N279AY

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 40,603 hrs · 6,016 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND DOOR EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PER AMM 25-64-00.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 40,477 hrs · 6,001 cycles

AIRCRAFT WAS GROUNDED: 3L EXIT SIGN KNOCKED DOWN. MAINTENANCE CLIPPED EXIT SIGN BACK INTO PLACE PER A330 AMM 33-51-17.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 39,029 hrs · 5,806 cycles

AIRCRAFT WAS GROUNDED: SLIDE PRESSURE LOW DOOR R2. TROUBLESHOT FOUND DEU-B (300RH4) NEEDS REPLACEMENT. REMOVED AND REPLACED DEU B 300RH4 IAW AMM 23-73-47, NO HELP. REMOVED AND REPLACED R2 DOOR SLIDE IAW CARD 33L00025001

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 38,570 hrs · 5,712 cycles

THE AIRCRAFT WAS GROUNDED. CRACK INDICATION FOUND ON R1 WINDSHIELD. REPLACED R1 WINDSHIELD PER JOB CARD 33L21056001.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 38,368 hrs · 5,666 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 AND 74 , YC1. THE AIRCRAFT WAS GROUNDED. REPLACED THE SEAT TRACK IAW SRM 51-41-14

Part: SLIDE — CONTAMINATED (R2 DOOR) · airframe 36,695 hrs · 5,390 cycles

WATER CONTAMINATION AT THE R2 DOOR EMERGENCY SLIDE. REPLACED THE SLIDE IAW AMM 25-62-41-400-804-A AND TESTED OK.

Part: SEAT TRACK — CORRODED (FRAMES 32-34) · airframe 36,695 hrs · 5,390 cycles

CORROSION FOUND ON THE SEAT TRACK, -Y1552.5 BETWEEN FRAMES 32 TO 34. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53275877.

Part: SEAT TRACK — CORRODED (FRAMES 32-33) · airframe 36,695 hrs · 5,390 cycles

CORROSION FOUND ON THE SEAT TRACK, -Y1959 BETWEEN FRAMES 32 TO 33. REPAIRED THE SEAT TRACK IAW SRM 53-21-15-300-002.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 36,211 hrs · 5,324 cycles

NITROGEN CHARGE ON THE L3 DOOR DAMPER BOTTLE WAS LOW. AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00. PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 36,211 hrs · 5,324 cycles

NITROGEN CHARGE ON THE L2 DOOR DAMPER BOTTLE WAS LOW. AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 35,246 hrs · 5,189 cycles

WHILE ACCOMPLISHING A BITE OF EMERGENCY EXIT LIGHTS, THE POWER SUPPLY BATTERY 11WL FAULTED. REPLACED THE BATTERY IAW AMM 33-51-38.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 34,956 hrs · 5,146 cycles

EMERGENCY EXIT LIGHT AT THE L3 DOOR FOUND DAMAGED. SECURED THE EMERGENCY LIGHT LENS. NO DAMAGED NOTED. OK FOR SERVICE IAW AMM 33-51-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,749 hrs · 5,098 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK AT FR 65 AT RBL Y-1959. REPAIRED SEAT TRACK PER SRM 53-00-15-300-001, FIGURE 20101, SHEET 3 AND EA 277459.

Part: SKIN — DELAMINATED (RUDDER) · airframe 34,749 hrs · 5,098 cycles

CRACK AND DELMAINATION FOUND ON THE RUDDER LOWER AFT TRAILING EDGE. REPLACED THE RUDDER IAW AMM 27-21-41-400-801-C.

Part: SEAT TRACK — CORRODED (FRAMES 72-73) · airframe 34,749 hrs · 5,098 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 72 AND 73, Y450. REPLACED THE SEAT TRACK IAW DRAWING 18F53478040, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 72-73) · airframe 34,749 hrs · 5,098 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 72 AND 73, Y450. REPLACED THE SEAT TRACK IAW DRAWING 18F53478040, AND SRM 51-42-11.

Part: BEAM — CORRODED · corrosion level 2 · airframe 34,749 hrs · 5,098 cycles

CORROSION FOUND ON LAV L74 AFT MOUNT AREA ON INBOARD AUXILIARY BEAM. REPLACED AUXILIARY BEAM IAW SRM 51-42-11.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 34,477 hrs · 5,044 cycles

EMERGENCY LIGHTS FAILED FUNCTIONAL CHECK IAW J/C 33C20033002. REPLACED THE POWER SUPPLY IAW MM 33-57-38. AIRCRAFT WAS GROUNDED

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,477 hrs · 5,044 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS FAILED FUNCTIONAL CHECK PER J/C 33C20033002 DURING A 4 CHECK. REPLACED 8 EMERGENCY POWER SUPPLY UNIT BATTERIES PER AMM 33-51-38.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 34,387 hrs · 5,022 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 36B SEAT MOUNTED EMERGENCY LIGHT LENS DAMAGED. REPLACED SEAT 36B EMERGENCY LIGHT ASSEMBLY.

Part: COVER — UNSECURE (CABIN) · airframe 34,295 hrs · 5,003 cycles

AIRCRAFT WAS NOT GROUNDED. 2L EMERGENCY LIGHT COVER FALLS OFF. REATTACHED 2L EMERGENCY LIGHT COVER.

Part: CIDS — MALFUNCTIONED (CABIN) · airframe 33,888 hrs · 4,933 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT SIGNS "ON" DURING FLT AT 1L, 2R, 3L. ALL OTHERS OFF. RESET CIDS. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 33,599 hrs · 4,893 cycles

L4 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: UNKNOWN — MALFUNCTIONED (EMERGENY LIGHT)

AIRCRAFT WAS NOT GROUNDED. WHILE PERFORMING L37 EMERGENCY LIGHTNING FUNCTIONAL CHECKS RECEIVED CLASS 1 ERROR FPEEPMS AISLE LT EPSU 15WL DOOR 3. SWAPPED EMERGENCY POWER SUPPLY UNIT WITH 13WL. PERFORMED GOOD BITE TEST. SWAPPED UNITS TO ORIGINAL POSITION WITH POSITIVE BITE TEST.

Part: CONNECTOR — MISSING (CABIN) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EXIT LIGHT AT L2 DOOR HARNESS 340RH HAS DAMAGE. INSTALLED MISSING CONNECTOR.

Part: LENS — BROKEN (CABIN) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT WAS NOT GROUNDED. FOUND RIGHT-HAND CEILING EMERGENCY LIGHT AFT LENS TO BE BROKEN ABOVE DOOR 3R.

Part: LEAD — DISCONNECTED (CABIN) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS IN SEAT 8GH ARE INOP. RECONNECTED LEADS AT 8GH.

Part: LEAD — DISCONNECTED (CABIN) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS IN SEAT 7GH ARE INOP. RECONNECTED LEADS AT 7GH.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y450 AND STRINGER 25L. REPLACED SEAT TRACK PER SRM 51-42-11 WITH FASTENER DEVIATION ON EA 27301.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,483 hrs · 4,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y450 AND STRINGER 25R. REPLACED SEAT TRACK PER SRM 51-42-11 WITH FASTENER DEVIATION ON EA 273013.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 32,899 hrs · 4,787 cycles

COVER ON EMERGENCY LIGHT AT THE L3 JUMPSEAT FELL OFF. SECURED THE LENS.

Part: GIRT BAR — OBSTRUCTED (R3 DOOR SLIDE) · airframe 32,875 hrs · 4,780 cycles

UNABLE TO ARM THE R3 DOOR. THE LEVER WITH NOT MOVE INTO ARM POSITION. DOOR SHOWS ARMED ON ECAM. REMOVED DEBRIS FROM GIRT BAR SYSTEM. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,661 hrs · 4,750 cycles

AIRCRAFT WAS NOT GROUNDED. DURING DAILY CHECK FOUND FLASHLIGHT AT JUMPSEAT 4R FACING AFT. DOES NOT CHARGE. REPLACED 4R FLASHLIGHT AND BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,661 hrs · 4,750 cycles

AIRCRAFT WAS NOT GROUNDED. DURING DAILY CHECK FOUND FLASHLIGHT AT JUMPSEAT 4R FACING AFT. DOES NOT CHARGE. REPLACED 4R FLASHLIGHT BATTERY.

Part: LENS — MISSING (CABIN) · airframe 32,008 hrs · 4,657 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS MISSING OUTSIDE OF LAV L53. INSTALLED EMERGENCY LIGHT LENS AT LAV L53.

Part: GIRT BAR — OBSTRUCTED (ZONE 800) · airframe 31,714 hrs · 4,603 cycles

AIRCRAFT WAS NOT GROUNDED. PASSENGER DOOR 2L WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR BASE DOOR 2L.

Part: LIGHT — DAMAGED (SEAT 23R) · airframe 31,699 hrs · 4,601 cycles

EMERGENCY LIGHT AT SEAT 23R DAMAGED. REPLACED THE LIGHT ASSEMBLY.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 30,761 hrs · 4,375 cycles

WHILE ACCOMPLISHING A 23 CHECK, THE EMERGENCY POWER SUPPLY UNIT BATTERY AT THE R4 DOOR (18WL) FAILED TO TEST. REPLACED THE BATTERY IAW AMM 33-51-38.

Part: MECHANISM — DIRTY (R2 DOOR) · airframe 28,900 hrs · 4,113 cycles

AIRCRAFT WAS NOT GNDED. EVACUATION SLIDE AT POSITION 2R WILL NOT ARM. CLEANED DEBRIS FROM MECHANISM. SYS CHECKED NORMAL.

Part: LENS — UNSECURE (CABIN) · airframe 28,729 hrs · 4,089 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR AREA EMER LIGHT LENS CAME OFF. RE-INSTALLED EMER EXIT LENS AT 3L DOOR.

Part: LENS — CRACKED (CABIN) · airframe 28,711 hrs · 4,085 cycles

AIRCRAFT WAS NOT GNDED. EMER EXIT LENS CRACKED & LOOSE. REPLACED EMER EXIT LENS.

Part: AIR DATA MODULE — DEFECTIVE (COCKPIT) · airframe 28,637 hrs · 4,065 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THERE WAS NO AIRSPEED INDICATION ON THE CAPTAINS SIDE & THE CREW ABORTED THE TAKEOFF AT 85 KNOTS. REPLACED THE AIR DATA MODULE 19FP1 & ACCOMPLISHED A SATISFACTORY FUNCTIONAL CHECK IAW AMM 34-11-17, 34-*13-00-740-803-A & 34-13-00-720-801-A.

Part: LENS — WRONG PART (CABIN) · airframe 28,626 hrs · 4,061 cycles

AIRCRAFT WAS NOT GNDED. EMER ESCAPE PATH LIGHT ON LAVATORY L74 HAS WRONG COLOR LENS INSTALLED, RED. REPLACED WITH CORRECT COLOR LENS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-12-000-816-A.

Part: LENS — WRONG PART (CABIN) · airframe 28,626 hrs · 4,061 cycles

AIRCRAFT WAS NOT GNDED. EMER ESCAPE PATH LIGHT ON LAVATORY L53 HAS WRONG COLOR LENS INSTALLED, RED. REPLACED WITH CORRECT COLOR LENS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-12-000-816-A.

Part: OVEN — ODOR (GALLEY) · airframe 28,479 hrs · 4,030 cycles

AIRCRAFT WAS GNDED. AFTER ENG START SMELLED CHEMICAL, LIKE CHLORINE, SMELL THROUGH A/C. SMELL WENT AWAY ON TAXI OUT & CAME BACK ON CLIMB OUT, THEN WENT AWAY AGAIN. FLIGHT CREW EXPERIENCED BURNING SENSATIONS & SORENESS IN THE NOSE & THROATS, NAUSEA & HEADACHES. COMPLETED CABIN AIR QUALITY CARD 33LOOO21001. FOUND WATER SYS WITH CHLORINE SMELL. CIRCULATED WATER SYS & FOUND OK FOR SERVICE. FOUND THAT THE NR 1 OVEN IN RT AFT GALLEY HAS CHEMICAL SMELL & REPLACED IT IAW AMM 25-35-19. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED & THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 28,442 hrs · 4,014 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR EXIT SIGN FELL OFF. SECURED DOOR EXIT SIGN.

Part: LENS — MISSING (CABIN) · airframe 28,401 hrs · 4,000 cycles

AIRCRAFT WAS NOT GNDED. WALL MOUNTED EMER LIGHT LENS MISSING FROM HANDICAP BATHROOM. LIGHT OPERATES NORMALLY, INSTALLED EMER LIGHT LENS.

Part: SIGN — BROKEN (CABIN) · airframe 28,192 hrs · 3,935 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN AT 3L HAS BROKEN MOUNT & DANGLING FROM CEILING. REPLACED 3L EXIT SIGN HOUSING IAW AMM 33-51-17-400-801A. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,042 hrs · 3,903 cycles

AIRCRAFT WAS NOT GNDED. DURING CABIN EMER LIGHTING BATTERY CAPACITY CHECK, 19 WL FAILED. REPLACED EMER POWER SUPPLY UNIT & BATTERY IAW AMM 33-51-38. SEE AALA201602069007 FOR ADDITIONAL PART INFORMATION.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 28,042 hrs · 3,903 cycles

AIRCRAFT WAS NOT GNDED. DURING CABIN EMER LIGHTING BATTERY CAPACITY CHECK, 19 WL FAILED. REPLACED EMER POWER SUPPLY UNIT & BATTERY IAW AMM 33-51-38. SEE AALA201602069008 FOR ADDITIONAL PART INFORMATION.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,779 hrs · 3,849 cycles

MID CABIN FLOOR, NEXT TO THE 2R DOOR, IS SOFT IN 3 INCH AREA, APPROX 12 INCHES FROM BASE OF 2R DOOR, PARALLEL TO THRESHOLD OF DOOR. REPLACED HEATED FLOOR PANEL 28DS IAW AMM 20-25-16.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 27,538 hrs · 3,793 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ENCOUNTERED BIRD STRIKE. FOLLOWED BY RT ENG VIBRATION, LOW OIL PRESS & ENG FIRE WARNING. SHUT RT ENG DOWN. RETURNED TO FIELD. R & R RT ENG IAW JC 33L40071003.

Part: LENS — DETACHED (EXIT SIGN) · airframe 27,425 hrs · 3,773 cycles

AIRCRAFT WAS NOT GNDED. 3L EXIT SIGN COVER FELL OFF. REPOSITIONED EXIT SIGN COVER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW 33L00005005.

Part: MONITOR — DEFECTIVE (ELECTRICAL SYS) · airframe 27,389 hrs · 3,767 cycles

AFTER TAKEOFF MULTIPLE CB INDICATIONS APPEARED ON THE ECAM, THAT CAUSED POSSIBLE UNSAFE CONDITIONS WITH FIRE DETECTION EQUIPMENT. THE ACFT RETURNED & LANDED WITH NO INCIDENTS. REPLACED THE CB MONITORING UNIT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 24-53-34-000-801-A.

Part: PRESSURE SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 26,980 hrs · 3,703 cycles

AIRCRAFT RT CTR FUEL PUMP AMBER & DASHED ON ECAM PAGE. REPLACED & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-26-15-00-801-A & 28-26-15-400-801-A.

Part: RELAY — TRIPPED (FUEL SYSTEM) · airframe 26,691 hrs · 3,666 cycles

FLIGHT 743 LEFT & RIGHT CTR PUMPS LOW PRESS INDICATION. ACCOMPLISHED TSM TASK 28-21-00-810-835-A. FOUND GFI RELAYS 97QL1 & 97QL2 TRIPPED. CHECKED WIRING FROM GFI RELAY SOCKETS TO PUMP PLUGS WITH NO PROBLEMS FOUND. PERFORMED VISUAL INSPECTION OF PUMP PLUGS & RECEPTACLES WITH NO FAULTS FOUND. FOUND 97QL2 GFI RELAY FOR RT PUMP PRESS TO TEST FUNCTION INOPERATIVE. REPLACED 97QL2 RELAY, REPLACED 97QL1 RELAY FOR LT PUMP AS PRECAUTION. PERFORMED OPERATIONAL CHECK OF CTR TANK TRANSFER SYS IAW AMM 28-26-00, OK AT THIS TIME. SEE ALSO AALA201509299013 FOR LT PUMP RELAY.

Part: RELAY — TRIPPED (FUEL SYSTEM) · airframe 26,691 hrs · 3,666 cycles

FLIGHT 743 LEFT & RIGHT CTR PUMPS LOW PRESS INDICATION. ACCOMPLISHED TSM TASK 28-21-00-810-835-A. FOUND GFI RELAYS 97QL1 & 97QL2 TRIPPED. CHECKED WIRING FROM GFI RELAY SOCKETS TO PUMP PLUGS WITH NO PROBLEMS FOUND. PERFORMED VISUAL INSPECTION OF PUMP PLUGS & RECEPTACLES WITH NO FAULTS FOUND. FOUND 97QL2 GFI RELAY FOR RT PUMP PRESS TO TEST FUNCTION INOPERATIVE. REPLACED 97QL2 RELAY. REPLACED 97QL1 RELAY FOR LT PUMP AS PRECAUTION. PERFORMED OPERATIONAL CHECK OF CTR TANK TRANSFER SYS IAW AMM 28-26-00. OK AT THIS TIME. SEE ALSO AALA201509299004 FOR RT PUMP RELAY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,716 hrs · 3,541 cycles

FLASHLIGHT AT 4L OTBD FLIGHT ATTENDANT JUMP SEAT IS BARELY BLINKING. REPLACED BATTERY, OK FOR SERVICE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 24,044 hrs · 3,290 cycles

MID GALLEY ESPRESSO MAKER 4 - 11 GAVE OFF SMOKE, UNIT WAS SHUT OFF & CB PULLED. UNIT WAS SOMEWHAT LOOSE IN THE RACK.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 24,044 hrs · 3,290 cycles

MID GALLEY ESPRESSO MAKER 4 - 11 GAVE OFF SMOKE, UNIT WAS SHUT OFF & CB PULLED. UNIT WAS SOMEWHAT LOOSE IN THE RACK. REPLACED MID GALLEY ESPRESSO MAKER 4 - 11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, LEVEL 2 GALVANIC CORROSION ON R4 DOOR SILL BETWEEN FRAME 73A TO 75A, Y2462. REPLACED R4 DOOR SILL BETWEEN FRAME 73A TO 75A, Y2462 IAW SRM 53-41-14, 51-44-11 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 251YF BETWEEN FRAME 40 TO 42 & BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 251YF IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 251JF BETWEEN FRAME 37.4 TO 39 & BETWEEN Y1959 TO Y1456. REPLACED FLOOR PANEL 251JF IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 232FF BETWEEN FRAME 19 TO 22 & BETWEEN -Y953 TO -Y450. REPLACED FLOOR PANEL 232FF IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOORBEAM AT FRAME 74, -Y1137.1. REPLACED AFT CABIN FLOORBEAM IAW SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 132HG BETWEEN FRAME 31 TO 36 & BETWEEN -Y2462 TO -Y145. REPLACED FLOOR PANEL 132HG IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOORBEAM AT FRAME 74, -Y794.3. REPLACED AFT CABIN FLOORBEAM IAW SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 261EH BETWEEN FRAME 60 TO 62 & BETWEEN Y1959 TO Y1456. REPLACED FLOOR PANEL 261EH IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FRAME 74, Y1137.1. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, 51-44-11 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 271GF BETWEEN FRAME 73 TO 76 & BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 271GF IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 40 TO 47, -Y450. REPLACED SEAT TRACK IAW SRM 53-31-15, 51-44-11 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 272AG BETWEEN FRAME 71 TO 73 & BETWEEN -Y2462 TO -Y1456. REPLACED FLOOR PANEL 272AG IAW SRM 53-02-00, PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 262YG BETWEEN FRAME 69 TO 71 & BETWEEN -Y1959 TO -Y953. REPLACED FLOOR PANEL 262YG IAW SRM 53-02-00 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 73 TO 74, -Y1640. REPLACED SEAT TRACK IAW SRM 53-00-15 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 272CF BETWEEN FRAME 71 TO 74 & BETWEEN -Y1959 TO -Y1456. REPLACED FLOOR PANEL 272CF IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 272GF BETWEEN FRAME 73 TO 76 & BETWEEN -Y2462 TO -Y1959. REPLACED FLOOR PANEL 272GF IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 271CF BETWEEN FRAME 71 TO 74 & BETWEEN Y1456 TO Y953. REPLACED FLOOR PANEL 271CF IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK DELAMINATION ON FLOOR PANEL 271FF BETWEEN FRAME 73 TO 75 & BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL 271FF IAW SRM 53-02-00 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 75, -Y450. REPLACED SEAT TRACK IAW SRM 53-00-15, 51-44-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 73 TO 74, Y1640. REPLACED SEAT TRACK IAW SRM 53-00-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 73 TO 74, Y1240. REPLACED SEAT TRACK IAW SRM 53-41-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 33, -Y45. REPAIRED SEAT TRACK IAW SRM 53-21-15 FIG 202.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

1S CHECK CABIN FLOOR Z PROFILE CORRODED BETWEEN FRAME 75A & 77 AT Y -2462. R & R PROFILE IAW SRM 53-41-14 FIG 102 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FRAME 73 TO 74, -Y1240. REPLACED SEAT TRACK IAW SRM 53-41-15 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FRAME 75A TO 76, Y2462. REPLACED FLOOR SUPPORT IAW SRM 51-73-00, 53-41-14 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FRAME 80 BETWEEN Y450 TO -Y450. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-41-14 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 162EF BETWEEN FRAME 69 TO 73 & BETWEEN Y0 TO Y1020. REPLACED FLOOR PANEL 162EF IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON UPPER SURFACE OF FLOOR PANEL 131HG BETWEEN FRAME 31 TO 36 & BETWEEN Y860 TO Y1400. REPLACED FLOOR PANEL 131HG IAW SRM 53-02-00, PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 131KG BETWEEN FRAME 36 TO 37.4 & BETWEEN Y860 TO Y1400. REPLACED FLOOR PANEL 131KG IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 132DG BETWEEN FRAME 37.4 TO 39.1 & BETWEEN -Y860 TO -Y1400. REPLACED FLOOR PANEL 132DG IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON FLOOR PANEL 131CG BETWEEN FRAME 37.4 TO 39.1 & BETWEEN Y860 TO Y1400. REPLACED FLOOR PANEL 131CG IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,676 hrs · 3,206 cycles

S1 CHECK, DELAMINATION ON UPPER SURFACE OF FLOOR PANEL 132CG BETWEEN FRAME 37.4 TO 39.1 & BETWEEN -Y200 TO -Y720. REPLACED FLOOR PANEL 132CG IAW SRM 53-02-00 PARA 5 I FIG 211.

Part: SIGN — MISSING (CABIN) · airframe 23,676 hrs · 3,206 cycles

EMERGENCY EXIT SIGN ABOVE R3 DOOR. R & R EMER EXIT SIGNS ABOVE R3 DOOR AS REQUIRED. OK FOR SERVICE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 22,947 hrs · 3,096 cycles

RON CABIN FLOOR PANEL 112DS DELAMINATED. FABRICATED & INSTALLED REPLACEMENT PANEL IAW EA 106189.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 22,947 hrs · 3,096 cycles

RON CABIN FLOOR PANEL 113DS DELAMINATED. FABRICATED & INSTALLED REPLACEMENT PANEL IAW EA 106189.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 22,844 hrs · 3,083 cycles

SEAT MOUNTED EMER LIGHT INOPERATIVE AT 6B. REPINED CONNECTOR AT SIDE WALL FOR SEAT 6AB EMER ESCAPE PATH LIGHT. OPERATIONAL CHECK IS GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 22,812 hrs · 3,079 cycles

RON VISIT SPONGY DELAMINATED AFT GALLEY FLOOR PANEL 40DS BETWEEN FRAME 72 TO 77. REPLACED IAW AMM 25-27-51-000-801A 400-801A.

Part: COVER — MISSING (EXIT SIGN) · airframe 21,653 hrs · 2,931 cycles

3L DOOR EMER SIGN NEEDS REPLACED. REINSTALLED FWD FACING, OVERHEAD EMER EXIT SIGN LENS COVER AT DOOR 3L. OK FOR SERVICE.

Part: APU — FAULTY (APU BAY) · airframe 21,613 hrs · 2,926 cycles

AFTER EXTERNAL AIR DISCONNECTED TURNED APU BLEED ON & SMOKE FILLED COCKPIT & CABIN. EYE IRRITATION WAS EXPERIENCED. R & R THE APU. THE LT & RT CONDENSERS, REHEATER, ACM'S & HEAT EXCHANGERS WERE ALSO R & R DUE TO CONTAMINATION.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

1L DOOR ASSIST BOTTLE PRESS BELOW 1783 PSI. MX 1L DOOR ASSIST BOTTLE PRESS.

Part: SIGN — DETACHED (CABIN) · airframe 21,235 hrs · 2,873 cycles

3R DOOR EXIT SIGN FELL OFF. REINSTALLED EXIT SIGN AT 3R DOOR, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,818 hrs · 2,808 cycles

FORWARD LT FLIGHT ATTENDANT SEAT EMERGENCY LIGHT INOPERATIVE. R & R BATTERY FOR FWD LT FLIGHT ATTENDANT SEAT EMERGENCY LIGHT, OPERATIONS NORMAL.

Part: LENS — CRACKED (CABIN) · airframe 20,663 hrs · 2,785 cycles

EXIT LIGHT FIXTURE AT DOOR 3R HAS FALLEN OFF & IS CRACKED. INSTALLED NEW EXIT LENS AT DOOR 3R.

Part: LENS — BROKEN (CABIN) · airframe 20,132 hrs · 2,670 cycles

EMERGENCY EXIT LIGHT LENS ROW 15 LT SIDE OF PLANE BROKEN. R & R EMERGENCY EXIT LIGHT LENS AT ROW 15 AB AS REQUIRED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,969 hrs · 2,639 cycles

C1 CHECK MULTIPLE AREAS OF DELAMINATION ON CARGO FLOOR PANEL BETWEEN FRAME 69 TO FRAME 73 & BETWEEN BL 0 TO RBL 37. REPLACED CARGO FLOOR PANEL BETWEEN FRAME 69 TO FRAME 73 & BETWEEN BL 0 TO RBL 37 IAW A330 AMM TASK 53-00-00-400-804-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,969 hrs · 2,639 cycles

C1 CHECK MULTIPLE AREAS OF DIS BONDING & DELAMINATION ON CARGO FLOOR PANEL BETWEEN FRAME 69 TO FRAME 73 & BETWEEN BL 0 TO LBL 37. REPLACED CARGO FLOOR PANEL BETWEEN FRAME 69 TO FRAME 73 & BETWEEN BL 0 TO LBL 37 IAW A330 AMM TASK 53-00-00-400-804-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,969 hrs · 2,639 cycles

C1 CHECK MULTIPLE AREAS OF DIS BONDING & DELAMINATION ON CARGO FLOOR PANEL BETWEEN FRAME 67 TO FRAME 69 & BETWEEN RBL 22 TO LBL 46. REPLACED CARGO FLOOR PANEL BETWEEN FRAME 67 TO FRAME 69 & BETWEEN RBL 22 TO LBL 46 IAW A330 AMM TASK 53-00-00-400-804-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,969 hrs · 2,639 cycles

C1 CHECK MULTIPLE AREAS OF DELAMINATION ON CARGO FLOOR PANEL BETWEEN FRAME 67 TO FRAME 69 & BETWEEN RBL 22 TO RBL 46. REPLACED CARGO FLOOR PANEL BETWEEN FRAME 67 TO FRAME 69 & BETWEEN RBL 22 TO RBL 46 IAW A330 AMM TASK 53-00-00-400-804-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 19,969 hrs · 2,639 cycles

C1 CHECK, CABIN FLOOR PANEL 38DS DELAMINATED. FABRICATED & INSTALLED NEW PANEL IAW EA 105495 & SRM 53-02-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,675 hrs · 2,422 cycles

LENS MISSING FROM FLOOR ESCAPE PATH MARKING LIGHTS AT LAV L53 FWD AND AFT CORNERS, LAV 54 AND LAV 74. MX INSTALLED LENS ON ESCAPE PATH LIGHTS AT LAVS L53, L54 & L74.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,584 hrs · 2,412 cycles

EMERGENCY FLASHLIGHT AT 3R, F/A STATION, INOPERATIVE. MAINTENANCE R & R EMERGENCY FLASHLIGHT AT SEAT 3R F/A STATION.

Part: COVER — BROKEN (EMERGENCY LIGHT)

LOWER RT SIDE PATH LIGHT COVER BROKEN BY LAVATORY (L-38). MX ADJUSTED EMERGENCY ESCAPE PATH LIGHT COVER. OPS CHECKED OK.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 17,368 hrs · 2,262 cycles

AREA EXIT LIGHT ABOVE 3R INOPERATIVE. MX FOUND WIRE OFF OF TERMINAL AND SECURED WIRE. OPS CHECKS OK AT THIS TIME.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 17,220 hrs · 2,243 cycles

FAILED EMERGENCY LIGHT BATTERIES AT 4L AND ALSO 2L. MAINTENANCE REPLACED BATTERIES 4L & ALSO 2L, OPERATIONAL CHECK IS OK.

Part: SIGN — DETACHED (CABIN)

3L DOOR EMERGERGENY LIGHT SIGN FELL OFF. MAINTENANCE ATTACHED SIGN, OPERATIONAL CHECK IS OKAY.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 16,620 hrs · 2,168 cycles

CABIN FILLED WITH STRONG ODOR AND GOT ECAM CONDITIONING RIGHT CABIN VENT FAULT. COND PAGE SHOWED FAN IN AMBER. MAINTENANCE REPLACED RIGHT RECIRULATION FAN (210HG) CHECKS GOOD.

Part: SIGN — MISSING (CABIN) · airframe 16,462 hrs · 2,149 cycles

EXIT SIGN IS MISSING ABOVE 2R DOOR. MAINTENANCE REPLACED 2R EXIT SIGN AS REQUIRED CHECKS OKAY.

Part: LENS — MISSING (CABIN) · airframe 15,969 hrs · 2,072 cycles

AISLE EMERGENCY EXIT PATH LIGHT AT LAV 53 MISSING LENS. MAINTENANCE INSTALLED LENS ON EMERGENCY EXIT LIGHT AT L53.

Part: SIGN — MISSING (CABIN)

EXIT SIGN MISSING AT SEAT 23A. SIGN PLACED ON COUNTER AT ROW 1. MAINTENANCE INSTALLED EXIT SIGN ASSEMBLY.

Part: COVER — DETACHED (CABIN) · airframe 15,877 hrs · 2,058 cycles

EXIT LIGHT COVER BECAME DETACHED AT 3L DOOR. MAINTENANCE RE-ATTACHED COVER.

Part: LENS — MISSING (CABIN) · airframe 15,764 hrs · 2,040 cycles

AISLE EMERGENCY EXIT PATH LIGHT MISSING LENS, FORWARD CORNER OF L53 LAV. MAINTENANCE INSTALLED EE LIGHT LENS AT LAV L53, OPS CHECKS OK.

Part: OVEN — DIRTY (GALLEY)

FIRE IN AFT GALLEY OVEN, NEED TO HAVE GREASE CLEANED OUT. MAINTENANCE - ALL THREE OVENS FIRMLY CLEANED.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 14,942 hrs · 1,913 cycles

STRONG ELECTRICAL SMELL NEAR VIDEO SYSTEM. MAINTENANCE TROUBLESHOOT CABIN AIR QUALITY. RAN BOTH ENGINES AND APU NO ODOR NOTED. INSPECTED GALLEYS AND LAVS AND CABIN AREA. REPLACED MID GALLEY COFFEEMAKER DUE TO BURNING ODOR. NO OTHER ODORS NOTED. REPLACED VIDEO CREW TERMINAL ASSEMBLY AS PRECAUTIONARY.

Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM)

FLIGHT 702, PHL-FRA - APPROXIMATELY 1 HOUR INTO FLIGHT AT FL370-GREEN HYDRAULIC LOW QUANITY-MONITORED-AND STILL CONTINUED TO DROP B/O MID HASH MARK. COMPLETED PROCEDURE, FREE FELL GEAR NORMAL (NOT OVERWEIGHT) LANDING. MAINTENANCE FOUND GREEN HYDRAULIC SYSTEM LINE LEAKING FROM HYDRAULIC PRESS REGULATOR TO MANIFOLD, REMOVED AND REPLACED HYDRAULIC LINE, LEAK CHECKS GOOD.

Part: LENS — MISSING (CABIN) · airframe 13,666 hrs · 1,744 cycles

EMERGENCY LIGHT LEN'S MISSING 21 AB. MAINTENANCE INSTALLED LEN'S AS REQUIRED, OPS CHECKS GOOD.

Part: LENS — MISSING (CABIN)

EMERGENCY LIGHT COVER 23C MISSING (AT TOILET FRONT WALL). MAINTENANCE INSTALLED REQUIRED LENS.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 11,768 hrs · 1,506 cycles

R-3 DOOR EMERGENCY ASSIST CYLINDER PRESSURE LOW. MAINTENANCE SERVICED R-3 DOOR ASSIST CYL PER MM 52-10-00-600-802, LEAK CHECK OK.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 11,169 hrs · 1,429 cycles

C2 CHECK - DISBONDED HEATED FLOOR PANEL AT R4 DOORWAY AT FR76 IN AFT GALLEY AREA. REPLACED HEATED FLOOR PANEL AT R4 DOORWAY IAW EA # 102315.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 11,169 hrs · 1,429 cycles

C2 CHECK - DISBONDED HEATED FLOOR PANEL AT R4 DOORWAY AT FR76 IN AFT GALLEY AREA. REPLACED HEATED FLOOR PANEL AT R4 DOORWAY IAW EA 102315.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 10,858 hrs · 1,390 cycles

PHL - FOUND FLASHLIGHT RED LED NOT FLASHING AT L2 DOOR. REPLACED BATTERY PACK ON FLASHLIGHT NEAR L2 DOOR.

Part: APU — ODOR · airframe 10,796 hrs · 1,381 cycles

FLIGHT 9195, ODOR IN CABIN BELOW FL250, WHEN ENGINES AT IDLE DURING DESCENT, WOULD DISSIPATE WHEN ENGINES CAME BACK UP. APU WAS OFF, ENGINE BLEEDS ON. ON PREVIOUS FLIGHT 796 DURING DESCENT CABIN AND COCKPIT AIR QUALITY DIMINISHED WITH AN ODOR SIMILAR TO DIRTY SOCKS. MAINTENANCE FOUND NO FAULTS, ACFT RELEASED FOR MAINTENANCE FERRY FLIGHT. MAINTENANCE REMOVED AND REPLACED THE APU. ALSO REPLACED THE LEFT AND RIGHT PACK HEAT EXCHANGERS, OZONE CONVERTERS, AND CONDENSERS. ACCOMPLISHED DECONTAMINATION OF THE ESC SYSTEM.

Part: CONTROL UNIT — OVERHEATED (CABIN) · airframe 10,588 hrs · 1,356 cycles

FLIGHT 755, CDG-PHL - APPEARS TO BE EXCESSIVE HEATING ON FLOOR BY R2 DOOR. HOLE IN VINYL LOOKS TO BE CAUSED BY THE HEAT. F/A REPORTS THAT WASN'T THERE PRIOR TO FLIGHT. MAINTENANCE REPLACED IPCU 14DS PER AMM 25-27-35. ALSO REPLACED 2R HEAT PANELS 28DS AND 26DS PER AMM 25-27-51. REPLACED 2R FLOOR MAT PER AMM 25-48-42.

Part: LENS — MISSING (CABIN) · airframe 10,371 hrs · 1,328 cycles

PHL - EMERGENCY EXIT LIGHT ON LAV L37 MISSING LENS AND DAMAGED. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSY ON LAV L37 W/LENS. OPS CHECK GOOD.

Part: LENS — LOOSE (CABIN) · airframe 10,371 hrs · 1,328 cycles

PHL - EMERGENCY EXIT LIGHT LENS LOOSE AT LAV L61. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT LENS AT L61, OPS CHECKS OK.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 9,918 hrs · 1,274 cycles

TLV - DOOR 1R PRESSURE INDICATOR MESSAGE ON CIDS PANEL. MAINTENANCE DOOR 1R EMERGENCY OPENING ACTUATOR AT LOW PRESSURE (RED BAND). DOOR 1R DAMPER AND EMERGENCY OPS CYLINDER RECHARGED TO GREEN BAND.

Part: SIGN — DETACHED (CABIN) · airframe 9,149 hrs · 1,177 cycles

BCN - THE EXIT SIGN AT THE 3L DOOR FELL OFF NEEDS TO BE RE-ATTACHED. MAINTENANCE FOUND AND RE-ATTACHED 3L EXIT SIGN.

Part: FILTER — CLOGGED (CABIN) · airframe 9,119 hrs · 1,171 cycles

FLIGHT 9196, TLV - PHL - DURING DESCENT ON FERRY FLIGHT THE ODOR RETURNED THROUGH THE CABIN FROM PREVIOUS FLIGHT. THE ODOR IS DESCRIBED AS "ACRID - BURNT OIL" SMELL. THE ODOR WOULD DISSIPATE WHEN THRUST WAS NOT AT IDLE. MAINTENANCE INSPECTED AND CLEANED APU BLEED AIR DUCT. REMOVED, CLEANED AND INSPECTED BOTH HP BLEED VALVES FOR CONTAMINATION. ACCOMPLISHED BORESCOPE BOTH ENGINES HP COMPRESS BLADES STAGES 3 THRU 6. REPLACED CABIN RECIRC FILTERS. ACCOMPLISHED HIGH POWER ENGINE RUN.

Part: APU — ODOR · airframe 9,119 hrs · 1,171 cycles

FLIGHT 796, DESCENDING THROUGH 18,000 FT A VERY FOUL ODOR WAS DETECTED IN COCKPIT & CABIN (APPEARS TO BE COMING FROM THE AIR CONDITIONING SYSTEM). MAINTENANCE REPLACED THE APU ASSEMBLY.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 8,948 hrs · 1,150 cycles

PHL - R-1 DOOR ASSIST CYLINDER PRESSURE LOW. MAINTENANCE SERVICED THE R1 DOOR ASSIST CYLINDER PER MM 52-10-00-600-802. LEAK CHECK IS GOOD.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,656 hrs · 725 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 272BF BETWEEN FR74 TO FR75 & BETWEEN -Y794.3 TO -Y1137. REPLACED CABIN FLOOR PANEL 272BF BETWEEN FR74 TO FR75 & BETWEEN -Y794.3 TO -Y1137 IAW EA 102315.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 5,656 hrs · 725 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 272CF BETWEEN FR74 TO FR75 & BETWEEN -Y450 TO -Y794.3. REPLACED CABIN FLOOR PANEL 272CF BETWEEN FR74 TO FR75 & BETWEEN -Y450 TO -Y794.3 IAW EA 102315.

Part: PRESSURE SWITCH — FAULTY (JHYDRAULIC SYS)

CLT FLT 786 CLT TO CDG. ECAM: NORM BRAKE AND AUTOBRAKE. NO BRAKES, ACCUMULATOR PRESSURE ONLY. TOWED IN. GREEN SYSTEM HYDRAULIC PRESSURE SWITCH 7JS1 REPLACED.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

TLV - FOUND ONE LEFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT.

Part: BOTTLE — LOW PRESSURE (R3 DOOR)

TLV - FOUND DOOR DAMPER BOTTLE CHARGE OUT OF GREEN BAND; DOOR R3. CHARGED DAMPER PRESSURE AT R3.