N420UA

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 89,522 hrs · 35,350 cycles

PDA 1 FUEL CAP FOUND MISSING COMPLIED WITH GMM 02-30-95. TOMC CONTACTED. REPLACED FUEL CAP REF AMM 28-25-41 PARTS USED:31-2825-9-0001,QTY :1. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1686935 SN OFF 1610.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 87,894 hrs · 34,582 cycles

LOSS OF GREEN HYD SYS REPORTED. ITEM LOCKED BY TOMC ITEM UNLOCK FOR RDU MX TO CLEAR FOUND STEERING ACTUATOR B-NUT LEAKING, RE TORQUED B- NUT REF AMM 20-21-12, SERVICED GREEN SYSTEM HYD. REF 12-12-29 AND LEAKED CHECK GREEN SYSTEM REF 29-14-00. NO LEAKS NOTED AT THIS TIME. OK FOR SERVICE

Part: NONE — NONE (WATER TANK/FR35) · airframe 85,138 hrs · 33,295 cycles

WATER LEAKING FROM OUTSIDE OF BOTH FWD PIT BELLY DRAINS. WITHIN 7 DAYS ACCOMPLISH ECRA 2011-01000 CARGO CARPARTMENT SPILL CLEAN UP IN THE APPROXIMATE AREA UNDER THE FWD CARGO PIT FROM FRESH WATER SPILL. ADD EMP:U348584 APPROVED TO CARRY REF ECRA 2011-01000 REV AB WITHIN 7 DAYS TOMC-APPROVAL FROM SC1ELBYC COMMENT ACCOMPLISH ECRA 2011-01000 CARGO COMPARTMENT SPILL SECTION 2.B IN THE FWD CARGO COMPARTMENT THE FORWARD PIT, AFT CENTER ACCESS PANEL, OPENED FOR REPLACED O RING FOR WATER SUPPLY LINE. REF IPC 38-11-03. ITEM RECORDS UPDATEO.VD TROUBLESHOOTING. 130. NO LEAKS NOTED AFTER PRESURIZATION OF WATER SYSTEM T/A: 7 DAYS.OVD/U353583 QC REVIEWED. TOMC UPDATE ACCOMPLISH CLEAN UP FROM FR 24 TO 34 BETWEEN QC STGR27R-STGR27L COMPLIED WITH EC/RA#:2011-01001 STEP (2) (B) (2 THRU 5) , COMPLIED WITH EC/RA#:2011-01000 STEP (2) (B) (2 THRU 5) , REMOVED FWD CARGO FLOOR PANELS 131AF ,131EF AND 131HF REF. AMM REMOVED FWD CARGO FLOOR PANELS 131AF ,131EF AND 131HF REF. AMM 53-22-14. 53-22-14.

Part: SLAT SYSTEM — FAULTED · airframe 85,046 hrs · 33,240 cycles

*DECLARED EMERGENY*SLATS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL ITEM LOCKED CONTACT TOMC 847-700-9980. REF TSM 27-81-00-810-810-A...BSS SYSTEM 2. WE ARE IN PROCESS OF REMOVING SYSTEM 2 PCU HYD MOTOR REF AMM 27-84-54-000-002-A THROUGH STEP 4A(3). ITEM UNLOCKED FOR SHIFT CHANGE UPDATE. CONTACT TOMC ONCE LOG HAS BEEN UPDATED....TOMC SMITH REF TSM 27-81-00-810-810A , WE ACP 3A INCLUDING 3A3 SLAT SYS OPS ITEM FLAGGED FOR SDR. CHECK.SYSTEM OPERATED NORMALLY WITH NO FAULTS NOTED, ALL SLATS AND FLAPS OPERATED NORMALLY. NO BINDING OR LAGGING SLATS. WE PROCEEDED TO STEP 4B DURING THE TIME TEST WE FOUND THE BLUE SYSTEM WAS TEN SECONDS FASTER THAN THE GREEN WHICH IS SLAT ADD EMP:U142517 COMPLETED INSTALLATION OF HYD MOTOR. AMM 27-54-54-400-002A PERFORMED RII IINSPECTION OF SYSTEM 2 PCU HYD MOTOR PER AMM27-54-54-400-002A

Part: SEAL — DAMAGED (NR 1 GEARBOX) · airframe 84,452 hrs · 32,969 cycles

ON #1 ENG DO AN IDLE LEAK CHECK (TEST NO. 3) (REF. TASK 71-00-00-710-012-B). DUE TO DE-OILER GEARBOX SEAL REPLACEMENT. REF LP 6963611 AND 6961808. ACP IDLE LEAK CHECK( TEST #3) ON #1 ENG REF TASK 71-00-00-710-012-B. NO LEAKS NOTED FOR DE-OILER REPLACEMENT ADD EMP:110100

Part: LANYARD — MISSING (RT WING FUEL CAP) · airframe 84,329 hrs · 32,908 cycles

FUEL CAP LANYARD R/H WING REFUEL/DEFUEL CAP MISSING LANYARD ONLY, CAP IS STILL PRESENT DISPATCH DESK: 012 NAME: BS DATE: 05-AUG-21- APPROVED ITEM PLACED ON CDL FOUND FUEL CAP MISSING ON ARRIVAL. CONTINUE CDL 28A DEFERRAL. AIRCRAFT ARRIVED TO STATION WITH A MISSING FUEL CAP FROM PREVIOUS STATION. ADDED TO CDL MISSING FUEL CAP. DDP. C/W.

Part: CAP — MISSING (RT WING FUEL) · airframe 84,290 hrs · 32,892 cycles

PDA 2 MISSING FUEL CAP ON ARRIVAL. FUEL CAP LANYARD R/H WING REFUEL/DEFUEL CAP MISSING LANYARD ONLY, CAP IS STILL PRESENT ITEM PLACED ON CDL DISPATCH DESK: 012 NAME: BS DATE: 05-AUG-21- APPROVED FOUND FUEL CAP MISSING ON ARRIVAL. CONTINUE CDL 28A DEFERRAL.

Part: STRINGER — BENT (ZONE 100) · airframe 83,034 hrs · 32,336 cycles

STRINGER 42 LT BENT 8.5 INCHES FWD OF FRAME 63. NEW STRINGER SPLICED IN PER SRM 53-00-13-300-001 BETWEEN FRAME 62 AND 64. PER SRI 53-00-13-205-001 TABLE 006 NEED TO ACCOMPLISH INITIAL INSP AT 60,000 CYCLES OR 120,000 FLIGHT HOURS WHICHEVER COMES FIRST FROM REPAIR EMBODIMENT. SUBSEQUENT INSPECTIONS TO BE DETERMINED. WORK ACCOMP DURING C2 VISIT IN LCQ ON NR 9298004. OK TO CARRY PER SRI 53-00-13-205-001, INITIAL INSPECTION REQUIRED 60000 F/C'S OR 120000 F/HS FROM REPAIR EMBODIMENT. SUBSEQUENT INSPECTIONS AT INTERVALS TBD. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED. TOMC APPROVED: QC REVIEWED. RECORDS UPDATE T/A: 60,000FC/120,000FH FROM REPAIR BK/245861.

Part: SKIN — DENTED (ZONE 100) · airframe 83,034 hrs · 32,336 cycles

AIRCRAFT EXTERIOR HAS A DENT 23.7 X 8.8 X .326D LOCATED BETWEEN FR 63-FR 64 AND STR 41L-43L. SEE LOG PAGE 5477310 FOR HIDDEN DAMAGE INSPECTION. NO CRACKS FOUND. PER LOG PAGE 5477310: ACCOMPLISHED HIDDEN DAMAGE INSPECTION FRAME 62.5 TO FRAME 64 STRINGER 40L TO 40R USING 10X, DVI INSPECTION. NO CRACKS NOTED. AERSALE N/RS GENERATED 508564 AND 508565. REF ELB 5477392 AND 5477401. WORKED PERFORMED AT AERSALE ROW BY ASI QC-43. THIS ITEM LOCKED FOR REPAIR BY MIA MAINTENANCE. AIRCRAFT ARRIVED AT LCQ ITEM UNLOCKED FOR MAINTENANCE. PERFORMED INTERIM REPAIR, PER ECRA 5331-02690 AT LCQ ON HAECO NR# 9298001. THIS DIP IS CREATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE JULY 5, 2021. PLANNING TO CONTACT ENGINEERING IR. NOTE TO PLANNING: THIS ECRA IS BEING EVALUATED FOR DAMAGE TOLERANCE UNDER 14CFR26.43(D) AND WILL LIKELY BE MADE PERMANENT AFTER MAY 5, 2021, BUT BEFORE JUNE 5, 2021 FOR THE PERMANENT REPAIR WITH REPEAT INSPECTIONS. PART 2-INSPECTION REQUIREMENTS: NONE. PART 3-PERMANENT REPAIR: TO BE DETERMINED BY ENGINEERING. OK TO CARRY FOR PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 05JUL2021. PLANNING TO CONTACT ENGINEERING AFTER 5MAY2021 BU BEFORE 05JUN2021 FOR PERMANENT REPAIR.

Part: SHEAR TIE — CRACKED (FRAME 43) · airframe 83,034 hrs · 32,336 cycles

AD 2020-18-06; FRAME FOOT AT LEFT FR 43 CRACKED AT FASTENER HOLE BETWEEN STGR 21-22, FRAME CRACKED THROUGH. REPAIR BEFORE NEXT F LIGHT, PER HACEO LCQ NR 9298323/30323 GENERATED BY V061671. REMOVED AND REPLACED FR 43 FOOT LT ON EA 5330-06692 003.

Part: SKIN — DAMAGED (FRAME 72) · airframe 83,034 hrs · 32,336 cycles

SKIN PROTRUSION ON THE LEFT HAND AIRCRAFT EXTERIOR SKIN, 1.2L X 0.8W, LOCATED APPROX 4.6" AFT OF FRAME 72 AND 1.2" ABOVE STR 28L. EVALUATED SKIN PROTRUSION ON AIRCRAFT EXTERIOR SKIN. FOUND PROTRUSION TO MEASURE .2"(L) X .8"(W) X .030"(D). FOUND TO OUT OF SRM LIMITS, REF UA AIRBUS SRM 53-00-11-991-001 REV 134. EVAL DONE AT AERSALE ROW ON NR 507692. THIS ITEM LOCKED FOR MAINTENANCE FERRY FROM ROW FOR REPAIR BY LCQ. DAMAGE IS IN THE NON-PRESSURIZED AREA LOCATED 4.6 IN AFT OF FR 72 AND 1.2 IN ABOVE STR 28L. PROTRUSION MEASURE AS FOLLOWS: 1.2IN (L) X 0.8IN (W) X .030IN (D). HFEC WAS COMPLETED WITH NO CRACK INDICATIONS NOTED, REF AIRBUS SRM 53-00-11-991-001. ARMENTA TOMC 17NOV20. AIRCRAFT ARRIVED AT LCQ-ITEM UNLOCKED FOR MAINTENANCE. ACCOMPLISHED SMALL CUTOUT REPAIR, IAW SRM 53-51-11-300-008. THIS REPAIR IS CATEGORY B AND REQUIRES INSPECTION AT DEFINED INTERVAL S, PER SRI 53-51-11-205-012. INSPECTION FROM TIME OF ADL/REPAIR EMBODIMENT AT 60000 FC AND 120000 FH, WHICHEVER VALUE IS ACHIEVED FIRST. CURRENT FC=32336, FH=83033:55. SUBSEQUENT INSPECTION INTERVALS AND METHODS TBD. SMALL CUTOUT REPAIR ACCOMPLISHED AT HAECO -LCQ ON HAECO N/R 929 8003. ACCOMPLISHED SMALL CUTOUT REPAIR, IAW SRM 53-51-11-300-008. THIS REPAIR IS CATEGORY B AND REQUIRES INSPECTION AT DEFINED INTERVALS, PER SRI 53-51-11-205-012. INSPECTION FROM TIME OF ADL/REPAIR INSTRUCTIONS 12/14/2020 12:27 LCQ U098775 E, HILSABECK EMBODIMENT AT 60000 FC AND 120000 FH, WHICHEVER VALUE IS ACHIEVED FIRST. TOMC-APPROVAL FROM SC.

Part: SKIN — DENTED (FUSELAGE) · airframe 83,034 hrs · 32,336 cycles

SKIN PROTRUSION ON THE LEFT HAND AIRCRAFT EXTERIOR SKIN 1.2L X 0.8W. LOCATED APPROXIMATELY 4.6" AFT OF FRAME 72 AND 1.2" ABOVE STR 28L. EVALUATED SKIN PROTRUSION ON AIRCRAFT EXTERIOR SKIN. FOUND PROTRUSION TO MEASURE 1.2"(L) X .8" (W) X .030" (D). FOUND TO OUT OF SRM LIMITS, REF UA AIRBUS SRM 53-00-11-991-001 REV 134. EVALUATION DONE AT AERSALE ROW ON NR 507692. THIS ITEM LOCKED FOR MAINTENANCE FERRY FROM ROW FOR REPAIR BY LCQ. DAMAGE IS IN THE NON-PRESSURIZED AREA LOCATED 4.6 IN AFT OF FR 72 AND 1.2 IN ABOVE STR 28L. PROTRUSION MEASURE AS FOLLOWS: 1.2IN (L) X 0.8IN (W) X .030IN (D). HFEC WAS COMPLETED WITH NO CRACK INDICATIONS NOTED, REF AIRBUS SRM 53-00-11-991-001. ARMENTA TOMC 17NOV20 AIRCRAFT ARRIVED AT LCQ, ITEM UNLOCKED FOR MAINTENANCE.

Part: STRINGER — CORRODED (FRAME 66) · airframe 79,230 hrs · 30,600 cycles

(A3NB-533-6185)(L-69-003) CORROSION FOUND ON STR 39R AFT OF FR66 AAR NONROUTINE 9020117 REPAIRED STR 39 AFT OF FR66 IAW A320 SRM 53-00-13-300-001 AAR N ONROUTINE 9020117 ADD EMP:V918822

Part: DOUBLER — NOT REPORTED (AFT CARGO) · airframe 79,230 hrs · 30,600 cycles

A3NB-53-3-6179(A33-124) AFT CARGO BAY FUSELAGE INTERNAL REINFOR EMENT DOUBLER IAW A320 SRM 51-72-11-911-001, INSTALLED FASTENERS COMMON TO LAV SERVICE CAP IAW ECRA 5341-01140 AAR NONROUTINE 9019887 REMOVED AND REPLACED INTERNAL REINFORCMENT DOUBLER IAW A320 SRM 51-72-11911-001, INSTALLED FASTENERS COMMON TO LAVE SERVICE CAP IAW ECRA 5341-01140 ADD EMP:V918733 CREATED SHOULD HAVE BEEN: A3NB-53-3-6179(A33-124) AFT CARGO BAY FUSELAGE INTERNAL STRUCTURE AT FR64-65 AND STR38R IS CORRODED AAR NONROUTINE 9019887

Part: PLATE — CORRODED (FRAMES 65-66) · airframe 79,230 hrs · 30,600 cycles

(SPEC A3NB-53-3-6185 A-41 L-46 DOT 042) REINFORCEMENT PLATE U NDER STRGR 39R FROM FR 65-FR66 CORRODED IN MULTIPLE AREAS AAR N ONROUTINE 9019926 REMOVED AND REPLACED REINFORCEMENT PLAT UNDER STR 39R IAW A320 S RM 51-72-11-911-001. INSTALLED FASTENERS COMMON TO LAV PAN SERVI CE CUP IAW ECRA 5341-01140 ADD EMP:V918733

Part: SKIN — CRACKED (FRAME 35) · airframe 79,230 hrs · 30,600 cycles

REFERENCE AAR LOG ITEM 9019374, ROTO PROBE INSEPCTION SHOWS CRAC K INDICATION IN MULTIPLE LAYERS @ FR35, STR 30L LOWER AFT HOLE AAR ACCOMPLISHED INTERIM REPAIR, PART 1 STEPS 1-23 OF ECRA 5331- 02304. NEED TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 ON OR BE FORE 13 MAY 19. PLANNING TO CONTACT ENGINEERING AFTER 23 APR 19 BUT BEFORE 3 MAY 19 FOR PERMANENT REPAIR INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5331-02304.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

STR 40R TO STR 41R BETWEEN FR 67-FR 68 HAS MULTIPLE CORRODED FASTENERS. REMOVED AND REPLACED FASTENERS AT STR 40R BETWEEN FR 67-FR 68. BLENDED CORROSION AT STR 41R BETWEEN FR 67-FR 68. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR 41R AT FR 64-FR 69. RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11-911-001, SRM 51-7 4-00-001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

FWD CARGO BAY STR 41R CORRODED AT FR 32-33 BLENDED CORRODED AREA TO REMOVE CORR, AREA FOUND TO BE OUT OF LIMITS DUE TO THE PROXIMITY TO ADJACENT REPAIRS. REMOVED STGR41R, SLICES, AND FISHPLATES FROM FR 29.8-33.2, MATCH DRILLED NEW STR SEC FR 29.8-33.2 AND SPLICE BETWEEN FR 30-31, INSTALLED NEW STR AND SPLICE COUPLINGS, INSTALL FISHPLATES AND RESTORED SURFACE PROTECTION IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

DURING REMOVAL OF STR 41R CORRODED REPAIR SPLICE AT FR 29-30, THE CONNECTING STR FOUND CORRODED & DAMAGED FROM POINT OF CONNECTION AT FR 30-31 FWD OF FR 30 TRIMMED, LOCATED AND MATCH DRILL AND INSTALLED NEW REPAIR SPLICE BETWEEN FR 29-30 ON STR 41R IAW SRM 53-21-13-300-003. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

AFT CARGO BAY STR 39R AT FR58-64 IS CORRODED. AFTER EVALUATION OF STR 39R AT FR58-64 FOUND CORROSION NEXT TO PRODUCTION SPLICE, PROXIMITY OF MINIMUM REPAIR DISTANCE NOT MEET, FOUND TO BE OUT OF LIMITS. PREFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13-205 ADL/REPAIR EMBODIMENT 60,000FC/120,000FH INTERVALS TBD. REPAIR AT STR 39R AT FRAME 58-64 PER SRM 53-00-13- 300-001 AND SRI 53-00-13-205-001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

AFT CARGO BAY STR 40R AT FR58-64IS CORRODED. AFTER EVALUATION OF STR40R AT FR58-FR64 FOUND CORROSION UNDER FR 59. FOUND TO BE OUT OF LIMITS DUE TO LOCATION OF CORROSION. PERFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13-205-001.

Part: SPRING — DEFECTIVE (L2 DOOR) · airframe 79,230 hrs · 30,600 cycles

WHEN DOOR 2 LEFT IS CLOSED AND LOCKED LOWER ECAM SHOWS OPEN INDICATION, COMPLIED WITH MEL 5270P. DOOR LOCKS AND CLOSES AND OPENS NORMAL, DOES NOT AFFECT OPERATION OF DOOR. MX CONFIRMED THEY ARE ABLE TO VERIFY DOOR IS CLOSED AS LOCKED AT POSITION 2L. ADJUSTED PROXIMITY SWITCH OF THE LOCKING HOOK OF THE PASSENGER/CREW DOORS WITH THE ECAM DU. CHECK GOOD. OPERATIONAL TEST ACCOMPLISHED ON CUSTOMER CARD. REMOVED AND REPLACED PROXIMITY SWITCH ROLLER SPRING.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 79,230 hrs · 30,600 cycles

AAR N/R SEQ. NO. 9019667. A3NB-53-3-6105. FWD CARGO BAY STRINGER SPLICE/FITTING CORRODED @FR30-31 AND STR41R. REMOVED AND REPLACED STRINGER SPLICE/FITTING ON STR41R AT FR 3D. 8 IAW A320 SRM 51-72-11-911-001.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

A3NB-05-3-6165 A3-15 RT AFT EMERGENCY EXIT FWD & AFT IB VERTICAL FRAMES ARE CRACKED REMOVED AND REPLACED FWD AND AFT INBD VERTICLE FRAMES AT RT AFT EMERGENCY DOOR EXIT IAW A320 SRM 51-42-11, 51-44-11, AND 51-75-1 2.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

RT FWD EMERGENCY EXIT FWD AND AFT IB VERTICAL FRAMES ARE CRACKED. REMOVED AND REPLACED FWD AND AFT INBD VERTICAL FRAMES AT RT FWD EMERGENCY EXIT DOOR IAW SRM 51-42-11, 51-44-11, AND 51-75-12.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

AFT CARGO BAY STR 43L AT FR54-60 IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED STRINGER AT 43L FROM FR54-FR60 DUE TO CORROSION OUT OF LIMITS, REINSTALLED PRODUCTION SPLICE AT FR 54 AND CLIP AT FR 56 IAW SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER5100R01017 REV E.

Part: SUPPORT — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

AFT LT EMERG EXIT AFT VERTICAL SUPPORT CRACKED. REMOVED AND REPLACED VERTICAL SUPPORT AT LT EMERG EXIT DOOR, AF T LOCATION, IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-75-12.

Part: SUPPORT — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

AFT LT EMERG EXIT FWD VERTICAL SUPPORT CRACKED. REMOVED AND REPLACED FWD VERTICAL SUPPORT AT LT AFT EMERGENCY EXIT IAW SRM 51-42-11 AND 51-44-11, AND 51-75-12.

Part: SUPPORT — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

FWD LT EMERG EXIT DOOR AFT VERTICAL SUPPORT CRACKED. REMOVED AND REPLACED FWD LT EMERGENCY EXIT DOOR, AFT VERTICAL SUPPORT IAW SRM 51-42-11, SRM 51-44-11, SRM 51-75-12.

Part: SUPPORT — CRACKED (EMERGENCY EXIT) · airframe 79,230 hrs · 30,600 cycles

FWD LT EMERG EXIT DOOR FWD VERTICAL SUPPORT CRACKED. REMOVED AND REPLACED FWD LT EMERGENCY EXIT DOOR FWD VERTICAL SUPPORT IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-75-12.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

AFT CARGO BAY STR39R AT FR58-64 IS CORRODED. AFTER EVALUATION OF STR 39R AT FR58-64, FOUND CORROSION NEXT TO PRODUCTION SPLICE, PROXIMITYOF MINIMUM REPAIR DISTANCE NOT MEET, FOUND TO BE OUT OF LIMITS. PREFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13-205.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

AFT CARGO BAY STR 40R AT FR58-64IS CORRODED AFTER EVALUATION OF STR40R AT FR58-FR64. CORROSION UNDER FR 59 FOUND TO BE OUT OF LIMITS DUE TO LOCATION OF CORROSION. PERFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13-205-001.

Part: COVER — CORRODED (TORSION BOX) · airframe 79,230 hrs · 30,600 cycles

FWD CARGO BAY ENTRY TORSION BOX COVER IS CORRODED IN MULTIPLE AR EAS. REMOVED AND REPLACED FWD CARGO BAY TORSION BOX COVER IAW A320 SR M 51-72-11-911-001. AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS .029 ALLOWABLE .051 IAW A320 SRM 51 -21-13-283-002. AAR N/R 9019636. ADD EMP:V918825

Part: COVER — CORRODED (TORSION BOX) · airframe 79,230 hrs · 30,600 cycles

FWD CARGO BAY ENTRY TORSION BOX COVER IS CORRODED IN MULTIPLE AR EAS. REMOVED AND REPLACED FWD CARGO BAY TORSION BOX COVER IAW A320 SR M 51-72-11-911-001. AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS .029 ALLOWABLE .051 IAW A320 SRM 51 -21-13-283-002. AAR N/R 9019636. ADD EMP:V918825

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · airframe 79,230 hrs · 30,600 cycles

LH AFT 1292 JUST AFT OF FRAME 68 IS CORRODED AROUND HARD POINT.A AR N/R 9019742. REMOVED CORRODED SEGMENT OF Y1292 FLOOR BEAM FROM FR 68-69, INST ALLED NEW SEGMENT IAW A320 SRM 51-72-11-911-001 FLOOR BEAM REPLA CED DUE TO CORROSION OUT OF LIMITS IAW A320 UAL MT-53025.

Part: FITTING — CORRODED (GIRT BAR) · airframe 79,230 hrs · 30,600 cycles

AAR N/R SEQ NO. 9019739. UPON REMOVAL OF L2 LOWER GIRTBAR FITTIN GS, FOUND SILL TO BE CORRODED IN MULTIPLE AREAS THAT ARE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR SILL. REF A320 SRM 51-72-11-911-001

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 79,230 hrs · 30,600 cycles

(A2NB-53-3-6186 L22-007) R2 SILL CORRORED ON I/B EDGE JUST FWD OF FR68 AAR NONROUTINE 9019745 BLENDED CORROSION ON R2 DOOR SILL I/B EDGE FWD OF FRAME 68. FOUN D TO BE OUT OF LIMITS IAW A320 SRM 53-41-14-283-002 REPAIRED R2 DOOR SILL IAW A320 SRM 53-41-14-300-001 REPAIR 5 FIG 20101 (SHE ET 3) RESTORED SURFACE PROTECTION IAW A320 SRM 51-75-12-911-002 AAR NONROUTINE 9019745 ADD EMP:V918713

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

L1 DOORSILL CORRODED AROUND AFT GIRTBAR FITTING AFT OUTBOARD HOLE. CORROSION REMOVED, NDT''D, AND REPAIR WASHER INSTALLED PER SRM 53-11-14-283-005 FIG 10108 SHEETS 1-5. PER STEP 1F OF SAME SRM NEED TO ACCOMPLISH INSPECTIONS PER SRI 53-11-14-205-001. PER TABLE 30101 OF SRI NEED TO INSPECT REPAIR AT PTC 60,000 FROM ACFT FIRST FLIGHT WITH SUBSEQUENT INSPECTIONS TBD. WORK ACCOMPLISHED ON DLH NR 9019993. DIP APPROVED, NEED TO REINSPECT REPAIR AT 60000 CYCLES WITH SUBSEQUENT INSPECTION TBD. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

L1 DOORSILL CORRODED AROUND AFT GIRT BAR FITTING AFT OUTBOARD HOLE. CORROSION REMOVED, NDT'D, AND REPAIR WASHER INSTALLED PER SRM 53-11-14-283-005 FIG 10108 SHEETS 1-5.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 79,230 hrs · 30,600 cycles

FWD CARGO BAY FASTENERS CORRODED @ FR 32 AND STR 39R-40R. REMOVED AND REPLACED CORRODED FASTENERS AT CLEAT AT FR 32 BTWN S TR 39R AND 40R AND RESTORED SURFACE PROTECTION IAW SRM 51-7 2-11-911-001, ER 5100R01017 REV E. AAR N/R 9019696.

Part: LIGHT — BROKEN (CABIN) · airframe 79,230 hrs · 30,600 cycles

OVERHEAD BIN EMERGENCY LIGHT 22WL AT ROW 11DEF HAS BROKEN ATTACH LEGS. REMOVED AND REPLACED OVERHEAD BIN EMERGENCY LIGHT 22WL (P/N: 10- 1266-1) AT ROW 11 DEF IAW AMM 33-51-11-000-001-A AND AMM 33 -51-11-400-001-A. OPERATIONAL CHECK ACCOMPLISHED ON TASK CARD 18 -3351-1-7907 SEQ 546.

Part: SCREW — WORN (R2 DOOR) · airframe 79,230 hrs · 30,600 cycles

REMOVED AND REPLACED LOWER AFT STOP SCREW ON R2 DOOR IAW AMM 52-13-31-400-002-A SUBTASK 52-13-31-420-056-A. N LMR AFT STOP SCREW WORN BEYOND LIMITS ON R2 DOOR.

Part: LIGHT — SMOKE (FIRST OFFICER'S) · airframe 79,183 hrs · 30,577 cycles

CREW REPORTED ELECTRIC SMELL IN THE COCKPIT FOUND FIRST OFFICER''S MAP LIGHT SMOKING AND HOT TO TOUCH. FOUND CO-PILOTS MAP LIGHT AS SOURCE OF ELECTRIC SMELL CIRCUIT BREAKER Z06 ON PANEL LOCKED OUT PER AMM 33-12-12-000-002-A. SEE TSM 05-50-00-810-831-A, TYPE 9. REF TSM 05-50-00-810-831-A. TRACED ODER DOWN TO F/O''S SLIDING WINDOW MAP READING LIGHT. REPLACED LIGHT ASSY REF AMM33-12-12-000-003-A. RESET C/B, LIGHT CHECKS OK. NO DAMAGE TO A/C WIRES FOUND, ALL CONTAINED TO LIGHT ASSY RHEOSTAT. OK FOR SERVICE.

Part: OVEN — ODOR (GALLEY) · airframe 76,735 hrs · 29,482 cycles

ELECTRICAL SMELL FROM F/C OVEN NUMBER 105. REPLACED OVEN AT LOC 105 PER AMM 25-35-19. OPS CHECK GOOD.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 76,723 hrs · 29,476 cycles

ECAM CAUTION MESSAGE - Y ENG PUMP LO PR MESSAGE INOP. HYD YELLOW ENG 2 PUMP ECAM ON DEPARTURE WITH ASSOCIATED SOUND HEARD IN CABIN. PTU GOOD. EMERGENCY DECLARED. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-13-51. ALSO REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PRESSURE SWITCH PER MM 29-13-17. OPS AND LEAK CHKS GOOD.

Part: FITTING — OUT OF ADJUST (R2 DOOR) · airframe 75,536 hrs · 28,944 cycles

DOOR 2R SHOWS ARMED ON THE GROUND BUT NOT AT ALTITUDE. ACP'D AMM 52-13-22-820-001-A STEP F, ADJ GIRT BAR FITTINGS TO BRING J6 AND J7 WITHIN LIMITS. OP CHK DOOR AND SLIDE IND PASS REF AMM 52-73-00.

Part: CABLE — FAULTY (R2 DOOR) · airframe 75,509 hrs · 28,930 cycles

DOOR 2R SLIDE ARMED INDICATION INTERMITTENT. FINISHED INSTALLING NEW FLEXIBLE CONTROL CABLE FOR DOOR 2R PER A MM 52-13-22-400-001A.

Part: PROXIMITY SWITCH — OUT OF ADJUST (R2 DOOR) · airframe 75,390 hrs · 28,870 cycles

THE R2 DOOR WILL NOT STAY ARMED. ARMING HANDLE IN ARMED POSITION BUT SLIDE ICON INTERMITTENT. ADJUSTED THE R2 DOOR PROXIMITY SWITCH AND DOOR GIRT BAR FITTINGS IAW AMM 52-71-00-820-002-A01, AND AMM 52-13-22-820-001-A. OPS CKECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 75,393 hrs · 28,872 cycles

LEFT OVERWING EMERGENCY EXIT POWER SUPPLY FAILED TO TEST. REPLACED THE POWER SUPPLY IAW MM 33-51-38. TESTED OK.

Part: FITTING — CORRODED (FRAME 68) · airframe 75,348 hrs · 28,850 cycles

R2 DOORWAY, FRAME 68, STRINGER 23R FITTING CORRODED. THE FITTING WAS REPAIRED IAW ECRA 5310-07152.

Part: STRINGER — DAMAGED (FRAME 67) · airframe 75,348 hrs · 28,850 cycles

FOUR RIVET HOLES ELONGATED ON STRINGER 31R FWD OF FRAME 67. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11-001, REV 118.

Part: SLIDE — DELAMINATED (OVERWING EXIT) · airframe 75,348 hrs · 28,850 cycles

LT OVERWING SLIDE HAS 10" OF DELAMINATION ALONG AFT O/B EDGE. PROCURED NEW LT OVER WING SLIDE, SLIDE TO BE INSTALLED.

Part: STRINGER — CORRODED (FRAMES 66-67) · airframe 75,348 hrs · 28,850 cycles

STRINGER 25R FOUND CORRODED BETWEEN FRAMES 66 AND 67. REMOVED AND REPLACED THE STRINGER SECTION FROM FRAMES 64 TO 67 IAW SRM 51-72-11-001, REV 118.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 75,348 hrs · 28,850 cycles

R2 DOOR SILL HAS SEVERE CORROSION AT FRAME 68 UNDER GIRT BAR FITTING BLANKING PLATE, REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-001, REV 118.

Part: STRINGER SPLICE — CORRODED (FRAME 67) · airframe 75,348 hrs · 28,850 cycles

R2 DOORWAY FRAME 67, STRINGER SPLICE 31R CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11-001, REV 118.

Part: STRINGER — CORRODED (FRAMES 66-67) · airframe 75,348 hrs · 28,850 cycles

STRINGER 26R BETWEEN FRAMES 66 - 67 HAS CORROSION. REMOVED AND REPLACED THE STRINGER IAW 51-72-11-001, REV 118.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 36 ABC) · airframe 72,780 hrs · 27,711 cycles

PASSENGER OXYGEN MASK DROPPED AT SEAT 36 ABC. INSPECTION OXYGEN CONTAINER ASSEMBLY AND REPACKED THE MASKS

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,279 hrs · 27,484 cycles

CIDS EMER LIGHT TEST FAILS FOR TO MSG'S, BATTERY EMER RT & BATTERY LT. REMOVED & REINSTALL BOTH BATTERY PACKS. FAULT CLEARED & TESTED OKAY.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 70,583 hrs · 26,731 cycles

LEFT FRAME 20 CROSSBEAM SPLICE AT FLOORBEAM HAS CRACK INDICATION IN 2ND FASTENER HOLE FROM OTBD. REPAIRED LT FRAME 20 CROSSBEAM SPLICE AT FLOORBEAM 2ND HOLE OTBD IAW SRM 51-44-11 & RFT S 6000, NO SRI REQUIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,339 hrs · 22,613 cycles

SKIN DAMAGE BETWEEN FRAME 68 - 69 AT STRINGER 29L. MAJOR REPAIR. SKIN REPAIRED IAW SRM 53-41-11 FIG 215.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 70,501 hrs · 26,685 cycles

AIR RETURN DUE TO FIRST OFFICER SLIDING WINDOW CRACKED. EMER DECLARED, FIRST OFFICERS WINDOW SHATTERED. REPLACED WINDOW IAW 56-12-11-400-002A. OPERATIONS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 70,193 hrs · 26,549 cycles

NR 1 ENGINE ANTI-ICE VALVE FAILED CLOSED, DIVERTED. R & R THE ANTI-ICE VALVE IAW AMM 30-21-51. OPERATIONS CHECKED GOOD.

Part: LANDING GEAR — LOW PRESSURE (NLG) · airframe 67,161 hrs · 25,293 cycles

LANDING GEAR WOULD NOT RETRACT WHEN HANDLE SELECTED UP. FAULTING NLG EXTEND PROX SENSORS 24GA & 25GA. CHARGED NLG NITROGEN PRESS IAW AMM 12-14-614-004A.

Part: UNKNOWN — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 66,484 hrs · 25,051 cycles

AUTO FLIGHT, A - THR OFF, DISPLAYED ON UPPER ECAM SCREEN. FIRST OFFICER`S SPEED FLASH XX THEN BACK. RESET FMGC 1 & 2 FOUND FAC1 MSG RESET FAC 1. ACCOMPLISHED AFS TEST ALL PASSED, ACCOMPLISHED AUTO THROTTLE TEST IAW AMM 22-30-00-040-004-A TEST PASSED. INSPECTED BRAKES & TIRES, NO ISSUES. NO FAULT MSG'S PRESENT, OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 65,649 hrs · 24,722 cycles

ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. CYCLED CB'S L41 & L42. TRIED SECOND START ATTEMPT, APU DID NOT START. NO FLAME AT START ATTEMPT. LISTEN FOR CLICKING SOUND. IF CLICKING HEARD SUSPECT FUEL, IF NO CLICKING HEARD CHECK IGN LEADS & PLUGS FOR CONNECTION ARCHING WEAR & REPAIR OR REPLACE AS NEEDED.

Part: QUICK DISCONNECT — WORN (FIRE BOTTLE) · airframe 65,635 hrs · 24,714 cycles

NR 2 ENG, 1 FIRE EXTINGUISHER BOTTLE QUICK DISCONNECT PIPE HAS WORN GROOVE FROM NUT, NOT BEEN CONNECTED & SAFETIED. ACCOMPLISHED ON C-CHECK WU M0057H.

Part: FASTENER — MISSING · airframe 65,627 hrs · 24,712 cycles

MISSING FASTENER PANEL 191BB JUST AFT HIGH PRESS PORT, REPLACED MISSING FASTENER.

Part: FUEL CAP — MISSING (RT WING) · airframe 65,465 hrs · 24,650 cycles

UNDERWING FUEL CAP MISSING ON RT WING. REPLACED FUEL CAP ASSEMBLY, OPERATIONS CHECKED NORMAL.

Part: ENGINE — DAMAGED (NR 2) · airframe 65,374 hrs · 24,616 cycles

NR 2 ENG FOUND EXIST GUIDE VANE OUTER PLATFORM BASE MATERIAL MISSING 1.5 X 6 INCHES WITH CRACKS EXTENDING INTO VANE SLOTS. THREE EACH PLATFORM CRACKS IN EACH VANE SLOT. IAW AMM 72-32-88-200-010-B13 ITEM 4.9A. ENG WILL NEED TO BE REMOVED FOR REPAIR IAW MT 71-017. INSTALL V10015 MOVED TO ELR005 AT TIME OF ENG CHANGE.

Part: CENTERING CAM — OUT OF ADJUST (NLG) · airframe 65,369 hrs · 24,612 cycles

AIRCRAFT PULLING TO THE RT DURING TAXI. NULL FEEDBACK SENSORS 3GC & 4GC IAW AMM 32-51-00- 820-002-A02. ADJUSTMENT OF NWS ZERO POSITION, NLG CENTERING CAMS WILL REQUIRE JACKING OF NOSE. REQUIRED 18 UNITS OF TRIM OR MORE THAN HALF PEDAL DEFLECTION TO TRACK STRAIGHT. RT BRAKE TEMP 95-90 RT TEMP 140- 160.

Part: CONTROL UNIT — FAULTY (BRAKE SYSTEM) · airframe 65,366 hrs · 24,611 cycles

NOSE WHEEL STEERING PULLING RT & REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM UNITS LT OR RT TO BE SET. FULL LT RUDDER REQUIRED TO KEEP NOSE STRAIGHT IAW TOMC, REPLACED BSCU IAW A320 AMM, BITE CHECKED GOOD. LAND TEST 3 PASSED IAW AMM 22-97-00.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 65,283 hrs · 24,584 cycles

FIRST OFFICER`S NAV DISPLAY GOES BLANK. REPLACED FIRST OFFICER`S CRT DISPLAY AMM 31-63-22.

Part: POST — GOUGED (WINDOW FRAME) · airframe 64,768 hrs · 24,397 cycles

FOUND LT SIDE LOWER ATTACHMENT AREA OF WINDSHIELD SIDE POST GOUGED ON TOP SIDE OF AREA IAW 53-11-00-210-014-A PAGE 5. BLENDED GOUGE IAW SRM 51-73-00.

Part: POST — GOUGED (FUSELAGE) · airframe 64,768 hrs · 24,397 cycles

WHILE ACCOMPLISHING EQ3412 FOUND LEFT SIDE LOWER ATTACHMENT AREA OF WINDSHIELD SIDE POST GOUGED ON TOP SIDE OF AREA. BLENDED GOUGE REF SRM 51- 73-00. BLENDED AREA AFTER REWORK IS 1.75"X1.25"X.020" DEEP. ORIGINAL MATERIAL THICKNESS AT AREA IS .600". PER FIG 1, PAGE 8 WITHIN SERVICEABLE LIMITS, WILL NEED HFEC & PAINT RESTORED.

Part: O-RING — LEAKING (RT ENGINE) · airframe 64,747 hrs · 24,391 cycles

RT ENGINE DRIPPING OIL. REPLACED O-RING ON OIL SCAVENGE TUBE, RAN ENGINE NO LEAKS FOUND.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 64,621 hrs · 24,347 cycles

CABIN PR#1 MESSAGE AT DEPARTURE TIME. REPLACED NR 1 CABIN PRESSURE CONT IAW TO MM & BITE TEST, NO FAULT.

Part: SEAL — TORN (MLG DOOR) · airframe 64,529 hrs · 24,313 cycles

NINE INCH SECTION OF RT MLG DOOR SEAL IS TORN AWAY. SEAL TRIM GOOD TO GO.

Part: COMPUTER — FAULTY (NR 2 ELAC) · airframe 64,276 hrs · 24,218 cycles

NR 2 ELAC FAULT LIGHT INOPERATIVE. NR 2 ELAC PITCH TRIM FAULT RESET SUCCESSFUL. ELAC FAULTED A SECOND TIME WHEN NR 2 ELAC TURNED OFF ACFT HAD A SUDDEN SLIGHT PITCH. REPLACED NR 2 ELAC IAW AMM AND ACCOMPLISHED TEST IAW AMM. ALL PASS NO FAULTS.

Part: TORQUE LINK — WORN (NLG) · airframe 64,159 hrs · 24,175 cycles

TURNING RIGHT TO GATE NLG MAKES CLUNKING - THUMPING NOISE. ON MX TAXI LOUD CLUNKING NOISE COULD BE HEARD AND FELT FROM PILOT, AND COPILOTS TILLERS, WHEN TURNNG ACFT EITHER LT OR RT. NO CLUNKING NOISE WHEN USING RUDDER PEDALS. REF TSM 32-20-00-810-801-A01, LUBED TORQUE LINKS, NO HELP. FOUND UPPER AND LOWER TORQUE LINKS WITH EXCESSIVE PLAY AND SHIFTING CAUSING CLUNKING IN TURN.

Part: SCREW — MISSING (NR 1 NACELLE) · airframe 63,925 hrs · 24,079 cycles

SCREW MISSING AT UPPER FWD CORNER PANEL 414CR ON INBD SIDE NR 1 ENG PYLON. REPLACED SCREW.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 63,565 hrs · 23,936 cycles

WITH LOSS OF POWER, ONLY HALF OF EMERGENCY LIGHTS ILLUMINATE. REPLACED FWD EPSU AND BATTERY REF AMM 33-51-38. REPLACED MID CABIN LEFT BATTERY PER AMM 33-51-38. OPS CHECKED OK.

Part: SEAT — LOOSE (CABIN) · airframe 63,521 hrs · 23,923 cycles

F/A STATES PAX COMMENTS THAT SEAT GROUP 11ABC SHIFTS WITH PASSENGER MOVEMENTS IN SEAT. SECURED 11ABC SEAT TO SEAT TRACK.

Part: TRANSCOWL — DELAMINATED (NR 1 ENGINE) · airframe 63,302 hrs · 23,830 cycles

DURING SCHK FOUND AREA OF DELAM IN NR 1 ENG EXHAUST AT 5 O'CLOCK POSITION AFT LOOKING FWD APPROX 15" X 12". PERFORMED INTERIM REPAIR PER MT 78 -010. REPLACED NR 1 ENG INBD TRANSLATING COWL PER MM, OPS CHK NORMAL NO FAULTS NOTED.

Part: COMPUTER — FAULTY (FUEL SYSTEM) · airframe 63,291 hrs · 23,827 cycles

DISCREPANCY WAS 370 MORE ON BOARD VS BOARDED MINUS BURN. FOUND RIGHT FUEL TANK INNER CELL READING 610 POUNDS HIGHER THEN DRIP STICK READINGS. REPLACED FQIC PER AMM.

Part: FIRE BOTTLE — LOW PRESSURE (LAVATORY) · airframe 63,258 hrs · 23,812 cycles

FORWARD AFT LAV FIRE EXTINGUISHER PRESSURE IS LOW. REPLACED FIRE EXT BOTTLE REF AMM 26-25-400-001-A.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 63,233 hrs · 23,802 cycles

CREW REPORTED NR 1 ENGINE EGT OVERLIMIT DURING START. NO RED TIC MARK DISPLAYED. INTERROGATED CFDS AND NO LIMITS EXCEEDED. ACCOMPLISHED MANUAL ENGINE START AND EGT WENT TO 625 AND ABORTED START WITH EGT OVERLIMIT AND START FAULT. REPLACED 7TH STAGE BLEED VALVE PER MM. RAN ENG NORMAL START. 7TH STAGE VALVE WAS LOWER LEFT.

Part: WIRE — CHAFED (COCKPIT) · airframe 62,903 hrs · 23,673 cycles

CREW REPORT: F/O MAP LIGHT HAS STRONG ELEC ODOR WHEN WARM. FBO MAINT REPORTS REF WD 33-12-07-001 POWER AND GND WIRES BEHIND F/O MAP LIGHT(42LE) CHAFED.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 62,797 hrs · 23,636 cycles

RIGHT WING HAS EVIDENCE OF FUEL LEAKS PANEL 640JB OUTBOARD. FOUND FUEL LEAKING FROM ACCESS PANELS. ALL PANELS SCREWS TORQUED. LEAK CHECKED OKAY.

Part: OXYGEN MASK — DISLODGED (SEAT ROW 30) · airframe 62,630 hrs · 23,568 cycles

OXYGEN MASK ROW 30 FELL WHEN F/A WAS PUTTING BAG IN OVERHEAD BIN. REPACKED IAW MT35-002, OP CHECKED NORMAL.

Part: WHEEL — VIBRATION (NLG) · airframe 62,521 hrs · 23,527 cycles

HEAVY VIBRATION FROM NOSEWHEEL AFTER GEAR RETRACTION. REPLACED LEFT AND RIGHT NOSE TIRES.

Part: TARGET — FAULTY (NLG) · airframe 61,754 hrs · 23,213 cycles

CREW REPORTED LANDING GEAR WOULD NOT RETRACT. FOUND TARGET LEVERS ITEM 100 & 120 REF IPC 32-21-11-14, EXTREMELY WORN AND SUPPORT ITEM 70 HAD A LOOSE ATTACHMENT BOLT REF IPC. SECURED BOLT ON SUPPORT AND REPLACED 2EA TARGET LEVERS FOR SYS 1 & 2. ALSO REPLACED SENSOR 24GA AS A PRECAUTION, BITE OKAY.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 61,542 hrs · 23,119 cycles

NR 1 ENGINE HP VALVE HAS BROKEN LOCK OUT PIN. NEED NEW VALVE. REPLACED VALVE.

Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 60,390 hrs · 22,635 cycles

AFT OVERWING EMERGENCY EXIT WINDOW AT ROW 21 ON THE RIGHT SIDE IS LEAKING WATER. PRESSURIZED ACFT TO 3 LBS NO LEAKS NOTED CLEANED AREA OF WATER. NO OTHER LEAKS NOTED AT THIS TIME, FLASH RAIN STORM AT TIME OF LEAK.

Part: STRINGER — CORRODED (31 RIGHT) · corrosion level 2 · airframe 60,339 hrs · 22,613 cycles

STRINGER 31R BELOW OUTFLOW VALVE IS CORRODED. REMOVED AND REPLACED STRINGER IAW SRM 51-42-11. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,339 hrs · 22,613 cycles

SKIN DAMAGED BETWEEN FR 68 - 69 AT STRINGER 29L. SKIN REPAIRED IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,339 hrs · 22,613 cycles

DENT FOUND IN SKIN BELOW DOOR 1L OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 53-11-11. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,339 hrs · 22,613 cycles

SKIN DENT OUT OF LIMITS BETWEEN FR 24-25 STR 22L AFT OF MAIN ENTRY DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-11-11 FIG 212. MAJOR REPAIR.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 60,339 hrs · 22,613 cycles

FWD END OF NR 2 PYLON, INTERNAL WEB IS CRACKED. STOP DRILLED CRACK, REF S RM54-52-12. ACCOMPLISHED WELD REPAIR PER SRM 54-50-00. INSTALLED DOUBLER REPAIR OVER WELD PER SRM 54-52-12 FIG 207, SHEET 2. N-R F1834T.

Part: BUSHING — DAMAGED (FLAP TRACK) · airframe 60,339 hrs · 22,613 cycles

RT WING NR 3 FLAP TRACK HAS EXCESSIVE PLAY AT AFT WING ATTACH POINT. REPLACED AFT SPIGOT PIN AND BUSHING PER CMM 57-51-41.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,339 hrs · 22,613 cycles

STRINGER 43L CORRODED BETWEEN FR 54 AND 56. INSTALLED NEW STRINGER.

Part: TRANSMITTER — LEAKING (HYDRAULIC SYS) · airframe 59,515 hrs · 22,244 cycles

HYDRAULIC LEAK COMING FROM MAIN GEAR WHEEL WELL. LEAK COMING FROM BASE OF HIGH PRESSURE TRANSMITTER, ON YELLOW SYS MODULE. ADJACENT TO YELLOW SYS RES. REPLACED TRANSMITTER PER AMM. NO LEAKS NOTED.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 59,274 hrs · 22,126 cycles

AFTER TAKE OFF MLG DID NOT RETRACT. ECAM DOORS NOT CLOSED & GEAR NOT UPLOCKED ILLUMINATED. RECYCLED OK. REPLACED NLG PROXIMITY SENSOR PER MM. OPERATED NOSE GEAR PER MM, ALL INDICATIONS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 58,832 hrs · 21,938 cycles

EMERGENCY EXIT LIGHTING AT OVERWING SEATS MISSING RED LENS IN 2 OF 3 ROWS REQUIRING RED LENS. REPLACED LIGHT ASSY'S PER MM.

Part: SEAT — LOOSE (CABIN) · airframe 58,801 hrs · 21,922 cycles

SEAT 37B & C DETACHED FROM FLOOR. SEAT 37 ABC OTBD FLOOR FITTING OUT OF FLOOR TRACK. TRACK FULL OF DEBRIS. INSTALLED FITTING IN TRACK AND SECURED LOCKING TAB.

Part: DOOR — OBSTRUCTED (RT OVERWING) · airframe 58,758 hrs · 21,904 cycles

RIGHT AFT OVERWING EMERGENCY DOOR REMOVED DUE TO WATER LEAKAGE. ACCOMPLISED INSTALLATION OF AFT RT OVERWING EXIT AFTER REMOVING DEBRIS & SMOOTHING ROUGH SEALING AREAS.

Part: SIGHT GLASS — CRACKED (IDG) · airframe 58,068 hrs · 21,609 cycles

NR 2 ENGINE IDG SIGHT GLASS HAS A CRACK. SIGHT GLASS IS NOT LEAKING: REPLACED IDG IAW 24-21-51-401 OPS AND LEAK CHECKED GOOD.

Part: ENGINE — STALLED (NR 2) · airframe 58,067 hrs · 21,608 cycles

NR 2 ENG STALL, FLIGHT DIVERTED. NEED TO VISUALLY CHECK THE ENGINE INLET & EXHAUST AND INTERROGATE CFDS PER TSM. CALL SAMC ENGINE DESK PRIOR TO GOING TO AIRCRAFT. LOCAL FBO AMT VISUALLY CHECKED NR 2 ENGINE INLET & TAILPIPE PER TSM WITH NO DEFECTS NOTED. CFDS INTERROGATION SHOWED FAULT CODE PRPSTL ON FADEC 2A & 2B. BOROSCOPE INSPECTION, HI-PWR RUN AND VSV LUBE TO BE PERFORMED BY EFS CREW ON LOG 2.

Part: ASPIRATOR — FAULTY (R1 DOOR SLIDE) · airframe 57,912 hrs · 21,538 cycles

SLIDE RECEIVED WITH VACUUM CAP STILL ATTACHED TO ASPIRATOR. CAUSE AND CORRECTIVE ACTION: UPON DISASSEMBLY, FOUND THE VACUUM CAP ATTACHED THAT WAS USED TO DEFLATE THE SLIDE AND MAINTAIN A VACUUM DURING PACK. VACUUM CAP IS TO BE REMOVED WHEN PACKING IS COMPLETE. IF VACUUM CAP IS STILL ATTACHED, THE SLIDE WILL NOT INFLATE UPON DEPLOYMENT. REMOVED VACUUM CAP AND PERFORMED FUNCTION TEST.

Part: LATCH — OBSTRUCTED (OXYGEN MASK) · airframe 56,628 hrs · 20,950 cycles

DURING DROP CHECK OF PASS O2 MASKS. FOUND MASKS IN AFT LAV DID NOT DEPLOY. FOUND AND CLEARED OBSTRUCTION IN LATCHING MECHANISM. OPS CHECKED GOOD REF MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,518 hrs · 20,895 cycles

NO SMOKING FASTEN SEAT BELT SIGNS NOT WORKING THROUGHOUT THE CABIN. SAMC TEXT: WORKS FINE FROM ROW 21 AFT, BUT ALL OTHER SECTIONS INOP AT VARIOUS LOCATIONS. MOST BULBS APPEAR BURNT OUT. NUMEROUS LIGHT BULBS NEED REPLACED IN THE NO SMOKING AND SEAT BELTS SIGNS. RELAMPED ALL NO SMOKING & SEAT BELT SIGNS IN CABIN AS REQUIRED REF MM. ALL OPS CHECK NORMAL.

Part: PLACARD — OUT OF POSITION (CABIN) · airframe 55,511 hrs · 20,415 cycles

DOOR 2R HAS LEFT SIDE PACK COVER ON RIGHT SIDE THUS COVERING VISUAL INDICATOR. SUPPLEMENTAL DATA UPDATE REMOVED WRONG PLACARD, INSTALLED INTERIM PLACARD PER GN. DOOR 2R HAS LEFT SIDE PACK COVER ON RIGHT SIDE THUS COVERING VISUAL INDICATOR. PLACARD FOR SLIDE COVER ON AOG. REPLACED SLIDE COVER LOCK-UNLOCK (2 EA) PLACARD ON DOOR 2R AND DOOR 1R.

Part: RAM AIR TURB — UNWANTED DEPLOY · airframe 55,200 hrs · 20,274 cycles

THE RAM AIR TURBINE DEPLOYED ON THE GROUND. FIELDS RETRACT IAW AMM29-22-00-201, TASK 29-22-00-869-002. RESTOWED RAT.

Part: WIRE — FRAYED (ANTI ICE DUCT) · airframe 54,529 hrs · 20,008 cycles

NR 1 ENGINE UPPER PYLON, ABOVE HIGH STAGE AND ANTI-ICE DUCT HAS SEVERAL WIRE BUNDLES WITH FRAID AND MELTED INSULATION AREAS. PTT'S 5296038 AND 5296 037, 3 EA HARNESSES REPLACED. ALL OPS CHECKS NORMAL.

Part: OXYGEN MASK — FAILED (CABIN) · airframe 54,447 hrs · 19,964 cycles

F/O 02 MASK FAILS TO TEST. REPLACED MASK AND BOX ASSY.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 53,931 hrs · 19,712 cycles

BLUE SYS LOW, RTFL. CREW TURNED OFF SYS WHILE STILL HAVING PRESSURE. INVESTIGATING SOURCE OF LEAK FOUND IN WHEEL WELL AREA OF BLUE ELECTRIC PUMP. MX FOUND LINE BETWEEN PUMP AND DAMPENER CHAFFED THROUGH AND LEAKING. REPLACED LINE AND BLED HYD SYSTEM. ENGINE ONE EPR INDICATION LOST AFTER STARTING BOTH ENGS. A-THR MSG. SAMC TEXT: CREW CYC A4 & R41 AND FADEC SW. NO HELP. CREW COMPLIED WITH MEL7320D. DEFERRED PER SAMC. FBO SWAPPED EIU'S. PROBLEM FOLLOWED. FBO RPL EIU -1 PER MM. ACP TEST. ALL TEST PASSED. NO MSGS.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 53,299 hrs · 19,396 cycles

EMERGENCY LIGHT TEST SHOWS AFT LT LOADS, NO GREEN LIGHT. NR 2 RT AFT SLIDE ASSY, EMERGENCY LIGHT TEST NOW HAS GREEN LIGHT AND CKS GOOD. INSP SLIDE AT DOOR 2R, SLIDE SECURED ON DOOR, SLIDE PIN REMOVED AND STOWED, ASSIST BOTTLE PIN REMOVED AND REARMED AND SAFETIED, EMERGENCY LIGHT TESTS OK.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 52,677 hrs · 19,080 cycles

GREEN HYD FAILURE, FLIGHT DIVERTED. REPLACED LEAKING HYD LINE FOR THE GREEN SYSTEM. SERVICED GREEN HYD. LEAK CHECKED HYD LINE. CHECKED OKAY. OPERATED SYSTEM TO VERIFY FULL. LINE REPLACED IN PYLON, FILTERS CHECKED, EMERGENCY EXT HANDLE RESET. A/C OK FOR SERVICE.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 51,976 hrs · 18,786 cycles

CIDS MSG INTERNAL LOAD AFT LEFT. *S/D* REPLACED LT AFT EPSU. OPS CHECKS NORMAL.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 47,886 hrs · 17,119 cycles

MESSAGE "ATA 33-51-38 INT LOADS AFT L" SHOWS AFTER THE TEST. POWER SUPPLY FAILURE. REPLACED POWER SUPPLY AND BATTERY. OPS CHECKED NORMALLY.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,451 hrs · 16,970 cycles

ODOR IN COCKPIT SMELLED ELECTRICALLY HOT TURNED BLOWER FAN TO OVRD, SMELL DISSIPATED.

Part: PRESSURE SWITCH — LEAKING (NLG) · airframe 46,611 hrs · 16,681 cycles

HYD G SYS LO PR LOST NW STEERING. NWS SYSTEM PRESSURE SWITCH LEAK. REPLACED NWS ELECTRICAL BOX WITH THE SYSTEM PRESSURE SWITCH.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 46,201 hrs · 16,539 cycles

SMOKE LAVATORY DETECTOR FAULT ECAM. SWAPPED DETECTOR WITH AFT LAV AND RETESTED, ALL NORMAL.

Part: TEST UNIT — MALFUNCTIONED (FIRE WARNING) · airframe 46,011 hrs · 16,480 cycles

APU FIRE TEST NOT WORKING. RESET APU FDU SYSTEM, OPERATES/TESTS NORMALLY.

Part: UNKNOWN — LEAKING (OXYGEN SYSTEM) · airframe 44,717 hrs · 16,019 cycles

CREW REPORT: CREW O2 APPEARS TO LEAK. SHOWS 40 PSI AND AA REG LOW PR WARNING.

Part: SWITCH — LOOSE (OXYGEN MASK) · airframe 44,577 hrs · 15,973 cycles

REGUL LO PR DISPLAYED ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. *S/D* LEAKING F/O MASK (PRESS TO TEST SWITCH LOOSE). RESEATED PRESS TO TEST BUTTON AND SERVICED O2 SYSTEM.

Part: MASK — MISINSTALLED (OXYGEN SYS) · airframe 44,366 hrs · 15,893 cycles

REGUL LO PR DISPLAYED ON DOOR-OXY SYSTEM ECAM PAGE, DOOR-OXY. IMPROPER STOWAGE OF MASK. RESTOWED FIRST OFFICER'S MASK AND RESERVICED CREW O2 SYSTEM.

Part: SHUTOFF VALVE — LEAKING (O2 SYSTEM) · airframe 44,138 hrs · 15,804 cycles

THE O2 DECREASED TO 50 PSI AT CRUISE FL 380. LEAK AT SHUTOFF VALVE IN CAPTAIN`S SYSTEM. LEAK WAS STOPPED AND SYSTEM WAS SERVICED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 44,071 hrs · 15,783 cycles

FIRST OFFICERS O2 MASK IS LEAKING.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 43,752 hrs · 15,679 cycles

THERMOGRAPHIC INSPECTION OF THE LEFT ELEVATOR UPPER SKIN AN INDICATION OF POSSIBLE LIGHTNING STRIKE DAMAGE WAS NOTED AT 25.25 INCHES FROM I/B EDGE AND 18.5 INCHES FROM AFT EDGE OF ELEVATOR. [06-26-07] UPPER SKIN WAS CUT OUT IN AREA OF INDICATION FOR EVALUATION OF HONEYCOMB MATERIAL. NO DAMAGE TO HONEYCOMB MATERIAL WAS NOTED. SKIN WAS REPAIRED PER UA ENGINEERING SPECIFICATIONS.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 43,416 hrs · 15,554 cycles

CREW O2 EMPTY ONLY 50 PSI AT SHUTDOWN. [06-22-07] "PRESS TO TEST" SLIDE SWITCH ON CAPTAIN'S O2 MASK STOWAGE BOX STICKS, ALLOWING SLOW LEAK THROUGH TEST FUNCTION. REPLACED OXYGEN MASK STOWAGE BOX.

Part: SEAT — MISINSTALLED (CABIN) · airframe 42,926 hrs · 15,366 cycles

PAX SEAT ROW 10R FOUND INSTALLED TOO FAR FWD AND INTERFERES WITH THE REMOVAL OF THE FWD RIGHT OVERWING EMERGENCY EXIT HATCH. ERROR WAS MADE WHEN ATTACHMENT SCREWS FOR SEATS 10DEF WERE REMOVED FOR USE ON ANOTHER AIRCRAFT ON 1/19/2007 AT IAD. SEAT ROW WAS ACCIDENTALLY SHIFTED AND THEN RESECURED TOO FAR FORWARD.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 42,926 hrs · 15,366 cycles

BELLY FAIRING SUPPORT BRACKET UPPER ANGLE -Y127 (LT SIDE) AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPAIRED UPPER ANGLE PER SRM 53-35-11-FIG 229.

Part: POWER SUPPLY — FAULTY (AFT LEFT) · airframe 41,038 hrs · 14,663 cycles

EMERGENCY LIGHT TEST FAULTED AFT LEFT POWER SUPPLY. SUPPLEMENTAL DATA UPDATE

Part: COMPUTER — MALFUNCTIONED (FLT MANAGE) · airframe 39,629 hrs · 14,157 cycles

BOTH FMGC DUMPED ALL DATA ON DEPARTURE CLIMBING THRU FL180 PROMPTING RTFL. TROUBLESHOOTING CHECKS RETURNED NO DEFECTS.

Part: FUEL SYS — UNKNOWN (UNKNOWN) · airframe 38,700 hrs · 13,815 cycles

FLIGHT DIVERTED DUE TO UNPLANNED/UNEXPLAINED FUEL BURN. NO FUEL LEAK INDICATIONS NOTED. TASKS ACCOMPLIHSED WERE: DRIP STICK READINGS TAKEN ON ALL AIRCRAFT FUEL TANKS AND RESULTED IN ALL WITHIN LIMITS. REVIEWED POST FLIGHT REPORT FOR SIGNS OF FAULTS AND RESULTED IN NO FINDINGS AND VISUAL INSPECTED BOTH ENGINES ALONG WITH ALL AIRCRAFT FUEL TANKS AND RESULTED IN NO VISIBLE SIGNS OF FUEL LEAKS. ENGINEERING WILL CONTINUE TO MONITOR FOR RELATED UNEXPLAINED FUEL BURN.

Part: SEAL — LEAKING (HYD PUMP) · airframe 38,603 hrs · 13,786 cycles

FLIGHT DIVERTED DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. LOSS OF GREEN HYD SYSTEM. FOUND EDP LEAKING AT MATING FLANGE. REPLACED PUMP REF MM29-11-51. RAN ENG, NO LEAKS, LEVELS NORMAL.

Part: LIGHT — FAILED (CABIN) · airframe 37,667 hrs · 13,448 cycles

CABIN EMERGENCY LIGHT TEST FAILED, INDICATES ON MESSAGE, FWD BATTERY LOW ON THE FIRST TEST. FOLLOWED BY INT LOADS FWD L MESSAGE AFTER FEW MORE TEST. REPLACED EMERGENCY POWER SUPPLY AND BATTERY

Part: SILL — CORRODED (RT PAX DOOR) · airframe 37,257 hrs · 13,288 cycles

AFT RIGHT CABIN DOOR SILL PLATE HAS CORROSION UNDER AFT SLIDE MOUNT.

Part: STRINGER — CORRODED (FR 31-32) · airframe 37,257 hrs · 13,288 cycles

STR 41R HAS CORROSION BETWEEN FS 31-32. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF STRINGER PER SRM 53-21-13 FIG 203.

Part: STRINGER — CORRODED (FR 58-59) · airframe 37,257 hrs · 13,288 cycles

STR 43L HAS CORROSION BETWEEN FS 58-59. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION REF SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FS 54-56) · airframe 37,257 hrs · 13,288 cycles

STR 43L HAS CORROSION BETWEEN FRAMES 54-56. CUT-OUT DAMAGED SECTION ACP SPLICE REPAIR PER SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FR 33-34) · airframe 37,257 hrs · 13,288 cycles

STRINGER 41R HAS CORROSION BETWEEN FRAMES 33-34. CUT-OUT DAMAGED SECTION, SPLICED IN NEW SECTION REF SRM 53-21-13 FIG 203 .

Part: EPSU — INOPERATIVE (EMERGNECY LIGHT) · airframe 32,931 hrs · 11,735 cycles

EMERGENCY LIGHTS FAIL TEST INT LOADS LEFT. REPLACED POWER SUPPLY UNIT. CABIN EMERGENCY LIGHTS NOW PASS.

Part: LATCH — CONTAMINATED (CARGO DOOR) · airframe 29,907 hrs · 10,582 cycles

FWD CARGO DOOR WARNING LIGHT CAME ON. DOOR HANDLE LATCH FOUND CONTAMINATED WITH DEBRIS OF AN UNKNOWN NATURE PREVENTING FULL SEATING. LATCH WAS CLEANED OF DEBRIS AND LUBRICATED.

Part: WIRE — SHORTED (RT ENGINE) · airframe 26,167 hrs · 9,071 cycles

NUMEROUS ECAM FAULT MESSAGES FROM THE NUMBER TWO ENGINE. FOUND NUMEROUS WIRES SHORTED IN THE RIGHT ENGINE OUTBOARD PYLON AREA. AREA WAS CHECKED FOR DAMAGE AND NEW WIRES INSTALLED AS REQUIRED.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 23,811 hrs · 8,188 cycles

HYDRAULIC LOW LEVEL WARNING INDICATION. *S/D* REPLACED GREEN HYDRAULIC SYSTEM RESERVOIR QUANTITY INDICATOR.

Part: UNKNOWN — ODOR (ROW 10 - 13) · airframe 20,131 hrs · 6,953 cycles

CREW REPORTED PASSENGERS COMPLAINED OF BURNING SMELL IN CABIN. *S/D* MAINTENANCE INVESTIGATED AND COULD NOT ISOLATE BURNING SMELL IN ROWS 10-13. NO FURTHER OCCURRENCES WERE NOTED. NO COMPONENTS WERE REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 19,709 hrs

EMERGENCY LIGHT TEST FAULT (BAT AFT LT) 33-51-38. *S/D* REPLACED POWER SUPPLY UNIT AND BATTERY IN AFT LEFT POSITION.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 19,505 hrs

EMERGENCY EXIT LIGHTS FAIL TEST WITH MESSAGE EPSU COM AFT. *S/D* REPLACED POWER SUPPLY PCN 565-0038.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,687 hrs

FLT EXPERIENCED A CRACKED OUTER WINDSHIELD ON THE CAPT SIDE AT FL390. FLT DESCENDED TO FL220 PER THE FLIGHT MANUAL. *S/D* WATER INGRESS THROUGH THE WEATHER SEAL REACHED THE WINDSHIELD''S BUSBAR, RESULTING IN ELECTRICAL ARCING AND SUBSEQUENT CRACKING OF THE WINDSHIELD OUTER FACE PLY. CRACKING OF THE OUTER FACE PLY DOES NOT AFFECT STRUCTURAL INTEGRITY, HOWEVER THE WINDSHIELD WAS REPLACED PRIOR TO THE AIRCRAFT''S NEXT FLIGHT.

Part: LIGHT — INOP (ROW 22C)

SEAT 22C EEL LIGHT INOP. REPLACED EEL LIGHT ASSEMBLY (P/N BR9644-21), OP-CHECKS OK.

Part: FMGC — MALFUNCTIONED (E & E COMPT)

FMGC 1 AND 2 FROZEN. NO RESPONSE TO INPUTS. USED STANDBY NAV ON THE RMP'S. *S/D* RESET SYSTEM AND PERFORMED CAT III CAPABILITY PER AMM 22-97-00 AND AFFS TEST. ALL TEST PASSED, NO FAULTS PRESENT. CHECK PLR AND PFR WITH NO FAULTS DETECTED. NO MORE PROBLEMS WITH FMGC SINCE THIS MRR.

Part: POWER SUPPLY — LOOSE (CABIN)

EMERGENCY LIGHTS FAILED TEST ON PTP PANEL. *S/D* RESEATED POWER SUPPLY BATTERY AND OPERATIONALLY CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS FAILED TEST. REPLACED POWER SUPPLY AND SYSTEM OPERATED NORMALLY.