N839UA

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 71,737 hrs · 32,101 cycles

DOOR 1L SLIDE GAUGE PRESSURE IN THE RED. BEGAN REMOVAL OF LEFT FWD ESCAPE SLIDE ASSY, REF AMM 25-62-44. REMOVED AND REPLACED 1L DOOR SLIDE IN REF WITH AMM 25-62-44. OK FOR SERVICE. COMPLIED WITH GMM 09-25-05 FOR REMOVAL AND INSTALLATION, NO DEFECTS NOTED COMPLIED WITH INSTALLATION REF AMM 25-62-44

Part: BATTERY — NO TEST (ZONE 200) · airframe 70,558 hrs · 31,482 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - BATTERY CAPACITY TEST SHOWING FAULT ON CIDS DISPLAY PANNEL. "EPSU COM AFT L". REMOVED AND REPLACED EPSU AFT L BATTERY PACK IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD.

Part: BATTERY — NO TEST (ZONE 200) · airframe 70,527 hrs · 31,470 cycles

OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FOUND FAULT EPSU BATTERY AFT LEFT REPLACED EPSU 13WL BATTERY PER AMM TASK 33-51-38-000/400-002-A. EMERGENCY LIGHTING TEST OK. NO FAULTS FOUND.PARTS USED: 18-3351-3-0001, QTY :1

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 70,275 hrs · 31,346 cycles

EMERGENCY LIGHT FAULTING 13WL POWER SUPPLY REMOVED AND REPLACED POWER SUPPLY PER REF AMM 33-51-38 OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 70,275 hrs · 31,346 cycles

EMERGENCY LIGHT FAULTING 12WL BATTERY REMOVED AND REPLACED EMERGENY POWER SUPPL BATTERY PER REF AMM 33-51-38. OPS CHECK GOOD.

Part: FUEL CAP — MISSING · airframe 69,783 hrs · 31,058 cycles

PDA 2 REF LG PG 9557478, FUEL CAP FOUND TO BE MISSING UPON ARRIVAL REF LG PG 9557478 FOR CDL IN REF REFUEL/DEFUEL CAP FOUND MISSING ADD EMP:U352788

Part: LAMP — MISSING (LANDING LIGHT) · airframe 69,055 hrs · 30,667 cycles

PDA 2 REF 8504124, RIGHT SIDE LANDING LIGHT IS MISSING. REF PDA CATEGORY CAT 2, ITEM REPORTED ON SDR AS REQUIRED, REF GMM 04-20-16.3.B.19. ITEM PLACED ON DEFERRAL ON ORIGINATING LOG.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 67,940 hrs · 30,076 cycles

HOT BRAKES ECAM AFTER DEPARTURE. LGCIU1 FAULTECAM AND REVERSER 1 INOPECAM. REMOVED AND REPLACED SWITCH LANDIND GEAR CONTROL LEVER. OPS CHK. GOOD. REF AMM 32-31-11-000/400-001-A. PARTS USED: 1681089,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1681089 SN OFF 2624 IPC REFERENCE # 32-31-08-01A UNIT, CONTROL I OFF 31-3231-9-0002 1605 ON 31-3231-9-0002 1959 UNIT, CONTROL I OFF 31-3231-9-0002 1605 ON 0000 REPLACED LGCIU1, REF AMM 32-31-71. INSTALL TEST AND BITE TEST O.K. NO MSGS. ALL RELATED CB CONFIRMED CLOSED. PARTS USED: 31-3231-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1770643 SN OFF 1605.

Part: SKIN — CONTAMINATED (LH ELEVATOR) · airframe 67,829 hrs · 30,024 cycles

WATER INGRESS WAS FOUND IN THE UPPER SKIN IN TWO SPOT ON LH ELEVATOR SEQ:690 EA 5520-01462 PREFORMED PERMANET REPAIR ON DAMAGE AREA OF LH ELEVATOR TOP SKIN ZONE 3. AS PER AIRBUS A320 SRM 55-21-11-300-005 REV147

Part: SKIN — DAMAGED (FUSELAGE, FR24) · airframe 67,829 hrs · 30,024 cycles

PSEVERAL PREVIOUS REWORK ON FUS SURF FR 24-30 STRG 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 PSEVERAL PREVIOUS REWORK WERE FOUND ON FUSELAGE SKIN FR 24-30 STGR 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 M 53-21-11-283-018 REV. 147. PERFORMED PERMANENT REPAIR DOUBLER N THRESHOLD AT 60,000FC / 120,000FH FROM THE TIME OF ADL/REPAIR 21-11-205-060 REV 147. CURRENT: 30,024FC / 67,828.54FH PER SRM 53-21-11-300-076 REV 147, REPAIR CATEGORY "B". INSPECTIO EMBODIMENT. SUBSEQUENT INSP INTERVALS AND METHOD TBD PER SRI 53- DEPTH OF REWORK HAS 30.9% OF NOMINAL MATERIAL THICKNESS, CLASSIF IED AS DAMAGE SIZE 2 WITH REPAIR CATEGORY "C" (TEMPORARY) PER SR PREVIOUS REWORK ON FUSELAGE SKIN BETWEEN FR27 - FR28 STGR 42RH - 43RH. DVI AND HFEC INSPECTED WITH NO FINDINGS.

Part: SKIN — UNKNOWN (FUSELAGE, FR24) · airframe 67,829 hrs · 30,024 cycles

PSEVERAL PREVIOUS REWORK WERE FOUND ON FUSELAGE SKIN FR 24-30 STGR 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 RM 53-21-11-283-018 REV. 147. PERFORMED PERMANENT REPAIR DOUBLER ON THRESHOLD AT 60,000FC / 120,000FH FROM THE TIME OF ADL/REPAIR -21-11-205-060 REV 147.CURRENT: 30,024FC / 67,828.54FH PER SRM 53-21-11-300-076 REV 147, REPAIR CATEGORY "B".INSPECTI EMBODIMENT. SUBSEQUENT INSP INTERVALS AND METHOD TBD PER SRI 53 DEPTH OF REWORK HAS 29.17% OF NOMINAL MATERIAL THICKNESS, CLASSI FIED AS DAMAGE SIZE 2 WITH REPAIR CATEGORY "C" (TEMPORARY) PER S PREVIOUS REWORK ON FUSELAGE SKIN BETWEEN FR24 - 24A STGR 42RH - 43RH. DVI AND HFEC INSPECTED WITH NO FINDINGS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,775 hrs · 29,997 cycles

CABIN/COCKPIT CREW BEGAN SMELLING FUMES OF UNKNOWN ORIGIN DURING DESCENTAFTR TURN ON ENG A/ICE. PERFORMED ENGINE RUN ON GATE AND CYCLED ANTI-ICE FOR SEVERAL MINUTES. NO ODOR WAS DETECTED IN CABIN OR FLIGHT DECK DURING SMOKE/ODOR INSPECTION PER AMM 05-51-10. FOLLOWING TSM 05-50-00-810-831-A INSPECTED APU ENGINE ONE INLET AND EXHAUST ENGINE TWO INLET AND EXHAUST BOTH PACK 1 AND 2 INLETS AND OUTLETS FOR SIGNS OF BIRD STRIKE NO BIRD STRIKE OR LEAKS NOTED. HYRDRAULIC SYSTEM INSPECTION NORMAL NO LEAKS ADD EMP:127243 RAN APU BLEED, ENGINE ONE AND ENGINE TWO , PACK 1 AND PACK 2 IN ISOLATION TO EACHOTHER NO DEFECTS NOTED AND NO ODOR IN FLIGHT DECK OR CABIN. INSPECTED GALLEY OVENS, COFFEE MAKERS, AND CABIN CONDITION NO ODORS NOTED. PERCAUTIONARY CHANGED BOTH RECIRCULATION FILTERS PER AMM 21-21-45 AND REPLACED AVIONIC VENTILATION FILTER PER 21-26-43 FOLLOWED TSM 05-50-00-810-831-A NO DEFECTS OR ODORS NOTED.

Part: UPLOCK — FAULTED (NLG DOOR) · airframe 67,608 hrs · 29,900 cycles

NOSE WHEEL DOOR DIDNOT FULLY RETRACTWITH GEAR RAISED.CYCLED GEAR 2 ADDITIONAL FLAGGED AS SDR ACCOMPLISHED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE LAND GEAR REF MM32-31-00-720-003-A. WHEN NOSE GEAR IS EXTENDED THE NOSE GEAR DOOR CLOSED INDICATION IS GREEN AND THE DOORS ARE CLOSED. WHEN THE NOSE LANDING GEAR IS RETRACTED, THE NOSE GEAR DOOR INDICATE AMBER INTRANSIT AND THE GEAR DOORS ARE CLOSED TIGHT. PHOTO IS WHEN THE GEAR IS RETRACTED AND THE GEAR DOORS ARE CLOSED. REPLACED NLG DOOR OPEN PROX SENSORS 36GA, 37GA, 38GA, 39GA REF AMM 32-31-73-000-005-A/32-31-73-400-005-A. ACP ADJUSTMENT OF PROX SENSORS REF AMM 32-31-73-200-002-A. NLG PROX SENSORS REQ BITE CHECK REF AMM 32-69-00-740-001-A. REMOVED AND REPLACED NOSE LANDING GEAR DOOR UPLOCK ASSY REF AMM 32-31-14-400-001-A UP TO STEP 4H PARTS USED: 40-0594-3-1310,QTY :1 31-3231-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1763550 SN OFF 1786 UPLOCK, ASSY, N OFF 31-3231-9-0001 1786 ON 31-3231-9-0001 8830 UPLOCK, ASSY, N OFF 31-3231-9-0001 1786 ON 0000 COMPLETED INSTALLATION OF NLG UPLOCK ASSY REF MM 32-31-14-400-001-A. ADJUSTED NLG MAIN DOOR CONTROL RODS REF MM32-31-41-400-001-A. ACCOMPLISHED 3 NORMAL EXTENTION AND RETRACTIONS OF THE NLG REF MM32-31-00-720-003-A. ALL NLG AND NLG ADD EMP:U026455 DOOR INDICATION NORMAL. PARTS USED: 00-0609-3-9664,QTY :1

Part: COMPRESSOR — FUMES (ENG #1) · airframe 66,644 hrs · 29,383 cycles

UPON TAKEOFF STRONGFUMES THROUGHOUTCABIN. NO SMOKE OR HAZEFUMES CAME AND WENT REF TSM TASK 71-00-00-810-801-A PARAGRAPH 4 FAULT ISOLATION, COMPLETED UP TO 4.J. ( BLIND CAP SEAL REPLACED ON LOG 4675692) . CONTINUE WITH BORESCOPE OF LP COMPRESSOR. REF TSM TASK 71-00-00-810-801 STEP 4 (A) UP TO AND INCLUDING G #1 ENG REFREF TSM TASK 71-00-00-810-801-A PARAGRAPH 4 FAULT (2) NO LEAKS NOTED ISOLATION,SEE ADDITIONAL LOG FOR PARA 4 H (1)(A) . COMPLETED ADD EMP:U386016,U397484 PARA J 1 AND 2 BORESCOPE, NO WETNESS FOUND . CONTINUE WITH STEP K ADD EMP:U118014 COMPLETED TSM 71-00-00-810-801-A PARA 4 STEP K. #1 ENGINE. SEE LOGS 4745082 , 4748197 FOR FURTHER TROUBLESHOOTING REF TSM TASK 05-50-00-810-831-A

Part: O-RING — CUT (WHEEL WELL) · airframe 66,330 hrs · 29,227 cycles

CREW REPORTED ECAM MSGS HYD B SYS LO PR AND HYD B RSVR LO LEVEL HYD PAGE SHOWING LOW LEVEL ON BLUE SYS. REFER TO L/P 4377610. WORK HAS BEEN COMPLIED. FOUND O-RING IN PRESSURE SWITCH ABOVE MANIFOLD BEHIND LEFT GEAR DOOR HANDLE PANEL LEAKING HYDRAULIC FLUID. REPLACED O-RING AND INNSTALLED PRESSURE SWITCH IN REFERENCE WITH AMM 29-12-17-400-001A. OPS CHECK PASSED NO LEAK NOTED AT THIS TIME. HYDRALIC SERVICED.

Part: THRUST REVERSER — FAULTED (ENG 1) · airframe 65,997 hrs · 29,067 cycles

FLIGHT CREW RETURNED TO FIELD FOR INFLIGHT "ENG 1 REVERSER FAULT" ECAM MSG INTERMITTANT THEY STATED STARTED FAULTING AT ABOUT 2000FT REF ATTACHED PICTURES FOR FAULTS AND T/S CONNECTORS J10 AND J4. NO DEFECTS NOTED. REF WDM 71-51-11. ACCOMPLISHED PREVIOUS LEG REPORT THRU THE MCDU AND FOUND REV PERFORMED OPERATIONAL TEST OF FADEC WITH CFDS. COULD NOT DUE TO REMOVAL OF CONNECTOR J4 AND J10 LAND VERIFY TEST IDT LDVT CHA/HC/EEC1 FAULT, FOUND TSM TASK 78-30-00-810-837-B FOR DUPLICATE FAULT BOTH CHANNELS 1A AND 1B . REF FIM REQUIRED. THIS FAULT SUGGEST ACCOMPLISHMENT OF THIS TASK 78-30-00-810-837-B PERFORMED TEST OF EIU . TEST NORMAL . REF AMM 73-22-00-810-801-A. INSPECTED CONTACTS AND PINS AT 4000VC(SEE BEFORE/AFTER PICS)VERIFIED RESISTANCE GOOD NOW. ALL OTHER WIRING CKD GOOD BETWEEN EEC AND HCU AND ACTRS. EEC CONNECTRS DISTURBED WERE J1,J3,J4,J7,J9&J10. ALL CONNECTRS REINSTALLED. COMPLETED IDT INSPECTION OF #1 ENGINE EEC CONNECTIONS DISTURBED FOR MAINTENANCE. EEC NOT REMOVED OR REPLACED. COMPLETED IAW GMM 9-10-05 REF SSM 73-25-16SCH16PG4 T/S AND FOUND HIGH RESISTANCE BETWEEN LEFT UPPER ACTR 4004KS PIN4 AND EEC J4 PIN . FURTHER T/S FOUND CONNECTOR 4000VC WAS COCKED/CROSSTHREADED, REMOVED AND INSPECTED CONNECTR FINDING NO DAMAGE TO PINS OR CONNECTOR,REINSTALLED ACCOMPLISHED FADEC SELF TEST REF. AMM TASK 73-22-00-710-040-A AND FADEC REVERSER TEST REF. AMM TASK 78-31-00-710-041-A TEST 3 TIMES EACH ON CHANNEL 1A AND CHANNEL 1B. NO FAULTS DETECTED. ACCOMPLISHED CAT III. TEST PA

Part: INTERCOSTAL — CRACKED (HOLE #3) · airframe 64,397 hrs · 28,245 cycles

RH FR16 DOOR STOP #7 LWR/IB HOLE #3 CRACK INDICATION NOTED AT 9 O''CLOCK POSITION (MARKED). GENERATED BY V913792 ON HAECO LCQ NR 9292306/22306 REMOVED AND REPLACED FR16 DOOR STOP #7 INTERCOSTAL IAW AIRBUS DR AWING R53113118 REV F. ACMP BY MECH V077956 INSP BY V892443

Part: SKIN — DENTED (FR54) · airframe 64,397 hrs · 28,245 cycles

FUSELAGE SKIN AT FR54 STR 23L HAS 2 EA DENTS ON HAECO LCQ REF 92 92057/22057 SPEC A3NB-53-4-6230. NR GENERATED BY V079881 0-11-300-047. CUT OUT DIM 3 X 4 INCH FILLER THKNS .063 DOUBLER D OF ADL REP EMBMNT AT 24100 FLT CYC / 48200 FLT HRS, SUBSQNT INSP 3-00-11-205-044 TABLE 1 FIG 1. IM 9 X 9.7 INCH .071 THKNS. REP IS CAT B INSP THRSHLD FROM TIME 5000 FLT CYC / 10000 FLT HRS INSP MTHD ULTRSNC / HFEC IAW SRI 5 PERFORMED LIMITED CUT OUT DOUBLER REPAIR AT FR 54, 2.5 INCH BELO W STR 23L REF SRM 53-41-11-14-B PG 40 FIG 13 CODE C IAW SRM 53-0 OK TO DIP FOR REINSPECT FROM TIMEOF REPAIR EMBMNT AT 24100 TOMC-APPROVAL FROM SC1ELBYC COMMENT FLT CYC / 48200 FLT HRS, SUBSQNT INSP 5000 FLT CYC / 10000 FLT HRS INSP MTHD ULTRSNC / HFEC IAW SRI 53-00-11-205-044 TABLE 1 FIG 1. REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: COMPUTER — MALFUNCTIONED (NR 3) · airframe 60,533 hrs · 26,328 cycles

GROUND SPOILER 1 AND 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL FOUND F/CTL GROUND SPOILER 1 & 2 FAULT DISPLAYED ON UPPER ECAM. PRINTED PFR, FOUND THE SAME WARNING MESSAGE, AND SEC3 OR INPUT OF L THROTTLE CTL UNIT 8KS1 FAILURE MESSAGE. TROUBLESHOT PER TSM 27-60-00-810-805. BITE EFCS, PER AMM 27-96-00-740-001, NO FAULT NOTED. WAS GOING TO REPLACE SEC3 FOR TROUBLESHOOTING, BUT RAN OUT OF TIME. PERFORMED TSM 27-6-00-81-805-A. REPLACED SEC 3, REF AMM 27-94-34. OPERATIONS CHECK GOOD, REF AMM 27-94-00-710-001-A.

Part: SEAL — DAMAGED (LT PYLON) · airframe 58,196 hrs · 25,196 cycles

PDA 2 LEFT ENG INBD T-R TO PYLON FLEX SEAL SEGMENT MISSING AND CRACKED - THIRD FLEX SEA FROM AFT - MISSING SEGMENT MEASURES 4IN BY 3IN. IT IS ITEM 90 ON FIG 3 OF ECRA 5450-02357 REV-B. PERFORMED INTERIM REPAIR PER PART 1D OF ECRA 5450-02357 REV-B. ISSUE DIP TO ACCOMPLISH VISUAL INSPECTIONPER PART 2A ONCE EVERY FLIGHT CYCLE & PERMAMNENT REPAIR PER PART 3 WITHIN 50 FLIGHT HRS.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 54,895 hrs · 23,462 cycles

AFTER TAKEOFF, THE OVEN CIRCUIT BREAKER TRIPPED. FA REPORTED A BURNING ODOR AND THAT THE OVEN WAS GETTING HOT. REMOVED THE OVEN NO FAULTS NOTED, WIRE INSPECTION ACCOMPLISHED, CONTROL PANEL INSPECTION ACCOMPLISHED, REMOVED AND REPLACED THE OVEN, OPS CHECKED GOOD IAW AMM 25-35-19.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,502 hrs · 23,271 cycles

EMERGENCY LIGHT LENS MISSING AT ROWS 26ABC AND 32ABC. INSTALLED A NEW LENS. OK FOR SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 54,453 hrs · 23,243 cycles

EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN ARMED ON BATTERY POWER, WITH NO POWER ON ACFT. PERFORMED AN OPS TEST OF THE EMERGENCY LIGHTS IAW 33-51-00-710-00 1-A. GROUND CHECKED NORMAL

Part: DOOR SILL — CORRODED (L2 DOORWAY) · airframe 54,247 hrs · 23,144 cycles

L2 DOOR SILL FRAME 68 GIRT BAR PLATE FASTNER HOLES CORRODED. REMOVED CORROSION ON L2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-283-002, INSTALLED A NEW DOOR SILL IAW SRM 51-42-11-001, AND 51-72-11-001,

Part: BLANKING PLATE — CORRODED (2R DOOR SILL) · airframe 54,247 hrs · 23,144 cycles

R2 DOOR SILL CORRODED UNDER AFT GIRT BAR BLANKING PLATE. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-42-11-001, PARA . 2E & 2F,

Part: SUPPORT — CORRODED (FRAMES 69-70) · airframe 54,247 hrs · 23,144 cycles

SUPPORT TASK, LT FR69 - FR70, SUPPORT FRAME UNDER SHEAR WEB CORROSION. REMOVED AND REPLACED LT FR69-70 FRAME SUPPORT IAW SRM 51- 42-11-001.

Part: UNKNOWN — ODOR (FWD LAVATORY) · airframe 52,411 hrs · 22,194 cycles

F/A REPORTED A SLIGHT OVERHEAT BURNING ODOR IN FWD LAVATORY. NO SMOKE OR FUMES DETECTED. INSPECTED THE FWD LAVATORY, UNDER SINK AREA. NO BURNING ODORS NOTED. OK FOR SRVICE.

Part: LINE — UNSECURE (APU) · airframe 51,873 hrs · 21,921 cycles

MUSTY ALMOST METALLIC SMELL NOTED IN DESCENT. SUSPECT SOMETHING LEAKING INTO BLEED SYSTEM. TROUBLESHOT SMELL TO APU BLEED. FOUND OIL SCAVENGE LINES TO AFT BEARING ON APU LEAKING OIL. SECURED LINES AND CLEANED AREA. RAN APU AND PACKS TILL SMELL DISSIPATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 50,388 hrs · 21,088 cycles

EPSU UNIT AFT L MESSAGE PRESENT AFTER ACCOMPLISHING CABIN OPS TEST. CYCLED CIDS 1&2 CB'S, RESET CIDS. RETEST OPS, ALL NORMAL

Part: STRUT — DEFECTIVE · airframe 48,607 hrs · 20,181 cycles

ABORTED TAKEOFF, POSSIBLE COMPRESSOR STALL, UNUSUAL NOISE. EDM DOES NOT CONFIRM A STALL OCCURRED. POWER ASSURANCE RUNS ACCOMPLISHED. LT & RT LOWER STRUT ASSEMBLIES REPLACED.

Part: SWITCH — UNSECURE (ANTI-ICE SYS) · airframe 43,504 hrs · 17,794 cycles

ENG 1 ANTI ICE SWITCH KEEPS FALLING OUT OF SOCKET. REPLACED NR 1 ENG ANTI ICE SWITCH & RAN ENG ALL NORMAL.

Part: LINKAGE — LACK OF LUBE (CABIN) · airframe 43,485 hrs · 17,788 cycles

RT AFT SLIDE INDICATION INOPERATIVE ON DOOR OXY SYS ECAM PAGE DOOR OXY PROG. LUBED LINKAGE A FROM ARM HANDLE, OPERATIONS CHECKED NORMAL NUMEROUS TIMES.

Part: SCREW — LOOSE (NR 2 PYLON) · airframe 43,360 hrs · 17,733 cycles

SCREW ON OUTSIDE OF NR 2 ENG PYLON STICKING OUT. PROBABLY SAME SCREW AS YESTERDAY. SECURED STICKING OUT FASTENER. COULD NOT ASCERTAIN CONDITION OF THIS FASTENER YESTERDAY.

Part: CABLE — FAULTY (R2 DOOR) · airframe 43,351 hrs · 17,728 cycles

EXIT DOOR 2R ARMING HANDLE DIFFICULT TO MOVE, FULLY OPERABLE. REPLACED DOOR 2R ARM FLEXIBLE CONTROL CABLE.

Part: COVER — MISSING (FLAP TRACK) · airframe 43,124 hrs · 17,637 cycles

NR 2 FLAP TRACK MISSING BOLT COVER. INSTALLED BOLT COVER AT FLAP NR 2 ALL OK.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 43,008 hrs · 17,580 cycles

CAPTAIN`S PFD BLANK. REPLACED CAPTAIN`S PFD & TESTED OK IAW AMM.

Part: SEALANT — MISSING (NR 2 ENGINE) · airframe 42,383 hrs · 17,310 cycles

ENGINE 2 TRIM SEALANT LOOSE & PROTRUDING. ENGINE 2 CNA HAS MISSING SEALANT RIGHT HAND SEALANT PLATE 6 O'CLOCK. IAW IPC 78-11-09-81 ITM #100. ACCOMPLISHED INTERIM REPAIR IAW ECRA 7811-01201.

Part: UNKNOWN — NOISE (CABIN) · airframe 41,944 hrs · 17,106 cycles

LOUD HUM OR SQUEAL OVERHEAD IN AFT ROWS AND LT AND RIGHT NR 2 DOORS. ONLY OCCURS BELOW 10,000 FT. INSPECTED DOOR SEALS, WI- FI ANTENNA POD SEALS, AFT VHF ANTENNA SEAL, OUTFLOW VALVE OPERATION. NO DAMAGE NOTED TO SEALS. OUTFLOW OPS NORMAL. PERFORMED GENERAL VISUAL INSPECTION OF GALLEY AREA AND OUTSIDE OF ACFT. NO ABNORMALITIES NOTED.

Part: TIRE — OUT OF ROUND (RT NLG) · airframe 41,921 hrs · 17,095 cycles

NOSE WHEELS HAVE EXCESSIVE VIBRATION DURING TAKEOFF. FOUND RT NOSE TIRE OUT OF ROUND, REPLACED IAW AMM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 41,660 hrs · 16,984 cycles

ON CLIMB AT FL200 RECEIVED CABIN PRESSURE EXCESSIVE CABIN ALT MESSAGE. REPORTED BY THE CREW. OUTFLOW VALVE CONNECTOR 1OHLA BACK SHELL BROKEN. REPLACED OUTFLOW VALVE. REPLACED BACKSHELL.

Part: FLOORBEAM — CRACKED (AFT CARGO BAY) · airframe 41,550 hrs · 16,943 cycles

AFT CARGO FLOORBEAM SECTION ABOVE FRAME 56 FOUND CRACKED. REPAIRED.

Part: IGNITER — ARCED (NR 1 ENGINE) · airframe 40,670 hrs · 16,573 cycles

CREW REPORTED NR 1 ENGINE DID NOT START USING THE "A' SYSTEM. FOUND ARCING INSIDE A IGNITOR. REPLACED IGNITOR AND LEAD. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (NR 1 ENGINE) · airframe 40,023 hrs · 16,294 cycles

ENGINE 1 SLOW TO SPOOL FROM IDLE ON TAKEOFF LAGS RIGHT BY 5 SECONDS. SAMC TEXT: CHECK ENGINE ACCELERATION AND DECEL PER JRH 2-40-64. IF FAULT CONFIRMED REF TSM 73-00-00-810-880. MAINT TEXT: PER CREW VERBAL: HAPPENED TWO LEGS IN A ROW, LAST TAKEOFF ENGINE POWER ON ACCELERATION UNBALANCED. PERFORMED HIGH POWER RUN PER JRH 2-40-64 ACCEL DECEL TEST. ACC TIME 7.0 SEC. TABLE ALLOWS 6.2 SECONDS. DECEL TIME 12 SECONDS. TABLE ALLOWS 7.0 SECONDS.

Part: BLADE — OUT OF TOLERANCE (NR 2 ENGINE) · airframe 39,805 hrs · 16,193 cycles

ENG2 FAN BLADE CHG OUT OF TIME. BLADE REPLACED AFTER BLADE DISTRIBUTION PERFORMED. ACP VIB SURVEY AND VIBS WERE WITHIN LIMITS.

Part: COMPUTER — FAULTY (NR 2) · airframe 39,697 hrs · 16,140 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL REPLACED ELAC 2.

Part: APPU — FAILED (TE FLAPS) · airframe 39,202 hrs · 15,928 cycles

CREW REPORTS FLAP LOCKED ON APPROACH, SLATS DEPLOYED NORMALLY. SUPPLEMENTAL DATA, APPU SHOWS APPROX 6 PLUS DEGREES LEFT AND LESS THAN 1 DEGREE RIGHT. NO FLAP TORQUE LIMITERS TRIPPED, LT FLAPS ARE MORE EXTENDED THAN RIGHT. REPLACED MISSING HARDWARE AND ACCOMPLISHED TORQUE SHAFT INSTALLATION IAW AMM. OPS CHECKED NORMAL. VISUALLY INSPECTED TORQUE SHAFT AND COUPLER, NO DAMAGE NOTED. DUE TO LT FLAP APPU OUT OF ADJUSTMENT IT REQUIRES CHANGING. REPLACED LT FLAP APPU. ALSO, ACCOMPLISHED ADJ OF APPU 29CV IAW AMM, OPS CHECKS NORMAL. NO FURTHER FAULTS.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,655 hrs · 13,074 cycles

CABIN EMERGENCY LIGHTS COME ON WHEN EXTERNAL POWER IS REMOVED FROM ACFT. TROUBLESHOT ITEM TO AFT F/A PANEL. REPLACED AFT F/A PANEL, EMERGENCY LIGHTS FUNCTION GOOD. SWITCH POWER BACK AND FORTH FROM APU AND EXTERNAL POWER AND LIGHT FUNCTION WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,646 hrs · 13,069 cycles

EMERGENCY LIGHTS COME ON IN CABIN WHEN AC POWER OFF AND EMERGENCY LIGHT SW OFF. REPLACED POWER SUPPLY AND BATTERY AT SIDEWALL 11A. ACP EMERGENCY LIGHTS TEST AND SYS OPS CHECKS NORMAL.

Part: GUARD — MISSING (CONTROL PANEL) · airframe 32,635 hrs · 13,065 cycles

EMERGENCY SWITCH AT DOOR 2L MISSING PROTECTIVE GUARD. REPLACED AFT CIDS CONTROL PANEL, TESTED OKAY.

Part: HEATER — FAULTY (COCKPIT WINDOW) · airframe 30,860 hrs · 12,254 cycles

CAPTAIN'S SLIDING WINDOW HEATING INOP. CREW COMMENTS: COLD SPOT ON LOWER FRONT CORNER. REPLACED CAPTAINS SLIDING WINDOW PANEL IAW MM. (FINAL TORQUE WAS ACCOMPLISHED) NEEDS TO BE ACCOMPLISHED TO END OF MM. COMPLETED INSTALLATION OF CAPT'S SLIDING WINDOW.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 26,069 hrs · 10,124 cycles

EXIT PATH LIGHT COVER MISSING ON SEAT 1B.

Part: ADIRU — MALFUNCTIONED (E&E BAY) · airframe 25,816 hrs · 10,023 cycles

FLIGHT CONTROL ALTERNATE LAW, RTFL. *S/D* RERACKED AND SECURED ALL THREE ADIRU-S IN RADIO RACK. ACCOMPLISHED TSM TASK 34-13-00-810-967 AND ACCOMPLISHED BITE TESTS OF ADIRU-S PER AMM 34-13-00 ALL GRD TESTED OK, NO FAULTS. ACCOMPLISHED AFS AND LAND TEST PER AMM 22-97-00. SYSTEM GRD TESTED NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 25,815 hrs · 10,021 cycles

CABIN EMERGENCY LIGHT OUT AT SEAT 23C. *S/D* SECURED CONNECTOR TO LIGHT, OPS OKAY.

Part: LIGHT — BURNED OUT (SEAT 20ABC) · airframe 24,189 hrs · 9,397 cycles

EMERGENCY PATH LIGHTING AT SEAT 20ABC BULB BURNT OUT. REPLACED LIGHT ASSEMBLY.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 23,961 hrs · 9,315 cycles

ELECTRICAL SMELL EMANATING FROM THE AFT GALLEY. UNKNOWN (POSSIBLE SHORT WITHIN COFFEE MAKER). REPLACED COFFEEMAKER AND OPS CHECKED OK, NO SMELL, NO REPEATS.

Part: DEOILER — LEAKING (NR 2 ENGINE) · airframe 21,482 hrs · 8,343 cycles

NR 2 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND NR 2 ENG DEOILER OVERBOARD AIR DRIPPING OIL AT A RATE OF 40 DROPS-MIN AT ABOVE IDLE SPEED. REPLACED DEOILER SEAL AND BREATHER TUBE PACKING.

Part: FIRE DETECTOR — FAULTY (NR 1 NACELLE) · airframe 21,469 hrs · 8,340 cycles

FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN - ENG 1. REPLACED NR 1 ENG FIRE DETECTOR UNIT AS PRECAUTION. COULD NOT DUPLICATE FIRE WARNING SIGNAL.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 21,432 hrs · 8,326 cycles

RT IB SEAT TRACK BETWEEN FRAME 42 -47 HAS WORN AREAS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 21,432 hrs · 8,326 cycles

LT OB SEAT TRACK BETWEEN FRAME 42 AND 47 HAS WORN AREAS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM.

Part: PLATE — CORRODED (DOOR 2R SILL) · airframe 21,432 hrs · 8,326 cycles

DOOR 2R SILL PLATE HAS CORROSION JUST FWD OF FRAME 68 AT RBL 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE DOUBLER REPAIR.

Part: CABLE — CUT (CABIN) · airframe 21,261 hrs · 8,256 cycles

FOUND EMERGENCY EXIT ROW LIGHT INOP AT SEAT 6. REPLACED CABLE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,493 hrs · 7,951 cycles

FOUND SEAT 6C AISLE EMERGENCY LIGHT INOPERATIVE. [5-1-07] RELAMPED, GROUND CHECKS NORMAL.

Part: WARNING MESSAGE — ILLUMINATED · airframe 19,717 hrs · 7,667 cycles

IN CRUISE -R OUTER TK HI TEMP- MESSAGE DISPLAYED. REPLACED FUEL QUANTITY INDICATION COMPUTER 3QT. OPS CHECK NORMAL.

Part: SILL — CORRODED (FUSELAGE) · airframe 17,514 hrs · 6,843 cycles

DOOR 2 RT SILL PLATE HAS CORROSION AT CLIP NUT HOLE AT FRAME 66. REMOVED CORROSION AND INSTALLED 2 EA REPAIR ANGLES REF SRM 53-41-14 FIG 201.

Part: FAN — FAILED (COCKPIT) · airframe 13,607 hrs · 5,377 cycles

FUMES IN COCKPIT WITH VIBRATIONS. REPLACED THE AVIONICS BLOWER FAN. TESTED OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,475 hrs · 3,436 cycles

LARGE DENT APPROX 1 FT BY 1 FT UNDER LT STATIC PORT. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 53-00-11 & SRM 51-47-00.