N928FR

Part: POWER SUPPLY — FAILED (CABIN) · airframe 35,836 hrs · 17,814 cycles

FORWARD LT EPSU FAILS EMER LIGHTS TEST. R & R FWD LT EPSU 10WL. OPERATIONAL CHECKED NORMAL IAW AMM 33-51-38 PAGE BLOCK 401.

Part: VALVE — CLOSED (BLEED AIR SYS) · airframe 35,480 hrs · 17,606 cycles

IN CRUISE AT 31000 FT UNABLE TO MAINTAIN CABIN PRESS. CABIN ALTITUDE ROSE TO 10,200. R & R NR 2 ENG PRV IAW AMM 36-11-52-PB 401. OPERATIONS & LEAK CHECKED VLV & NO LEAKS NOTED. PREFORMED OPERATIONAL TEST OF THE BLEED AIR SYS IAW AMM 36-11-00-710-003-A. OPERATIONAL TESTED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,905 hrs · 17,292 cycles

L1 DOOR EMER POWER SUPPLY UNIT INOPERATIVE 10WL. R & R L1 DOOR EMER POWER SUPPLY UNIT. OPERATIONS CHECKED GOOD IAW AMM 33-51-38 PB 401.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,463 hrs · 15,437 cycles

DURING C6 CHECK. AFT GALLEY FLOORBEAM AT FRAME 69 HAS LIGHT CORROSION AROUND FASTENER HOLE. CLEANED UP HOLE TO .354' IAW SRM 53-41-14, FIGURE 101, SRM 51-21-11 (4)(C) AND SRM 51-75-12. VERIFIED CORROSION REMOVAL WITH HPEC IAW NTM 51-10-02 B NOTE 3. NO FURTHER INDICATIONS WERE NOTED. ACFT IS SCHEDULED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,463 hrs · 15,437 cycles

ACFT WAS OUT OF SERVICE DUE TO C6 MX CHECK. AFT GALLEY FLOORBEAM AT FRAME 66, Y765 HAS LIGHT CORROSION AROUND FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-42-11. PARA 5. ACFT IS SCHEDULED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,463 hrs · 15,437 cycles

DURING C6 CHECK. AFT GALLEY FLOORBEAM AT FRAME 66 APPROX Y1292 HAS LIGHT CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND 6.B. ACFT SCHEDULED TO GO BACK INTO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,453 hrs · 15,430 cycles

EPSU, MIDDLE RIGHT, BATTERY FAILED TEST ON HEAVY SERVICE CHECK. R & R BATTERY ASSY MIDDLE RIGHT EPSU. OPS CHECK GOOD. REF AMM 33-51-38 PAGE BLOCK 401.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,268 hrs · 12,804 cycles

OVERWING EMERGENCY LIGHT 60WL HAD AFT BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT 60WL IAW AMM 33-51-15 PB 401. OPS CHECKED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 24,134 hrs · 11,746 cycles

YELLOW HYD FLUID & SYSTEM LOST ON APPROACH. R & R RT ENGINE HYD PUMP IAW AMM 29-13-51- PB 407. LEAK & OPS CHECKS OK.

Part: ENTERTAIN SYS — SMOKE (CABIN) · airframe 22,009 hrs · 10,732 cycles

REFERENCE LOG PAGE 529827 ITEM 1 AND LOG PAGE 529836 ITEM 1. SEAT 13A TV SMELLS HOT AND WAS SMOKING. INSPECTED ROW 13 ABC FOR SMOKE AND INSPECTED EPSU'S. NO DEFECTS NOTED. PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW LIVE TV AMM 44-25-00 PAGE 5042 THRU 5047. FOUND NO EVIDENCE OF ELECTRICAL BURNING. REPLACED SEB AT SEATS 13 ABC AND VDU FOR PRECAUTIONARY.

Part: COMPUTER — MALFUNCTIONED (SMOKE WARNING) · airframe 21,758 hrs · 10,619 cycles

PILOT REPORT REF LOG PAGE 524666 ITEMS 1 AND 2. SMOKE WARNING ACTUATED UPON LANDING. NO SMOKE NOTICED IN COCKPIT. BOTH BLOWER AND EXTRACT FAULTED AT SAME TIME ON THE VENTILLATION SYS. R & R AEVC COMPUTER.

Part: EPSU — INOPERATIVE (ZONE 200) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 CHECK, INSP NOTED EMERGENCY LIGHTS ON SEATS 6C, 12C, AND 13C INOPERATIVE. MX TROUBLESHOT SYS IAW TSM 33-51-00-810-813, DISCONNECTED EACH EPSU, CLEANED / DRIED THE PLUGS, AND RECONNECTED. OPS TEST NORMAL IAW AMM 33-51-00-710-009.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 CHECK INSP NOTED AFT CARGO PIT FLOOR PANEL 152UG DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW MCGILL 9701 REV. G

Part: COVER — CORRODED (ZONE 100) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 CHECK, INSP NOTED AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD AREA COVER SHEET CORRODED. MX R & R AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD AREA COVER SHEET IAW SRM 51-42-11 AND 51-72-11.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 CHECK INSP NOTED SHEAR WEB AT FRAME 69 AT AFT END OF BEAM -Y1292 HAS A FIFTEEN INCH CRACK. R & R SHEAR WEB IAW EO A0-53-31934 AND A319 SRM 51-72-11.

Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151TG PUNCTURED AND DELAMAINATED BEYOND ECONOMICAL LIMITS. MX R & R IAW AMM 53-12-14-400-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,086 hrs · 10,309 cycles

DURING C4 S1 INSP NOTED FLOORBEAM -Y765 BETWEEN FRAME 67 AND FRAME 68 HAD CORROSION ON UPPER SURFACE. REPAIRED FLOORBEAM IAW SRM 53-00-14 PARAGRAPH 4 D FIGURE 204.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 21,086 hrs · 10,309 cycles

REFERENCE NON ROUTINE N0014 AFT CABIN SHEAR WEB AT FRAME 69 AT AFT END OF BEAM =Y1292 HAS A CRACK. R & R SHEAR WEB IAW EO A0-53EO-31434 AND SRM 51-72-11.

Part: COVER — DEFECTIVE (CARGO DOOR) · airframe 16,779 hrs · 8,160 cycles

PILOT MADE AN AIR TURNBACK DUE TO AN AFT CARGO DOOR MESSAGE ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS. MX REMOVED AND REPLACED THE COVER ASSY AND PERFORMED OPERATIONAL CHECK IAW AMM 52-32-21-420-052.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50125. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261PF HAS A CORRODED INSERT ON THE LT HAND SIDE AND DELAMINATION IN THE SAME AREA. MX REPAIRED PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30588. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOORBEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM FRAME 66 TO FRAME 68 (L2 DOOR AREA). MX R&R THE FLOORBEAM IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR 19-53R-30587. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOOR SUPPORT Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM FRAME 66 TO FRAME 68 (L2 DOOR AREA). MX R&R THE FLOOR SUPPORT IAW THE REQUIREMENTS OF EA NR A9-53R-30587. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50040. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 67 TO FRAME 68. MAINTENANCE INSTALLED NEW FLOOR BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11 AND ENGINEERING AUTHORIZATION # A9-53R-30392. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 66 TO FRAME 67. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION INFORMATION BECOMES AVAILABLE. MX R&R FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, 51-42-00 AND 51-42-11, PAGE 24. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE C050039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM RT HAND FRAME 66 TO FRAME 67. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION INFORMATION BECOMES AVAILABLE. (OPEN)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE C050055. DURING C3 C-CHECK, INSP NOTED INDICATIONS OF CORROSION ON TOP OF RIGHT AFT SHEAR PLATE BETWEEN FRAME 68 AND FRAME 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE C049995. DURING C3 C-CHECK INSPECTION NOTED THE FORWARD OUTBOARD CORNER WAS DAMAGED ON FLOOR PANEL 242LF. MX REPAIRED DAMAGE TO PANEL 242LF IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30577. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE LT LATERAL SHEAR PLATE HAS LIGHT CORROSION AT CLIP NUT HOLES BETWEEN FR 68 AND FR 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IAW THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SILL — CORRODED (FUSELAGE) · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE CO50131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SILL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORRODED. MX INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30582. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SEAL — CORRODED (R2 DOOR) · airframe 15,560 hrs · 7,529 cycles

REFERENCE NON ROUTINE C050131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SEAL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORRODED. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION INFORMATION BECOMES AVAILABLE. (OPEN)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED R1 FORWARD GIRT BAR BLANKING PLATE HAS CORROSION AT HOLES. MAINTENANCE FABRICATED NEW NUT PLATE ASSEMBLY FOR GIRT BAR BLANKING PLATE AND INSTALLED IAW THE REQUIREMENTS OF AIRBUS DRAWING D531 12534 AND A319 SRM 51-42-11, PARAGRAPH 7. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD PIT PANEL 132EG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURED DAMAGE TO FLOOR PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, FIGURE 204.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152TG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152TG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 151UG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 161BF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 161BF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 162CF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 162CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 152UG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152WG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152XG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED FORWARD PIT PANEL 131CF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 131CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,560 hrs · 7,529 cycles

DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151BE WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 151BE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SMOKE WARNING — ACTIVATED (ZONE 100) · airframe 14,463 hrs · 6,962 cycles

AFTER ENGINES WERE SHUTOFF, THE CREW REPORTED THE LIVE TV SMOKE ALARM WENT OFF AND MAIN TV POWER SWITCH WAS PUSHED TO OFF AND ALARM WAS SILENCED. MAINTENANCE PERFORMED VISUAL INSPECTION OF LIVE TV AVIONICS COMPARTMENT AND FOUND NO DAMAGE AND NO SIGNS OF SMOKE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF TCM 24-00-00-810-823. UPON COMPLETION THE WORK IT WAS INSPECTED AND FOUND ACCEPTABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,166 hrs · 6,823 cycles

DURING RON SERVICE, INSPECTION REPORTED EMERGENCY EXIT PATH LIGHTING AT SEATS 6 ABC DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EPSU 10WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38 PB 401. UPON COMPLETION OF THE INSTALLATION THE LIGHTS TESTED OKAY.

Part: BEARING — FAILED (NR 1 ENGINE) · airframe 13,927 hrs · 6,706 cycles

DURING CRUISE, FLIGHT CREW REPORTED VIBRATION FOLLOWED BY ECAM WARNING OF NUMBER 1 ENGINE OIL FILTER CLOG, LOSS OF OIL PRESSURE, INCREASE IN OIL TEMPERATURE AND LOSS OF OIL LEVEL. THE ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AT THE DIVERSION AIRPORT. PRELIMINARY ENGINEERING EVALUATION INDICATES POSSIBLE FAILURE OF THE NUMBER 3 BEARING IN THE COMPRESSOR SECTION OF THE ENGINE. ENGINE CHANGE WILL BE ACCOMPLISHED. DAMAGED ENGINE WILL BE SENT FOR TEARDOWN. WHEN TEAR DOWN REPORT IS AVAILABLE, THIS SDR WILL BE UPDATED. ENGINE CHANGE COMPLETED AND AIRCRAFT RETURNED TO SERVICE. DAMAGED ENGINE EN ROUTE TO GE (STROTHER FACILITY) FOR TEAR DOWN.

Part: LIMITER — INOPERATIVE (BATTERY CHARGER) · airframe 13,604 hrs · 6,555 cycles

DURING TAKEOFF, THE FLIGHT CREW REPORTED AN ELAC BCL2 FAULT ON THE ECAM. THE FLIGHT CREW PERFORMED AN AIR TURN BACK AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 BATTERY CHARGE LIMITER IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 24-38-34-41. FOLLOWING COMPLETION OF THE INSTALLATION, THE UNIT WAS OPERATIONALLY TESTED AND FOUND OKAY. CORRECTED PART SERIAL NUMBER TO READ 2081/END.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,575 hrs · 6,542 cycles

DURING PERFORMANCE OF EO A9-25EO-02752, REV G, INSPECTION REPORTED EMERGENCY PATHWAY LIGHTS AT ROWS 1, 2, 5 AND 6 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMMM 33-51-38 PB 401. FOLLOWING COMPLETION OF THE MAINTENANCE ACTION, THE WORK WAS INSPECTED AND FOUND ACCEPTABLE.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,393 hrs · 5,514 cycles

AIRCRAFT RT ROWS 9 AND 10 - BURNING WIRE SMELL AT 02 COMPARTMENT IN OVERHEAD BIN. HOT TO TOUCH. INSPECTED LIGHTS, WIRING AND PAX OXYGEN GENERATORS FOR ACCIDENTAL DISCHARGE. NO DEFECTS NOTED AT SEAT ROWS 9 AND 10 DEF. REPLACED PASSENGER READING LIGHT POWER UNITS AS A PRECAUTIONARY MEASURE AT ROWS 9 AND 10 DEF IAW AMM 23-73-38, PB 401. OPS CHECKED GOOD.

Part: ODOR — DETECTED (COCPIT) · airframe 11,683 hrs · 5,436 cycles

FLIGHT CREW REPORTED A BURNING SMELL, STRONG ELECTRICAL ODOR BRIEFLY WHILE DESCENDING THRU FL190. NO VISIBLE SMOKE OBSERVED. ODOR WAS ONLY NOTICED BY COCKPIT CREW. INSPECTED AIRCRAFT PER TSM 24-00-00-810-823 FOR DAMAGE. NO DAMAGE FOUND. PERFORMED TROUBLESHOOTING OF APU AND ENGINE PER TASK CARD. NO DAMAGE FOUND. UNABLE TO DUPLICATE DISCREPANCY. REPLACED THE RECIRCULATION FAN FILTER AS PRECAUTIONARY. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIMITER — FAULTED (E/E BAY) · airframe 7,173 hrs · 3,392 cycles

AIR TURNBACK. FLIGHT CREW REPORTED BCL1 FAULT. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED BATTERY CHARGE LIMITER AT NR 1 POSITION. OPS CHECKED GOOD PER AMM 24-38-34, PAGE 401. ECAM STATUS NORMAL. PERFORMED OVERWEIGHT LANDING AT 140,300 LBS. NO EXCEEDANCES RECORDED.

Part: ACTUATOR — UNSERVICEABLE (FLT CONTROLS) · airframe 3,937 hrs · 1,825 cycles

THS FAILED SECTION -A- OF TASK CARD TC 27400-1. THS LOCKED IN FULL NOSE DOWN POSITION. REPLACED THS ACTUATOR PER MM 27-44-51-400-001. PERFORMED REQUIRED SYSTEM TEST PER MM 27-41-00-730-001 AND CHECKED GOOD.