N417UA

Part: BATTERY — FAILED (LH OVER WING) · airframe 88,626 hrs · 34,834 cycles

LH OVER WING EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. R+R RH OVERWING EMERGENCY LIGHT BATTERY REF 33-51-38. OPS TEST GOOD.

Part: NONE — FAILED (FWD EMER LT) · airframe 88,626 hrs · 34,834 cycles

FWD EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. R+R FWD EMERGENCY LIGHT BATTERY REF 33-51-38. OPS TEST GOOD. PARTS USED: 18-3351-3-0001,QTY :1

Part: TRANSMITTER — FAILED (BRAKE SYS 2) · airframe 87,998 hrs · 34,532 cycles

BRAKES SYS 2 FAULT CREW TOOK THESE SCREEN SHOTS, ATTACHED WITH THE LOG PAGE HERE REMOVED AND REPLACED TRANSMITTER REF AMM 32-42-47 PARTS USED: TRANSMITTER NEEDS ADJUSTMENT 31-3242-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1903078 SN OFF 1170 TRANSMITTER, AS OFF 31-3242-9-0002 1170 ON 31-3242-9-0002 1120 COMPLETED INSTALLATION FROM STEP 4.D. TO END REF AMM 32-42-47-400-001-A. BSCU BITE TEST PASSED OPS CHECK NORMAL.

Part: NONE — CRACKED (FR68) · airframe 87,704 hrs · 34,386 cycles

LEFT FR 68 AT STR 22 (UNDERSIDE) HAS CRACK INDICATION ALONG RADI US OF STR FLANGE, .30 INCHES FROM CAP, .70 INCHES LONG. GENERATE D BY V892444 ON HAECO LCQ NR 9290411/40411 LISH INITIAL INSPECTIONS ON FRAME REPAIR AT LH FR68 STR22 PER PA AIRCRAFT REACHES 54,086 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM R THEREAFTER. RT 2A OF THE LATEST REVISION OF ECRA 5341-01334 ON OR BEFORE THE EPEAT INSPECTIONS NOT TO EXCEED INTERVALS OF 4,900 FLIGHT CYCLES ACCOMPLISHED INTERIM REPAIR OF LEFT FR68 AT STR 22 IAW UAL EC/RA #: 5341-01334 & HAECO REO-L24043 PART 1. DIP REQUIRED TO ACCOMP ACCOMPLISH INITIAL INSPECTIONS ON FRAME REPAIR AT LH FR68 STR22 TOMC-APPROVAL FROM SC1ELBYC COMMENT PER PART 2A OF THE LATEST REVISION OF ECRA / 5341-01334 ON OR BEFORE THE AIRCRAFT REACHES 54,086 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS NOT TO / EXCEED INTERVALS OF 4,900 FLIGHT CYCLES THEREAFTER. RII COMPLETED BY LC38 QC RECORDS UPDATE....JM/U366569 QC REVIEW INIT : 54086 TAFC INIT WILL ITO TO RIR RIR : 4900 FC....JM/U366569

Part: NONE — CORRODED (RH DOOR SILL) · airframe 87,704 hrs · 34,386 cycles

CORROSION ON RH DOOR SILL AT FR68 INBD CORNER (2 PLACES). GENERA TED BY V892443 ON HAECO LCQ NR 9290188/40188 CORROSION REMOVAL RH DOOR SILL AT FR 68 FOUND TO BE BEYOND LIMIT S IAW A320 SRM 53-41-14-283-002, REMOVED AND REPLACED R2 DOOR SI LL FR 66-68 STR 23R IAW A320 SRM 51-72-11. ACMP BY MECH V039746 INSP BY V901665

Part: NONE — CRACKED (FR68) · airframe 87,704 hrs · 34,386 cycles

RIGHT FR 68 AT STR 22 (UNDERSIDE) HAS CRACK INDICATION ALONG RAD IUS OF STR FLANGE, .40 INCHES FROM CAP, .50 INCHES LONG. GENERAT ED BY V892444 ON HAECO LCQ NR 9290412/40412 PLISH INITIAL INSPECTIONS ON FRAME REPAIR AT RH FR68 STR22RH PER THE AIRCRAFT REACHES 54,086 TOTAL AIRCRAFT FLIGHT CYCLES. PERFOR LES THEREAFTER. PART 2A OF THE LATEST REVISION OF ECRA 5341-01336 ON OR BEFORE M REPEAT INSPECTIONS NOT TO EXCEED INTERVALS OF 4,700 FLIGHT CYC ACCOMPLISHED INTERIM REPAIR OF RIGHT FR68 AT STR 22 IAW UAL EC/R A #: 5341-01336 & HAECO REO-L24042 PART 1. DIP REQUIRED TO ACCOM ACCOMPLISH INITIAL INSPECTIONS ON FRAME REPAIR AT RH FR68 TOMC-APPROVAL FROM SC1ELBYC COMMENT STR22RH PER PART 2A OF THE LATEST REVISION OF ECRA5341-01336 ON OR BEFORE THE AIRCRAFT REACHES 54,086 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS NOT TOEXCEED INTERVALS OF 4,700 FLIGHT CYCLES THEREAFTER RII COMPLETED ,BY LC38 QC QC REVIEW INIT : 54086 TAFC (INIT WILL ITO TO RIR) RIR: 4700 F/C.................JM/U366569 RECORDS UPDATE...JM/U366569

Part: NONE — NONE (FR59,61,62,63) · airframe 87,704 hrs · 34,386 cycles

LEFT AFT CARGO FR 59, 61, 62, AND 63 VERTICAL WEB STGR 37 HAS OUT OF ROUND INDICATIONS AT AFT SIDE OF HOLE, HOLES ARE OUT OF ROUND.

Part: DOOR FRAME — CRACKED (RH AFT OVRWING) · airframe 87,704 hrs · 34,386 cycles

RH AFT OVER WING DOOR INTERNAL FRAME IS CRACKED (A3NB-52-4-6031). REMOVED AND REPLACED R/H AFT OVER WING DOOR INTERNAL FRAMES IAW A320 SRM 51-72-11-911-001. PERFORMED BY V918284 AND INSP BY B940 824.

Part: NONE — CRACKED (LH FWD EXIT DR) · airframe 87,704 hrs · 34,386 cycles

LH FWD OVER WING EXIT DOOR INTERNAL FRAME CRACKED (A3NB-52-04-60 31). GENERATED BY V892442 AT HAECO LCQ PER NR 9290372 (40372). REMOVED AND REPLACED L/H FWD OVER WING EXIT DOOR INTERNAL FRAMES IAW A320 SRM 51-72-11-911-001. PERFORMED BY V918284 AND INSP BY V940824.

Part: FRAME — CRACKED (RH FWD OVRWNG) · airframe 87,704 hrs · 34,386 cycles

RH FWD OVER WING DOOR INTERNAL FRAME IS CRACKED ON HAECO LCQ REF 9290377/40377 SPEC A3NB-52-4-6031. NR GENERATED BY V892442 REMOVED AND REPLACED CRACKED INTERNAL FRAME ON RH FWD OVERWING DOOR.

Part: NONE — CRACKED (LH AFT OVR WING) · airframe 87,704 hrs · 34,386 cycles

LH AFT OVER WING DOOR HAS INTERNAL FRAME CRACKED PER LCQ HAECO N R 9290375/40375 GENERATED BY V892442 (A3NB-52-4-6031) REMOVED & REPLACED 2EA INTERNAL FRAMES ON LH AFT OVERWNG DOOR IA W 51-72-11-911-001. PERFORMED BY V898898 INSP BY V940824

Part: NONE — NONE (FWD) · airframe 86,297 hrs · 33,708 cycles

ACRID SMELL IN FIRST CLASS AND FORWARD GALLEY. NO ACRID ODOR SMELL DETECTED, CREW COMPLIED WITH SMOKE/ODOR FORM 46-6020, FWD''D TO TOMC

Part: ACTUATOR — FAILED (NLG DOORS) · airframe 84,760 hrs · 33,009 cycles

N/LG DOORS NOT CLOSED DISPLAYED ON ECAM. CREW REPORTS NO BUFFETING AT 24K FT AND 225 KTS.. REPLACED NLG DOOR ACT. REF AMM 32-31-16 AND 32-31-16-991 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1216874 SN OFF 0266 ACTUATOR, NLG, OFF 31-3232-9-0001 0226 ON 31-3232-9-0001 1068

Part: ACTUATOR — FAILED (RT MLG DOOR) · airframe 84,753 hrs · 33,005 cycles

800 PSI HYDRAULIC DROP IN GREEN SYSTEM PRESSURE WHEN RIGHT HAND MLG DOOR GOES FROM OPEN TO THE CLOSED POSITION. THIS DOES NOT OCCUR WHEN THE LEFT MLG DOOR IS CLOSED INDEPENDENTLY OF THE RIGHT DOOR. THIS DROP IN PRESSURE CAUSES THE NOSE GEAR DOORS TO NOT SHOW CLOSED INDICATION IN THE FLIGHT DECK. REMOVED AND REPLACED RH MLG DOOR GROUND OPENING BYPASS VALVE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1180563 SN OFF 9493 PER AMM-32-31-13-400-001-A. NO HELP IPC REFERENCE # 32-31-03-46 VALVE, BYPASS, OFF 31-3231-9-9002 9493 ON 31-3231-9-9002 0193 IPC REFERENCE # 32-31-00 ACUATOR IS BY-PASSING INTERNALLY. RPL ACTUATOR PER AMM 32-31-35-400. ACP GEAR DOOR ACTUATION FIVE TIMES, HYD PSI REMAINED ABOVE 2800 PSI WITH RT GEAR DOOR CLOSED. NOSE GEAR DOOR REMAINED CLOSED AND INDICATED AS SUCH. ADD EMP:094603 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1193807 SN OFF 1898 FOUND RT MAIN GEAR DOOR ACUATOR HOT TO THE TOUCH, SUSPECT COMPLETED ACTUATOR INSTALL BY GREASING BOTH FITTINGS AND SEALING ATTACH POINTS.

Part: UPLOCK — FAULTED (NLG DOOR) · airframe 84,753 hrs · 33,005 cycles

NOSE LANDING GEAR DOORS WILL NOT STAY UP AND LOCKED CLOSED WHEN GREEN HYDRAULIC SYSTEM NOT PRESSURIZED-DOORS FALL OPEN. GROUND MANUAL DOOR RELEASE HANDLE POSITIONED IN THE DOWN POSITION FOR SAFETY WHEN HYDRAULICS PRESSURIZED. REF TSM 32-31-00-810-859 AND MM 32-31-14-000-001. LGCIU 1 & 2 FAULTING NOSE GEAR DOOR UPLOCK ASSY 2534 GM. NO NOTABLE PHYSICAL DAMAGE TO UPLOCK MECHANISM AND ROD ASSY. REMOVED NLG DOOR UPLOCK ASSY 2534GM. AWAITING PART FOR INSTALL. ADD EMP:104300

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 83,124 hrs · 32,286 cycles

DUE TO REPORT OF "F/CTL FLAPS LOCKED-ALIGNMENT" WITH FLAPS UNABLE TO EXTEND AT DESCENT AND BOTH SFCC'S IDENTIFYING CFDS FAULTS ON FLP 1 (2) LT MECH DRIVE UNITS. ACCOMPLISH TSM TASK 27-51-00-810-818-A, AS REQUIRED PAYING PARTICULAR ATTENTION TO LEFT HAND (LT) SIDE. REPLACE ANY WORN OR DAMAGED COMPONENTS NOTED. ADJUST THE LT FLAP DRIVE, LT INTERCONNECTING STRUT, AND LT INTERCONNECTING STRUT SENSOR, AS REQUIRED. TOMC 22OCT20 CONTACT TOMC WITH FINDINGS PRIOR TO SIGNING OFF THIS LOG PAGE. TOMC 22OCT20. PERFORMED DETAILED VISUAL INSPECTION OF LT FLAP TRANSMISSION CONDITIONS OBSERVED AT THIS TIME. FURTHER TROUBLE SHOOTING MUST CONTINUE, IAW AMM NR 27-54-00-220-007. ADD FAULT: N ASSEMBLY, IAW TASK NR 27-54-00-200-001-A. NO ANOMALOUS INTERCONNECTING STRUT. NO FAULTS NOTED. PERFORMED AMM TASK 27-51-44-820-001. ADJUSTMENT CHECK OF LT PERFORMED FLAP DRIVE SYSTEM CHECK, PER AMM TASK 27-54-00-220-007 UPTP AND INCLUDING STEP 4D(1), NO FAULTS NOTED. UNLOCKED FOR MAINTENANCE UPDATE. ARMENTA TOMC 23OCT20 FINISH CHECK 27-54-00-220-007 4D2 TO END, PREFORM CHECK FOUND AT THIS TIME. PERFORMED FLAP DRIVE SYSTEM, IAW AMM INTECONNECTING STRUT SENSOR, IAW AMM 27-51-44-400-002. NO DEFECTS 27-54-00-710-001 GOT "FLT/CTRL FLAP SYSTEM 1" ECAM MESSAGE ON UPPER ECAM FOR ABOUT 10 SEC THAN WENT AWAY WHEN SELECTING FLAPS FROM 0 TO 1 AND 1 TO 0 ALL OTHER POSITIONS. OPERATIONS CHECK NORMAL. PERFORMED BITE CHECK OF BOTH SFCC NO CURRENT FAULT OR CLASS 3 NO SFCC1 DATA" AND "FLP 2 NO SFCC 1 DATA" FAULTS, IN THE

Part: CIRCUIT BREAKER — TRIPPED (RT MLG) · airframe 82,569 hrs · 32,052 cycles

L/G LGCIU 1 FAULT MESSAGE ON ECAM FOLLOWED BY CB TRIPPED ON OVER HEAD PANEL AND REAR PANEL. FOUND LGCIU 1 CB TRIPPED. C/B SYS1 GND SPLY TRIPPED, LGCIU 1 RESET AND STAYED IN SYS1 GND SPLY POPPED AGAIN, CYLCLED GEAR HANDLE ON GO AROUND, ON NEXT APPROACH GEAR EXTENDED WITH GEAR HANDLE, BUT GEAR DOORS REMIANED OPEN AND NO NOSE GEAR STEERING ON GROUND. LIFTED AIRCRAFT ON JACKS REF MM 07-11-00-581-001A AND MM 32-00-00-860-001-A.

Part: FUEL CAP — MISSING (FUEL SYSTEM) · airframe 79,743 hrs · 30,823 cycles

PDA 2 REFERENCE LOGPAGE 9135632. FOUND FUEL CAP MISSING UPON ARRIVAL IN DFW. CHANGING ATA TO 2800 SDR FLAG CHANGED TO ''YES''. REFER TO LOGPAGE 9135632 FOR CORRECTIVE ACTION AND ROTABLE PART CHANGE INFORMATION.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 77,080 hrs · 29,617 cycles

LEFT PAX DOOR CUTOUT, FRAME 16 NR 1 DOOR STOP FITTING, NR 3 FASTENER HOLE HAS A CRACK INDICTAION. REPAIRED THE STOP FITTING IAW ECRA 5311-01925, STEPS 7-11.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 77,080 hrs · 29,617 cycles

LEFT FWD PAX DOOR CUTOUT FRAME 16, STOP FITTING NR 7 HAS A CRACK INDICATION. REPAIRED THE DOOR FRAME IAW ECRA 5311-01925, PART 1.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 77,080 hrs · 29,617 cycles

LEFT FWD PAX DOOR CUTOUT FRAME 20, DOOR STOP FITTING NR 1 HAS A CRACK INDICATION. REPAIRED THE DOOR FRAME IAW ECRA 5311-01925, PART 1.

Part: SKIN — CRACKED (FR35 STR30) · airframe 77,080 hrs · 29,617 cycles

SKIN AT FRAME 35, STRINGER 30L. HAD A CRACK INDICATION. REPAIRED THE SKIN IAW ECRA 5331-02200.

Part: FITTING — CRACKED (R1 DOOR) · airframe 77,080 hrs · 29,617 cycles

ROTO PROBE INSPECTION INDICATED A CRACK INDICATI ON THE RT PASSENGER DOOR FRAME AT FRAME 16, NR 1 FITTING. REPAIRED THE FITTING HOLE IAW ECRA 5311-01925 STE PS 18-22.

Part: FRAME — CRACKED (FRM 35) · airframe 77,080 hrs · 29,617 cycles

CRACK FOUND ON FRAME 35, STRINGER 30L. REPAIRED THE FRAME IAW ECRA 5331-02200.

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 77,080 hrs · 29,617 cycles

ROTO PROBE INSPECTION SHOWED A CRACK INDICATI ON THE RT DOOR FRAME AT FRAME 16 NR 1 FITTING NR 3 HOLE, REPAIRED IAW ECRA 53-11-01925, STEPS 18-22.

Part: STRINGER — CORRODED (FRAME 67) · airframe 77,080 hrs · 29,617 cycles

STRINGER 43R, FRAME 67 FOUND CORRODED. BLENDED THE CORROSION, FOUND OUT OF LIMITS. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED A NEW STRINGER IAW SRM 5 3-00-13-300-001.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,080 hrs · 29,617 cycles

LEFT EPSU BATTERY IS DISCHARGED 110WL2. REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW IAW AMM 33-51-38-000-001-A, 33-51-38-400-001-A, 33-51- 38-000-002A, AND 33-51-38-400-002A. OPS TESTED GOOD IAW 33-51-00-710-001-A.

Part: SKIN — DENTED (FRAMES 71-72) · airframe 77,080 hrs · 29,617 cycles

SKIN DENTED BETWEEN FRAMES 71 AND 72, STRINGER 23R & 24R. REPAIRED IAW ECRA 5331-02202.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 77,080 hrs · 29,617 cycles

AFT FUSLAGE STRINGER 38R BETWEEN FRAMES 58 AND 59 CORRODED. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (FRAME 59) · airframe 77,080 hrs · 29,617 cycles

CORROSION FOUND ON STRINGER 36R, BETWEEN FRAMES 59. REMOVED THE STRINGER SECTION, AND INSTALLED A NEW STRINGER IAW SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (FRAMES 62-63) · airframe 77,080 hrs · 29,617 cycles

STRINGER 32R CORRODED BETWEEN FRAMES 62 AND 63. REMOVED THE STRINGER SECTION AND INSTALLED A NEW STRINGER SECTION IAW SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 77,080 hrs · 29,617 cycles

AFT FUSELAGE, STRINGER 41R BETWEEN FRAMES 58 & 59 CORRODED. REMOVED THE STRINGER SPLICE, BLENDED CORROSION, AND FOUND TO BE OUT OF LIMITS. CUTOUT THE DAMAGED AREA ON THE STRINGER, INSTALLED A REPAIR IAW SRM 51-42-11-001, 51-72-11-911-001, 53-00-13-300-001 & 002. NTM 51-10-01, SRI 53-00- 13-205-001.

Part: STRINGER — CORRODED (FRAME 58-59) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY FRAMES 58 - 59, STRINGER 40R CORRODED NEAR THE SPLICE. REMOVED & REPLACED THE STRINGER IAW SRM 53-00-13-300-001, AND 51-42-11-001-2E.

Part: STRINGER — CORRODED (FRAME 56) · airframe 77,080 hrs · 29,617 cycles

STRINGER 42L, FRAME 56 CORRODED. REPAIRED THE STRINGER IAW SRM 53-10-00-13-300-002.

Part: COVER — CORRODED (AFT CARGO BOX) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY TORSION BOX HAS MULTIPLE AREAS WITH CORROSION. REMOVED AND REPLACED THE AFT CARGO TORSION BOX COVER.

Part: STRINGER — CORRODED (FRAMES 59-60) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY, STRINGER 41L UPPER SURFACE CORRODED BETWEEN FRAMES 59 - 60. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW STRINGER 41L AND INSTALLED.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY, FRAMES 58 - 59, STRINGER 43L, REPAIR SPLICE ANGLE AND THE STRINGER ARE CORRODED NEAR FWD AND AFT ENDS. REMOVED AND REPLACED THE STRINGER REPAIR.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 77,080 hrs · 29,617 cycles

INSPECTION OF THE RT AFT EMERGENCY EXIT DOOR FOUND CORRODED AT LOWER FWD INNER ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-72-11-911-001, 51-42-11-001-2D, AND 2.E.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 77,080 hrs · 29,617 cycles

ON REMOVAL OF FWD LOWER LATCH ON THE RT AFT EMERGENCY EXIT DOOR, FOUND LOWER FWD CURVED EDGE PROFILE CRACKED. CLEANED AREA OF CRACK ON RT AFT EMERGENCY DOOR, LOWER FWD CORNER, CRACK APPROXIMATELY.5 INCHES IN LENGTH. REMOVED AND REPLACED THE PROFILE IAW SRM 51-11-00-001, 51-72-11-911 -001, AND ER 5100R01017, REV D.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 77,080 hrs · 29,617 cycles

ON REMOVAL OF FWD LWR LATCH ON TH RT AFT EMERGENCY EXIT DOOR, FOUND LOWER FWD CURVED EDGE PROFILE CRACKED. CLEANED AREA, CRACK TO BE APPROXIMATELY .5 INCHES IN LENGTH. REMOVED AND REPLACED LOWER FWD CORNER PROFILE IAW SRM 51-11-00-001, 51-72-11-911 -001, AND ER 5100R01017, REV D.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 77,080 hrs · 29,617 cycles

INSPECTION OF THE RT A FT EMERGENCY EXIT DOOR FOUND CORRODED AT LOWER FWD INNER ANGLE. REMOVED CORRODED ANGLE, LOCATED AND MATCH DRILLED A NEW ANGLE AND INSTALLED FWD INNER ANGLE ON RT AFT EMERGENCY DOOR IAW SRM 51-72-11-911-001, 51-42-11-001-2D, AND 2.E

Part: DOOR SILL — CORRODED (FRAMES 53-56) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO DOOR SILL BETWEEN FRAMES 53 AND 56 HAS MULTIPLE AREAS OF CORROSION. BLENDED CORROSION. ACCOMPLISHED HFEC AND ROTOPROBE WITH NO DEFECTS NOTED, AND ACCOMPLISHED UT THICKNESS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-1 1-911-001, PARA 2E, SRM 51-72-11-911-001, SRM 53-41-49-283-003.

Part: STRINGER — CORRODED (FRAMES 59-60) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY, FRAMES 59-60, STRINGER 41R CORRODED ON THE UPPER SURFACE. BLENDED OUT THE CORROSION AND FOUND TO BE OUT OF LIMITS. INSTALLED A REPAIR.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 77,080 hrs · 29,617 cycles

AFT CARGO BAY, FRAMES 58 - 59, STRINGER 39R CORRODED NEAR PRODUCTION SPLICE. BLENED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001, 51-72-11-911, 53-00-13-300-0 01 002, 51-21-11-001, AND NTM 51-10-01.

Part: BUTT JOINT — CORRODED (FRAME 67) · airframe 77,080 hrs · 29,617 cycles

CORROSION FOUND ON THE BUTTSTRAP AT FRAME 67, STRINGER 29L. REMOVED AND REPLACED THE BUTT STRAP IAW SRM 51-72-11-911-011.

Part: STRINGER SPLICE — CORRODED (FRAME 67) · airframe 77,080 hrs · 29,617 cycles

SPLICE AT FRAME 67, STRINGER 29, CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 5-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,080 hrs · 29,617 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 30, STRINGERS 42 - 43L WAS CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-75-11-911-001, AND NTM 51-10-01.

Part: STRINGER — CORRODED (FRAME 67) · airframe 77,080 hrs · 29,617 cycles

STRINGER SPLICE 30L AT FRAME 67 CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 5 1-72-11-911-001.

Part: STRINGER SPLICE — CORRODED (FRAME 67) · airframe 77,080 hrs · 29,617 cycles

STRINGER SPLICE 28L AT FRAME 67, CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 77,080 hrs · 29,617 cycles

L2 DOOR SILL FR68 STGR 23 JUNCTION I S CRACKED. REFER TO NON-ROUTINE NUMBER 9011139. REMOVED AND REPLACED JUNCTION AT L2 DOOR SILL FR6 8 STGR 23 IAW SRM 51-72-11-911-001.

Part: UNKNOWN — ODOR (CABIN) · airframe 77,080 hrs · 29,617 cycles

HAD BRIEF ELECTRICAL BURNING ODOR AROUND ROW 11ABC. ACCOMPLISHED A COMPLETE INSPECTION OF ALL ELECTRICAL COMPONANTS IN AND AROUND SEAT ROW 11. REMOVED PANELS AS REQUIRED FOR ACCESS ON OVERHEAD & CHECKED UNDER SEATS IN ADJACENT ROWS. NO EVIDENCE OF ELECTRICAL DAMAGE NOTED. PER FLIGHT ATTENDANT PRESENT NOTED THAT ELECTRICAL SMELL WAS TRANSIENT & DISSIPATED QUICKLY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,589 hrs · 29,410 cycles

MISSING PROTECTIVE CAP COVER FOR EMERGENCY EXIT LIGHTING AT SEAT 29A AND 34A ON LOWER SIDEWALL PANEL. INSTALLED PROTECTIVE CAP COVERS

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 76,500 hrs · 29,366 cycles

FWD ATTENDANT PANEL CIDS PANEL FAILED CABIN EMERGENCY LIGHTS TEST ON #2 SERVICE CHECK. MESSAGE ESPU BATT FWD L DISPLAYED REF AMM 33-51-38. REMOVED AND REPLACED FWD L1 EMERGENCY BATTERY REF AMM 33-51-11 OPS CHECK GOOD

Part: SLIDE — NO TEST (L2 DOOR) · airframe 76,410 hrs · 29,325 cycles

DURING A SERVICE CHECK, THE EMERGENCY LIGHT FAILED TO TEST WITH A MAINT MESSAGE EPSU EXT LOAD AFT LT. TROUBLESHOT IAW TSM AND CONFIRMED THE AFT LEFT DOOR SLIDE DEFECTIVE. REMOVED AND REPLACED THE L2 DOOR SLIDE IAW AMM 25-62-44-400 -006-A, AND 25-62-44-000-002-A.

Part: CHIME — FALSE ACTIVATION · airframe 76,117 hrs · 29,172 cycles

EMERGENCY CHIME GOING OFF INTERMITTENTLY ON LANDING. CYCLED CIRCUIT BREAKER G2-G5, & M5-M14, ALSO CYCLED EVACUATION SWITCH, CHIMES STOPPED GOING OFF.

Part: SLIDE — FAILED (L2 DOOR) · airframe 75,802 hrs · 29,033 cycles

SLIDE AT 2L FAILED EMERGENCY LIGHT CHECK SLIDE. REPLACE NR 2 LT SLIDE ASSY REF MM 25-62-44-400-006A.

Part: SLIDE — FAILED (R2 DOOR) · airframe 75,802 hrs · 29,033 cycles

DOOR AT 2R FAILED EMERGENCY LIGHTS CHECK. REMOVED AND REPLACED SLIDE AT DOOR 2R PER AMM 25-62-44.

Part: VALVE — FAULTY (GALLEY) · airframe 75,429 hrs · 28,859 cycles

AFT COFFEE MAKER POURING OUT WATER. LOUD PUMP NOISE ELECTRIC SMELL. SHUT OFF VALVE INOP REPLACED AFT GALLEY WATER SUPPLY SHUTOFF VALVE, NO LEAKS NOTED. FOUND I/B COFFEE MAKER M42 SUPPLY LINE LEAKING, SECURED B-NUT NO LEAKS NOTED.

Part: LENS — LOOSE (R2 DOOR) · airframe 74,910 hrs · 28,646 cycles

2 RIGHT ARMING MECHANISM IS NOT FLUSH WHILE IN FLIGHT.. FOUND THE SLIDE PRESSURE INDICATOR LENS UNDER THE GIRT BAR. REMOVED LENS AND CLEANED AREA. REINSTALLED LENS. OPS CKED THE ARMING MECHANISM WITH NO DEFECTS NOTED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,626 hrs · 28,513 cycles

2EA EMERGENCY LIGHTS ABOVE 2L INOP. RELAMPED NO HELP. FOUND LOOSE LIGHT ASSY PLUG, SECURED OPS TEST NORMAL.

Part: BATTERY — FAULTY (CABIN) · airframe 74,626 hrs · 28,513 cycles

LT CENTER OVERWING EMERG PWR SUPPLY UNIT FAULTY BATTERY, REMOVED AND REPLACED LT CENTER OVERWING EMERGENCY PWR UNIT BATTERY TO CLEAR FAULT. REF AMM 33-51-38-400-002-A VERIFIED INSTALLATION AND OPERATIONAL TEST OF LT CENTER OVERWING EMERGENCY PWR UNIT BATTERY PER AMM 33-51-38-400-002-A.

Part: SLIDE — UNSERVICEABLE (2R DOOR) · airframe 74,625 hrs · 28,511 cycles

EMERGENCY LIGHTS FAILED TEST. FAULTING AFT LT EXTERNAL LOAD. REMOVED AND REPLACED R2 DOOR SLIDE ASSY. LIGHT OPS CHECK GOOD OK TO CONTINUE

Part: COMPUTER — FAULTY (FLT WARNING) · airframe 73,969 hrs · 28,223 cycles

NR 2 ENGINE FIRE LIGHTS ON WITHOUT AURAL WARNINGS REPORTED BY CREW. EMERGENCY DECLARED. R & R NR 1 FLIGHT WARNING COMPUTER AND NR 2 FLIGHT WARNING COMPUTER, IAW AMM 31-53-54, OPS NORMAL.

Part: FAN — FAULTY (E&E BAY) · airframe 73,529 hrs · 28,026 cycles

AVNCS VENT EXTRACT CB POPPED. SMOKE IN COCKPIT. ON GND IN RSW REPLACED AVNCS VENT EXTRACT FAN REF AMM 21-26-51-401.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 72,746 hrs · 27,663 cycles

RIGHT EMERGENCY EXIT OVERWING SLIDE LIGHT CAME ON DURING LANDING ROLLOUT. CHECKED THE EMERGENCY DOOR FOR SECURITY, ALL CLOSED AND SECURED

Part: SLIDE — MALFUNCTIONED · airframe 72,724 hrs · 27,656 cycles

EMERGENCY LIGHTS TEST FAILED FOR EXTERNAL LOADS FAULTY AFT LT. L2 DOOR AND R2 DOOR SLIDES REPLACED IAW AMM 25-62-44.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 72,724 hrs · 27,656 cycles

R2 DOOR SILL LOWER FWD FRAME AT FRAME 66 HAS CORROSION ON FRAME WEB FACE & AROUND NUTPLATE. BLENDED CORROSION AND IS OUT OF LIMITS. CUT OUT CORRODED AREA IS 1.4 INCH WIDE & 1.3 INCH TALL & INSTALLED A RPR FITTING IAW SRM 53-41-12 FIG 202. SRI 53-41-12 -2-002-00 PARA 3B TBL 204.

Part: DOOR SILL — CORRODED (R2) · corrosion level 2 · airframe 72,724 hrs · 27,656 cycles

AFT CABIN WET AREA R2 DOOR SILL HAS CORROSION AT AFT GIRT BAR FITTING. REMOVED DAMAGED SILL. INSTALLED NEW DOOR SILL IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 72,724 hrs · 27,656 cycles

2R DOOR SILL FRAME 68 LWR AREA HAS CORROSION FRAME WEB AROUND NUTPLATE. REPAIRED AREA WITH RPR FITTING IAW SRM 53-41-12 TBL 202 PARA 5B & FIG 202. SRI 53-41-12-2-002-00 PARA 3B TBL 205.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 72,246 hrs · 27,439 cycles

13WL EPSU FAILED LIGHT CHECK. REPLACED THE EPSU, OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 72,246 hrs · 27,439 cycles

EMERGENCY EXIT LIGHTS WILL NOT EXTENGUISH. CYCLED POWER, LIGHT OPS NORMAL

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 71,802 hrs · 27,245 cycles

AUTO BRAKE FAULT DISPLAYED ON UPPER ECAM SCREEN. TRIED NEW BSCU, SAME FAULTS, NO HELP. ACCOMPLISHED WIRING CHECK OF TACHOMETER WHEEL 4, 22GG, IAW AWD 32-11-02 & AWD 32-42-06. ALL CHECKED OK.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 71,441 hrs · 27,083 cycles

FAULT, INT LOADS AFT L, DISPLAYED DURING EMER EXIT LIGHT 2CVS TESTS. CYCLED EMER LIGHT CB`S, RESET SYS. OPERATIONS CHECKED GOOD.

Part: RELAY — FAULTY (LANDING GEAR) · airframe 71,281 hrs · 27,004 cycles

GEAR EXT LIGHTS DID NOT ILLUMINATE ON LANDING. GEAR PANEL ECAM WHEEL PAGE SHOWED MX TEXT. ALL GREEN INDICATIONS RETURNED ALL GREEN AT 500' RA. FOUND BOTH RED & GREEN LIGHTS NOT WORKING WHILE CYCLING GEAR. GREEN D & L WOULD COME ON AFT ER 3 - 5 MIN. REPLACED RELAY 53GA IAW ASM 32-61-01 PG 2 SH 1. CYCLED GEAR SEVERAL TIMES, ALL INDICATION NORMAL.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 70,737 hrs · 26,766 cycles

PASSENGER O2 MASKS IN ROW 21 ABC, FELL DOWN DURING TAKEOFF. REPACKED 02 MASK IAW AMM 35-21-43-550-801-A. INSPECTION REVEALED NO FINDINGS.

Part: CONNECTOR — DIRTY (NLG STEERING) · airframe 70,360 hrs · 26,603 cycles

ECAM FAULT SYS ONE, NOSE WHEEL IN FLIGHT. DECLARED EMER, REQUESTED LONGER RUNWAY. ACCOMPLISHED TSM 32-51-00-810-811, CFDS TESTS & CLEANED CONNECTORS AT 6GC, 4GC & 3GC. RESET SYS, TESTED GOOD, NO MOISTURE OR CORROSION FOUND.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 69,440 hrs · 26,226 cycles

CREW REPORT, ON FIRST ATTEMPT, GEAR HANDLE DOWN, GEAR DID NOT EXTEND, NO NOISE, NO INDICATION CHANGE, NO FAULTS. SECOND ATTEMPT, GEAR EXTENDED, DID NOT GET PROPER INDICATION. ON THIRD ATTEMPT, GEAR EXTENDED WITH NORMAL INDICATION. R & R LG CONTROL LEVER IAW AMM 32-31-11. PERFORMED GEAR EXTENSION & RETRACTION. OPERATIONS CHECKED IAW AMM 32-31-00. OPERATIONS CHECKED GOOD.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 69,440 hrs · 26,226 cycles

CREW REPORT, ON FIRST ATTEMPT, GEAR HANDLE DOWN, GEAR DID NOT EXTEND, NO NOISE, NO INDICATION CHANGE & NO FAULTS. SECOND ATTEMPT, GEAR EXTENDED, DID NOT GET PROPER INDICATION, ON THIRD ATTEMPT, GEAR EXTENDED WITH NORMAL INDICATION. R & R LG CONTROL LEVER IAW AMM 32-31-11. PERFORMED GEAR EXTENSION & RETRACTION. OPERATIONS CHECKED IAW AMM 32-31-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,387 hrs · 25,801 cycles

EMERGENCY LIGHTS, OPERATIONAL TEST FAILED, BATTERY FWD LT DISPLAYED. REPLACED NR 1 BATTERY FWD LT. LIGHTS CHECKED GOOD IAW AMM 33-51-38-400-02.

Part: ENGINE — ODOR (NR 2) · airframe 66,256 hrs · 24,964 cycles

IAW CREW ON TAKEOFF, GOT AIR BLEED 2 MSG & WITHIN 30 SECONDS SMOKE ALARM IN FWD LAVATORY WENT OFF. CABIN CREW SAID THEY STARTED GETTING SMELL & ODOR AROUND ROW 23 THEN SMELL MOVED FWD TO AROUND ROW 8 & SMELL STARTED TO INTENSIFY. SMELL WAS COMING FROM NR 2 ENG INSP ENG IAW MM 71-00-00-810-801-A 1 3, THRU STEP 4.G

Part: MOUNT BOLT — CORRODED (LT MLG DOOR) · airframe 66,115 hrs · 24,911 cycles

LEFT MLG FIXED DOOR B FTG MT BOLT TO GEAR CORRODED, REPLACED BOLT.

Part: ATTACH BOLT — CORRODED (LT MLG DOOR) · airframe 66,115 hrs · 24,911 cycles

LEFT MLG FIXED DOOR C MT FITTING BOLTS TO GEAR CORRODED, REPLACED BOLT.

Part: ATTACH BOLT — CORRODED (RT MLG DOOR) · airframe 66,115 hrs · 24,911 cycles

RIGHT MLG FIXED DOOR C MT FITTING, 1 ATTACH BOLT TO GEAR CORRODED. R & R HARDWARE REF AID BOOK IAW IPC 52-18-13-01.

Part: COMPUTER — FAULTED (NR 2 ELAC) · airframe 65,363 hrs · 24,613 cycles

ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN.

Part: SLIDE — UNKNOWN (CABIN) · airframe 65,235 hrs · 24,567 cycles

EMERGENCY LIGHT TEST INDICATED EXTERIOR LOADS AFT LT. SLUG DOORS AT 2L & 2R CONFIRMED FAULT AT DOOR 2R SLIDE PACK. REINSTALLED BOTH SLIDE PACKS IAW MM25-62-44-401.

Part: COWLING — DELAMINATED (NR 2 ENGINE) · airframe 65,104 hrs · 24,512 cycles

NR 2 ENG INLET COWL WIRE MESH HAS A LARGE AREA DELAMINATED FROM FRONT TO BACK, FROM THE 1-2 O'CLOCK POSITION.

Part: ACCELEROMETER — FAULTY (FLIGHT CONTROL) · airframe 64,989 hrs · 24,467 cycles

SEC 1 FAIL AFTER START. QRH RESET ON GROUND, NO HELP. TURNED OFF ALL HYDS SWITCH IAW TOM. IAW POST FLIGHT REPORT & AMIS HISTORY, REPLACED ACCELEROMETER 12CE2, IAW AMM 27-92-16-4 01. TEST PASSED, SEC 1 TEST PASSED IAW AMM 27-94-00-501.

Part: LENS — MISSING (R1 DOOR) · airframe 64,771 hrs · 24,380 cycles

DOOR 1R ARM DISARM SIGHT PLATE LENS MISSING. VISUAL INSPECTION OF AREA, APPLIED ONE LAYER OF CLEAR TAPE. FUNCTIONAL CHECK OF ARM DISARM, WITH NO INTERFERENCE & PROPER FUNCTION.

Part: NOSE COWL — CRACKED (NR 2 ENGINE) · airframe 64,581 hrs · 24,308 cycles

NR 2 ENG NOSE COWL HAS APPROXIMATELY HALF INCH CRACK AT 8 O'CLOCK POSITION. FOUND CRACK IS IN ZONE J, STOP DRILLED CRACK, MUST REPAIR NO LATER THAN 600 FLIGHT HOURS, 750 FLIGHT CYCLES OR 100 DAYS, CHECK CRACK EVERY FLIGHT TO MAKE SURE CRACK DOES NOT BECOME LATER IAW AMM.

Part: TRANSDUCER — FAULTY (PITCH TRIM) · airframe 64,486 hrs · 24,276 cycles

IAW EQ3055 ABILITY OF SEC 1 TO ACHIEVE PITCH CONT FAIL TO RETURN TO 0.0 + OR -0.3 IT IS AT 0.5 IAW AMM27-9 6-00-710-018-A STEP 32 PAGE 37. REPLACED SEC1 F1CE1 IAW AMM-2794-34-000-0001-A & AMM-27-34-400-0001-A, WITH NO HELP. REINSTALLED OLD UNIT. REPLACED NR 2 ELECTRONIC MODULE OF THE PITCH TRIM ACTUATOR PER MM27-44-57. NO HELP. REINSTALLED OLD UNIT. CONT OF AMIS ITEM 4862005, REPLACED MONITOR POSITION TRANSDUCER OF THE THIS ACTUATOR MM27-44-56. ALL PARAMETERS OF THE ABOVE CHECKED ARE NOW WITHIN LIMITS. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 64,402 hrs · 24,249 cycles

FUSELAGE DENT BETWEEN FR 63 & 64 AT STRINGER 21L. DENT OUT OF LIMIT, INSTALLED DOUBLER REPAIR.

Part: ANTENNA — DEFECTIVE (VHF COMM) · airframe 64,155 hrs · 24,162 cycles

RADIO HAS STATIC ON VHF NR 1. NR 1 VHF HAS CONSTANT STATIC. TRIED NEW VHF RADIO. NEW AMU, DISCONNECTED EACH ACP & RMP ONE AT A TIME. CHECKED COAX FOR SECURITY AT BENCH PLUG & ANTENNA, FOUND TIGHT. REPLACED VHF NR 1 ANTENNA PER AMM.

Part: BRAKE — CHATTERING (RT MLG) · airframe 63,897 hrs · 24,067 cycles

RIGHT BRAKES CHATTERING AND DRAGGING DURING TAXI IN. RIGHT BRAKES TEMP MUCH HIGHER, 400 VICE 135. BLEED BRAKES IAW MM, OPS CHECK NORMAL. NR 3 MLG BRAKE GRABBING.

Part: SKIN — WORN (FUSELAGE) · airframe 63,824 hrs · 24,041 cycles

EXTERNAL FUSELAGE SKIN, FRAME 34 S43L HAS DEEP WEAR CAUSED BY FAIRING. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-21-11.

Part: O-RING — LEAKING (CHECK VALVE) · airframe 63,576 hrs · 23,937 cycles

NR 2 PYLON LEAKING FUEL FROM DRAIN AFT OF ENG TAILPIPE. FOUND FUEL RECIRCULATION CHECK VALVE LEAKING. REPLACED MATING SURFACE O-RING, NO LEAKS NOTED.

Part: SENSOR — FAULTED (RT WING) · airframe 63,306 hrs · 23,833 cycles

RT WING LEAK DISPLAYED ON UPPER ECAM SCREEN. R & R HEAT EXCHANGER OUTLET TEMP SENSOR IAW AMM. RAN RT ENGINE AND OPERATED BOTH PACKS FOR SEVERAL MINUTES. NO FURTHER FAULTS OCCURRED.

Part: BONDING STRAP — FRAYED · airframe 63,095 hrs · 23,750 cycles

BONDING CABLE INSULATION FRAYED ON RIGHT ANTI-ICE DUCT OUTBOARD OF ANTI-ICE VALVE. REPLACED BONDING CABLE.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 63,070 hrs · 23,741 cycles

F/O O2 MASK MICROPHONE IS INOP. REPLACED THE F/O O2 STORAGE BOX WITH THE 3 OBS O2 STORAGE BOX.

Part: REHEATER — CRACKED (BLEED SYSTEM) · airframe 63,053 hrs · 23,734 cycles

RIGHT WING LEAK DISPLAYED ON UPPER ECAM SCREEN AIR. RAN APU BLEED "BOOSTED", RAN NR 2 PACK, CHECKED FOR AIR LEAKS AT FWD END OF PACK. ACCOMPLISHED MT 36-002 AND FOUND REHEATER CRACKED. REPLACED REHEATER. RAN ENGINE CHECKED ANTI-ICE SYSTEM CHECKED OKAY.

Part: COMPUTER — FAULTY (NR 2) · airframe 63,026 hrs · 23,726 cycles

RIGHT WING AIR LEAK MESSAGE DISPLAYED. CFDS REPORTING ISSUE WITH RIGHT WING LOOP B. REPLACED NR 2 BMC AS PER AMM, OPS GOOD.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 62,447 hrs · 23,492 cycles

IR 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. NAV CONFIRMED IR 2 AT FAULT BY SWAPPING PROBLEM FOLLOWS, INSTALLED INTO ORIGINAL NR 2 POS. ACFT DOWNGRADED TO AUTOLAND LIMIT, CAT II. PLACARD CAT II INSTALLED. IR 2 NAV MODE INOP. ACFT OK TO CONTINUE.

Part: PA SYSTEM — MALFUNCTIONED · airframe 62,337 hrs · 23,450 cycles

PA SYSTEM SCRATCHY AND INTERMITTENT ALONG WITH F/A PANEL CIDS CAUTION LIGHT ILLUMINATED. INITIAL CIDS RESET, NO HELP. FOUND SYS FAULT OF CAM CHPT. REMOVED AND INSTALLED CIDS DIR 1 REF AMM. CIDS FAULT CLEARED. FOUND FLIGHT ATTENDANT HANDSET SQUEAL AND FEEDBACK ASSOCIATED WITH GROUND HEADSET JACK. CLEANED JACK AND CYCLED HEADSET INTO JACK. BOTH FLIGHT ATTENDANT HAND SETS FUNCTION RESTORED. OPS CHECKED GOOD WITH NO FEEDBACK. RESET CIDS AT F-A FWD PANEL. ACP'D OPERATIONAL CHECK OF PA SYSTEM, AMM 23-73-00-710-005-A & MECH-GRD CALL AMM 23-42-00-710-001-A. BOTH SYSTEMS CK'D OK.

Part: LENS — MISSING (EXIT SIGN) · airframe 61,984 hrs · 23,319 cycles

DOOR 2R EXIT SIGN. MISSING PLACARD THAT SAYS -EXIT-. RPL LIGHT LENS.

Part: CONTROL UNIT — MALFUNCTIONED (CABIN) · airframe 61,328 hrs · 23,057 cycles

OPERATIONAL TEST OF SDCU 10WQ FAILS. CABIN INDICATIONS ARE NORMAL, STEP 4. A. NO FLIGHT DECK EFFECTS OCCUR (NO MSTR CAUTION, CONT CHIME OR ECAM ALERT) FOR ANY & ALL LAVS. REPLACED SDCU PER AMM, NO HELP. RE-INSTALLED ORIG UNIT. TESTED SYSTEM. TESTED SYSTEM REF AMM 26 -17-00 PG 503 AND EC-RA 2617-01002. SYSTEM PASSED TEST.

Part: UNKNOWN — MALFUNCTIONED (SMOKE WARNING) · airframe 61,328 hrs · 23,057 cycles

AFT LAV SMOKE ALARM SOUND THEN TURNED OFF ON ITS OWN. NO SMOKE OR FUMES WERE DETECTED. TESTED SYSTEM REF AMM 26-17-00 PG 503 AND EC-RA 2617-01002. SYSTEM PASSED TEST.

Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT) · airframe 61,156 hrs · 22,982 cycles

BOTH CAPT AND F/O SLIDING WINDOWS STUCK OPEN LUBED BOTH CAPT AND F/O SLIDING WINDOWS. OPS CHECK OK ON BOTH.

Part: TIRE — FAULTY (NLG) · airframe 60,643 hrs · 22,781 cycles

SIGNIFICANT NOSE WHEEL VIBRATION TAKEOFF AND LANDING. REPLACED BOTH NLG TIRE ASSYS.

Part: STRUCTURE — DELAMINATED (NR 1 INTAKE) · airframe 60,228 hrs · 22,615 cycles

DELAMINATION ON PATCH 1 ENGINE INTAKE. REFERENCE MT 71-006 ITEM 8 UNDER LIMITS OK TO CARRY FORWARD REPAIR FOR 10HRS, FOR SMALL HOLES UP TO ONE-QUARTER INCH HOLE IS .325 IN DIA , LOCATED AT THE 7:00 POSITION NR 1 ENG. ACCOMPLISHED REPAIR PER MT 71-006.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 59,833 hrs · 22,450 cycles

LEFT BRAKE PEDDLE MASTER CYLINDER IS BY PASSING WITH BRAKES OFF. LEFT IND SHOWS 1000LBS. REPLACED LEFT LOW PRESSURE BRAKE PEDDLE MASTER CYLINDER. NO HELP STILL SHOWS 1000 PSI ON TRIPLE INDICATOR WITH BRAKE OFF.

Part: BRAKE ASSY — OVERTEMP (MLG) · airframe 59,833 hrs · 22,450 cycles

DIVERTED TO DEPARTURE, DUE TO HOT BRAKES.

Part: SEAT — FAULTY (COCKPIT) · airframe 59,639 hrs · 22,371 cycles

FIRST OFFICER SEAT WILL NOT MOVE WITH MANUAL LEVER. ELECTRIC MOTOR OK. REPLACED SEAT ASSY.

Part: CONTROL PANEL — FAULTED (EMERGENCY LIGHT) · airframe 59,559 hrs · 22,336 cycles

CABIN EMERGENCY LIGHTS COME ON WHEN GROUND POWER TURNED OFF. REPLACED AFT FLIGHT ATT PANEL, OPS CHECKED GOOD. ACCOMPLISHED OPS CHECK OF EMERGENCY LIGHTS AND LIGHT PANEL ALL CHECKED OKAY.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 59,519 hrs · 22,322 cycles

L2 DOOR EMERGENCY LIGHT COVER MISSING. REPLACED AFT ATTENDANT LIGHT PANEL, OP CHECKED GOOD. EMERGENCY EXIT PATHWAY AND EXIT LIGHTING OPS CHECKED GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 59,090 hrs · 22,139 cycles

ROW 37 A-C EMERGENCY LIGHT WIRING CUT. FOUND THE INSULATION ON ONE WIRE WAS DAMAGED. INSTALLED ELECTRICAL TAPE. NO STRANDS OF WIRE WERE CUT. REPAIR THE CABLE PER MM 20-53-20.

Part: OXYGEN MASK — MISINSTALLED (CABIN) · airframe 59,061 hrs · 22,128 cycles

OXYGEN MASKS DROPPED AT ROW 31 DEF. COMPLIED WITH MAINT TIP 35-003 DROP TEST DUE IN 3D. INSTALLED MASK O2 PROPERLY CHECK CONTAINER O2 MASK ALL OK AND PERFORMED OPERATIONAL CHECK IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

FRAME 58 CORRODED AT STRINGER 43L. MAJOR REPAIR ACCOMPLISHED LNSTALLED REPAIR PER SRM 53-00-12 FIG 201 ON NR #'S V1974J, V1464I BY 395820 AND INSPECTED. MUST BE RE-INSPECTED AT 60000C FROM REPAIR EMBODIMENT CURRENT PTC IS 22107.

Part: SLIDE — DELAMINATED (RT OVERWING) · airframe 59,017 hrs · 22,107 cycles

RT OVERWING SLIDE ASSY HAS MULTIPLE POINTS ON OUTER FACE WITH DELAMINATION AND IS DEBONDED. REMOVED AND REPLACED RIGHT OVERWING SLIDE. OP CHECKED GOOD IAW AMM.

Part: SELECTOR VALVE — LEAKING (MLG) · airframe 59,017 hrs · 22,107 cycles

MLG GEAR DOOR SELECTOR MANIFOLD ASSY LEAKING. REMOVED AND REPLACED MLG DOOR SELECTOR VALVE. LEAK AND OPS CHECKED GOOD IAW MM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 59,017 hrs · 22,107 cycles

PRE-EXISTING FRAME REPAIR TO FR 76 BETWEEN STR 32L TO 32R. REMOVED EXISTING REPAIR PER SRM. PERFORMED ROCKWELL INSPECTION TEST AND VERIFIED 3 EACH REPAIR ANGLES ARE 2024-T4, REF: GN-MM 1-0-7-003. REINSTALLED SAME REPAIR PARTS PER SRM 53-00-12, FIG 203 ON NON ROUTINE V1411I. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVAL OF 60,000C FROM REPAIR 085625 EMBODIMENT FOR WEIGHT VARIANT 007. CURRENT PTC 22107.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,017 hrs · 22,107 cycles

DENT IN FUSELAGE SKIN BETWEEN FRAME STATIONS FR 63- TO FR 64 RT & STR 31R. EVALUATED DENT AND REWORKED SKIN PER SRM, TABLE 101 AND PARA. 4.I. ACCOMPLISHED HFEC PER NDT 6-51-10-08 AND NO CRACKS FOUND. DOCUMENTED ON NON ROUTINE V1445I. PER SRM 53-41-11, TABLE 101, DENT DRESS OUT REQUIRES FUTURE SUPPLEMENTAL INSPECTIONS PER SRI 53-41-11-1-9-0, AT 60,000C TOTAL AIRFRAME CYCLES.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 59,017 hrs · 22,107 cycles

PRE-EXISTING STRINGER REPAIR BETWEEN FRAMES FR 75 AND FR 76 AT STRINGER 34, (CENTERLINE), HAS NO DOCUMENTATION RECORDED IN HISTORY. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW REPAIR PER SRM ON NON ROUTINE V1420I. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVAL OF 60,000FC FROM REPAIR EMBODIMENT. CURRENT PTC IS 22107.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 59,017 hrs · 22,107 cycles

PRE-EXISTING STRINGER REPAIR BETWEEN FRAMES FR 75 AND FR 76 AT STRINGER 33R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW REPAIR PER SRM ON NON ROUTINE V1418I. PER SRM, THIS REPAIR MUST BE REINSPECTED AT DEFINED INTERVAL OF 60,000FC FROM REPAIR EMBODIMENT, REF: SRI 53- 00-13-2-001-00. CURRENT PTC IS 22107.

Part: STRINGER — UNKNOWN (FUSELAGE) · airframe 59,017 hrs · 22,107 cycles

PRE-EXISTING STRINGER REPAIR BETWEEN FR 75 AND FR 76 AT STRINGER 33L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW REPAIR PER SRM ON NON ROUTINE V1419I. PER SRM, THIS REPAIR MUST BE REINSPECTED AT DEFINED INTERVAL OF 60,000FC FROM REPAIR EMBODIMENT. REF: SRI 53- 00-13-2-001-00. CURRENT PTC IS 22107.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 39R HAS CORROSION BETWEEN FR 58 AND 59. INSTALLED STRINGER REPAIR PER SRM ON V1977J AND V1390I.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 40R HAS CORROSION BETWEEN FR 58 AND 59. INSTALLED STRINGER REPAIR PER SRM ON V1976J AND V1193I.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 39R HAS CORROSION BETWEEN FR 58 AND 59. INSTALLED STRINGER REPAIR PER SRM 53-00-13 FIG 201 ON V1977J AND V1390I. MAJOR REPAIR

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 40R HAS CORROSION BETWEEN FR 58 AND 59. INSTALLED STRINGER REPAIR PER SRM 53-00-13 FIG 201 ON V1976J AND V1193I. MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

SKIN CORRODED IN AFT CARGO BAY BETWEEN FR 58 AND 59 AND BETWEEN STR 42L AND 43L. AFTER FURTHER EVALUATION, FOUND DAMAGE TO BE WITHIN LIMIT OF SRM ON NR V1972J. AREA TREATED PRIMED AND PAINTED. MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 41L HAS CORROSION BETWEEN FR 57 AND 58. INSTALLED STRINGER REPAIR PER SRM ON V1705J AND V1192I.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

STRINGER 41L HAS CORROSION BETWEEN FR 57 AND 58. MAJOR REPAIR: INSTALLED STRINGER REPAIR PER SRM ON V1705J AND V1192I. MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,017 hrs · 22,107 cycles

MAJOR REPAIR, STRINGER 43R CORRODED AT FR68. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER 43R IAW SRM. NO DEFECTS NOTED.

Part: ACTUATOR — FAULTY (RUDDER PEDAL) · airframe 58,326 hrs · 21,820 cycles

CREW REPORT: CAPT RUDDER PEDDLES DON'T COME FORWARD WHEN TAB IS PULLED. REPLACED CAPT PEDAL ACTUATOR PER AMM. OPERATES NORMALLY.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 58,125 hrs · 21,734 cycles

CAPT OXYGEN PRESS TO TEST INOP YELLOW INDICATOR WILL NOT SHOW. REPLACED CAPT O2 MASK ASSY, SYSTEM OPS CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 57,657 hrs · 21,532 cycles

SMOKE LAV - CRG DET ECAM. NO TIME DENMM. REPLACED LAV 'F' SMOKE DETECTOR, ALL TESTS PASS.

Part: HINGE FITTING — FAULTY (L1 DOOR) · airframe 57,623 hrs · 21,516 cycles

DOOR 1L PRESSURE LEAK. IN PREPARATION FOR MAINT FERRY, PRESSURIZE THE AIRCRAFT AND ENSURE NO PRESSURIZATION LEAKS FROM DOOR 1L. ACCOMPLISHED PRESSURIZATION OF AIRCRAFT PER MM. NO LEAKS NOTED AT DOOR 1L; RAN AIRCRAFT UP TO 4.5 DPI. REMOVED L1 DOOR, ACP HIDDEN DAMAGE PER MM AND NDT OF SUSPECT AREAS PER NTM. REPLACED UPPER AND LOWER HINGE FITTINGS AND HARDWARE PER SRM ON NR`S V5086H, V5085H, NR B8063Z, B8068Z, V5081H AND B8062Z AND INSPECTED. REINSTALLED DOOR PER MM AND RIG CHECKED ACP'D. NOTICED THAT THE UPPER HINGE BEARING ON DOOR 1L DISTORTED. UPPER BEARING REPLACED WITH FITTING ASSEMBLY. FOUR CRAS WERE WELD REPAIRED ON THE AFT LAV SERVICE PNL AT INNER PAN FILLET AT C-04 VISIT PER UA-EVA-81154A. THERE WAS ONE CRACK ABOVE EACH HINGE AND BELOW EACH LATCH CLIP. ACCOMPLISH DVI OF THE WELDS AT 20 MONTH INTERVALS BEGINNING MARCH 4,2013.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 56,789 hrs · 21,152 cycles

SLIDE ARM LIGHT WILL NOT ILLUMINATE WITH DOOR CLOSED AND ARMED ALL THE TIME. SLIDE ARMED LIGHT IS INTERMITTENT. FOUND GIRT BAR INTERFERING WITH SCUFF PLATE. REMOVED EXCESS SEALANT UNDER SCUFF PLATE AND REINSTALLED. ARM HANDLE AND LIGHT INDICATION NORMAL.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 56,764 hrs · 21,141 cycles

CREW REPORTS LOSS OF CABIN PRESSURE WITH OUTFLOW VALVE FAILED. CREW REPORTS O2 MASKS ARE NOT DROPPED. DEPLOYED AND MANUAL FUNCTION OF OUTFLOW VLV INOP AS WELL. REPLACED OUTFLOW PER AMM AND NR 1 PRESSURE CONTROLLER AND TESTED.

Part: HANDLE — LACK OF LUBE (CARGO DOOR) · airframe 56,634 hrs · 21,076 cycles

AFT CARGO DOOR ECAM, RTFL AFT CARGO OVHT DOOR AFT CARGO. ECAM WRN: 21-43 COND AFT CRG HEAT FAULT. SUSPECT 644-0096 (11HC) PRESS REG VALVE, PROX SWITCH (50WV) 565-0047. PFR SHOWED DOOR AFT CARGO & COND AFT CARGO HEAT FAULT WITH LGCIU 1 REPORTED AFT CARGO DOOR HANDLE PROX SENSOR 34WV TGT POS. WHILE WORKING DF178 FOUND AFT CARGO PIT HANDLE HOOK STIFF AND BINDING. LUBED HANDLE COVER HOOK AND OPS CHECKED OK, LIGHT TESTED OK WITH HANDLE CYCLED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,293 hrs · 20,934 cycles

FAILS EMERGENCY LIGHT TEST EXT LOADS AFT LEFT MESSAGE. COMPLETED TEST OF AFT SLIDE RAFTS AND FOUND AFT RT HAS BAD LIGHT. REPLACED 2R DOOR SLIDE PER MM, OPS CHECKED NORMAL. VERIFIED INSTALLATION OF DOOR 2R SLIDE PER MM. SLIDE SHOWS ARMED AND CIDS TESTS NORMAL.

Part: SLEEVE — DELAMINATED (THRUST REVERSER) · airframe 56,071 hrs · 20,836 cycles

NR 2 ENG INBD THRUST REVERSER SLEEVE HAS WIRE MESH MISSING AND DELAMINATED. NR 2 ENG INBD REV SLEEVE, R & R SLEEVE.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 55,316 hrs · 20,472 cycles

RIGHT NR 2 SLAT HAS DENT. BEGAN REMOVING SLAT PER MM. DURING SLAT OPS CHECK, HAD NR 2 SFCC FAULT ONE CAM, COULD NOT RESET, SWAPPED MSG FOLLOWED, BACK TO ORIGINAL POS. REPLACED NR 2 SFCC REF AMM, GDN TEST PASSED, CAT III TEST WILL BE ON SMC13. LARGE DENT IN LE SLAT IMM OTBD OF RIGHT SIDE ENGINE. DENT IS 4 X 2.5 INCHES AND JUST SHY OF 3MM DEPTH. REPLACED NR 2 SLAT, OP CHECKED GOOD, NO FAULTS.

Part: COWLING — DELAMINATED (LT ENGINE) · airframe 54,802 hrs · 20,200 cycles

FOUND DELAMINATED ON NR1 ENGINE LT SIDE FAN COWL RT OF OIL ACCESS DOOR. REMOVED FAN COWL AND ROUTED TO SHOP 273. R & R REPLACED WITH FAN COWL FROM ANOTHER ACFT.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 54,648 hrs · 20,130 cycles

EMERGENCY EXIT LIGHT CHECK FAILED. EXTERNAL LOADS AFT L DISPLAYED. CYCLED CB'S, NO HELP. HAD 'EXTERIOR LOADS FAULT' ON 13WL AFT LEFT EPCU. REPLACED DOOR 2L SLIDE ASSY. INSPECTED DOOR SLIDE 2L INSTALLATION FOR SECURITY, ELEC CONNECTION AND CABLE ROUTING GOOD, BOTTLE PIN REMOVED FROM SLIDE, DOOR ASSIST BOTTLE REARMED. ALL TEST GOOD.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 54,515 hrs · 20,062 cycles

DURING TEST OF EMERGENCY LIGHT SYS GOT MESSAGES 'INT. LOADS FWD L', 'EXT LOADS FWD L', 'EXT LOADS AFT L'. FOR THE INT. LOADS FWD L FOUND EMERGENCY LIGHT AT SEAT 6ABC SHORTED. REPLACED LIGHT, LIGHT OP CHECKS OK. THE EXT LOADS AFT L, SUSPECT AFT LEFT SLIDE. REPLACED DOOR 2R SLIDE. SYSTEM NOW OPS CHECK NORMAL.

Part: SLIDE — FAULTY (LEFT) · airframe 54,153 hrs · 19,903 cycles

MESSAGE EXT LOADS LT AFT DISPLAYED ON PTP FOR EMERGENCY LIGHT TEST. REPLACED LT AFT DOOR ESCAPE SLIDE. INSP'D SLIDE AT DOOR 2L, SLIDE SECURED ON DOOR, PIN REMOVED AND STOWED, ASSIST BOTTLE RE-ARMED AND SAFETIED, EMERGENCY LIGHTS TEST OKAY. ACFT RETURNED TO NORMAL.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 54,024 hrs · 19,846 cycles

DURING CABIN CREW SERVICE CHECK AND 3SV MX CHECK OF THE EMERGENCY LIGHT CHECK, CIDS MESSAGE EXT. LOADS AFT L. 2L DOOR EMERGENCY LIGHTS INOP. ALL EMERGENCY LIGHTS ARE INOP AND ALSO THE AFT OUTER LT WING EMERGENCY LIGHT. CHECKED POWER PACK AND LIGHT FOUND TO CAUSED BY THE AFT LT SLIDE. ALL OTHER EMERGENCY LIGHT CHECKS OK FROM MASTER EMERGENCY LIGHT SWITCH IN COCKPIT AND ARMING INDICATION ON DOOR PAGE NORMAL. REPLACED SLIDE ON SMB W-U E3387D, TESTED CID, OK, NO MESSAGE.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 53,567 hrs · 19,631 cycles

EMERGENCY LIGHT TEST FAILS LT AFT EXT LOAD. CONFIRMED RT2 RT SLIDE ASSY FAILS EMERGENCY LIGHT TEST. REMOVED SLIDE ASSY. REPLACED IAW MM. INSPECTED THE INSTALLATION AND SAFETY OF THE DOOR 2R SLIDE ASSY. BOTTLE PIN REMOVED AND STOWED, DOOR ASSIST BOTTLE ARMED, CABLE ROUTING CORRECT AND EMERGENCY TESTS ARE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,567 hrs · 19,631 cycles

EMERGENCY LIGHT TEST FAILS LEFT FWD BATTERY. REPLACED BATTERY 10WL. CHECKED GOOD.

Part: SCREEN — DELAMINATED (THRUST REVERSER) · airframe 53,502 hrs · 19,605 cycles

ENG 2, LOOKING FROM AFT, ON LT \C\ DUCT (COLD AIR BYPASS), AT APPROX 7 TO 7:30' O CLK, ACOUSTIC MATERIAL IS TORN-MISSING. LCL FBO REPORTS LT 'C' DUCT SCREEN MESH IS DELAMINATED APPROX .22.2 INCH BY 9.0 INCH (199.80 SQ INCHES) WITHIN 25HRS FLY BACK LIMITS OF AMM. DO AN ADHESIVE REPAIR WITHIN 25HRS. AREA OF DELAM HAS GROWN TO 360 SQ IN, REPAIRED IAW MX TIP 78-010.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 53,419 hrs · 19,564 cycles

PARTIAL ILLUMINATION OF EMERGENCY EXIT SIGNS AT BOTH DOORS AND SOME CABIN LIGHTS. REPLACED AFT LT EPSU AND BATTERY, SYS TEST OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 52,899 hrs · 19,322 cycles

SEAT 14C AISLE EMERGENCY EXIT LIGHT INOPERATIVE. FOUND CONNECTION UNDER SEAT 14A SEU COMPARTMENT DISCONNECTED. REPAIRED CONNECTION.

Part: CYLINDER — LOW (L2 DOOR) · airframe 52,899 hrs · 19,322 cycles

DOOR 2L EMERGENCY DAMPER CYLINDER BELOW 3 SVC TEMP, ADJUSTED PRESSURE. SERVICED IAW MM. NO LEAK FOUND DURING LEAK CHECK. PRESSURE WAS 800 PSI BEFORE SERVICING.

Part: FITTING — DIRTY (R2 GIRT BAR) · airframe 52,575 hrs · 19,156 cycles

DOOR 2R ARMING LEVER DOESN'T STAY DOWN IN FLIGHT. ACCOMPLISHED COLD WEATHER DOOR MX PRATICES IAW MM 12-31-52 PAGE 201. CLEANED DRAIN HOLES & CLEANED GIRT BAR FITTINGS.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 51,934 hrs · 18,860 cycles

CIDS REPORTS FAILURE OF EMERGENCY LIGHTING IN AFT LEFT DOOR SLIDE. FOUND BAD SLIDE LIGHTING. REPLACED SLIDE. ACCOMPLISHED INSPECTION OF SLIDE 2L INSTALLATION.

Part: BATTERY — FAILED (CABIN) · airframe 51,730 hrs · 18,752 cycles

LT FWD EMERGENCY BATTERY FAILS CHECK PER 3 SVC. REPLACED BATTERY, OP CHECKED OKAY.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 50,926 hrs · 18,396 cycles

CABIN EMERGENCY LIGHTS FAIL. EPSU EXT LOADS AFT L. TROUBLESHOT SYSTEM. FOUND DOORS 2L AND 2R SLIDE LIGHTS INOP WILL NEED 2 SLIDES. REPLACED AFT RIGHT DOOR SLIDE AND THE LEFT AFT DOOR SLIDE. REPLACED AFT RIGHT DOOR SLIDE AND THE LEFT AFT DOOR SLIDE.

Part: SLIDE — FAULTY (DOOR) · airframe 50,346 hrs · 18,170 cycles

CABIN EMERGENCY LIGHT TEST FAILED. FAULTS \EXT LOADS AFT L. INSTALLED SERVICABLE CONTROLLER & BATTERY. RAN TEST STILL FAULTS 'EXT LOADS AFT L 33-51-38'. RETURNED ORIGINAL UNIT BACK TO ACFT, SUSPECT EMERGENCY SLIDE EITHER LT OR RT. REPLACED LT AFT DOOR SLIDE. TESTS OK.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 49,932 hrs · 17,986 cycles

FIRST OBSERVERS O2 INOP. REPLACED 2ND OBSERVER'S O2 MASK. ACCOMPLISHED OPS TEST. TESTS OKAY.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 49,932 hrs · 17,986 cycles

EMERGENCY EXIT LIGHT TEST FAILS FAULTING EXT LOADS AFT L. DOOR 2RT SLIDE CAUSING TEST TO FAIL, NEEDS SLIDE REPLACEMENT. REPLACED DOOR 2 RT ESCAPE SLIDE. ACCOMPLISHED EMERGENCY LIGHT TEST AND TEST PASSED.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 48,607 hrs · 17,386 cycles

EMERGENCY LIGHTS FAILED TEST, FAULTING L AFT EXTERNAL LOAD. REPLACED 2R EMERGENCY ESCAPE SLIDE. ACCOMPLISHED EMERGENCY LIGHT TEST. NO DEFECTS NOTED. INSPECTED SLIDE AT 2R, FOUND SECURED ON DOOR, CABLE ROUTED CORRECTLY, EMERGENCY LIGHT TESTS OK.

Part: SLIDE — NO TEST (L2 DOOR) · airframe 48,202 hrs · 17,242 cycles

CABIN EMERGENCY SLIDE CHECK DID NOT PASS.

Part: LIGHT — FAILED (CABIN) · airframe 47,597 hrs · 17,040 cycles

THE 3 SVC EMERGENCY LIGHT TEST FAILS, "EXT LOADS L AFT".

Part: CONNECTOR — UNSECURE (CABIN) · airframe 47,478 hrs · 16,994 cycles

NR 3 SERVICE CABIN EMER LIGHT CHECK FAILED. INT LOADS EMER R AND EXT LOADS AFT L. REMOVED AFT LT SLIDE AND RESET CONNECTOR AND RE-INSTALLED AND TEST NOW OK.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 46,820 hrs · 16,773 cycles

WHILE ACCOMPLISHING TEST OF EMERGENCY LIGHTING SYSTEM, HAVING FAULT MESSAGE EPSU EXT LOAD AFT LEFT. INTERNAL ELECTRICAL FAILURE IN SLIDE 2L. REPLACED SLIDE 2L WITH BORROWED PART.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 46,669 hrs · 16,726 cycles

ON PTP PANEL TEST GOT EXT LOADS AFT L MESSAGE. INTERNAL SHORT IN 2L SLIDE. REPLACED DOOR 2L SLIDE. OPS CHECKED NORMAL.

Part: CIRCUIT BREAKER — OUT OF TOLERANCE (CABIN) · airframe 46,559 hrs · 16,686 cycles

FOUND EXT LOADS AFT L ON 3 SVC. RESET EMERGENCY LIGHT CIRCUIT BREAKER, OPS CHECKED NORMAL.

Part: CONTROL HANDLE — WORN (COCKPIT) · airframe 46,143 hrs · 16,550 cycles

AFTER TAKEOFF TOOK 3 ATTEMPTS TO RAISE GEAR HANDLE. WEAR/PLAY IN THE LANDING GEAR CONTROL HANDLE. REPLACED THE LANDING GEAR CONTROL HANDLE. GEAR SWINGS ARE NORMAL.

Part: UNKNOWN — UNKNOWN (NAVIGATION) · airframe 46,103 hrs · 16,538 cycles

CAPT LOST PARTIAL NAV DISPLAY FROM 80 MILE RANGE TO 10 RANGE. F/O LOST PARTIAL NAV DISPLAY. RMP FAILURE. SHOP COULD FIND NO IMMEDIATE FINDINGS -CHRONIC UNIT- UNIT WAS REPROGRAMMED BUT NOT YET REINSTALLED ON ANY A/C.

Part: OXYGEN SYSTEM — LOW (CREW O2) · airframe 46,004 hrs · 16,503 cycles

THE O2 NEEDS SERVICE. SERVICED CREW O2.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 44,602 hrs · 15,985 cycles

ECAM WARNING LANDING GEAR NOT DOWN AND LOCKED. TWO TIMES NO LGCIU FAULTS OR OTHER INDICATIONS. UNABLE TO DUPLICATE ON GROUND, BUT REPLACED LGCIU AS PRECAUTION. SEVERAL GEAR SWINGS, SYSTEM CHECKS OUT NORMAL. NO REPEATS SINCE ORIGINAL.

Part: RESERVOIR — UNKNOWN (EMERGENCY EXIT) · airframe 44,253 hrs · 15,854 cycles

CIDS CAUTION LIGHT ON AT THE F-AS PANEL. REPLACED LT OVERWING RESERVOIR AS PRECAUTION. NO CIDS CAUTION LIGHT.

Part: BELLOWS — RUPTURED (A/C PACK) · airframe 44,149 hrs · 15,816 cycles

UNABLE TO COOL COCKPIT. FULL COLD SUPPLIES 80 DEGREE AIR WITH HOT AIR SWITCH OFF. STILL 80 DEGREES. FOUND LEFT PACK BELLOWS HAS LARGE RUPTURE BETWEEN AIR PACK 1 OUTLET AND MIXER UNIT. ALSO FOUND DUCTING PARTIALLY CLOGGED WITH LINT. REPAIRED BELLOWS AND REMOVED LINT. REPLACED NR 1 PACK ANTI ICE VLV, ZONE TEMP CONTROLLER, COCKPIT CABIN TEMP SENSOR, LT RECIRC FILTER, 24HK LT MIXER UNIT TEMPERATURE SENSOR AS PRECAUTIONARY.

Part: CIRCUIT BREAKER — POPPED (CABIN) · airframe 44,091 hrs · 15,796 cycles

EXIT PATH LIGHTING DOES NOT ILLUMINATE ROWS 12, 13, 14, 18, 19 & 20. RESET CIRCUIT BREAKER & TESTED EMERGENCY LIGHTS, OPS CHECK NORMAL.

Part: A/C PACK — OVERHEATED · airframe 43,745 hrs · 15,670 cycles

RTFL DUE TO PACK OVERHEAT PROBLEM.

Part: WIRE — DAMAGED (EVAC SLIDE IND) · airframe 43,730 hrs · 15,662 cycles

CIDS DISPLAY LEFT EMERGENCY SLIDE BOTTLE LOW PRESSURE. [06-26-07] FOUND OPEN WIRE DEU-B (300RH4) PIN 36 TO PLUG 7555VC-A PIN A. BOTH CONNECTORS VERIFIED OK. SUSPECT LOST CONNECTION AT TERMINAL BLOCK 7225VT OR 7223VT. RESEATED PINS 3CD AT TERMINAL BLOCK 7223VT JUST FWD OF WALLBOX 50MK3.

Part: BUTT JOINT — DAMAGED (FUSELAGE) · airframe 43,644 hrs · 15,627 cycles

REINSTALLED DOUBLER REPAIR AFTER AFT SKIN REPLACEMENT. DOUBLER LOCATED AT FR 70 BUTT JOINT STR 34. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW DOUBLER AT BUTT JOINT.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 42,239 hrs · 15,119 cycles

DOOR 1L FAILED EMERGENCY LIGHT TEST. REPLACED EPSU. OPS TESTS OK.

Part: BRACKET — BROKEN (SLIDE) · airframe 42,044 hrs · 15,049 cycles

FWD RIGHT MED EMERGENCY SLIDE PACK DOOR SUPPORT BRACKET BROKEN. REPLACED FORWARD RT DOOR SLIDE.

Part: LIGHT — NO TEST (CABIN) · airframe 41,607 hrs · 14,879 cycles

EMERGENCY LIGHTS FAIL 3 SVC TEST, EXT LOADS AFT L. REPLACED RIGHT AFT DOOR SLIDE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 41,175 hrs · 14,706 cycles

EMERGENCY LIGHT TEST FAULTS -BATTERY AFT L-. REPLACED BATTERY. TEST PASSED.

Part: LIGHT — ODOR (CABIN LIGHT) · airframe 40,878 hrs · 14,591 cycles

HOT ELEC SMELL AT DOOR 1L. ENTRY LIGHT WARM. TURNED OFF LIGHT AND SMELL GONE. DROPPED LIGHT PANEL AND INSPECTED AREA NO SMELL NOTED, ALSO BALLEST NOT HOT.

Part: SKIN — DAMAGED (2R DOOR) · airframe 38,885 hrs · 13,864 cycles

DOOR 2R PUSHED WAS UP BY GROUND EQUIPMENT CAUSING A 2.5 INCH HIGH AND 30 INCH LONG BEND IN THE LOWER AFT EDGE OF THE DOOR. LOWER EDGE OF THE DOOR WAS ALSO BENT INBOARD 1 INCH. PERFORMED A DOUBLER REPAIR PER SRM 52-10-00-201. MAJOR REPAIR ON A PSE PER UNITED DECISION DIAGRAM. REPLACED RETAINER CLIP & ANGLE "X"MEMBER, T4626. PRESSURE CHECKED WITH NO LEAKING FOUND.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,030 hrs · 13,188 cycles

FIRST OFFICER'S WINDSHIELD CRACKED. REPLACED WINDOW DUE TO CRACKING AND DELAMINATION.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 34,131 hrs · 12,145 cycles

LANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC SYSTEM. *S/D* AIRCRAFT EXPERIENCED GREEN HYDRAULIC QUANTITY LOSS INFLIGHT. FOUND B-NUT LOOSE AT BRAKE PRESSURE ACCUMULATOR. TIGHTENED B-NUT, NO LEAKS.

Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 34,119 hrs · 12,140 cycles

FLT EXPERIENCED LOSS OF ALL QTY GREEN HYDRAULIC SYSTEM. DECLARED EMERGENCY & CONTINUED TO PLANNED DESTINATION. AIRCRAFT LOST GREEN HYDRAULIC QUANTITY INFLIGHT. LANDING GEAR EXTENDED VIA GRAVITY. OAKLAND SERVICED GREEN SYSTEM TO FULL. RAN ALL SYSTEMS, VERIFIED NO LEAKS AND CHECKED ECAM FOR QUANTITY AND PRESSURE. ALL INDICATIONS NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENGINE) · airframe 33,126 hrs · 11,813 cycles

ENG 1 AGENT 1 DISCHARGE LIGHT STAYS ILLUMINATED. FLIGHT DIVERTED. CLEANED BOTTLE, RESET FDU, TESTED OK.

Part: CONTROL UNIT — MALFUNCTIONED (SMOKE DETECTION) · airframe 28,447 hrs · 10,005 cycles

FLIGHT MADE AN EMERGENCY LANDING DUE TO A FIRE WARNING IN THE AFT CARGO PIT. SMOKE DETECTOR CONTROL UNIT WAS REPLACED.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 26,454 hrs · 9,197 cycles

CARGO (FORWARD) DOOR ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE SHOWED OPEN PASSING 10,000 FEET. AIRCRAFT RETURNED TO FIELD. HANDLE WAS STOWED AND LIGHT EXTINGUISHED.

Part: ENGINE — STALLED (WING) · airframe 18,052 hrs

FLT CREW REPORTS SUSPECTED ENGINE STALL WHEN PULLING THROTTLE BACK TO NEAR IDLE IN ORDER TO SLOW ACFT. ALTITUDE WAS FL 350. IGNITION MSG DISPLAYED FOR APPROX 7 SECS. UNABLE TO DETERMINE WHICH ENG STALLED. *S/D* CHRONIC TOP-OF-DESCENT STALLS HAVE BEEN UNDER INVESTIGATION BY UA AND THE ENGINE MANUFACTURER IAE FOR SIX MONTHS. DURING THIS TIME FRAME INTERIM MEASURES HAVE BEEN IMPLEMENTED BY RECOMMENDING FLIGHT CREW USE OF ANTI-ICE BLEED WHEN MAKING SIGNIFICANT POWER REDUCTIONS ABOVE FLIGHT LEVEL 290. THIS HAS ELIMINATED ALL EVENTS OF STALLS SINCE THIS INCIDENT OCCURRED. A FINAL FIX FROM THE MANUFACTURER IS EXPECTED BY MARCH 2000.

Part: LIGHT — INOPERATIVE (CABIN)

EEL LIGHT INOP AT 12C. REPLACE LIGHT ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT SYSTEM TEST FAILURE DURING MAINTENANCE, NUMBER 3 SERVICE. REPLACED AFT LEFT BATTERY AND POWER SUPPLY.

Part: BEARING SEAL — WORN (NR 3 POSITION)

CREW REPORTS ON CLIMB, OIL SMELL IN CABIN. ADDED 2 QTS OF OIL, RAN ENGINE ADDED 4 MORE QTS. HAVE OIL PUDDLE IN TAILPIPE AND OIL IN LOW STAGE DUCTS. ALSO, FOUND METAL IN BLEED SCREEN. *S/D* OIL SMELL IN CABIN CAUSED BY A WORN NUMBER 3 BEARING CARBON SEAL ALLOWING OIL TO SEEP INTO THE HIGH PRESSURE COMPRESSOR GAS PATH.

Part: IDG — FAILED (NR 1)

ABORTED TAKEOFF AT ORD BETWEEN 80 AND 100 KNOTS, DUE TO NR 1 IDG LOW OIL PRESSURE WARNING LIGHT. REPLACED NR 1 IDG. IDG WAS FOUND TO HAVE A FAILED LEFT HAND FIXED UNIT BEARING SET RUBBING AGAINST THE HOUSING. THE RUBBING GENERATED SUFFICIENT METAL TO PLUG THE FILTER AND CAUSE THE WARNING LIGHT TO COME ON.

Part: RETRACT MECH — MALFUNCTIONED (NLG)

AT FL 330 MACH .80, EXPERIENCED A LOUD BANG WITH RED NOSE GEAR WARNING AND UNCOMMANDED NOSE GEAR EXTENSION. SLOWED AIRCRAFT AND GEAR RETRACTED.

Part: FLIGHT CONTROLS — MALFUNCTIONED (CONTROL SYST)

CREW REPORTED THAT AFTER TAKEOFF, AIRCRAFT WANTED TO FLY RIGHT WING DOWN, NOT STRAIGHT. AFTER ALTITUDE WAS REACHED, PROBLEM WENT AWAY. AFTER REACHING AN ALTITUDE OF 12788 CREW STATED THAT IN CLIMB AIRCRAFT TENDED TO FAVOR LT WING LOW AND AT HIGHER THAN NORMAL CRUISE FAVORED RT WING LOW CREW HAD NO ECAM MESSAGES AND NO MESSAGES ON POST FLIGHT REPORT.