N808AW

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 79,047 hrs · 37,370 cycles

AIRCRAFT WAS NOT GROUNDED: R1 CABIN DOOR SLIDE ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED R1 DOOR DAMPER TO CORRECT SPECIFICATION PER AMM 52-10-00.

Part: LIGHT — NO TEST (ZONE 200) · airframe 78,960 hrs · 37,317 cycles

AIRCRAFT WAS NOT GROUNDED: FLOOR PROXIMITY LIGHT AT 8C INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LOCATION, SEAT/WALL MOUNTED IAW AMM 33-51-18.

Part: SHADE — STUCK (ZONE 800) · airframe 78,641 hrs · 37,098 cycles

AIRCRAFT WAS NOT GROUNDED: 14 F EMERGENCY EXIT WINDOW SHADE WILL NOT OPEN. MAINTENANCE REPLACED 14F EMERGENCY EXIT WINDOW BLIND SHADE IAW AMM 25-23-43.

Part: SHADE — INOPERATIVE (ZONE 200) · airframe 78,641 hrs · 37,098 cycles

AIRCRAFT WAS NOT GROUNDED: 14 F EMERGENCY EXIT WINDOW SHADE WILL NOT OPEN. (OPEN)

Part: BATTERY — NO TEST (ZONE 200) · airframe 77,670 hrs · 36,476 cycles

AIRCRAFT WAS NOT GROUNDED: RH EMR EXIT BATTERY FAILED TEST. MAINTENANCE REPLACED RH EMR BATT IAW AMM 33-51-38 OPS CK GOOD.

Part: LIFE LINE — UNPACKED (ZONE 200 - FUSE) · airframe 76,661 hrs · 35,839 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIFE ROPE NEEDS TO BE REPACKED. MAINTENANCE REPACKED LIFELINE AS REQUIRED AND STOWED IN CABIN.

Part: OIL SYSTEM — LEAKING (APU) · airframe 75,929 hrs · 35,353 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A DIRTY SOCK SMELL ON IDLE DECENT INTO DFW THRU 10,000. WENT AWAY THRU APPROXIMATLEY 5000 FT. MAINTENANCE FOUND SIGNIFICANT OIL CONTAMINATION AT THE APU INLET AND CONFIRMED THE V-BAND SEAL WAS COMPLETELY SATURATED WITH OIL. MAINTENANCE REPLACED THE APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L31049003.

Part: OIL SYSTEM — LEAKING (APU) · airframe 75,929 hrs · 35,353 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A DIRTY SOCK SMELL ON IDLE DECENT INTO DFW THRU 10,000. WENT AWAY THRU APPROXIMATLEY 5000 FT. MAINTENANCE FOUND SIGNIFICANT OIL CONTAMINATION AT THE APU INLET AND CONFIRMED THE V-BAND SEAL WAS COMPLETELY SATURATED WITH OIL. (OPEN)

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 75,698 hrs · 35,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL. AFTER TAKEOFF FLIGHT CREW RECEIVED RIGHT GEAR HOT BRAKES INDICATIONS. ONCE GEAR TEMPERATURE WAS BELOW 200 C, THE FLIGHT CREW RAISED GEAR AND NOTED THAT IT WAS SLOW TO RETRACT. EVENTUALLY THEY GOT AN UNSAFE GEAR ECAM MESSAGE. THE WHEEL PAGE SHOWED THE GEAR UP AND ALL DOORS OPENED. TRIPLE INDICATOR SHOWED 3 REDS ABOVE GEAR HANDLE. THEY FOLLOWED ECAM/QRH PROCEDURES, CYCLED THE GEAR AND RECEIVED LANDING GEAR NOT UPLOCKED ECAM MESSAGE, HOWEVER THE GEAR SHOWED 3 GREEN ON TRIPLE INDICATOR AND WHEEL PAGE SHOWED DOORS GREEN CLOSED. GEAR HANDLE DOWN. ECAM CALLED TO RECYCLE GEAR, BUT IT WAS DECIDED SINCE THE GEAR WAS GREEN AND DOWN NOT TO KEEP RECYCLING AND RETURN TO PHL WHERE IT LANDED SAFELY. THE FLIGHT CREW REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR DISAGREE ECAM. MESSAGE. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR PROXIMITY SENSOR 36GA HAD FAILED AND REPLACED IT. (AALA202407105343) MAINTENANCE FOUND ALL 3 HYDRAULIC SYSTEMS WERE OVERSERVICED AND CORRECTLY SERVICED ALL 3 HYDRAULIC SYSTEMS. (AALA202407108311) MAINTENANCE ALSO FOUND THE GREEN AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE UNIT 1360GM HAD FAILED AND REPLACED IT. (AALA202407108722). MAINTENANCE ALSO FOUND THE BRAKE STEERING CONTROL UNIT (BSCU) HAD MULTIPLE FAULTS AND REPLACED IT. (AALA202407108208) A SATISFACTORY OPERATIONAL CHECK OF THE LANDING GEAR AND BRAKE SYSTEM WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: HYDRAULIC SYSTEM — OVERSERVICED (ZONE 100) · airframe 75,698 hrs · 35,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL. AFTER TAKEOFF FLIGHT CREW RECEIVED RIGHT GEAR HOT BRAKES INDICATIONS. ONCE GEAR TEMPERATURE WAS BELOW 200 C, THE FLIGHT CREW RAISED GEAR AND NOTED THAT IT WAS SLOW TO RETRACT. EVENTUALLY THEY GOT AN UNSAFE GEAR ECAM MESSAGE. THE WHEEL PAGE SHOWED THE GEAR UP AND ALL DOORS OPENED. TRIPLE INDICATOR SHOWED 3 REDS ABOVE GEAR HANDLE. THEY FOLLOWED ECAM/QRH PROCEDURES, CYCLED THE GEAR AND RECEIVED LANDING GEAR NOT UPLOCKED ECAM MESSAGE, HOWEVER THE GEAR SHOWED 3 GREEN ON TRIPLE INDICATOR AND WHEEL PAGE SHOWED DOORS GREEN CLOSED. GEAR HANDLE DOWN. ECAM CALLED TO RECYCLE GEAR, BUT IT WAS DECIDED SINCE THE GEAR WAS GREEN AND DOWN NOT TO KEEP RECYCLING AND RETURN TO PHL WHERE IT LANDED SAFELY. THE FLIGHT CREW REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR DISAGREE ECAM. MESSAGE. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR PROXIMITY SENSOR 36GA HAD FAILED AND REPLACED IT. (AALA202407105343) MAINTENANCE FOUND ALL 3 HYDRAULIC SYSTEMS WERE OVERSERVICED AND CORRECTLY SERVICED ALL 3 HYDRAULIC SYSTEMS. (AALA202407108311) MAINTENANCE ALSO FOUND THE GREEN AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE UNIT 1360GM HAD FAILED AND REPLACED IT. (AALA202407108722). MAINTENANCE ALSO FOUND THE BRAKE STEERING CONTROL UNIT (BSCU) HAD MULTIPLE FAULTS AND REPLACED IT. (AALA202407108208) A SATISFACTORY OPERATIONAL CHECK OF THE LANDING GEAR AND BRAKE SYSTEM WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: CONTROL UNIT — FAULTED (RT MLG BRAKES) · airframe 75,698 hrs · 35,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL. AFTER TAKEOFF FLIGHT CREW RECEIVED RIGHT GEAR HOT BRAKES INDICATIONS. ONCE GEAR TEMPERATURE WAS BELOW 200 C, THE FLIGHT CREW RAISED GEAR AND NOTED THAT IT WAS SLOW TO RETRACT. EVENTUALLY THEY GOT AN UNSAFE GEAR ECAM MESSAGE. THE WHEEL PAGE SHOWED THE GEAR UP AND ALL DOORS OPENED. TRIPLE INDICATOR SHOWED 3 REDS ABOVE GEAR HANDLE. THEY FOLLOWED ECAM/QRH PROCEDURES, CYCLED THE GEAR AND RECEIVED LANDING GEAR NOT UPLOCKED ECAM MESSAGE, HOWEVER THE GEAR SHOWED 3 GREEN ON TRIPLE INDICATOR AND WHEEL PAGE SHOWED DOORS GREEN CLOSED. GEAR HANDLE DOWN. ECAM CALLED TO RECYCLE GEAR, BUT IT WAS DECIDED SINCE THE GEAR WAS GREEN AND DOWN NOT TO KEEP RECYCLING AND RETURN TO PHL WHERE IT LANDED SAFELY. THE FLIGHT CREW REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR DISAGREE ECAM. MESSAGE. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR PROXIMITY SENSOR 36GA HAD FAILED AND REPLACED IT. (AALA202407105343) MAINTENANCE FOUND ALL 3 HYDRAULIC SYSTEMS WERE OVERSERVICED AND CORRECTLY SERVICED ALL 3 HYDRAULIC SYSTEMS. (AALA202407108311) MAINTENANCE ALSO FOUND THE GREEN AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE UNIT 1360GM HAD FAILED AND REPLACED IT. (AALA202407108722). MAINTENANCE ALSO FOUND THE BRAKE STEERING CONTROL UNIT (BSCU) HAD MULTIPLE FAULTS AND REPLACED IT. (AALA202407108208) A SATISFACTORY OPERATIONAL CHECK OF THE LANDING GEAR AND BRAKE SYSTEM WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: RESERVOIR — FAILED (RT BRAKES) · airframe 75,698 hrs · 35,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL. AFTER TAKEOFF FLIGHT CREW RECEIVED RIGHT GEAR HOT BRAKES INDICATIONS. ONCE GEAR TEMPERATURE WAS BELOW 200 C, THE FLIGHT CREW RAISED GEAR AND NOTED THAT IT WAS SLOW TO RETRACT. EVENTUALLY THEY GOT AN UNSAFE GEAR ECAM MESSAGE. THE WHEEL PAGE SHOWED THE GEAR UP AND ALL DOORS OPENED. TRIPLE INDICATOR SHOWED 3 REDS ABOVE GEAR HANDLE. THEY FOLLOWED ECAM/QRH PROCEDURES, CYCLED THE GEAR AND RECEIVED LANDING GEAR NOT UPLOCKED ECAM MESSAGE, HOWEVER THE GEAR SHOWED 3 GREEN ON TRIPLE INDICATOR AND WHEEL PAGE SHOWED DOORS GREEN CLOSED. GEAR HANDLE DOWN. ECAM CALLED TO RECYCLE GEAR, BUT IT WAS DECIDED SINCE THE GEAR WAS GREEN AND DOWN NOT TO KEEP RECYCLING AND RETURN TO PHL WHERE IT LANDED SAFELY. THE FLIGHT CREW REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR DISAGREE ECAM. MESSAGE. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR PROXIMITY SENSOR 36GA HAD FAILED AND REPLACED IT. (AALA202407105343) MAINTENANCE FOUND ALL 3 HYDRAULIC SYSTEMS WERE OVERSERVICED AND CORRECTLY SERVICED ALL 3 HYDRAULIC SYSTEMS. (AALA202407108311) MAINTENANCE ALSO FOUND THE GREEN AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE UNIT 1360GM HAD FAILED AND REPLACED IT. (AALA202407108722). MAINTENANCE ALSO FOUND THE BRAKE STEERING CONTROL UNIT (BSCU) HAD MULTIPLE FAULTS AND REPLACED IT. (AALA202407108208) A SATISFACTORY OPERATIONAL CHECK OF THE LANDING GEAR AND BRAKE SYSTEM WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 73,997 hrs · 34,120 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DO NOT PASS OPERATIONAL TEST DAMPING FUNCTION DAMPER PASSENGER CREW DOOR 831 AT FWD GALLEY AREA. REPLACED DAMPER PASSENGER CREW DOOR 831 AT FWD GALLEY AREA.

Part: HINGE FITTING — WORN (ZONE 700 - GEARS) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING WORN AT FR 42 AND S42L. REPLACED HINGE FITTING PER CMM 52-81-18

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 73,997 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: DID NOT PASS OPERATIONAL TEST DAMPING FUNCTION DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA. REPLACED DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA PER AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 73,997 hrs · 34,120 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DO NOT PASS OPERATIONAL TEST DAMPING FUNCTION DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACED DAMPER OF THE PASSENGER/CREW DOOR 832.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK#9 FORWARD BOLT BETWEEN WS 10204 AND WS 10729. REPLACED BOLT PER AMM 27-84-66.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #12 LOWER FORWARD BOLT BETWEEN WS 13464 AND WS 14057, BETWEEN RIBS 25 AND 26. REPLACED BOLT PER AMM 27-84-67.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 LOWER AFT BOLT BETWEEN WS 8744 AND WS 9235, BETWEEN RIBS 16 AND 17. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 LOWER FORWARD BOLT BETWEEN WS 8744 AND WS 9235, BETWEEN RIBS 16 AND 17. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 UPPER FORWARD BOLT BETWEEN WS 8744 AND WS 9235, BETWEEN RIBS 16 AND 17. REPLACED BOLT PER AMM 27-84-65.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: STOP — DETERIORATED (ZONE 800 - DOORS) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 842 FORWARD DOOR STOP SCREW AT POSITION 2 DETERIORATED. REPLACED DOOR STOP SCREW PER AMM 52-13-31.

Part: BOLT — CORRODED (ZONE 500) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 MID AFT BOLT AT WS 1406 AND RIB 3. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 MID FORWARD BOLT AT WS 700 AT RIB 2. REPLACED BOLT PER TASK CARD 26C51057005.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231XG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV L.

Part: SLEEVE — WORN (ZONE 400 - NAC/P) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD AFT ATTACH FITING LOWER SLEEVE WORN. REPLACED SLEEVE PER TASK CARD 26C42554028

Part: SLEEVE — WORN (ZONE 400 - NAC/P) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD AFT ATTACH FITING UPPER SLEEVE WORN. REPLACED SLEEVE PER TASK CARD 26C42554028

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 73,997 hrs · 34,120 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER FAILED THE DAMPING FUNCTIONAL TEST. REPLACED DAMPER PER AMM 52-11-14.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FLANGE #6 FASTENER HOLE FOR DOOR STOP #7 AT FR 16 AND S5L. REPAIRED FRAME PER EA 348341.

Part: SKIN PANEL — CORRODED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FUSELAGE SKIN AT FR 70 AND S2R. REPAIRED SKIN PER EA 348858 .

Part: BRACKET — EXCESS PLAY (ZONE 500 - LH WI) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP REAR SPAR FITTING / BRACKET HAS EXCESSIVE PLAY, AT RIB 14. REPLACED BRACKET PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEAR PLATE IN AFT GALLEY AREA LOCATED BETWEEN FR 69 AND FR 70, AND AT STR 23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 20 AND -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRMS 65-67) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 65 AND FR 67 AT -Y318. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 68 AND FR 69 AT -Y1162. REPLACED BEAM PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347841.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB AFT FACE HORIZONTAL FLANGE LOWER RADII AT FR 68 AND S22L. REPAIRED FRAME PER EA 347766.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347841.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST UPPER TENSION BOLT AREA AT FR 2 AND Y0. REPAIRED FRAME PER EA 347841.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,996 hrs · 34,120 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST UPPER RADIUS AREA AT FR 2 AND Y0. REPAIRED FRAME PER EA 347841.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,997 hrs · 34,120 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERATIVE AT EXIT 2R. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT PER AMM 33-00-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DIM (ZONE 200 - FUSE) · airframe 73,718 hrs · 33,970 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EXIT SIGN DIM. REPLACED L1 DOOR EXIT SIGN PER AMM 33-20-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FORK — WORN (ZONE 100 - FUSE) · airframe 73,843 hrs · 34,045 cycles

AIRCRAFT IN BASE MAINTENANCE: 8OVU RACK RIGHT HAND LOWER LATERAL FORK END FITTING WORN AT FR 24 AND S32R. REPLACED FORK END FITTING PER EA 347890.

Part: FORK — WORN (ZONE 100 - FUSE) · airframe 73,843 hrs · 34,045 cycles

AIRCRAFT IN BASE MAINTENANCE: 8OVU RACK LEFT HAND LOWER LATERAL FORK END FITTING WORN AT FR 24 AND S32L. REPLACED FORK END FITTING PER EA 347890.

Part: TRIM PANEL — LOOSE (ZONE 900 - LAV/G) · airframe 73,074 hrs · 33,573 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE SECURED LOOSE TRIM PER CMM 25-41-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR LATCH — LACK OF LUBE (ZONE 800 - DOORS) · airframe 72,205 hrs · 33,046 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR CONTROL HANDLE DIFFICULT TO OPERATE 2R. MAINTENANCE LUBRICATED GIRT BAR ARMING LATCHES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: CENTER AISLE OVERHEAD EXIT SIGN NEAR ROW 14 HAS 8 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND OVER WING SIDEWALL EXIT SIGN HAS 11 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: CENTER AISLE OVERHEAD EXIT SIGN NEAR ROW 13 HAS 6 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN ABOVE L-2 DOOR HAS 7 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN FWD CENTER AISLE HAS 4 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: AFT CENTER AISLE EXIT SIGN (IN BETWEEN LAVATORIES) HAS 8 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,383 hrs · 32,555 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN ABOVE R-1 DOOR HAS 6 LAMPS INOPERATIVE. RELAMPED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: MEGAPHONE — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,524 hrs · 32,036 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS REAR MEGAPHONE NOT WORKING PROPERLY. REMOVED AND REPLACED BATTERIES ON REAR MEGAPHONE, OPERATIONS CHECK GOOD PER AMM 25-61-51.

Part: LIGHT — ODOR (ZONE 200 - FUSE) · airframe 70,494 hrs · 32,021 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL SMOKE SMELL IN AFT GALLEY ON DESCENT. REPLACED AFT GALLEY WORK LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-27-12. NO ODORS NOTED.

Part: SAFETY VALVE — DEFECTIVE (ZONE 200 - FUSE) · airframe 70,429 hrs · 31,985 cycles

AIRCRAFT WAS GROUNDED: INBOUND TO DFW ON ARRIVAL FMS DEVIATED FROM VERTICAL PROFILE. STD QNH STARTED FLASHING AT FLASHING AT FL 270. FMS TOTALLY OFF PROFILE. ECAM CABIN PRESSURE SAFETY VALVE OPEN WITH LOW DIFF PR ABOUT FL 17,000 FT. CABIN PRESSURE LOST AT 8,000 FT. LANDED UN-PRESSURIZED. **ORIGIANL REPORT WAS AALA202204075432** REPLACED BOTH SAFETY VALVES 6HL AND 7HL (AALA202204086106) PER AMM 21-31-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: NONE — NONE · airframe 70,429 hrs · 31,985 cycles

AIRCRAFT WAS GROUNDED: INBOUND TO DFW ON ARRIVAL FMS DEVIATED FROM VERTICAL PROFILE. STD QNH STARTED FLASHING AT FLASHING AT FL 270. FMS TOTALLY OFF PROFILE. ECAM CABIN PRESSURE SAFETY VALVE OPEN WITH LOW DIFF PR ABOUT FL 17,000 FT. CABIN PRESSURE LOST AT 8,000 FT. LANDED UN-PRESSURIZED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SAFETY VALVE — DEFECTIVE (ZONE 200 - FUSE) · airframe 70,429 hrs · 31,985 cycles

AIRCRAFT WAS GROUNDED: INBOUND TO DFW ON ARRIVAL FMS DEVIATED FROM VERTICAL PROFILE. STD QNH STARTED FLASHING AT FLASHING AT FL 270. FMS TOTALLY OFF PROFILE. ECAM CABIN PRESSURE SAFETY VALVE OPEN WITH LOW DIFF PR ABOUT FL 17,000 FT. CABIN PRESSURE LOST AT 8,000 FT. LANDED UN-PRESSURIZED. **SUPPLEMENTAL REPORT FOR AALA202204075432: REPLACED BOTH SAFETY VALVES 6HL AND 7HL (AALA202204086106) PER AMM 21-31-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: LIGHT — ILLUMINATED (ZONE 200 - FUSE) · airframe 70,227 hrs · 31,865 cycles

AIRCRAFT WAS NOT GROUNDED: APU AGENT DISCHARGE LIGHT ILLUMINATED. MAINTENANCE PERFORMED AN OPERATIONAL AND VISUAL CHECK OF THE APU FIRE PROTECTION SYSTEM PER AMM 26-22-00 WITH NO DEFECTS NOTED AND THE AGENT DISCHARGE LIGHT WAS NOT ILLUMINATED.

Part: TRANSMITTER — FAULT MESSAGE (ZONE 200 - FUSE) · airframe 69,881 hrs · 31,636 cycles

AIRCRAFT WAS GROUNDED: CREW ABORTED TAKE OFF AT 20 KNOTS DUE TO A BRAKE SYSTEM 2 ECAM FAULT. REPLACED BRAKE PEDAL TRANSMITTER UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-42-47.

Part: ENGINE — FOD (ZONE 400 - NAC/P) · airframe 69,675 hrs · 31,523 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW REPORTED MULTIPLE BIRD STRIKES WITH #1 ENGINE INGESTION FOLLOWED BY A STALL AND ROLL BACK OF THE #1 ENGINE. PASSENGERS AND FLIGHT ATTENDANTS REPORTED FLAMES OUT THE BACK OF THE ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DSM WHERE IT LANDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. ** SUPPLEMENTAL REPORT FOR AALA202112074827: REPLACED #1 ENGINE AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L40071004. ** (CLOSED)

Part: ENGINE — FOD (ZONE 400 - NAC/P) · airframe 69,675 hrs · 31,523 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW REPORTED MULTIPLE BIRD STRIKES WITH #1 ENGINE INGESTION FOLLOWED BY A STALL AND ROLL BACK OF THE #1 ENGINE. PASSENGERS AND FLIGHT ATTENDANTS REPORTED FLAMES OUT THE BACK OF THE ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DSM WHERE IT LANDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. ** SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: PIN — BROKEN (ZONE 200 - FUSE) · airframe 69,553 hrs · 31,453 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT PATH LIGHTING INOP AT ROW 19. FOUND WIRE BROKEN UNDERNEATH SEAT TRACK CONNECTOR. **SUPPLEMENTAL REPORT FOR AALA202111195370: REPLACED PIN PER ESPM 20-48-25** (CLOSED)

Part: NONE — NONE · airframe 69,553 hrs · 31,453 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT PATH LIGHTING INOP AT ROW 19. FOUND WIRE BROKEN UNDERNEATH SEAT TRACK CONNECTOR. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 69,020 hrs · 31,147 cycles

AIRCRAFT WAS GROUNDED: LEFT WING OUTBOARD TRAILING EDGE FLAP TRAILING EDGE SEPARATED OUTBOARD OF INBOARD CANOE. **SUPPLEMENTAL REPORT FOR AALA202108316193: REPAIRED FLAP PER EA 330294.**(CLOSED)

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 69,020 hrs · 31,147 cycles

AIRCRAFT WAS GROUNDED: LEFT WING OUTBOARD TRAILING EDGE FLAP TRAILING EDGE SEPARATED OUTBOARD OF INBOARD CANOE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN)

Part: SLIDING WINDOW — FAILED (COCKPIT LEFT) · airframe 69,020 hrs · 31,146 cycles

AIRCRAFT WAS GROUNDED: CAPTAINS SLIDING COCKPIT WINDOW SHATTERED WHILE AT THE GATE. REPLACED SLIDING WINDOW PER AMM 56-12-11-000-000-2A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,863 hrs · 31,047 cycles

AIRCRAFT WAS GROUNDED: OVER DOOR EMERGENCY EXIT SIGNS BULBS INOPERATIVE. RELAMPED PER AMM 33-51-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 68,863 hrs · 31,047 cycles

AIRCRAFT WAS GROUNDED: L1 OVER DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED SIGN PER AMM 33-51-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,863 hrs · 31,047 cycles

AIRCRAFT WAS GROUNDED: OVERHEAD EMERGENCY EXIT SIGNS BULBS INOPERATIVE. RELAMPED PER AMM 33-51-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,813 hrs · 31,017 cycles

AIRCRAFT WAS GROUNDED: EXIT SIGN ABOVE DOOR 2L HAS SEVERAL LIGHTS BURNED OUT. REPLACED R2 DOOR EXIT SIGN BULB PLATE OPERATIONS CHECK GOOD PER AMM 33-51-16.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 67,734 hrs · 30,449 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED BATTERIES PER AMM 25-65-51

Part: SUPPORT FRAME — WORN (LT WING) · airframe 67,527 hrs · 30,343 cycles

AIRCRAFT WAS GROUNDED. LEFT WING TRAILING EDGE FRAME SUPPORT, AILERON HINGE SUPPORT ASSEMBLY NR 3 BEARING WORN. LEFT AILERON SUPPORT FRAME ASSEMBLY NR 3 REPLACED, PER AMM 57-51-31.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 67,201 hrs · 30,180 cycles

AIRCRAFT WAS GROUNDED. STRONG ELECTRICAL ODOR IN FLIGHT DECK, DECLARED EMERGENCY AND DIVERTED TO LAS. TROUBLESHOOTING DETERMINED LOWER ECAM DISPLAY UNIT INOPERABLE. REPLACED LOWER ECAM DU, IAW AMM 31-63-22. OPERATIONS CHECK GOOD.

Part: SKIN — DENTED (RT WING SLAT) · airframe 66,523 hrs · 29,797 cycles

AIRCRAFT WAS GROUNDED. DENT FOUND ON RIGHT NR 1 SLAT UPPER SKIN. REPAIRED THE SLAT SKIN IAW SRM 57-40-00-300-90.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 65,844 hrs · 29,402 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS NR 2 ENG COWL SMOKE & DRIPPING FLUID. REMOVED & REPLACED NR 2 HYDRAULIC EDP IAW AMM 29-10-00, LEAK CHECK - OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,755 hrs · 28,225 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT DOOR 1L INDICATED LOW OR DEAD BATTERY. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-27-15.

Part: FITTING — WORN (MLG DOOR ACT) · airframe 63,058 hrs · 27,825 cycles

DURING A GEAR CHANGE, MAINTENANCE REPORTED WEAR ON THE BORE COMMON TO THE LEFT FORWARD MLG DOOR ACTUATOR FITTING. THE DAMAGE NOT REPAIRABLE. REPLACED THE FITTING IAW EA 288080.

Part: FITTING — DAMAGED (FRAMES 42-43) · airframe 63,058 hrs · 27,825 cycles

FITTING OUT OF LIMITS ON THE LUG BORE, OUT OF ROUND, FRAMES 42 TO 43, -Z381. REPLACED THE FITTING IAW EA 288080.

Part: FITTING — WORN (FRAMES 42-43) · airframe 63,058 hrs · 27,825 cycles

DURING A GEAR CHANGE, MAINTENANCE FOUND WEAR ON THE BORE COMMON TO THE LEFT FORWARD MLG DOOR ACTUATOR FITTING BETWEEN FRAMES 42-43. REPLACED THE FITTING IAW EA 288080.

Part: PINTLE PIN — CORRODED (RT MLG) · airframe 63,058 hrs · 27,825 cycles

RIGHT MAIN LANDING GEAR REAR PINTLE PIN WAS CORRODED. REPLACED THE PINTLE PIN IAW JC 26T00032001.

Part: APU — ODOR (APU BAY) · airframe 62,439 hrs · 27,454 cycles

ROWS 14 TO BACK GALLEY THERE WAS AN ODOR OF ENGINE OIL FUMES COMING INTO CABIN. APU COOLING FAN WAS BLOWING OILY MIST, REMOVED COOLING FAN AND FOUND LARGE HOLE IN AFT RIGHT SIDE OF PLENUM. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE APU IAW 26L31049005 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 62,303 hrs · 27,365 cycles

DURING DECENT, WITH IDLE THRUST HIGH PRESSURE VALVE ON THE NR 2 ENGINE INTERMITTENTLY FAILED. FOUND HP VALVE CONNECTOR & BACKSHELL DAMAGED. REPLACED THE NR 2 ENGINE BLEED HIGH PRESSURE VALVE IAW AMM 36-11-51.

Part: TACHOMETER — FAULTED (BRAKE SYSTEM) · airframe 62,259 hrs · 27,332 cycles

ECAM FOR BRAKES, AUTO BRAKE FAULT. BRAKES RELEASED SHORTLY AFTER TAKEOFF AND MESSAGE CLEARED AFTER ENGINE SHUTDOWN. REPLACED THE NR 3 20GG TACHOMETER IAW AMM 32-42-57. TESTED GOOD IAW AMM 32-42-00-720-003-A.

Part: CONTROL UNIT — FAULTED (BRAKE SYS) · airframe 61,602 hrs · 26,883 cycles

AT 80 KNOTS DURING TAKEOFF ROLL, AUTO BRAKE FAULT, BRAKES RELEASED MESSAGE ON ECAM. MAINTENANCE REPLACED THE BRAKING AND STEERING CONTROL UNIT IAW AMM 32-42-34, BITE TEST OF THE BRAKING AND STEERING CONTROL UNIT IAW AMM 32-46-00-740-001A, AND PERFORMED SATISFACTORY OPS CHECK.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,269 hrs · 26,693 cycles

DIRTY SOCK ODOR DURING DESCENT, STRONG IN BACK. NO CONTAMINATION FOUND. REPLACED COOLING FAN ON APU IAW AMM 49-52-51, CLEANED, POWER WASHED APU COMPARTMENT AS REQUIRED NO LEAKS. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,269 hrs · 26,693 cycles

REPORT OF CABIN ODOR ON APPROACH. AIRCRAFT WAS GROUNDED

Part: UNKNOWN — ODOR (CABIN) · airframe 61,141 hrs · 26,613 cycles

FLIGHT ATTENDANT REPORTED A FUME EVENT THAT LASTED FIVE MINUTES ON DESENT. EVENT WAS PRIMARLLY IN THE AFT GALLEY AREA. NO FUMES WERE EXPERIENCED IN THE FLIGHT DECK. ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLESHOOTING. CLEANED ALL COFFEE MAKERS AND OPS CHECKED GOOD. CLEANED AFT EXTRACTION FILTERS. ADDED OIL TO APU. OPERATED APU BLEED SYSTEM INDEPENDENTLY. THEN BOTH PACKS INDIVIDUALLY. NO ODER NOTED AT THIS TIME.

Part: APU — OVERSERVICED · airframe 60,317 hrs · 26,166 cycles

VERY FAINT DIRTY SOCK ODOR IN THE FLIGHT DECK & CABIN. TROUBLESHOT TO APU OIL OVERSERVICED. REMOVED EXCESSIVE OIL AS REQUIRED. AIRCRAFT WAS GROUNDED.

Part: BEARING — FAILED (COOLING FAN) · airframe 60,044 hrs · 26,023 cycles

RIGHT AFTER TAKE OFF, HAD A STRONG ELECTRICAL ODOR. FLIGHT ATTENDANT SMELLED THE ODOR NEAR THE FWD LAVATORY. FOUND INLET FAN BEARINGS FAILED. REMOVED AND REPLACED INLET FAN.

Part: RESERVOIR — MISSING (OVERWING SLIDE) · airframe 62,710 hrs · 27,929 cycles

MISSING RESERVOIR OVERWING ESCAPE SLIDE, RT SIDE, IN THE AFT CARGO BAY. REPLACED THE RESERVOIR IAW AMM.

Part: STRUT — CORRODED (TE FLAP) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING INBOARD FLAP INTERCONNECTING STRUT BETWEEN RIBS 9 AND 10. REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.

Part: STRUT — CORRODED (TE FLAP) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING INBOARD FLAP INTERCONNECTING STRUT BETWEEN RIBS 8 AND 9. REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.

Part: BOLT — CORRODED (LT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON LEFT SLAT TRACK NR 8 UPPER AFT BOLT BETWEEN RIBS 16 AND 19. REPLACED BOLT IAW AMM 27-84-65.

Part: BOLT — CORRODED (LT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON LEFT WING SLAT TRACK NR 10 LOWER MID BOLT. REPLACED THE BOLT IAW AMM 27-84-66.

Part: BOLT — CORRODED (LT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON LEFT WING SLAT TRACK NR 9 FORWARD BOLT. REPLACED THE BOLT IAW AMM 27-84-66.

Part: BOLT — CORRODED (LT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON LEFT WING SLAT TRACK NR 1 LOWER BOLT. REPLACED THE BOLT IAW AMM 27-84-63.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON RIGHT WING SLAT TRACK NR 10 LOWER MID BOLT BETWEEN RIBS 21 AND 22. REPLACED THE BOLT IAW AMM 27-84-66.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON RIGHT WING SLAT TRACK NR 11 FORWARD LOWER BOLT. REPLACED THE BOLT IAW AMM 27-84-67.

Part: LINK ROD — OUT OF ADJUST (PAX DOOR) · airframe 59,965 hrs · 25,966 cycles

OUT OF ADJUSTMENT FINGER DOOR DAMPER PASSENGER DOOR. ADJUSTED THE LINK ROD.

Part: LINK ROD — OUT OF ADJUST (PAX DOOR) · airframe 59,965 hrs · 25,966 cycles

OUT OF ADJUSTMENT FINGER DOOR DAMPER PASSENGER DOOR. ADJUSTED IAW AMM.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON LEFT HAND AFT NOSE LANDING GEAR DOOR HINGE FITTING AT STRINGER 42L. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-A AND AMM 32-22-13-010-001-A.

Part: HINGE FITTING — WORN (LT SPOILER) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. WEAR ON LEFT HAND WING SPOILER 2 STOP BOLT OF SERVO CONTROL ATTACH FITTING BETWEEN RIB 10 AND 13. REPAIR ON CENTER HINGE FITTING ANTIROTATION WEB (STOP BOLT) PER SRM 57-70-00-300-003.

Part: FLOOR PANEL — DELAMINATED (FRAMES 59-63) · airframe 59,965 hrs · 25,966 cycles

DELAMINATION ON THE AFT CARGO BAY FLOOR PANEL 161NF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT COVER SHEET AT STRINGER 40R, BETWEEN FR 55A AND FR 59. REPLACED COVER SHEET ASSEMBLY PER SRM 51-72-11 AND DWG D53477000.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON RIGHT HAND AFT GALLEY FRAME 66 IN LOWER INBOARD HOLE DOOR STOP FITTING. REPAIRED LOWER FRAME 66 PER SRM 53-41-12-300-009.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT -Y1162 BETWEEN FRAMES 68 AND 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11 AND DRAWING D53472780.

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON RIGHT SIDE AFT GALLEY LOWER SUPPORT AT STRINGER 23R AND FRAME 66. REPAIRED THE SUPPORT IAW SRM 53-41-14-300-001.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION ON FORWARD GALLEY SEAT TRACK AT -Y765 BETWEEN FRAME 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-42-11, 51-72-11 AND DRAWINGS 53112812, D53918123.

Part: FLOOR PANEL — DELAMINATED (FRAMES 64-66) · airframe 59,965 hrs · 25,966 cycles

DELAMINATION ON AFT GALLEY FLOOR PANEL 261AG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND IRM REVISION G.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 59,965 hrs · 25,966 cycles

CORROSION AFT GALLEY FLOOR SUPPORT AT -Y765 BETWEEN FRAMES 66 AND 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, DRAWINGS D53472816 AND D53472780.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261DF. REPLACED FLOOR PANEL PER EA 273080, SRM 53-02-00 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 64-66) · airframe 59,965 hrs · 25,966 cycles

DELAMINATION ON THE AFT GALLEY FLOOR PANEL 261BG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 12-16) · airframe 59,965 hrs · 25,966 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222CF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701 REVISION G.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 59,965 hrs · 25,966 cycles

WATER TRAPPED INDICATION ON LEFT ELEVATOR UPPER SKIN BETWEEN 26 INCHES TO 91 INCHES OTBD FROM RIB 5 AND 3.1 INCHES TO 3.5 INCHES FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-11-300-05.

Part: HINGE ARM — WORN (RUDDER) · airframe 59,965 hrs · 25,966 cycles

EXCESSIVE PLAY ON RUDDER HINGE ARM NR 2 BEARING ON VERTICAL STABILIZER. REPLACED HINGE ARM IAW AMM 55-36-41.

Part: HINGE ARM — WORN (VERTICAL STAB) · airframe 59,965 hrs · 25,966 cycles

EXCESSIVE PLAY ON RUDDER HINGE ARM NR 4 BEARING ON VERTICAL STABILIZER. REPLACED HINGE ARM IAW AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 59,965 hrs · 25,966 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RUDDER HINGE ARM NR 7 BEARING. REPLACED HINGE ARM FITTING ASSEMBLY (FORKED END) PER AMM 55-36-41-400-001-A.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 59,694 hrs · 25,774 cycles

SEAT 10L EMERGENCY EXIT LIGHT COVER ON LOWER SEAT LOOSE. SECURED LOOSE FASTENERS ON LIGHT COVER AT SEAT 10L.

Part: ACTUATOR — FAULTY (NLG DOORS) · airframe 59,448 hrs · 25,657 cycles

AFTER TAKEOFF AND GEAR UP, NOSE GEAR DOORS DID NOT CLOSE. AFTER 3 MINS THE NOSE GEAR DOORS CLOSED, OPS OK. REPLACED NLG DOOR ACTUATOR.

Part: UPLOCK — FAULTED (NLG) · airframe 59,429 hrs · 25,643 cycles

AFTER TAKEOFF, RECEIVED A LANDING GEAR DOORS NOT CLOSED ON ECAM. PERFORMED ECAM PROCEDURE, DOOR INDICATED CLOSED AFTER GEAR CYCLED. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY IAW AMM 32-31-14. ACCOMPLISHED SATISFACTORY OPS CHECK IAW AMM 32-31-00. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,394 hrs · 25,127 cycles

MISSING EXIT LENS AT THE L2 DOOR. REPLACED LENS AND ACCOMPLISHED SATISFACTORY OPS CHECK.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 58,378 hrs · 25,120 cycles

AIRCRAFT WAS NOT GROUNDED. DELAMINATED AFT CARGO ENTRY PANEL 151ZG. REPAIRED FLOOR PANEL AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,891 hrs · 24,883 cycles

L1 DOOR EXIT SIGN BROKEN. INSTALLED NEW LENS COVER.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 57,531 hrs · 24,680 cycles

FORWARD LAVATORY SMOKE DETECTOR WENT OFF DUING TAKE OFF & WOULD NOT TURN OFF. NO ECAM & CHIME BEFORE THE STEADY ALARM AND DID NOT TURN OFF UNTIL LANDING. LAVATORY SMOKE DETECTORS OPERATIONAL CHECKED GOOD IAW AMM 26-17-00-710-001-A.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,352 hrs · 24,559 cycles

RIGHT WING OTBD FLAP, INBD T/E WEDGE OTBD CORNER DELAMINATED AND SEPARATED. REPLACED RT WING OTBD FLAP INBD T/E WEDGE IAW EA 263463.

Part: APU — LEAKING (ENGINE) · airframe 57,170 hrs · 24,436 cycles

THE FLIGHT CREW REPORTED A DIRTY SOCK ODOR WHILE THE AIRCRAFT WAS AT THE GATE DURING THE BOARDING PROCESS. THE ODOR STARTED IN THE COCKPIT AND WORKED IT'S WAY TO THE BACK OF THE AIRCRAFT. MAINTENANCE FOUND AN OIL LEAK IN THE APU COMPARTMENT, REPAIRED THE LEAK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH BOTH ENGINES AND THE APU RUNNING WITH NO ODORS BEING NOTED. CABIN CREW AGAIN DETECTED AN ODOR, DESCENDING THROUGH 10,000 ON ARRIVAL. MAINTENANCE SUSPECT THE APU IS LEAKING OIL FROM THE TURBINE SHAFT.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 24,001 hrs · 56,357 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM UPPER FLANGE, NR 3 FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 24,001 hrs · 56,357 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM UPPER FLANGE, NR 3 & 4 FASTENER HOLES HAVE CRACK INDICATION AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,102 hrs · 23,438 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED POWER SUPPLY UNIT 12WL. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BATTERY PACK — FAULTY (CABIN)

FOUND EPSU FWD LT BATTERY FAULTED. REPLACED FWD LT EPSU BATTERY PACK IAW AMM 33-51-38. OPERATIONS TESTED SATISFACTORY.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 53,042 hrs · 22,302 cycles

L2 DOOR CTR SCUFF PLATE CORROSION ON SUPPORTING STRUCTURE. REPLACED L2 DOOR SILL SHAPE IAW SRM 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,583 hrs · 22,077 cycles

FORWARD LT FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,093 hrs · 21,790 cycles

EMERGENCY EXIT LIGHT ABOVE R2 DOOR INOPERATIVE. REPLACED EMER LIGHT ASSEMBLY ABOVE R2 DOOR. OPERATIONS CHECKED NORMAL.

Part: OVEN — SMOKE (GALLEY) · airframe 52,040 hrs · 21,763 cycles

WHILE ENROUTE NR 1 OVEN FWD GALLEY ACFT LT BEGAN TO PRODUCE SMOKE DURING MEAL PREP OVEN WAS TURNED OFF & SMOKE STOPPED. NO INDICATION OR FLAME OBSERVED. SMOKE EVACUATED AS LIGHT. NO EXTINGUISHER USED. REPLACED NR 1 LT OVEN IAW AMM 25-35-19. OPERATIONS CHECKED GOOD IAW AMM 25-35-00-710-015-A.

Part: PIN — BENT (EMERGENCY LIGHT) · airframe 51,594 hrs · 21,485 cycles

THE EXIT SIGN ABOVE 2R DOOR INOPERATIVE. REMOVED COVER & FOUND PINS BENT, NOT MAKING CONTACT. REPOSITIONED PINS, OPERATIONS CHECKED GOOD IAW AMM 33-51-17.

Part: SKIN PANEL — DELAMINATED (RT ELEVATOR) · airframe 51,340 hrs · 21,310 cycles

C11 CHECK RT ELEVATOR SKIN IS DELAMINATED FROM 12 INCHES TO 20 INCHES FWD OF TE & 20 INCHES OTBD OF INBD EDGE. R & R ELEVATOR IAW AMM 27-34-41-400-001-A.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 51,340 hrs · 21,310 cycles

C11 SY6 CHECK DIS-BOND & AREA OF WATER EGRESS ON LT ELEVATOR UPPER SURFACE APPROX 18 INCHES TO 22 INCHES FROM INBD END & 14 INCHES TO 18 INCHES FROM TE. REPLACED LT ELEVATOR IAW AMM 27-34-41-400-001-A.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 51,340 hrs · 21,310 cycles

C11 CHECK UPPER COATING IS PEELING ON FLOOR PNL 261HG BETWEEN FRAME 64 TO 66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PNL 261HG IAW SRM 53-32-12.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 51,340 hrs · 21,310 cycles

C11 CHECK UPPER COATING IS PEELING ON FLOOR PNL 261CG BETWEEN FRAME 64 TO 66 & BETWEEN Y254 TO Y765. REPLACED FLOOR PNL 261CG IAW SRM 53-32-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,340 hrs · 21,310 cycles

C11 & SY6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 14 TO 16, BL0. REPLACED FLOORBEAM BETWEEN FRAME 14 TO 16, BL0 IAW SRM 51-72-11.

Part: COVER — UNSECURE (MEGAPHONE) · airframe 51,219 hrs · 21,248 cycles

THE FWD ENTRY WAY MEGA PHONE COVER FELL OFF. ATTACHED FWD MEGA PHONE COVER AS REQUIRED, CHECKED OK.

Part: LENS — MISSING (CABIN) · airframe 51,034 hrs · 21,153 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 1C. REPLACED EMERGENCY LIGHT LENS AT SEAT 1C.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 50,750 hrs · 21,016 cycles

MOD LINE FWD CARGO FLOOR PANEL 131CG HAS EDGE LIFTING UP BETWEEN FRAME 28 TO FRAME 34 & BETWEEN STRINGER 38L TO STRINGER 38R, BL0. REPLACED FWD CARGO FLOOR PANEL 131CG IAW AMM 53-22-14, PB 401.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 50,750 hrs · 21,016 cycles

MOD LINE FWD CARGO FLOOR PANEL 131AF HAS METAL FACE LIFTING UP AT CARGO NET FLOOR FITTING BETWEEN FRAME 24 TO FRAME 28 & BETWEEN STRINGER 38L TO STRINGER 38R, BL0. REPLACED FWD CARGO FLOOR PANEL 131AF IAW AMM 53-22-14, PB 401.

Part: ACTUATOR — FAULTY (NLG) · airframe 50,417 hrs · 20,876 cycles

AFTER TAKEOFF FROM RNO, CREW REPORTED A NOSE GEAR DOOR UNLOCK & LG SYS DISAGREE AFTER LANDING PHX. CYCLE GEAR AFTER TAKEOFF FROM RNO, SYSTEM NORMAL. REPLACED NLG UP LOCK ACTUATOR IAW JOB CARD 26L70032005. OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 50,032 hrs · 20,723 cycles

WIRE BROKEN AT EMERGENCY SEAT LIGHT 8L. REPAIRED BROKEN WIRE, OPERATIONS CHECKED GOOD.

Part: HYDRAULIC LINE — CHAFED (THRUST REVERSER) · airframe 49,980 hrs · 20,696 cycles

EN ROUTE FROM PHX TO DTW, CREW REPORTED HYD GREEN RESERVOIR LOW LEVEL. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. R & R A CHAFED GREEN SYS HYD LINE TO THRUST REVERSER ISOLATION VLV FILTER IAW AMM 78-37-51. OPERATIONS & LEAK CHECKED NORMAL. COMPLIED WITH TASK 29-00-00-280-006-A01, CHECK OF GREEN HYD SYS & TASK 32-00-00-860-003-A, OPERATIONS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,692 hrs · 20,584 cycles

EN ROUTE FROM CLT TO TPA, CREW REPORTED A DIRTY SOCK SMELL IN CABIN DURING DESCENT. FLIGHT ATTENDANTS WERE NAUSEOUS. AFTER LANDING,. ACCOMPLISHED JOB CARD 26L00021001. NO ISSUES WERE FOUND AT THIS TIME, ACFT OK FOR SERVICE.

Part: COVER — UNSECURE (CABIN) · airframe 46,759 hrs · 19,285 cycles

CREW REPORTED THE EXIT PLACARD AT LEFT OVERWING FELL OFF. MAINTENANCE INSTALLED LEFT OVERWING EMERGENCY LENS COVER.

Part: CONTROL SERVO — FAULTY (AILERON) · airframe 45,537 hrs · 18,732 cycles

IN CRUISE, AILERON SERVO FAULT/ ELAC 1 PITCH FAULT AND AIRCRAFT ROLLED 5 DEGREES RIGHT PLUS SLIGHT PITCH UP. FLIGHT CONTROL SHOWS RIGHT AILERON GREEN SYSTEM IN AMBER. REMOVED AND REPLACED RIGHT GREEN AILERON SERVO CONTROL ACTUATOR PER AMM 27-14-51-400-001-A. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 45,031 hrs · 18,493 cycles

FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IN FORWARD EMERGENCY FLASHLIGHT.

Part: SELECTOR VALVE — LEAKING (CARGO DOOR) · airframe 44,271 hrs · 18,159 cycles

EXTREME BAD ODOR IN CABIN &COCKPIT. SEE CABIN AIR QUALITY REPORT. FOUND FORWARD CARGO SELECTOR LEVEL DRIPPING HYDRAULIC FLUID. REMOVED AND REPLACED FORWARD CARGO MANUAL SELECTOR VALVE IAW AMM 52-36-15. OPS CHECKED GOOD AND NO LEAKS NOTED.

Part: WINDOW — ARCED (COCKPIT) · airframe 43,724 hrs · 17,905 cycles

CAPTAIN'S WINDSHIELD ARCING. REMOVED AND REPLACED NR 1 WINDOW HEAT COMPUTER PER COMPANY CONVENIENCE AS PRECAUTION.

Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 43,658 hrs · 17,871 cycles

FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT SEAL BROKEN. REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT.

Part: LENS — BROKEN (CABIN) · airframe 43,431 hrs · 17,764 cycles

SEAT 1C ESCAPE LIGHT BROKEN. REPLACED EMERGENCY LIGHT LENS AT SEAT 1C IAW AIRBUS MAINTENANCE MANUAL 33-51-00.

Part: WIRE — DAMAGED (CABIN) · airframe 42,770 hrs · 17,462 cycles

WIRING EXPOSED UNDER SEAT 4B THAT POWERS AISLE EMERGENCY LIGHT AND LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRES IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-53-50.

Part: LENS — MISSING (CABIN) · airframe 42,598 hrs · 17,378 cycles

EMERGENCY LIGHT LENS COVER MISSING ON ROW 8 LEFT. INSTALLED LENS COVER ON ROW 8 LEFT.

Part: WIRE — BROKEN (CABIN) · airframe 41,432 hrs · 16,848 cycles

FLT 149 - ANC-PHX - EMERGENCY LIGHTS - EMERGENCY PATH LIGHT AT ROW 20 LEFT INOPERATIVE. FOUND BROKEN WIRE, REPAIRED EMERGENCY LIGHT WIRE IAW ESPM 20-43-11. OPERATIONAL CHECK WAS GOOD.

Part: SWITCH — FAULTY (CABIN) · airframe 41,384 hrs · 16,824 cycles

FLT 9205 - OAK-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHTS STAY ON WITH EMERGENCY EXIT LOWER SWITCH IN ARMED. REMOVED AND REPLACED TOGGLE SWITCH 4WL IN LIGHTING PANEL 25VU. OPERATIONAL CHECK WAS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,905 hrs · 16,623 cycles

BFM - S4 - CORROSION ON MAIN CABIN SEAT TRACK AT FR66, Y765. REPLACED MAIN CABIN SEAT TRACK AT FR66, Y765 IAW A319 SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 40,905 hrs · 16,623 cycles

BFM - S4 - CORROSION ON MAIN CABIN FLOOR DUMMY RAIL AT FR16 BETWEEN Y254 TO Y765. REPLACED MAIN CABIN FLOOR DUMMY RAIL AT FR16 BETWEEN Y254 TO Y765 IAW A319 SRM 51-42-11.

Part: WIRE — BROKEN (CABIN) · airframe 40,547 hrs · 16,447 cycles

FLT 338 - PHX-SJD - EMERGENCY LIGHTS - LEFT ROW 4 HAS A BROKEN WIRE AT EMERGENCY LIGHT CONNECTOR. REPLACED SEAT 4L EMERGENCY LIGHT CABLE. SYSTEM OPS CHECK GOOD PER AMM 33-51-19.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 36,047 hrs · 14,441 cycles

LOGPAGE:8558629 - FLT 321 - LAS-ORD - EMERGENCY LIGHTS - FLOOR LEVEL RED EMERGENCY LIGHT AT ROW 8 LEFTHAND SIDE INOPERATIVE. FOUND WIRE BROKEN FROM CONNECTOR UNDER SEAT ASSEMBLY. COMPLIED WITH TEMPORARY REPAIR TO EMERGENCY LIGHT BROKEN WIRE. REINSPECTION WEEKLY AND FINAL REPAIR NO LATER THAN AUGUST 3, 2009. REPLACED WIRE HARNESS ROW 8 LEFTHAND EMERGENCY EXIT PATH LIGHTS, CONNECTOR 7261VC1 TO AISLE LIGHT PER SWPM.

Part: WIRE — BROKEN (CABIN) · airframe 36,047 hrs · 14,441 cycles

FLT 321 - LAS - ORD - EMERGENCY LIGHTS - FLOOR LEVEL RED EMERGENCY LIGHT AT ROW 8 LEFT SIDE INOPERATIVE. FOUND WIRE BROKEN FROM CONNECTOR UNDER SEAT ASSEMBLY. COMPLIED WITH TEMPORARY REPAIR TO EMERGENCY LIGHT BROKEN WIRE. REINSPECTION WEEKLY AND FINAL REPAIR NO LATER THAN AUGUST 3, 2009. ***SUPPLEMENTAL*** WILL SUBMIT FINAL REPAIR INFORMATION UPON RECEIPT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,019 hrs · 13,486 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM AT FR 65 AND FR 66, -Y480. REPLACED FLOORBEAM AT FR 64 AND FR 67, BETWEEN -Y465 AND -Y480 IAW A319 SRM 51-72-11.

Part: HINGE PIN — CRACKED (NLG) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - MAJOR REPAIR - DURING PENETRANT INSPECTION, NOSE LANDING GEAR CENTER HINGE PIN WAS FOUND CRACKED. REPLACED NOSE LANDING GEAR CENTER HINGE PIN IAW A319 AMM 32-21-27.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 34,019 hrs · 13,486 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SHEAR PLATE AT FR 69 AND FR 70, -Y1732, S23R - S24R. REPLACED SHEAR PLATE AT FR 69 AND FR 70, -Y1732, S23R - S24R IAW A319 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON CENTER FITTING OF LOWER SILL AT FR66 TO FR68, S23R. REPLACED CENTER FITTING OF LOWER SILL AT FR67 +15, S23R IAW A319 SRM 57-72-11.

Part: DUMMY RAIL — CORRODED (ZONE 100) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - CORROSION ON DUMMY RAIL AT FR16, Y503. REPAIRED DUMMY RAIL AT FR16, Y503 IAW A319 SRM 51-74-00 AND 53-11-14.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - CORROSION ON WEB SUPPORT FRAME AT FR 64 TO FR 70, S23R TO S24R. REPAIRED WEB SUPPORT FRAME AT FR 64 TO FR 70, S23R TO S24R IAW A319 SRM 51-72-11.

Part: PLATE — CRACKED (ZONE 200) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - MAJOR REPAIR - CRACK ON COVER PLATE BETWEEN FR 68 TO FR 69, S23R. REPLACED COVER PLATE BETWEEN FR 68 TO FR 69, S23R IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR 68, -Y1292. REPLACED FLOORBEAM AT FR 68, -Y1292 IAW SRM 51-72-11.

Part: WEB — CORRODED (ZONE 200) · airframe 34,019 hrs · 13,486 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SHEAR PLATE WEB AT FR 69 - FR 70, +Y1732. REPLACED SHEAR PLATE WEB AT FR 69 - FR 70, +Y1732 IAW SRM 51-72-11.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 34,019 hrs · 13,486 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ALONG PLATE STIFFENER ASSEMBLY AT FR12 +6, -Y1292. REPLACED PLATE STIFFENER ASSEMBLY AT FR12 +6, -Y1292 IAW A319 SRM 51-72-11.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 33,505 hrs · 13,254 cycles

FLT 472 YYC PHX EEL FORWARD CABIN FLASHLIGHT NOT CHARGING. INSTALLED NEW BATTERY PACK. ALSO INSTALLED NEW SAFETY STRIP. OPS CHECK WAS GOOD.

Part: ACTUATOR — FAILED (NR 1 ENGINE)

ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE ACC ACTUATOR. OPERATIONALLY CHECKS OK.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE)

ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE SEVENTH STAGE, LOWER RIGHT (7B), BLEED VALVE. OPERATIONALLY CHECKS OK.

Part: SOLENOID — FAULTY (NR 1 ENGINE)

ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE SOLENOID 7B. OPERATIONALLY CHECKS OK.

Part: SLIDE — FAILED (R1 DOOR) · airframe 29,198 hrs · 11,431 cycles

MCN - EES - BC-6 CHECK - LOG PAGE # 7739211 AND NR # 5980808, THE R1 DOOR SLIDE WAS DEPLOYED AND THE SLIDE FAILED TO INFLATE. REPLACED THE R1 DOOR SLIDE IAW AWA TASK CARD R1C25305.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,198 hrs · 11,431 cycles

MCN - EEL - BC-6 CHECK - NR# 5980805, EMERGENCY RIGHT MID CABIN POWER SUPPLY UNIT INDICATES UNIT FAILURE DURING TEST. CHARGED AND OPERATIONAL CHECKED THE EMERGENCY RIGHT MID CABIN EMERGENCY BATTERY IAW A319 AMM, 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (FLASHLIGHT) · airframe 29,198 hrs · 11,431 cycles

MCN - EEL - BC-06 CHECK - NR# 5941740, THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT POWER UNIT.

Part: FLASHLIGHT — DISCHARGED (CABIN) · airframe 29,198 hrs · 11,431 cycles

MCN - EEL - BC-06 CHECK - NR# 5981399, LEFT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE LEFT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 29,198 hrs · 11,431 cycles

EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS DAMAGED AT SEAT ROWS 4L, 10L, 12L AND 22L. REPLACED AND OPERATIONAL CHECKED THE EMERGENCY ESCAPE PATH LIGHTING HARNESS DAMAGED AT SEAT ROWS 4L, 10L, 12L AND 22L IAW A319 AMM 33-51-19.

Part: SILL — CORRODED (ZONE 200) · airframe 29,198 hrs · 11,431 cycles

MCN - MAJOR REPAIR - BC-06 CHECK - NR 5980887, CORROSION ON THE R2 DOOR CUT OUT SHAPE SILL, BS 2880 - BS 2884, RBL 1732, WL 240. REPAIRED THE R2 DOOR CUT OUT SHAPE SILL, BS 2880 - BS 2884, RBL 1732, WL 240 IAW A319 SRM 53-41-14.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 27,948 hrs · 10,931 cycles

PHX - EEL - FOUND EMERGENCY EXIT" PUSH BUTTON" TEST FAULTING "EPSU UNIT EMER R ". MX REMOVED AND REPLACED THE BATTERY IAW 33-51-38. OPERATIONAL CHECK WAS GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,739 hrs · 10,835 cycles

PHX - CORROSION ON MAIN CABIN SEAT TRACK, FS 16, +Y765, AT THE FORWARD GALLEY ATTACH POINT. REPAIRED MAIN CABIN SEAT TRACK, FR 16, +Y765, AT THE FORWARD GALLEY ATTACH POINT IAW A319 SRM 53-11-15 FIGURE 202.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,173 hrs · 9,275 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 8L EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED BROKEN WIRE. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 21,087 hrs · 8,101 cycles

DEN - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE LEADING TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD.

Part: FLASHLIGHT — DISCHARGED (ZONE 900) · airframe 18,446 hrs · 7,168 cycles

FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED DUMMY RAIL Y503 LEFT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765 LT BETWEEN AT FR 16. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PART IAW A319 SRM 53-11-15 FIG 202.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LEFT AT FR 17. MAINTENANCE CUT OUT CORRODED SECTION OF FLOOR SUPPORT Y254 LEFT AT FR 17; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14 FIG 201.

Part: BEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RIGHT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RIGHT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y1292 RIGHT BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y1292 RIGHT FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LEFT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LEFT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 8 - 12 & 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT FROM FR 67 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,219 hrs · 7,101 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53472209245; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8.

Part: PROBE — FAILED (ZONE 120) · airframe 14,484 hrs · 5,788 cycles

ON TAKEOFF AT PHX EN ROUTE FOR EWR RECEIVED ECAM MESSAGE FOR CAPTAINS PITOT PROBE FAILURE. DUE TO ICING CONDITIONS AT EWR TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED PITOT PROBE (9DA1), OPERATIONAL TEST WAS GOOD PER AMM 34-11-15. VENDOR CONFIRMED FAILURE OF PITOT PROBE S/N 7385, UNIT BEYOND ECONOMICAL REPAIR, SCRAPPED AT VENDOR.

Part: CABLE — BROKEN (SEAT ROW 14 L/H) · corrosion level 0 · airframe 13,065 hrs · 5,228 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 L/H, OPERATIONAL CHECK WAS GOOD.

Part: CABLE — BROKEN (SEAT ROW 12 L/H) · corrosion level 0 · airframe 8,904 hrs · 3,649 cycles

CMH - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES ON ESCAPE PATH LIGHT AT SEAT ROW 12 L/H; SPLICED BROKEN WIRES; OPERATIONAL CHECK WAS GOOD.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 10,930 hrs · 4,452 cycles

EWR - ABORTED TAKEOFF - FLT 0688 - DURING TAKEOFF ROLL AT EWR EN ROUTE PHX ECAM INDICATED A VENT SKIN VALVE FAULT, WITH ASSOCIATED AVIONICS SYSTEM FAULT. REJECTED TAKEOFF AT 70 KTS. MAINTENANCE PERFORMED PROCEDURES FOR MEL 21-26-04, COND 1, EXTRACT VALVE INOPERATIVE. PARTS ORDERED. VENDOR BENCH TEST OF SKIN AIR VALVE WAS NO FAULT FOUND, UNIT WAS FUNCTIONAL TESTED AND RETURNED TO SERVICE.

Part: VALVE — FAILED (ZONE 126) · airframe 10,560 hrs · 4,311 cycles

DEN - AIR TURN BACK - FLT 0543 - AFTER TAKEOFF FROM DEN EN ROUTE TO LAS RECEIVED ECAM MESSAGE FOR "VENT SKIN VALVE FAULT" ACCOMPLISHED ECAM ACTIONS AND RETURNED TO DEN. MAINTENANCE PLACED VENT SKIN AIR VALVE ON MEL 21-26-04 COND. 1, EXTRACT VALVE INOPERATIVE. ON 07/06/2002 IN PHX MAINTENANCE REMOVED AND REPLACED THE VENT SKIN AIR VALVE (22HG) IAW AMM 21-26-53-401, OPERATIONAL CHECK WAS GOOD AND THE MEL PLACARD WAS REMOVED. **SUPP** VENDOR BENCH TEST OF SKIN AIR VALVE S/N 2125 COULD NOT CONFIRM FAILURE (NO FAULT FOUND), UNIT RETURNED TO SERVICE.

Part: SKIN — PUNCTURED · airframe 9,072 hrs · 3,715 cycles

TUS - GROUND DAMAGE - "C" - WHILE POSITIONING AIR-STAIR TRUCK TO R1 DOOR THE TRUCK STRUCK THE FUSELAGE PUNCTURING THE SKIN BELOW THE R1 DOOR 6" FWD OF FR 20, AND 4" BELOW STR 29. MAINTENANCE PERFORMED TEMPORARY REPAIR ER 25-5331-02033-ES1 AND AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX. IN PHX MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN FABRICATED A DOUBLER, FILLER, AND SHIM, AND INSTALLED REPAIR IAW SRM 53-00-11 FIG. 209.

Part: O-RING — LEAKING (NR 2 ENGINE) · airframe 3,275 hrs · 1,334 cycles

EMERGENCY DECLARED, ECAM SHOWS YELLOW HYDRAULIC SYS LOW LEVEL. FOUND NR 2 ENGINE HYD PRESS SWITCH LEAKING. REMOVED AND REPLACED PRESSURE SWITCH O-RING. LEAK AND OPS CK GOOD, RESERVICED 3 GAL SKYDROL.

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT 10 DEF INOP. REPAIRED WIRING OPS CK GOOD.