OIL LO PR DISPLAYED ON UPPER ECAM. MEL 2420E REQUESTED, VERIFIED #1 ENG GENERATOR IDG IS STATING (AUTOLAND LIMIT CAT 3 SINGLE) OTBD OF CAPTS PFD. #1 ENG IDG PLACED ON MEL 2420E, MEL DDP C/W. NOTE: PRIOR TO SERVICE, PYLON MOUNTED IDG CONNECTORS MUST BE VISUALLY INSPECTED AD2011-19-01 R1 REQUIREMENTS. C/W DAILY REQUIREMENTS REF MEL 2420E. DAILY REQUIREMENT CW DISCONNECTED, C/W LOAD SHED DDP, AND PLACED 44-0017 PLACARD CLEARING THIS DEFERRED ITEM AND RESTORING INOPERATIVE IDG TO FOR ARCING CONDITIONS (REF. AMM 24-21-43-210-048C1), REF TSM 24-20-00-810-847-A TO ASSIST, T/S NO DEFECTS NOTED. REMOVED ENG #1 IDG REF AMM TASK 24-21-51-000-010-A INSTALLED IDG FEEDER CABLES REF AMM 24-21-51. REQUIRES #1 ENGINE VERIFIED PARTS AND TORQUES OF IDG AND IDG FEEDER. INSPECTION BUYBACK FOR INSTALLATION TORQUE. CABLES,INSPECTED CABLES FOR DAMAGE AND ARCING, PER AMM 24-21-51 REPLACED ENG #1 IDG REF AMM 24-21-51. PERFORMED IDLE RUN LEAK TEST REF 71-00-00 TEST 3. NO LEAKS FOUND. PERFORMED OPS CHECK OF IDG REF AMM 24-21-00-720-042-A. NO FAULTS FOUND OK TO CONTINUE.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 74,633 hrs · 30,406 cycles

G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD DEBRIEFED CREW. CREW STATED THAT AFTER DEPLOYING GEAR, RECEIVED RH RETRACT ACTUATOR HOSE LEAK REMOVED AND REPLACED BOTH RH MLG DOOR ACTUATOR HYD GRN RSVR LO LVL ECAM. CREW CHECKED GREEN QTY INDICATION AND LINES..SERVICED GREEN SYSTEM. REF AMM 32-31-38..STILL NEED LEAK NOTED IT WAS EMPTY. LEAK COMINNG FROM RIGHT WHEEL WELL. GAUGE CK AND OPS CK. AND MORE CLEANING OF THE AREA. PARTS USED: SHOWS SYSTEM EMPTY. 18-3231-3-0081,QTY :1 CLEANED UP AREAS AROUND NEW HOSE REPLACEMENT, AND UNDER BELLY FUSELAGE. SERVICED GREEN HYDRAULIC LEVEL TO TOP. CYCLED GEAR DOORS EIGHT TIMES -- NO AVTIVE LEAKS NOTED. NO ECAM MSG NOTED.

Part: PROXIMITY SENSOR — UNKNOWN (L/G) · airframe 72,050 hrs · 29,190 cycles

SHOCK ABSORBER FAULT DISPLAYED ON UPPER ECAM SCREEN - L-G L/G SHOCK ABSORBER FAULT AT FL360. AP AND AUTOTHRUST LOST 3 MIN LATER. LIMITS. TARGETS ALSO OUT OF LIMITS AFT OF SENSORS. REPLACED BOTH SENSORS PRECAUTIONARY REF AMM TASK 32-31-73-400-005-A. ADJUSTED GAPS AND TARGET POSITION REF AMM TASK 32-31-73-820-006-A. SENSOR INDUCTANCE CHECKS GOOD REF AMM TASK 32-31-73-820-009-A. LOCKED LOG PAGE DUE TO HISTORY ASSOCIATED MESSAGE ''N LG SHOCK ABSORBER (2526GM)'' SHOWING W/BOTH NEED TO ACCOMPLISH LANDING GEAR BITE TEST REF AMM TASK LGCIU''S AS SOURCE. REF TSM 32-31-00-810-868-A, REFERS TO FAULT 32-69-00-740-001-A FOR REPLACEMENT OF SENSORS. SUGGEST SHOWING FOR ''NLG EXT PROX SNSR 24GA TGT POS''. REF TSM TASK ACCOMPLISH NLG STRUT SERVICE AND GEAR SWING DO TO RECENT HEAVY 32-31-00-810-842-A, FOUND 24GA AND 25GA TARGET GAP OUT OF VISIT. ADD EMP:101154 ITEM UNLOCKED FOR CLEARING ACTION ACCOMPLISHED NOSE GEAR SWING OPS CHECKED, SWITCHES OPERATED OK, NO MSGS NOTED. BITE CHECKED OK.

Part: SHOCK ABSORBER — UNKNOWN (LANDING GEAR) · airframe 72,050 hrs · 29,190 cycles

IN FLIGHT RECEIVEDL/G SHOCK ABSORBERFAULT. DIVERSION ON HVY MX CHK FERRY FLT. NLG SHOCK ABSORBER FAULT ON MM TASK 32-69-00-740-001-A) NO FAULTS. ALSO INSPECTED NLG FOR PFR (24GA). INSPECTED SENSOR AND FOUND CONNECTOR NOT COMPLETELY OBVIOUS DEFECTS, NONE NOTED. SEE PHOTO OF PFR, LLR, AND LGCIU''S LOCKED. CONNECTED SAME AND ALL FAULTS ERASED. CONNECTOR IS NOW LLR. ALL CKS NORMAL AND SYSTEMS RETURNED TO NORMAL. ACFT IS OK SECURELY LOCKED IN PLACE. PERF LGCIU BITE ON BOTH LGCIU''S, (REF FOR SERVICE.

Part: BATTERY PACK — NO TEST (13WL) · airframe 72,035 hrs · 29,182 cycles

EPSU BATTERY 13WL TEST FAILED, BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001232932-0010. ESPU BATT.(13WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (13WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:261409 QTY 1EA P/N:AD3214-31 S/N ON: 242257 QTY:1EA.

Part: BATTERY PACK — NO TEST (12WL) · airframe 72,035 hrs · 29,182 cycles

ESPU BATTERY (12WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001232931-0010. ESPU BATT.(12WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (12WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:252801 QTY 1EA P/N:AD3214-31 S/N ON: 278854 QTY:1EA.

Part: BATTERY PACK — NO TEST (10WL) · airframe 72,035 hrs · 29,182 cycles

EPSU BATTERY (10WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001232929-0010. ESPU BATTERY (10WL) FAILED ON EMERGENCY LIGHTING BATTERY P/N ON:AS3214-31 S/N ON:279092 QTY:1EA WORK ACCOMPLISHED CAPACITY TEST.BATTERY REPLACEMENT OF (10WL) PERFORMED IAW AMM: 5P1122 AND INSPECTED BY 5P0620. 33-51-38-000-002 REV.119 AND AMM:33-51-38-400-002 REV.119. TEST SATISFACTORY. P/N OFF:AD3214-31 S/N OFF:287045 QTY:1EA

Part: BATTERY — NO TEST (11WL) · airframe 72,035 hrs · 29,182 cycles

EPSU BATTERY (11WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001232930-0010. ESPU BATT.(11WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (11WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:242320 QTY: 1EA P/N:AD3214-3 S/N ON: 273851 QTY:1EA.

Part: SEAL — MISSING (AFT LT LWR WING) · airframe 71,815 hrs · 29,072 cycles

PDA 3, AFT LOWER LEFT WING TO BODY FAIRING MISSING SECTION OF SEAL LOWER SERFACE. REPAIRED DAMAGED SEAL PER ECRA 5335-01125. PARTS USED: 18-5335-3-0005.

Part: NONE — MISSING (FUEL CAP) · airframe 69,734 hrs · 28,044 cycles

PDA 3 OPS REPORTS FUEL CAP LANYARD MISSING WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSING PER CDL DISPATCH DESK: 21 NAME: AL DATE: 16-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. CDL 28A MAC RELATED WORK ORDER 000000003044366 AND PRTR WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSING PER CDL REPLACED DAMAGED CHAIN/ LANYARD AND REINSTALLED CAP REF AMM 28-25-41 OPS CK GOOD

Part: GENERATOR — FAILED (ENG 1) · airframe 68,904 hrs · 27,663 cycles

ELEC GEN 1 FAULT ON ECAM WITH NUMEROUS FAILURES UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECKED. WIRING OF THE DISCONECT IDG PER ASM 24-21-01 S 010-009, AND 24-21-51-400-040, PER FAILURE OF THE TDC AC SENSOR ACCPD TSM PERFORMED MSG ELEC GEN 1 FAULT REMAIN , OPEN MEL 2420E OK TO DEFER PER MEL . FOUND OPEN SOLENOID, REPLACED IDG ENG 1 PER AMM 24-21-51-000-040 24-22-00-810-809, REPLACED ENG OIL PRESS RELAY 7XT, AFTER WORK ROTABLE PARTS CHANGE WAS INDICATED - TT # 1111726 SN OFF 9167 ADD EMP:U230133 IPC REFERENCE # 24-21-51 APPROVED FOR MEL2420E ACCOMPLISHED INPECTION CHECK OF IDG REPLACEMENT, ALL STEEPS IAW AMM 24-21-51-000-040. ADDED IDG PLATE PICTURE SIDE OF ENG PYLON REF WD 24-22-01 PG 9, REQUIRES ADDITIONAL OPEN UP TO FURTHER EVAL DAMAGE CHECKED WIRING FROM IDG TO 9XU1 AND FOUND FEEDER T3 SHORTED TO GND, FURTHER T/S FOUND FEEDER CABLES BURNT AT 400VT1 AT GENERATOR, INTE OFF 31-2411-9-0001 9167 ON 31-2411-9-0001 0987 PYLON HARRNESS DG 200.REF AMM 24-21-43,AWM 24-22-01, AND ESPM 20-48-11. REPLACED 400VT1,RETERMINATED CABLES 2422-4504,2422-4505, AND 2422-4506,2422-4507 AT 400VT1.STILL REQUIRES REPLACEMENT OF IDG ADD EMP:U231871 REMOVED AND REPLACED #1 ENGINE IDG FEEDERS ON PYLON, REF AMM 24-92-00-400-001-A

Part: RADOME — NONE (RADOME AND WINDO) · airframe 68,156 hrs · 27,333 cycles

BIRD STRIKE ON CLIMB.8000AGL. 250KIAS.FLAPS UP. PIC ADDED CLEANED BIRD IMPACT AREA AT TOP OF RADOME AND CAPT WINDOW. PERFORMED BIRD STRIKE INSPECTION REF AMM 05-51-14-200-803-A. NO DAMAGE FOUND. OK TO CONTINUE.

Part: NONE — CRACKED (COCKPIT L3 WINDO) · airframe 67,994 hrs · 27,247 cycles

COCKPIT WINDOW L3 SHATTERED. 2 SEPERATE TIMES APPROX 14000MSL/26 00 CABIN ALT UP LOAD PHOTOS INFORMATION ONLY FOR L3 WINDOW INFORMATION ONLY BY CAPTAIN NO OVER WEIGHT LANDING. LANDING WAS REMOVED COCKPIT L3 WINDOW REF AMM 56-11-12-000-001-A WINDOW IN POSITION. ORDERED NEW SCREWS SINCE OLD SCREW HEADS INSTALLATION OF NEW WINDOW AMM 56-11-12-400-002-A THRU STEP 4A 1 NORMAL. TOO WORN TO ACHIEVE PROPER TORQUE. CONTINUED INSTALLATION OF L3 WINDOW FROM 56-11-12-000-001-A, STEP 4A1 TO END. OPERATIONAL CHECK GOOD. ADD EMP:U334021

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,555 hrs · 26,187 cycles

EMER EXIT LIGHT TEST GIVES MESSAGE OF ESPU BATTERY EMERGENCY LIGHT &ESPU BATTERY . RESET BOTH ESPUS, NO HELP. REPLACED THE BATTERY PACK FOR ESPU 11WL & 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A, OPS CHECKED OK. ACCOMPLISHED THE INSPECTION OF THE INSTALLATION OF BATTERY PACKS AT 11WL AND 12WL AND OPERATIONAL CHECK.

Part: SKIN — DAMAGED (RT WING) · airframe 62,419 hrs · 24,841 cycles

REF N/R 9024440, RT WING LOWER SURFACE CUTOUT PANEL 640LB FA STENER HOLES IN WING STRUCTURE DAMAGED MULTIPLE LOCATIONS REPAIRED DAMAGED FASTENER HOLES AT RT WING LOWER SURFACE CUTOUT PANEL 640LB IAW SRM 57-27-11-283-002 AND SRM 57-21-11-300-0 03. ACCOMPLISHED ROTO PROBE AND HFEC INSPECTION OF REWORKED HOLES AND ADJACENT AREA, NO CRACKS FOUND, IAW NTM 51-10-01 AND 5 1-10-03. REMOVED AND REPLACED GANG CHANNEL IAW SRM 51-42-11 AND SRM 57-21-11-300-003. THIS IS A CATEGORY "B" REPAIR I 57-21-11-205-037. CURRENT FH IS 62419/ FC 24841. H, SUBSEQUENT INSPECTIONS AT INTERVALS OF 1500 FC/3000 FH IAW SR INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT 16000 FC/32400 F PANEL 640LB INSTALLED ON CUSTOMER CARD ZONE 640 CLOSE SEQUENCE 2 267 APPROVED DIP FOR REPAIR TO PANEL 640LB FASTENER HOLES PER SRM 57-27-11-283-002 AND SRM 57-21-11-300-003. CAT B REPAIR REQUIRES REINSPECTIONS.

Part: UNKNOWN — MALFUNCTIONED (WASTE DISPOSAL) · airframe 62,419 hrs · 24,841 cycles

N/R 9023966 (A3NB-53-4-6179, A27-NO DOT) AFT CARGO WASTE SPILL, TOILET PAPER FOUND AT FRAME 63-65 STR 37-39 REMOVED AND INSTALLED INSULATION. CLEANED AFT CARGO WASTE SPILL IAW EC/RA 2011-01000 REV AA AND AMM 25-80-00-000-001-A, AMM 25-80-00-400-001-A, AMM 12-21-12-100-006-A.

Part: DOOR SILL — CORRODED (AFT CARGO DOOR) · airframe 62,419 hrs · 24,841 cycles

AFT CARGO, DOOR SILL TORSION BOX HAS COR ROSION AND DEEP PREVIOUS BLEND OUTS. AAR N/R S/N 9024001 REMOVED CORRODED AFT CARGO DOOR SILL TORSIONBOX IAW A320 SRM 51- TOR SION BOX IAW A320 SRM 51-46-11-001 REMOVED TO F.O.M. AND REI NSTALLED HORSE SHOE TOP PLATE IAW A320 SRM 51-42-11-001. INSTALL ED NEW AFT CARGODOOR SILL TORSION BOX COVER IAW A320 SRM ADD EMP:V919097 42-11-001. LOCATED DRILLED & COUTERSUNK NEW AFT CARGO DOOR SILL 1-001. 51-72-11-911-001. RESTORED PROTECTIVE COATING IAWA32 SRM 51-23-1

Part: DOOR SILL — CORRODED (R2) · airframe 62,419 hrs · 24,841 cycles

R-2 DOOR SILL HAS CORROSION AROUND AFT GIRT BAR FITTINGS. AAR NO NROUTINE 9024225 BLENDED AND REMOVED CORROSION IAW SRM 51-74-00. NO CORROS ION ALLOWED IN AREA I.A.W A320 53-41-14-283-002. REMOVED AND REPL ACED DOOR SILL IAW SRM 51-42-11 ON R2 DOOR

Part: DOOR SILL — CORRODED (L2 AREA) · airframe 62,419 hrs · 24,841 cycles

L-2 DOOR SILL HAS CORROSION AROUND AFT GIRT BAR FITTINGS. AAR NO NROUTINE 9024224 BLENDED AND REMOVED CORROSION I.A.W A320 SRM 51-74-00. NO CORROS ION ALLOWED I.A.W A320 SRM 53-41-14-283-002 REMOVED AND REPLACED DOOR SILL N L2 I.A.W A320 SRM 51-42-11

Part: OUTLET — UNKNOWN (SEAT 2F) · airframe 58,863 hrs · 23,272 cycles

SEAT 2F WHEN PAX HAD DEVICE PLUGGED IN, HAD AN ELECTRICAL ODOR. STOPPED WHEN UNPLUGGED, NO FAULT CONFIRMED, PLUGGED IN DEVICE. NO SMOKE COMING OUT. REMOVED OUTLET. VISUALLY INSPECTED HARNESS CONNECTION TO OUTLET. OUTLET CHECKED GOOD. WORK PERFORMED IAW AMM 25-21-89

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 56,918 hrs · 22,391 cycles

EMERGENCY LIGHTS TEST DISPLAYED EPSU BATTERY AFT LEFT RESET SYSTEM. OPS CKS GOOD.

Part: PIN — OUT OF POSITION (OVERWING EXIT) · airframe 56,336 hrs · 22,146 cycles

LEFT OVERWING EXIT DOES NOT SHOW ARMED USING RENDER CHECK LIST AND AMM 52-71-00-70-001-A FOUND LT FWD OVER WING EMERGENCY EXIT LATCH PIN OUT OF DETENT. PLACED PIN IN CORRECT POSITION IAW AMM. ALL INDICATIONS NORMAL.

Part: BATTERY — FAULTED (CABIN) · airframe 55,876 hrs · 21,961 cycles

EPSU FWD AND RT BATTERY FAULT LIGHT DURING TEST. REPLACED EMERGENCY BATTERIES PER AMM 33-51-38.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 55,518 hrs · 21,791 cycles

FLIGHT INCURRED YELLOW HYD SYSTEM LOW PRESSURE LIGHT ENROUTE. EMERGENCY DECLARED. REPLACED ORING ON MANIFOLD ASSY IPC 29-13-14-05A ITEM 40. LEAK CHECK AND ENG RUN GOOD.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,484 hrs · 18,781 cycles

EXTERIOR FUSELAGE SKIN HAS SCRATCH JUST BELOW AOA VANE MOUNT PLATE. BLENDED SCRATCH ON LT FUSELAGE SKIN, 6.5 INCHES FWD OF FRAME 24 ABOVE SKIN LAP AT STRINGER 28 IAW SRM 51-73-00 PARA F PG 5. HFEC REVEALED NO CRACK INDICATION.

Part: SENSOR — FAULTED (LANDING GEAR) · airframe 47,571 hrs · 18,428 cycles

LANDING GEAR SENSOR FAULT ON DESCENT.

Part: MODULATING VALVE — FAULTY (OIL SYSTEM) · airframe 46,996 hrs · 18,206 cycles

AIR EXCHANGER FAULT DISPLAYED ON UPPER ECAM SCREEN, AIR VLV CLOSED ENG 2. IAW TOMC SHUTDOWN ENGINE, RESET A05, Q40, Q07 & F01, NO HELP. REPLACED ACOC MODULATING VLV IAW AMM79-21-51401. TESTED SYS IAW AMM79-21-51-400-010-A PARA 5AB, ALL OPERATIONS & LEAK CHECKED NORMAL. REMOVED ACOC MODULATING VLV MR 79218 DID NOT HAVE A DASH, ONLY SN1384.

Part: RESERVOIR — OVERSERVICED (HYDRAULIC SYS) · airframe 46,679 hrs · 18,087 cycles

BLUE RESERVOIR LOW AIR PRESS DISPLAYED ON UPPER ECAM SCREEN. HYD BLUE SYS HYD RESERVOIR OVER SERVICED. DRAINED & REPLACED YELLOW HYD SYS RESERVOIR DRAIN VALVE, ON ACCOUNT OF STUCK OPEN WHEN DRAINING SYSTEM DUE TO OVER SERVICE.

Part: MOTOR — INOPERATIVE (WINDSHIELD WIPER) · airframe 46,683 hrs · 18,089 cycles

CAPTAIN`S WINDSHIELD WIPER INOPERATIVE. WIPER MOTOR PCN 565-9005 AMM 30-45-51. SWITCH PCN 565-0615, TSM 30-45-00-810-801. ADJUSTED CAPTAIN`S WIPER BLADE, CYCLED SEVERAL TIMES & OPERATIONS CHECKED NORMAL IAW AMM.

Part: CONNECTOR — BROKEN (WINDOW HEAT) · airframe 46,676 hrs · 18,085 cycles

RT WS HT COMPARTMENT 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 46,628 hrs · 18,065 cycles

RT WINDOW DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. REPLACED RT WHC 2DG2 IAW AMM, OPERATIONS CHECKED OKAY.

Part: CONNECTOR — DIRTY (WINDOW HEAT) · airframe 46,623 hrs · 18,064 cycles

RT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. CLEANED & RESET CONNECTOR ON WHC 2. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — BROKEN (WINDSHEAR) · airframe 46,628 hrs · 18,065 cycles

RT WS HT COMP 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.

Part: SLIDING WINDOW — FAULTY (R2) · airframe 45,512 hrs · 17,645 cycles

F/O`S SLIDING WINDOW HEATING INOPERATIVE. COLD SPOT ON FWD 1-3 OF WINDOW. RUNS VERTICALLY THE LENGTH OF WINDOW. CONDENSATION AS WELL. REPLACED WINDOW PANE, WINDOW HEAT TESTS OK.

Part: SCREW — LOOSE (CABIN) · airframe 45,361 hrs · 17,589 cycles

LOOSE SCREW ABOVE COCKPIT DOOR. REPLACED SCREW ON FWD UPPER LT CORNER ON FWD SIDE OF COCKPIT DOOR.

Part: COVER — MISSING (SWITCH) · airframe 45,233 hrs · 17,538 cycles

PLASTIC COVER OVER EMERGENCY LIGHT SWITCH ON AFT F/A PANEL MISSING. REPLACED EMERGENCY LIGHT SWITCH COVER. SAFE AND FUNCTIONAL.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 45,159 hrs · 17,512 cycles

PANEL AFT OF DOUBLE DRAINS ON FWD FUSELAGE L/E EXPOSED AND SCREW PULLING THRU-POS DELAMINATED. APPLIED SPEED TAPE IAW MT 53-00-02, PANEL MUST BE REPLACED WITHIN 300 HOURS.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 44,479 hrs · 17,252 cycles

1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. CREW COMMENTS: SMALL CREASE IN F/O WINDSHIELD IN DIRECT FIELD OF VISION THAT CAUSES SLIGHT DISTORTION. REMOVED AND REPLACED WINDSHIELD.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 44,448 hrs · 17,239 cycles

CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). SWAPPED CAPTS OXYGEN MASK SERIAL 94410 WITH SEC OBS SEC OBS MASK SER 71814 NOW IN CAPT POS PER TASK 35-12-41 PAGE BLOCK 0401. OPS CHECK TASK 23-51-00-710-004 -A AND TASK 35-12-41-710-001-A. OPS CHECK GOOD. PLACED SEC OBS SEAT ON DEFERRAL DF472. RPL- :REPLACED O2 MASK. OPS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,964 hrs · 17,037 cycles

CABIN EMERGENCY LIGHT CHECK FAILED ON 2 2SVC. REPLACED AFT EPSU BATTERY PER MM,TEST PASSED OPS CHECKS GOOD.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 43,964 hrs · 17,037 cycles

EMERGENCY LIGHT CHECK FAILED ON 2 2SVC. REPLACED AFT EPSU BATTERY, TEST PASSED. OPS CHECKED GOOD.

Part: BUTTON — INOPERATIVE (O2 MASK PTT) · airframe 43,869 hrs · 16,999 cycles

CAPTAIN'S O2 MASK PRESS TO TEST NOT WORKING. REPLACED CAPTAIN`S 02 BOX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,459 hrs · 16,837 cycles

FOUND ON NR 2 SERVICE LAV SMOKE CHECK, CALL LIGHT FOR LAV F DOES NOT ILLUMINATE (591RH6) ASM23-73-18. ALSO CIDS CLASS 3 FAULTS "PAX CALL LAMP LAV F" FAULTED. SWAPPED LAMPS WITH KNOWN GOOD LAMPS, NO HELP. FOUND WIRES BEHIND LIGHT ASSY NOT CONNECTED. SECURED CONNECTOR AND OP-CHECK SATSFACTORY.

Part: FASTENER — MISSING (FUSELAGE) · airframe 43,386 hrs · 16,809 cycles

FASTENER MISSING LEFT SIDE FUSELAGE NEAR TRAILING EDGE OF INBOARD FLAP. SAMC TEXT: PANEL 197BB. REPLACED FASTENER LEFT SIDE FUSELAGE AT BLUE HYD SERVICE PANEL.

Part: COMPUTER — FAULTY (SLAT SYSTEM) · airframe 43,155 hrs · 16,714 cycles

SLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL. REPLACED SFCC1 AND OP CHECK SATISFACTORY.

Part: REGULATOR VALVE — FAULTY (CARGO BAY) · airframe 43,106 hrs · 16,694 cycles

AFT CARGO MIX VALVE STAYS FULL COLD EVEN WITH TEMP CONTROL KNOB ROTATED TO FULL HOT. DEFFERED AFT CARGO HEAT HOT AIR PRESS REG VALVE. COMPLETED REQUIREMENTS OF MEL ITEM 2143B. REMOVED AND REPLACED AFT CARGO HEAT PRESS REG VALVE REF AMM 21-43-52, OPS CHECKS GOOD.

Part: BLOWOUT PANEL — UNSECURE (NR 1 PYLON) · airframe 43,077 hrs · 16,684 cycles

NR 1 OUTBOARD PYLON BLOW OUT PANEL 471BL FOUND OPEN AT ARRIVAL. INSPECTED DUCTS AND LEAK CHECKED OK.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,068 hrs · 16,679 cycles

CORROSION AT L2 DOOR THRESHOLD AT AFT INBOARD CORNER. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR PER SRM 53-41-14 FIG 201 ON NR 25483.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,068 hrs · 16,679 cycles

EXT FUSELAGE DENTED BETWEEN FR 23 AND 24 AND BETWEEN STR 42R AND 43R. FOUND OUT OF LIMITS. INSTALLED EXT DOUBLER PER SRM 53-11-11 FIG 104.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,068 hrs · 16,679 cycles

EXT FUSELAGE DENTED BETWEEN FR 21 AND 22 AND BETWEEN STR 22L AND 23L. MAJOR REPAIR ACCOMPLISHED: FOUND OUT OF LIMITS. INSTALLED EXT DOUBLER PER SRM.

Part: ATTACH FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 43,068 hrs · 16,679 cycles

LEFT WING SIDESTAY UPPER CARDAN ATTACH FITTING OUTBOARD LUG BORE HAS PITTING CORROSION. BUSHING REMOVED, BORE CLEANED AND BUSHING REPLACED PER SRM.

Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 43,068 hrs · 16,679 cycles

RIGHT WING SIDESTAY UPPER CARDAN ATTACH FITTING OUTBOARD LUG BORE HAS PITTING CORROSION. BUSHING REMOVED, BORE CLEANED, AND BUSHING REPLACED PER SRM.

Part: TRANSMITTER — FAILED (OIL PRESSURE) · airframe 42,604 hrs · 16,485 cycles

LT ENG OIL PRESSURE READS ALMOST FULL SCALE 298PSI ON TAKEOFF, NOTICED MOMENTARY FLUCTUATION. REMOVED AND REPLACED OIL PRESSURE TRANSMITER, PER MM 79-33-15-000-010-A 13,79-33-15-400-0 10-A 13.

Part: CONTROL UNIT — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 41,917 hrs · 16,211 cycles

L1 DOOR SLIDE SHOWS ARMED WITH DOOR OPEN, ECAM SLIDE MESSAGE ON, WITH DOOR OPEN AND IN DISARMED. REPLACED SDAC-1 PER TSM 52-11-00-810 -804. AND AMM 31-55-34-000-001 MESSAGE CLEARED. OPS CHECKED GOOD

Part: SDAC — MALFUNCTIONED (NR 1) · airframe 41,893 hrs · 16,199 cycles

DOOR 1L SLIDE SHOWS ARMED WITH DOOR OPEN. ECAM SLIDE MSG ON WITH DO OR OPEN AND IN DISARMED. REPLACED PROX SWITCH 4WN1 AND RELAY EO245-28AO, NO HELP. REPLACED 1WN1 SLIDE ARMED INDICATOR LIGHT. NO HELP. REPLACED SDAC-1 PER TSM, MESSAGE CLEARED. OPS CHECKS GOOD.

Part: OXYGEN BOTTLE — FAILED (AFT CABIN) · airframe 41,646 hrs · 16,089 cycles

OXYGEN BOTTLE MISSING, USED AT AFT CABIN, FWD CABIN FLIGHT ATTENDANT REPORTED THAT THE OXYGEN BOTTLE WAS FULL BUT FAILED TO PROVIDE OXYGEN TO PASSENGER. REPLACED OXYGEN BOTTLE AT AFT CABIN.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 41,356 hrs · 15,978 cycles

1ST OFFICER'S SLIDING WINDOW'S VISIBILITY IS IMPAIRED. CLEANED WINDOW FOR BETTER FLIGHT VISIBILITY, WINDOW WITHIN LIMITS. BUBBLES DO NOT IMPAIR FLIGHT VISIBILITY.

Part: VALVE — LEAKING (NR 2 ENGINE) · airframe 41,123 hrs · 15,886 cycles

NR 2 ENG FIRE LOOP A TB 450VT2 NEED OP CHECK AFTER SUPPORT BRACKT INSTALLATION. REPLACED BRACKET AND BURNDY BLOCK. NR 2 ENG STILL HAS "A" LOOP FAULT AFTER ENG START. FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FIRE LOOP, OPS CHECKS GOOD. MESSAGE RETURNED. REPLACED 4000WD1 AND 3WD2. CHKD OK ON ENG RUN AND BITE TEST. FAULT REOCCURED ON TAXI OUT. RING OUT ALL WIRING AND LOOPS ALL CHECK GOOD. WITH ENG BLEED ON FIRE LOOP 'A' FAULTING. WITH APU BLEED ON AND BOOST 1 SELECTED, NR 2 ENG FIRE LOOP 'A' FAULTS. LARGE LEAK FOUND AT OVERPRESSURE VALVE ON NR 2 ENG. REPLACED OVERPRESS VALVE, NO LEAKS. REPLACED FDU PER MM WITH APU BLEED ON, NO FIRE DET FAULTS. RAN ENG FOR 10 MIN WITH BLEED ON, NO FAULTS.

Part: FIRE LOOP — DEFECTIVE (NR 2 ENGINE) · airframe 41,104 hrs · 15,875 cycles

INTERMITTANT DISPLAY OF ECAM ENG 2 FIRE LOOP 'A' FAULT. REPLACED FIRE LOOP 4001WD2. REF AMM 26-12-17. OPS CHECKS GOOD REF. 26-12-00-710-00 1." REOPENED ON 03MAR12 FOR: MESSAGE RETURNED REPLACED LOOPS 4000WD1 & 3WD2, CHK'D OK ON ENG RUN.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 41,104 hrs · 15,875 cycles

FIRE LOOP 'A' FAULT DISPLAYED ON UPPER ECAM SCREEN. -ENG 2. SAMC TEXT: CREW COMPLIED WITH MEL, APPLIED DF STICKER: DEFERRED PER SAMC NO HARD FAULT. REPLACED FIRE LOOP 4001WD2 REF, AMM 26-12-17 OPS CHECKS GOOD. REF AMM26-12-00-710-001", REOPENED ON 03MAR12 FOR: MESSAGE RETURNED.

Part: FIRE LOOP — DEFECTIVE (NR 2 ENGINE) · airframe 41,104 hrs · 15,875 cycles

INTERMITTANT DISPLAY OF ECAM ENG2 FIRE LOOP 'A' FAULT. MEASURED RESISTANCE AT FDC 2 BTWN PIN J AND K, OHMS READ 1510, IS WITHIN LIMIT NEED MORE T-S TIME. NO HARD FAULT. VISUAL INSPECTION OF FIRE LOOPS CHECKS GOOD. REPLACED FIRE LOOP 4001WD2. OPS CHECKS GOOD.

Part: COMPUTER — FAULTED (E/E BAY) · airframe 40,988 hrs · 15,823 cycles

AVIONICS VENT FAULT, FLIGHT DIVERTED. REPLACED AVIONICS EQUIPMENT VENTILATION COMPUTER AND TESTED SEVERAL TIMES WITH NORMAL INDICATION.

Part: TRANSDUCER — FAILED (ELAC) · airframe 40,070 hrs · 15,397 cycles

ELAC FAULT. REPLACED CAPT'S ROLL SIDE STICK TRANSDUCER 4CE1 REF AMM AND COMPLETED REJECTION FOLLOW-UP #RFU224068.

Part: FITTING — FAILED (FUSELAGE) · airframe 40,060 hrs · 15,393 cycles

DURING REMOVAL OF AFT LAV MODULE, FOUND OVERHEAD TURNBUCKLE BRACKET SHEARED OFF. REPLACED OVERHEAD FITTING FOR AFT FWD LAV HOLD ROD.

Part: FLOORBEAM — CORRODED · airframe 40,060 hrs · 15,393 cycles

FLOORBEAM CORRODED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,044 hrs · 15,385 cycles

CABIN EMERGENCY LIGHTS FAILED TEST. SHOWS EPSU BATTERY FWD LT. REPLACED EPSU 10WL BATTERY PACK, OPS NORMAL.

Part: COMPUTER — MALFUNCTIONED (NR 1 ELAC) · airframe 40,042 hrs · 15,384 cycles

CYCLIC VERTICAL BUMPING-PITCHING FELT AT CRUISE. FLIGHT CONTROL SD SHOWED LT & RT AILERONS MOVING UP & DOWN IN UNISON WITH BUMPING. CONSULTED FMC ELAC 1-2 FAULT, IRREGULAR. TURNED OFF ELAC 1, AILERON MOVEMENT STOPPED. NO FURTHER OCCURRENCE OF BUMPING-PITCHING. PERFORM MM 27-14-00 P.601, AND 613.

Part: SMOKE DETECTOR — FAULTY (E&E BAY) · airframe 39,416 hrs · 15,113 cycles

AVIONICS SMOKE MSG APPEARED ON LANDING, PER CREW. REPLACED AVIONICS SMOKE DETECTOR 1WA PER MM. OPS NORMAL, MSG GONE.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 39,314 hrs · 15,071 cycles

FIRST OFFICER`S WINDSHIELD HEAT IS INOPERATIVE. REPLACED WHC NR 2 PER AMM. PERFORMED BITE TEST. CHECKED GOOD.

Part: SEAT — EXCESS PLAY (COCKPIT) · airframe 39,115 hrs · 14,970 cycles

F/O SEAT HAS EXCESSIVE PLAY IN PEDESTAL. REPLACED F/O'S SEAT ASSY, OP'S CHECK GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 38,164 hrs · 14,544 cycles

OUTER PANE SHATTERED ON 2L SLIDING WINDOW. REMOVED 2L SLIDING WINDOW PER MM. INSTALLED NEW PANEL IN WINDOW FRAME. COMPLETED WINDOW INSTALLATION IAW MM.

Part: DOOR — UNSECURE (FWD CABIN LAV) · airframe 36,721 hrs · 13,862 cycles

LAVATORY WASTE DOOR BENT OR WON'T OPEN-CLOSE FWD CAB LT LAV. FORWARD LAV DOOR WHICH HOLDS THE FIRE EXTINGUISHER FELL OFF. DOOR FALLS OFF BECAUSE THE HOLDER AT THE BOTTOM IS DAMAGED AND DOOR WILL NOT STAY IN PLACE SECURELY. NO TIME ORD. SECURED WITH SAFETY WIRE. SAFTIED LOWER HINGE POINT. DOOR OPERATES NORMALLY.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 36,168 hrs · 13,583 cycles

PACK AIR HAS STRONG SMELL. PACK AIR HAS STRONG SMELL REPEAT ITEM. THE OZONE FILTER IS MOST LIKELY BAD. NONE IN STOCK ORD. REPLACED APU AND RAN PACKS TO BURN OUT SMELL.

Part: SELECTOR VALVE — FAULTED (NLG STEERING) · airframe 35,432 hrs · 13,252 cycles

LOST NOSE WHEEL STEERING ON LANDING. RED ECAM MESSAGE WITH AUDIBLE DINGS FOR L/G GEAR NOT DOWN LOCKED, WENT AWAY AFTER 10 SEC THEN GOT \NOSE WHEEL STEERING FAULT. NEITHER TILLER HAD INPUT. STEERING DISCONNECT WAS NO HELP. REPLACED 19GA IAW MM. REPLACED SELECTOR VALVE 41GA AND TEST GOOD. REPLACED SAFETY VALVE 2629 GM AND TEST GOOD.

Part: VALVE — FAULTY (MLG) · airframe 35,357 hrs · 13,213 cycles

LGCIU FAULT. ON APPCH L/G DID NOT EXTEND ON FIRST ATTEMPT. HAS HISTORY. ACFT IS UP ON JACKS T-S'ING. NEED TO REPLACE PRIORITY VALVE. PRIORITY VALVE REPLACED. ACCOMPLISHED SUCCESSFUL LEAK CHECK. CYCLED GEAR SEVERAL TIMES, OPS OK. NO MESSAGES. ALSO CK'D FREE FALL EXTENSION PRECAUTIONARY. REPLACED BSCU. R & R NLG OPENING 2630G M SAFETY VALVE. WHILE ACFT ON JACKS ALL DOORS AND GEAR OPERATED NORMALLY WITH HYD POWER. REPLACED GREEN SYS LANDING GEAR SAFETY VALVE. 49 GA. VALVE REQUIRES OPS CK. T/S FOUND FAULT WITH NR 1 LGCIU, AND NLG DOOR ACT. REPLACED NR 1 LGCIU, CYCLED GEAR 10 TIMES NO FAULTS, ACP'D MANUAL EXTENSION 6 TIMES, EACH TIME SYS OPERATED NORMAL. REPLACED NLG DOOR ACTUATING CYLINDER.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,216 hrs · 13,148 cycles

FA'S HAD A BURNING ODOR IN AFT GALLEY AREA. NOW AFT GALLEY CHILLER MALFUNCTION LIGHT IS ON. CHECKED COFFEEMAKERS, COFFEE WARMERS, FLORESCENT LIGHTS (BALLASTS) OPERATING OK. NO ODOR DETECTED. DEACTIVATED CHILLER C31 (FWD CHILLER FOR AFT GALLEY COMPLEX). RAN CHILLER FOR SEVERAL HRS DID NOT SMELL OR NOTICE ANYTHING BURNING. NFF.

Part: SHAFT — CONTAMINATED (NR 2 LP) · airframe 34,864 hrs · 12,977 cycles

STRONG ODOR IN COCKPIT, RTFL. REMOVED NR 2 ENG INLET CONE AND FAIRING. FOUND OIL IN THE EXTENSION SHAFT. REPLACED BLIND CAP AND SEAL. NEED TO ACP PACK BURN OUT AND REPLACEMENT OF RECIRC FILTER. ACCMP'D PACK BURNOUT. RAN ENGINES AT CLIMB POWER FOR ABOUT 15 MINS. NO OIL SMELL NOTED.

Part: FAN — FAULTY (AVIONICS VENT EX) · airframe 34,558 hrs · 12,834 cycles

STRONG ELECTRIC BURNING ODOR DETECTED. REPLACED AVIONICS VENT EXT FAN 18HQ SYS. CFDS TEST CHECKED GOOD.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 34,469 hrs · 12,784 cycles

EMERGENCY LIGHT SWITCH COVER FELL OFF. SECURED SWITCH COVER.

Part: ELBOW — LEAKING (HYD SYSTEM) · airframe 34,040 hrs · 12,590 cycles

GREEN SYSTEM HYD LOSS. REPLACED RIGHT MLG DOOR HYD SWIVEL ELBOW FITTINGS ON DOOR ACTUATOR. REPLACED NR 1 ENG DRIVEN PUMP, REPLACED HP FILTER, REPLACED CASE DRAIN FILTER AND GREEN SYS MAIN FILTER. LEAK AND OPS CKS OKAY.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 33,637 hrs · 12,403 cycles

EMERGENCY LIGHT TEST FAILED FAULTING EPSU BATTERY EMERGENCY RIGHT AND LEFT SIDE. REPLACED RT BATTERY, OPS CHECKS NORMAL REPLACED LT POWER SUPPLY, OPS CHECKS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 28,361 hrs · 10,315 cycles

EMERGENCY AISLE LIGHT AT SEAT 18C IS MISSING LENS. REPLACED SEAT LIGHT. OP CHECKS OKAY.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 28,361 hrs · 10,315 cycles

EPSU INT LOAD EMER R MESSAGE AT CIDS DURING OPERATIONAL TEST OF EMERGENCY CABIN LIGHTS AND SIGN CK. FOUND EPSU FAILED. REPLACED RT O/W EPSU, CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,908 hrs · 10,159 cycles

ROW 21 EEL LIGHT INOP. SUPPLEMENTAL DATA UPDATE CAUSE, LAMP INOP. RELAMPED ASSY. OPS CHECKED NORMALLY.

Part: CONTROL PANEL — FAULTY (FIRE) · airframe 27,521 hrs · 10,019 cycles

APU FIRE BOTTLE DISCHARGE LIGHT IS ILLUMINATED BLOW OUT DISK IS INTACT LOW PRESSURE. FOUND APU FIRE TEST SWITCH INTERMITTENT STUCK, CAUSED APU BOTTLE DISCHARGE LIGHT PROBLEM. REPLACED ENG, APU FIRE PANEL (1WD) THEN OP-TEST NO FAULT.

Part: FILLER — LEAKING (OXYGEN SYSTEM) · airframe 27,405 hrs · 9,965 cycles

AIRCRAFT O2 LOW. SUPPLEMENTAL DATA UPDATE CAUSE: LEAKING FILL PORT ON CREW O2 SERVICING PANEL. REPLACED FILL PORT AND SERVICED CREW O2 TO FULL, NO LEAKS NOTED.

Part: OXYGEN SYSTEM — FAULTY (CREW O2) · airframe 27,059 hrs · 9,846 cycles

OXYGEN HIGH PRESSURE INDICATION AMBER ON DOOR-OXY SYSTEM ECAM. SERVICED CREW O2 SYSTEM, NO REPEATS.

Part: DRAIN — DEFECTIVE (FUSELAGE) · airframe 27,043 hrs · 9,839 cycles

FLIGHT DIVERTED DUE TO LOUD SQUEAL IN COCKPIT. PRESSURIZED A/C TO 5.7 PSI NO LEAKS, NO SQUEAL DUPLICATED. REPLACED THE FWD LOWER DRAIN. NO REPEATS SINCE ORIGINAL WRITE UP.

Part: B-NUT — LEAKING (OXYGEN SYS) · airframe 26,999 hrs · 9,825 cycles

CREW OXYGEN PRESSURE IS 1310 PSI ON ECAM. FOUND LEAKING B-NUT AT CAPT LOCATION. TIGHTENED B-NUT AND CHECKED ALL LOCATIONS IN COCKPIT. NO LEAKS NOTED. SERVICED 02 SYSTEM TO FULL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 26,131 hrs · 9,533 cycles

CABIN EMERGENCY LIGHT CHECK FAILED. 10-19-07 FOUND LT FWD POWER SUPPLY FAULTY. REPLACED LT FWD POWER SUPPLY.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 24,975 hrs · 9,120 cycles

RTFL DUE TO ALL 3 ZONES INDICATING 100F. *S/D* FAULTY ZONE TEMP CONTROLLER. REPLACED ZONE TEMP (150) CONTROLLER. SHOP FINDINGS: NO FAULT FOUND.

Part: HEATER — INOPERATIVE (COCKPIT WINDOW) · airframe 24,790 hrs · 9,053 cycles

LOWER FRONT SIDE OF CAPT SLIDING WINDOW HEAT INOP. WINDOW AREAS COLD AND FOGS UP LIMITING VISIBILITY. REPLACED NR 2 WINDOW

Part: OVEN — SMOKE (GALLEY) · airframe 23,254 hrs · 8,482 cycles

OVEN 105R11 WAS SMOKING IN FLT SHUT OFF POWER AND SMOKE STOPPED. REPLACED OVEN. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 21,943 hrs · 8,013 cycles

EMERGENCY LIGHTS FAILED TEST. MULTIPLE FWD AND RIGHT SIDE LIGHTS INOPERATIVE. REPLACED BATTERIES FOR 10WL, 12WL, AND TESTED OK.

Part: BLADES — FAILED (NR 2 COMPRESSOR) · airframe 21,680 hrs · 7,919 cycles

ENG 2 STALL. TRANSIENT STALL SHORT ECAM THEN ALL PARAMETERS NORMAL AT TOP OF DESCENT. NR 2 ENGINE S/N V10784 HAS ONE HPC 6TH STAGE BLADE MISSING 1/2 AMOUNT OF BLADE. ALL OTHER 6TH STAGE HPC BLADES HAVE NUMEROUS AMOUNTS OF DAMAGE AND MATERIAL LOSS. ENGINE FAILED COMPRESSOR STALL BORESCOPE. REMOVED ENGINE S/N V10784 FROM POSITION 2. INSTALLED ENGINE S/N V10171 AT POSITION 2. HPC DAMAGE CAUSED BY RELEASE OF LINER FOR THE R6 BLADES.

Part: CAP — DAMAGED (TORQUE BOX) · airframe 21,658 hrs · 7,907 cycles

AFT PIT THRESHOLD TORQUE BOX UPPER CAP DAMAGED AT AFT END IB CORNER. MAJOR REPAIR. REPLACED THRESHOLD COVER AND INSPECTED.

Part: EPSU — FAILED (CABIN) · airframe 21,539 hrs · 7,869 cycles

L FWD EPSU FAILED ON EMERGENCY LIGHT TEST. REPLACED EPSU AND BATTERY.

Part: SLIDE — DISLODGED (DOOR 1R) · airframe 21,388 hrs · 7,810 cycles

DOOR 1R SLIDE FELL OUT OF DOOR.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 20,154 hrs · 7,347 cycles

THE AFT CARGO PIT FLOOR CENTERLINE SUPPORT BEAM LOCATED JUST FWD OF FR56 HAS A HOLE DRILLED THRU THE UPPER CAP LEFT FLANGE. MAJOR REPAIR: INTERIM DOUBLER INSTALLED.

Part: TORQUE BOX — DAMAGED (FUSELAGE) · airframe 20,154 hrs · 7,347 cycles

THE AFT CARGO PIT THRESHOLD TORQUE BOX UPPER CAP AFT END INBOARD CORNER JUST FWD OF FR56 HAS A HOLE DRILLED THRU IT AND SEVERAL NICKS. MAJOR REPAIR: INTERIM REPAIR DOUBLER INSTALLED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,762 hrs · 3,954 cycles

EEL LIGHTS ARE OUT AT 6ABC AND 17ABC. REPLACED BAD EEL LIGHTS.

Part: CABLE — BURNED (ELECTRICAL) · airframe 9,266 hrs · 3,400 cycles

FLIGHT DIVERTED DUE TO SMOKE ODOR IN THE CABIN. FOUND PIN 'A' OF CONNECTOR 400VCA SEVERELY BURNED, ALONG WITH RECEPTICLE. REPLACED IDG POWER CABLE AND PYLON POWER CABLE.

Part: FAN — FAILED (E/E BAY) · airframe 8,052 hrs · 2,939 cycles

BURNING ELECTRICAL SMELL IN THE COCKPIT ACCOMPANIED BY AIRCRAFT VIBRATION. REPLACED AEVC BLOWER FAN, WHICH HAD EXPERIENCED BEARING FAILURE.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 7,064 hrs · 2,567 cycles

ABORTED TAKEOFF AT 90 KNOTS DUE TO AN AVIONICS VENT MESSAGE. THE AVIONIC EQUIPMENT COOLING COMPUTER WAS RESET AND THE AIRCRAFT FLEW FUTURE FLIGHTS WITH NO INCIDENCE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 2,551 hrs · 832 cycles

FWD LT EMERGENCY POWER SUPPLY UNIT, EMERGENCY LIGHT TEST FAILS. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY, TESTS OK.