N820AW

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 73,083 hrs · 34,417 cycles

AIRCRAFT WAS NOT GROUNDED: FA FWD JUMPSEAT FLASHLIGHT NOT BLINKING AND TAMPER SEAL BROKEN. MAINTENANCE REPLACED FA FWD JUMPSEAT FLASHLIGHT AND TAMPER SEAL REF AMM 25-22-00.

Part: FIRST AID KIT — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH IAW EA 362868.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.190 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE RH IAW EA 362868.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE RH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE RH IAW EA 362868.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA 27 INTERNAL SIDE LH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH IAW EA 362868.

Part: FRAME — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN RADIUS OF AFT UPPER CORNER BTW STR 8 AND STR 9 LH SIDE FROM FR68 WEB DOOR FRAME. CRACK LENGTH 0.563 INCH. MAINTENANCE PERFORMED INTERIM REPAIR INSTRUCTIONS ON RADIUS OF AFT UPPER CORNER BTW STR8 AND STR9 LH SIDE FROM FR68 WEB DOOR FRAME IAW EA 363510 AND A319 SRM 53-41-12-300-012.

Part: FRAME — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN RADIUS OF AFT UPPER CORNER BTW STR 8 AND STR 9 LH SIDE FROM FR68 WEB DOOR FRAME. CRACK LENGTH 0.563 INCH. MAINTENANCE PERFORMED INTERIM REPAIR INSTRUCTIONS ON RADIUS OF AFT UPPER CORNER BTW STR8 AND STR9 LH SIDE FROM FR68 WEB DOOR FRAME IAW EA 363510 AND A319 SRM 53-41-12-300-012.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA. MAINTENANCE REPLACED SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-72-11-911-001 AND DWG D53474180.

Part: ATTACH FITTING — CRACKED (ZONE 700) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FWD ATTACHMENT HINGE FITTINGS AFT LUG POSITION ON LH MAIN LANDING GEAR, CRACK LENGTH IS: 0.200 INCH APPROX. MAINTENANCE REPLACED FWD ATTACHMENT HINGE FITTING AFT LUG POSITION ON LH MAIN LANDING GEAR DOOR AND CONNECTING PLATE AND FASTENER IAW. A319 SRM 51-42-11-801 AND EA 363624 AND DWG R53370500 ISSUE F, D53370622, D53370600.

Part: HINGE FITTING — CRACKED (ZONE 700) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FWD ATTACHMENT AFT LUG POSITION ON RH MAIN LANDING GEAR, CRACK LENGTH IS: 0.250 INCH APROX. MAINTENANCE REPLACED FWD ATTACH FITTING AFT LUG POSITION ON RH MAIN LANDING GEAR DOOR AND CONNECTING PLATE AND FASTENERS IAW A319 SRM 51-42-11-801 AND EA 363625 AND DWG R53370500 ISSUE F, D53370622, D53370600.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON THE UPPER CORNER FROM HOLE LOCATED AT FR 68 AND BELOW S-8L. MAINTNANCE REPLACED UPPER CORNER LOCATED AT FR68 LH AT LEVEL STR 8L IAW A319 SRM 51-42-11-801 AND DWG D53480505.

Part: FRAME — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK UPPER CORNER FRAME 68 RH SIDE AT AFT GALLEY AREA. LENGTH 0.200 INCHES. MAINTENANCE REPLACED UPPER CONER LOCATED FRAME 68 RH SIDE AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-011 AND DWG D53480505.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION STR 31 RH SIDE AT LEVEL FR65 ON AFT BULK CARGO COMPARTMENT. MEASURES OF CORROSION IS: L= 3.591 IN, W= 0.871 IN. MAINTENANCE REPLACED SECTION STRINGER LOCATED STR 31R FR64 TO FR67 ON AFT BULK CARGO COMPARTMENT IAW A319 SRM 51-72-11-911-001 AND DWG D53480030, D53480505, D53476160.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL FR 66 AT LEVEL STR 23R AT AFT GALLEY AREA. MAINTENANCE REPLACED LOWER SILL LOC BTW FR66 TO FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, DWG D53474250 AND DWG D53480019.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. MAINTENANCE REPLACED SERVICEABLE LOWER SPIGOT FITTING RECEPTACLE ON LH PYLON IAW A319 SRM 54-51-12-300-002.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER P/NON: FE240-006 S/N ON: RFM29378 IN PASSENGER CREW DOOR 832 AT AFTGALLEY AREA I.A.WAMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B REFER TO INDIVIDUAL SING OFFENTRIES FOR WORK STEPS PERFORMED, FORM ME-0470 COMPLETE.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR 66 LEVEL STR23R AT AFT GALLEY AREA. MAINTENANCE REPLACED INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL 23R AT AFT GALLEY AREA IAW A319 SRM 51-72-11-801 AND DWG D53474250.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED AT LEVEL STR23L FR66 AT AFT GALLEY AREA. ,MEASURE OF CRACK IS: L=0.250 INCH. MAINTENANCE REPLACED INTERNAL STRUCTURE SECTION CONNECTION LOCATED AT LEVEL STR23L FR66 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53474250.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 4 ON RH HORIZONTALSTABILIZER (1EA). MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 6 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 1 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 3 ON RH HORIZONTALSTABILIZER (1EA). MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.

Part: PLATE — CRACKED (ZONE 800) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 HATCH CONTROL HANDLE PLATE CRACKED. REPLACED CONTROL HANDLE PLATE PER AMM 52-21-11.

Part: PLATE — CRACKED (ZONE 800) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844 HATCH CONTROL HANDLE PLATE CRACKED. REPLACED CONTROL HANDLE PLATE PER AMM 52-21-11.

Part: HINGE FITTING — INOPERATIVE (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 3 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 1 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 END FITTING ON LH HORIZONTAL STABILIZER). MAINTENANCE REPLACED ELEVATOR HINGE ARM 5 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 4 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 72,971 hrs · 34,348 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 END FITTING ON LH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 6 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 71,862 hrs · 33,596 cycles

AIRCRAFT WAS NOT GROUNDED: FWD FA JUMP SEAT FLASHLIGHT'S RED LIGHT NOT BLINKING. REPLACED BATTERY FWD F/A FLASHLIGHT. SECURED AND OPS NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 71,798 hrs · 33,547 cycles

AIRCRAFT WAS GROUNDED: 2L DOOR EXIT SIGN PLACARD DOES NOT LIGHT UP. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY AT L2 DOOR AND WALL MOUNT ASSEMBLY AT RH SIDE OVERWING EXIT AS REQUIRED.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 71,634 hrs · 33,428 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND EMERERGENCY SYSTEM EMERGENCY POWER SUPPLY UNIT ON THE FORWARD LEFT WITH A FAULT 33-51-38 WHILE PREPARING FOR OVER-WING SLIDE REPLACEMENT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: OVEN — ODOR (ZONE 900) · airframe 71,491 hrs · 33,327 cycles

AIRCRAFT WAS NOT GROUNDED: OVEN IN FIRST CLASS GALLEY HAS FOUL ODOR WHEN USED AS FOOD WAS LEFT IN IT WHILE AIRCRAFT WAS DOWN FOR MAINTENANCE AND HAD SPOILED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: OVEN — ODOR (ZONE 900) · airframe 71,491 hrs · 33,327 cycles

AIRCRAFT WAS NOT GROUNDED: OVEN IN FIRST CLASS GALLEY HAS FOUL ODOR WHEN USED AS FOOD WAS LEFT IN IT WHILE AIRCRAFT WAS DOWN FOR MAINTENANCE AND HAD SPOILED. **SUPPLEMENTAL REPORT FOR AALA202407292686: MAINTENANCE CLEANED OVEN IN FIRST CLASS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-33-00 ** (CLEANED)

Part: HYDRAULIC LINE — RUPTURED (ZONE 400) · airframe 71,479 hrs · 33,320 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THE LOSS OF THE GREEN HYDRAUILIC SYSTEM QUANTITY SHORTLY AFTER DEPARTURE. THE AIRCRAFT LANDED SAFELY AT PHL WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202407151665: MAINTENANCE FOUND A RUPTURED HYDRAULIC LINE IN THE LEFT PYLON AND REPLACED IT. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: HYDRAULIC SYSTEM — FAILED (GREEN SYS) · airframe 71,479 hrs · 33,320 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THE LOSS OF THE GREEN HYDRAUILIC SYSTEM QUANTITY SHORTLY AFTER DEPARTURE. THE AIRCRAFT LANDED SAFELY AT PHL WITHOUT FURTHER INCIDENT. (OPEN)

Part: RESERVOIR — OVERSERVICED (YELLOW HYD SYS) · airframe 71,161 hrs · 33,098 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE THE FLIGHT CREW REPORTING A YELLOW HYDRAULIC RESERVOIR LOW LEVEL MESSAGE. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE YELLOW HYDRAULIC SYSTEM RESERVOIR WAS ACTUALLY OVERSERVICED AND DRAINED THE SYSTEM TO THE CORRECT LEVEL. A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO DEFECTS NOTED.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 70,984 hrs · 32,982 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR EMERGENCY CYLINDER LOW PRESSURE, 950 PSI 73F. SERVICED L4 DOOR CYLINDER BOTTLE

Part: BULB — INOPERATIVE (OVERWING SIGN) · airframe 70,936 hrs · 32,955 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND OVERWING EXIT SIGN LIGHT NOT FULLY ILLUMINATED. REPLACED LIGHT BULB AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: DOOR — OUT OF ADJUST (AFT CARGO) · airframe 70,902 hrs · 32,926 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO RDU. FLIGHT CREW REPORTED A DOOR AFT CARGO ECAM MESSAGE AFTER TAKEOFF PASSING THROUGH 2000 FT. MESSAGE EXTINGUISHED AFTER LANDING WITH AC UN-PRESSURIZED. THE AIRCRAFT LANDED SAFELY AT RDU WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE AFT CARGO DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. ** (CLOSED)

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 70,780 hrs · 32,853 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING JOB CARD 26L000005005 (PS CHECK) CABIN EMERGENCY LIGHTS TEST FAILED. REMOVED AND REPLACED FWD EPSU (10WL) (AALA202404052728) AND BATTERY (AALA202404054733)

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 70,780 hrs · 32,853 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING JOB CARD 26L000005005 (PS CHECK) CABIN EMERGENCY LIGHTS TEST FAILED. REMOVED AND REPLACED FWD EPSU (10WL) (AALA202404052728) AND BATTERY (AALA202404054733)

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,302 hrs · 31,962 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT HAND ENTRY DOOR DAMPER AND EMERGENCY CYLINDER HAS LOW PRESSURE. SERVICED DAMPER AND EMERGENCY CYLINDER PER AMM 52-10-00.

Part: OVEN — ODOR (ZONE 900 - LAV/G) · airframe 67,495 hrs · 30,848 cycles

AIRCRAFT WAS GROUNDED: ONE HOUR INTO THE FLIGHT A SLIGHT ACRID SMELL IN FLIGHT DECK AT FL370. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE FORWARD GALLEY OVENS. REPLACED THE FORWARD GALLEY #1 OVEN (AALA202301201664) AND #2 OVEN (AALA202301208187) PER AMM 25-35-19. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: OVEN — ODOR (ZONE 900 - LAV/G) · airframe 67,495 hrs · 30,848 cycles

AIRCRAFT WAS GROUNDED: ONE HOUR INTO THE FLIGHT A SLIGHT ACRID SMELL IN FLIGHT DECK AT FL370. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE FORWARD GALLEY OVENS. REPLACED THE FORWARD GALLEY #1 OVEN (AALA202301201664) AND #2 OVEN (AALA202301208187) PER AMM 25-35-19. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 67,030 hrs · 30,588 cycles

AIRCRAFT WAS GROUNDED: LEFT OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED LEFT EMERGENCY OVERWING EXIT LIGHT, PER AMM 33-51-15.

Part: DISPLAY — FAILED (ZONE 200 - FUSE) · airframe 66,578 hrs · 30,313 cycles

AIRCRAFT WAS GROUNDED: CAPTAINS NAVIGATIONAL DISPLAY FLASHED ON OFF WITH DIAGONAL LINE THEN WENT BLANK SHORTLY AFTER A ELECTRICAL SMOKE SMELL WAS DETECTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IND WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**M (OPEN)

Part: DISPLAY — FAILED (ZONE 200 - FUSE) · airframe 66,578 hrs · 30,313 cycles

AIRCRAFT WAS GROUNDED: CAPTAINS NAVIGATIONAL DISPLAY FLASHED ON OFF WITH DIAGONAL LINE THEN WENT BLANK SHORTLY AFTER A ELECTRICAL SMOKE SMELL WAS DETECTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IND WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR : AALA202209168773: REPLACED NAVIGATIONAL DISPLAY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 31-63-22.** (CLOSED)

Part: CONTAINER — DEFECTIVE (ZONE 200 - FUSE) · airframe 66,370 hrs · 30,164 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE IDENTIFIED THAT EMERGENCY OXYGEN CONTAINER ABOVE L2 PASSENGER AND CREW DOOR REQUIRES REPLACEMENT BECAUSE IT DID NOT DEPLOY PROPERLY. (SEE AALA202208191997 FOR ASSOCIATED CABIN PRESSURIZATION LOSS EVENT) REPLACED EMERGENCY OXYGEN CONTAINER ABOVE L2 DOOR PER AMM 35-21-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR SEAL — LEAKING (ZONE 800 - DOORS) · airframe 66,370 hrs · 30,164 cycles

AIRCRAFT WAS GROUNDED: ABOUT 30 MINUTES FROM CLT WHICH WAS THE SCHEDULED ARRIVAL STATION, THE FLIGHT CREW REPORTED THAT THEY HAD LOST CABIN PRESSURIZATION ALONG WITH AN ECAM WARNING FOR CABIN HI PRESSURE ABOVE 10/0 AT FL 27/0. CREW PERFORMED ECAM ACTIONS AND DESCENDED TO 10, 000 FEET. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT CLT WITHOUT FURTHER INCIDENT. IT WAS REPORTED THAT THE OXYGEN MASK DID DEPLOY AND THAT ARFF MET THE FLIGHT WITH NO PASSENGER / CREW INJURIES REPORTED. MAINTENANCE ACCOMPLISHED A PRESSURIZATION CHECK AND FOUND THE FORWARD CARGO DOOR SEAL WAS INSTALLED BACKWARDS CAUSING EXCESSIVE LEAKAGE LEADING TO THE PRESSURIZATION FAULTS. THE FORWARD CARGO DOOR SEAL WAS REPLACED PER AMM 52-31-18. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.

Part: CONTROL CABLE — BINDING (ZONE 800 - DOORS) · airframe 66,365 hrs · 30,158 cycles

AIRCRAFT WAS GROUNDED: DOOR 1R DIFFICULT TO MOVE ARM LEVER TO ARM AND DISARM. MAINTENANCE FOUND THE ARM / DISARM FLEXIBLE CONTROL CABLE BINDING AND REPLACED IT PER AMM 52-11-22. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BUSHING — OUT OF TOLERANCE (ZONE 300 - STABS) · airframe 80,310 hrs · 10,264 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 6 ELEVATOR HINGE FITTING INBOARD BUSHING OUT OF LIMITS. **SUPPLEMENTAL REPORT FOR AALA202208052614: INSTALLED REPAIRED BUSHING PER EA 500537A.** (CLOSED)**

Part: FITTING — WORN · airframe 80,310 hrs · 10,264 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 6 ELEVATOR HINGE FITTING INBOARD BUSHING OUT OF LIMITS. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 66,363 hrs · 30,155 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 6 ELEVATOR HINGE FITTING BEARING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — CORRODED (ZONE 300 - STABS) · airframe 66,363 hrs · 30,155 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR NUMBER 4 HINGE FITTING HAS CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR NUMBER 4 HINGE FITTING PER A319 AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 66,363 hrs · 30,155 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 3 ELEVATOR HINGE FITTING BEARING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 66,363 hrs · 30,155 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER # 5 ELEVATOR HINGE FITTING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 65,650 hrs · 29,720 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT STATION #2 INOPERATIVE. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.

Part: TRUNNION — WORN (ZONE 500 - LH WI) · airframe 65,581 hrs · 29,688 cycles

AIRCRAFT WAS GROUNDED: LEFT WING FLAP TRUNNION FITTING HAS WEAR DAMAGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: TRUNNION — WORN (ZONE 500 - LH WI) · airframe 65,581 hrs · 29,688 cycles

AIRCRAFT WAS GROUNDED: LEFT WING FLAP TRUNNION FITTING HAS WEAR DAMAGE. **SUPPLEMENTAL REPORT FOR AALA202203315128: REPLACED LEFT HAND #1 FLAP TRACK TRUNNION PER TASK CARD 26L00027003** (CLOSED)

Part: ACTUATOR — FAULTY (ZONE 300 - STABS) · airframe 65,338 hrs · 29,560 cycles

AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF AT APPROXIMATELY 70 KNOTS DUE ECAM ENGINE #2 ECAM COMPRESSOR VANE FAULT. REPLACED ENGINE #2 VSV ACTUATOR PER JOB CARD 26T40075005. NO LEAKS NOTED. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BULB — INOPERATIVE (ZONE 200 - FUSE) · airframe 64,368 hrs · 29,028 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXT SIGN AIRCRAFT CENTER INOPERATIVE. RELAMPED INOPERATIVE BULBS ON EXIT SIGNS, OPERATIONS NORMAL, PER AMM 33-51-00.

Part: GIRT BAR — OUT OF POSITION (ZONE 800 - DOORS) · airframe 64,180 hrs · 28,922 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTED L1 DOOR HARD TO ARM (GIRT BAR WILL NOT TRAVEL FAR IN THE HOOKS). ARMING HANDLE SPONGY LAST INCH OF TRAVEL. REMOVED L1 DOOR SLIDE TO FACILITATE OTHER MAINTENANCE. REPOSITIONED GIRT PROPERLY AND RE-INSTALLED SAME SLIDE PER AMM 25-62-44.

Part: WIRE HARNESS — DAMAGED (NR 1 GENERATOR) · airframe 63,469 hrs · 28,543 cycles

AIRCRAFT WAS GROUNDED: MULTIPLE FAILURES INCLUDING AUTOPILOT INOPERATIVE, AUTOTHRUST INOPERATIVE, AUTO FLIGHT RUDDER TRIM 1 FAULT, YAW DAMPER 1 INOPERATIVE. CAPTAINS ALTIMETER UNRELIABLE. NO LIGHTS IN CABIN UNTIL GEAR CAME DOWN. UPPER AND LOWER ECAM DISPLAYS ON AND OFF MULTIPLE TIMES. RETURNED TO DFW. EMERGENCY DECLARED. FOUND #1 GEN PHASE (A) DAMAGED AT LOWER DISCONNECT. REPLACED #1 IDG FEEDER HARNESS TO THE LOWER / UPPER PYLON DISCONNECT. SYSTEM OPERATIONAL CHECKS NORMAL. ALL FAULTS CLEARED PER AMM 24-21-43.

Part: PRESSURE SWITCH — INOPERATIVE (RT FUEL PUMP) · airframe 63,188 hrs · 28,372 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP #2 LOW PRESSURE FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL PUMP PRESSURE SWITCH (AALA202105029001) IAW AMM 28-21-15. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED FUEL CENTER TANK BOOST PUMP SWITCH (AALA202105039011) IAW ESPM 20-45-11.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL BOOST PUMP) · airframe 63,188 hrs · 28,372 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP #2 LOW PRESSURE FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL PUMP PRESSURE SWITCH (AALA202105029001) IAW AMM 28-21-15. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED FUEL CENTER TANK BOOST PUMP SWITCH (AALA202105039011) IAW ESPM 20-45-11.

Part: BATTERY — DISCHARGED (FWD FLASHLIGHT) · airframe 63,069 hrs · 28,312 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY FLASHLIGHT AT FWD ENTRY IS NOT CHARGING. SUPPLEMENTAL REPORT: REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK, PER AMM 25-65-53.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,965 hrs · 28,266 cycles

AIRCRAFT WAS NOT GROUNDED. ROW 14L EMERGENCY ROW EXIT LIGHT HAS 7 OUT OF 14 BULBS WORKING. RELAMPED EXIT LIGHTS OPERATIONS CHECK GOOD, PER AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,956 hrs · 28,263 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AISLE ACROSS FROM ROW 13 ONLY HAS 3 OUT OF 14 BULBS WORKING. RELAMPED EXIT LIGHT OPERATIONS CHECK GOOD, PER AMM 33-51-00.

Part: HOSE — LEAKING (GREEN HYD SYS) · airframe 62,332 hrs · 27,929 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI, THE AIRCRAFT EXPERIENCED A LOSS OF GREEN HYDRAULIC SYSTEM WITH A SUBSEQUENT LOSS OF NOSE WHEEL STEERING. AIRCRAFT WAS ABLE TO STOP THE AIRCRAFT AT A DEICING PAD. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS UNABLE TO BE TOWED TO THE GATE SO THE PASSENGERS WERE DEDPLANED USING AIRSTAIRS AND TRANSPORTED TO THE TERMINAL VIA A BUS. FOUND 4 HYDRAULIC DRESSING FLEXIBLE HOSES ON THE LEFT HAND MAIN LANDING GEAR FOR ALTERNATE BRAKES LEAKING. REPLACED FLEXIBLE HOSE #29 (AALA202007279032), #32 (AALA202008059025), #65 (AALA202008059026) AND #66 (AALA202008059027) PER AMM 32-11-12-00-001A AND AMM 32-11-12-400-001-A. ALSO FOUND POWER TRANSFER UNIT HYDRAULIC HOSE LINE 1569GM B-NUT LOOSE AND LEAKING AT THE ELBOW; TIGHTENED B-NUT PER AMM 20-21-12. (AALA202008059028) A SATISFACTORY OPERATIONAL AND LEAK CHECK WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOSE — LEAKING (GREEN HYD SYS) · airframe 62,332 hrs · 27,929 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI, THE AIRCRAFT EXPERIENCED A LOSS OF GREEN HYDRAULIC SYSTEM WITH A SUBNSEQUENT LOOS OF NOSE WHEEL STEERING. AIRCRAFT WAS ABLE TO STOP THE AIRCRAFT AT A DEICING PAD. NO EMERGENCY WAS DECLARED. FOUND 4 HYDRAULIC DRESSING FLEXIBLE HOSES ON THE LEFT MAIN LANDING GEAR FOR ALTERNATE BRAKES LEAKING. REPLACED FLEXIBLE HOSE 29, 32, 65, & 66 IAW AMM 32-11-12-00-001A & AMM 32-11-12-400-001-A. ALSO FOUND POWER TRANSFER UNIT HYDRAULIC HOSE LINE 1569GM B-NUT LOOSE & LEAKING AT THE ELBOW. TIGHTENED B-NUT IAW AMM 20-21-12. OPS & LEAK CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOSE — LEAKING (GREEN HYD SYS) · airframe 62,332 hrs · 27,929 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI, THE AIRCRAFT EXPERIENCED A LOSS OF GREEN HYDRAULIC SYSTEM WITH A SUBSEQUENT LOSS OF NOSE WHEEL STEERING. AIRCRAFT WAS ABLE TO STOP THE AIRCRAFT AT A DEICING PAD. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS UNABLE TO BE TOWED TO THE GATE SO THE PASSENGERS WERE DEDPLANED USING AIRSTAIRS AND TRANSPORTED TO THE TERMINAL VIA A BUS. FOUND 4 HYDRAULIC DRESSING FLEXIBLE HOSES ON THE LEFT HAND MAIN LANDING GEAR FOR ALTERNATE BRAKES LEAKING. REPLACED FLEXIBLE HOSE #29 (AALA202007279032), #32 (AALA202008059025), #65 (AALA202008059026) AND #66 (AALA202008059027) PER AMM 32-11-12-00-001A AND AMM 32-11-12-400-001-A. ALSO FOUND POWER TRANSFER UNIT HYDRAULIC HOSE LINE 1569GM B-NUT LOOSE AND LEAKING AT THE ELBOW; TIGHTENED B-NUT PER AMM 20-21-12. (AALA202008059028) A SATISFACTORY OPERATIONAL AND LEAK CHECK WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOSE — LEAKING (GREEN HYD SYS) · airframe 62,332 hrs · 27,929 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI, THE AIRCRAFT EXPERIENCED A LOSS OF GREEN HYDRAULIC SYSTEM WITH A SUBSEQUENT LOSS OF NOSE WHEEL STEERING. AIRCRAFT WAS ABLE TO STOP THE AIRCRAFT AT A DEICING PAD. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS UNABLE TO BE TOWED TO THE GATE SO THE PASSENGERS WERE DEDPLANED USING AIRSTAIRS AND TRANSPORTED TO THE TERMINAL VIA A BUS. FOUND 4 HYDRAULIC DRESSING FLEXIBLE HOSES ON THE LEFT HAND MAIN LANDING GEAR FOR ALTERNATE BRAKES LEAKING. REPLACED FLEXIBLE HOSE #29 (AALA202007279032), #32 (AALA202008059025), #65 (AALA202008059026) AND #66 (AALA202008059027) PER AMM 32-11-12-00-001A AND AMM 32-11-12-400-001-A. ALSO FOUND POWER TRANSFER UNIT HYDRAULIC HOSE LINE 1569GM B-NUT LOOSE AND LEAKING AT THE ELBOW; TIGHTENED B-NUT PER AMM 20-21-12. (AALA202008059028) A SATISFACTORY OPERATIONAL AND LEAK CHECK WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: B-NUT — LEAKING (GREEN HYD SYS) · airframe 62,332 hrs · 27,929 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI, THE AIRCRAFT EXPERIENCED A LOSS OF GREEN HYDRAULIC SYSTEM WITH A SUBSEQUENT LOSS OF NOSE WHEEL STEERING. AIRCRAFT WAS ABLE TO STOP THE AIRCRAFT AT A DEICING PAD. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS UNABLE TO BE TOWED TO THE GATE SO THE PASSENGERS WERE DEDPLANED USING AIRSTAIRS AND TRANSPORTED TO THE TERMINAL VIA A BUS. FOUND 4 HYDRAULIC DRESSING FLEXIBLE HOSES ON THE LEFT HAND MAIN LANDING GEAR FOR ALTERNATE BRAKES LEAKING. REPLACED FLEXIBLE HOSE #29 (AALA202007279032), #32 (AALA202008059025), #65 (AALA202008059026) AND #66 (AALA202008059027) PER AMM 32-11-12-00-001A AND AMM 32-11-12-400-001-A. ALSO FOUND POWER TRANSFER UNIT HYDRAULIC HOSE LINE 1569GM B-NUT LOOSE AND LEAKING AT THE ELBOW; TIGHTENED B-NUT PER AMM 20-21-12. (AALA202008059028) A SATISFACTORY OPERATIONAL AND LEAK CHECK WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 61,900 hrs · 27,685 cycles

AIRCRAFT WAS NOT GROUNDED: MAIN CABIN AISLE FLOOR PANEL 241EF CRACKED AT SEAT ROW 13-14. REPLACED FLOOR PANEL PER AMM 53-12-12.

Part: APU — FIRE · airframe 60,700 hrs · 27,057 cycles

AIRCRAFT WAS GROUNDED: APU AUTO SHUTDOWN AT GATE, RAMP REPORTS SEEING FLAMES & SMELL OF FUEL AT AFT SECTION OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED APU IAW JOB CARD 26L31049005 LEAK AND OPS CHECK GOOD.

Part: COOLING FAN — LEAKING (APU) · airframe 60,479 hrs · 26,944 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK SMELL WITH PACKS ON GND & CRUISE. MAINTENANCE FOUND SOURCE TO BE FROM APU. ***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU OIL COOLING FAN IAW AMM 49-52-51 AND ACCOMPLISHED APU WASH IAW AMM 49-00-00-100-001-A. OPS GOOD, NO LEAKS FOUND.*** (CLOSED)

Part: INLET — CONTAMINATED (APU) · airframe 60,278 hrs · 26,831 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS MUSTY ODOR SMELLED THROUGHOUT CABIN AND COCKPIT ONCE APU BLEED TURNED ON. MAINTENANCE ACCOMPLISHED CABIN ODOR TROUBLESHOOTING IAW JOB CARD 26L00021001 & 26L00021002. APU IDENTIFIED AS SOURCE OF ODOR FOR THIS EVENT. ***SUPPLEMENTAL INFORMATION: MAINTENANCE CLEANED APU INLET AND DOOR. ALSO PERFORMED APU BLEED DUCT BLAST. NO NOTABLE ODER NOTICED AT THIS TIME.*** (CLOSED)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 59,971 hrs · 26,639 cycles

AIRCRAFT WAS NOT GROUNDED: AT CRUISE FLIGHT ECAM WARNING SMOKE, LAVATORY INDICATION DISPLAYED. MAINTENANCE REPORTED NO CURRENT FAULTS AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CONTROL UNIT — MALFUNCTIONED (SMOKE DETECTOR) · airframe 59,937 hrs · 26,616 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ECAM SMOKE DETECT. MAINTENANCE REPORTS SYSTEM FAULTED LAV A RESET SDCU RAN BITE TEST GOOD IAW AMM 26-16-00. ALL DISPLAYS NORMAL.

Part: ACTUATOR — FAULTY (NR 1 ENGINE) · airframe 59,853 hrs · 26,572 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT OR ABOUT 80 KIAS ON TAKE-OFF ROLL, AMBER ECAM ENG 1 COMPRESSOR VANE MEMO, NO OTHER ECAM ACTIONS NOTED. CONTINUED T/O. ECAM CLEARED IN LESS THAN 5 SEC. (CONT'D) ON LANDING ECAM ENG. 1 COMPRESSOR VANE WITH ACCOMPANIED ECAM ACTION. ECAM DID NOT CLEAR UNTIL ENGINE SHUTDOWN. MAINTENANCE REMOVED & REPLACED VSV ACTUATOR IAW AMM 75-32-41. ALL GRD CHECKS NORMAL. PERFORMED IDLE CHECK & HIGH POWER ASSURANCE TEST IAW AMM 71-00-00. ALL GRD CHECKS NORMAL.

Part: RELIEF VALVE — DAMAGED (APU) · airframe 59,749 hrs · 26,522 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS OIL SMELL ON A/C PACKS ON DESENT & AND ON THE GROUND WITH ENGINES & APU BLEED. MAINTENANCE ACCOMPLISHED CARD 26L00021001. DETERMINED APU TO BE SOURCE OF ODOR. FOUND BLOCK ASSEMBLY LEAKING ON APU. ***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU PRESSURE RELIEF VALVE IAW AMM. PERFORMED CARD 26L00021004, NO SMELL NOTED THIS TIME.*** (CLOSED)

Part: SKIN — DAMAGED (RUDDER) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER LEFT HAND SURFACE HAS EVIDENCE OF TRAPPED WATER AROUND THE LOWER FORWARD HOITING POINT. REPLACED RUDDER PER AMM 27-21-400-001-A.

Part: RIB — CRACKED (CARGO DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT DOOR SUPPORT WEB RIB. REPLACED SUPPORT WEB RIB PER SRM 51-72-11.

Part: SPLICE — ELONGATED (FRAME 64) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: OUTBOARD LOWER SPLICE LOCATED AT FR 64 AND -Y1292 HAS ELONGATED HOLE. REPLACED SPLICE PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 221DF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 222EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 261AG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 221EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006.

Part: SUPPORT ANGLE — CRACKED (FRAME 46) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BULKHEAD AFT FACE SUPPORT ANGLE AT FR 46 AND S38L IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE PER SRM 51-72-11.

Part: BOLT — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #4 LOWER BOLT. REPLACED BOLT PER AMM 27-84-63-400-002-A.

Part: BOLT — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #11 LOWER BOLT. REPLACED BOLT PER AMM 27-84-67-400-002.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #3 HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #2 HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #5 HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #4 HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD INBOARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE OUTBOARD HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER CMM 52-82-32.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE INBOARD HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER CMM 52-82-32.

Part: COUPLING — ELONGATED (FRAME 64) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: SPLICE COUPLING AT FR 64 AND -Y1292 HAS ELONGATED HOLE. REPLACED COUPLING PER SRM 51-72-11.

Part: HINGE — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD OUTBOARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY / WORN. REPLACED HINGE FITTING PER CMM 52-82-32.

Part: COUPLING — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER INBOARD SPLICE COUPLING AT FR 66 AND -Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11.

Part: HINGE — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR AFT OUTBOARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: HINGE — WORN (NLG DOOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR AFT INBOARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: FLOOR SPLICE — DAMAGED (FRAME 64) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: FLOOR BEAM SPLICE COUPLING HAS ELONGATED HOLE AT FR 64 AND -Y765. REPLACED COUPLING PER SRM 51-72-11.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT FR 66 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 PRINCIPLE 9.

Part: FLOORBEAM — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM BETWEEN FR 66 AND FR 68 AT +Y1225. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND RIB 9, 9.75" OUTBOARD OF LIGHTING STRIP 4 AND 4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM BETWEEN FR 64 AND FR 66 AT -Y1292. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR PANEL 131CG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-67) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM BETWEEN FR 64 AND FR 67 AT -Y465. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 3 AND RIB 4, 8.5" OUTBOARD OF LIGHTING STRIP 1 AND 3.25 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND RIB 9, 17" OUTBOARD OF LIGHTING STRIP 4 AND 4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM BETWEEN FR 64 AND FR 66 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON DUMMY RAIL BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM BETWEEN FR 12 AND FR 24 AT -Y254. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL AT FR 16 AND S10L. REPLACED INTERCOSTAL PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY FLOOR BEM BETWEEN FR 12 AND FR 24 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM BETWEEN FR 64 AND FR 66 AT +Y1292. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: STOP FITTING — CRACKED (FRAME 16) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT HAND AT THE #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 2 AND RIB 3, 3.5 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,298 hrs · 26,252 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y765. REPLACED SEATTRACK PER SRM 51-72-11.

Part: DIAPHRAGM — FAILED (R1 ASSIST BOTTLE) · airframe 58,691 hrs · 25,960 cycles

R1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. REMOVED AND REPLACED DIAPHRAGM ON THE DOOR ASSIST BOTTLE AND SERVICED THE BOTTLE IAW AMM 52-10-00-610-001.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 58,046 hrs · 25,570 cycles

AISLE EMERGENCY LIGHT COVER WAS DAMAGED AT SEAT 9C. REPLACED THE LIGHT COVER IAW AMM 33-50-00.

Part: GIRT BAR — FOD (R1 DOOR SLIDE) · airframe 57,789 hrs · 25,405 cycles

R1 DOOR DIFFICULT TO ARM. REMOVED DEBRIS FROM GIRT BAR FITTING. OPS CHECKED OK IAW AMM 25-62-00.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 57,690 hrs · 25,349 cycles

L2 DOOR EMERGENCY CYLINDER HAD LOW PRESSURE. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 56,404 hrs · 24,572 cycles

L2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00-614-001-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 56,404 hrs · 24,572 cycles

R2 DOOR ASSIST BOTTLE LOW. MAINTENANCE CHARGED THE R2 DOOR CYLINDER TO PROPER PRESSURE IAW AMM 52-10-00-614-001-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: APU — ODOR · airframe 56,079 hrs · 24,351 cycles

FLIGHT ATTENDANTS REPORTED AN ODOR IN THE REAR OF AIRCRAFT. MAINTENANCE FOUND APU TO BE SOURCE OF ODOR AND REPLACED THE APU IAW JC 26L31049005. AIRCRAFT WAS GROUNDED.

Part: BUSHING — MIGRATED (RT MLG DOOR) · airframe 55,988 hrs · 24,299 cycles

MIGRATING BUSHING, LUG WORN. ACCOMPLISHED RIGHT HAND MLG DOOR AFT ACTUATOR FITTING REPLACEMENT IN COMPLIANCE WITH EA 276221A.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 55,874 hrs · 24,221 cycles

AIRCRAFT NOT GROUNDED. ODOR THROUGHOUT A/C CABIN AND COCKPIT DESCENDING STARTED AT 70000 MSL TAT PLUS 12 DEGS SAT PLUS 10 DEGS. APU FOUND TO BE THE SOURCE DECONTAMINATED BLEED SYS APU PLACED ON MEL. SUPPLEMENTAL REPORTED TO BE PROVIDED LATER TO INCLUDE CORRECTIVE ACTION AND PART INFORMATION.

Part: DIFFUSER — DIRTY (APU) · airframe 55,640 hrs · 24,106 cycles

OIL ODOR DURING TAXI OUT AND CLIMB, ODOR BEGAN AGAIN DURING DESCENT. CLEANED APU DOOR DIFFUSER. OPS CHECKED GOOD.

Part: PACKING — LEAKING (APU OIL) · airframe 55,603 hrs · 24,089 cycles

F/A'S REPORTED A DIRTY SOCK ODOR DURING TAKEOFF, AT ABOUT 10,000 FT, UNTIL TOUCH DOWN. FOUND OIL INGESTED IN APU COMPRESSOR SECTION. APU LEAKING OIL FROM GENERATOR MOUNT GASKET. REPLACED APU TURBINE CAVITY VENT TUBE PACKING IAW AMM.

Part: HOUSING — BROKEN (CABIN) · airframe 55,358 hrs · 23,941 cycles

AIRCRAFT IN BASE MAINTENANCE. BROKEN EMERGENCY PATH LIGHT HOUSING AT SEAT 14C. REPLACED EMERGENCY PATH LIGHT HOUSING AT SEAT 14C PER CMM 25-22-52.

Part: LEVER — LACK OF LUBE (L1 DOOR ARMING) · airframe 55,288 hrs · 23,913 cycles

L1 DOOR, FA REPORTS ARMING LEVER STIFF, NOT SMOOTH LIKE IT NORMALLY IS. LUBRICATED ARMING LEVER LINKAGE IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 55,113 hrs · 23,782 cycles

L2 DOOR EMERGENCY LIGHT LENS FELL OFF THE PACK. REPLACED THE LENS. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — FAULTED (NR 1 ENGINE VS) · airframe 54,157 hrs · 23,222 cycles

APPLIED TAKE-OFF POWER AND RECEIVED ECAM MESSAGE AT 50-60KTS FOR NR 1 ENGINE COMPRESSOR VANE, SHUTDOWN ENGINE AND RETURED TO GATE. REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR ACTUATOR. AIRCRAFT WAS GROUNDED

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 54,088 hrs · 23,190 cycles

EMERGENCY EXIT FLOOR LIGHT LENS FELL OFF AT R2 DOOR. REPLACED THE LENS.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 53,893 hrs · 23,084 cycles

CREW REPORTED STRONG DIRTY SOCK ODOR IN AFT CABIN WHILE ON FINAL APPROACH. FOUND APU OVERSERVICED. DRAINED APU OIL TO PROPER LEVEL.

Part: FAN — ODOR (E/E BAY) · airframe 53,635 hrs · 22,945 cycles

IN CRUISE AT 360 APPROXIMATELY, 1 HOUR OF FLIGHT , FLIGHT CREW SMELLED STRONG CHEMICAL/PLASTIC DOOR . FLIGHT ATTENDANT SAID OVEN HAD BEEN ON, ODOR DISSIPATED SOME WHAT, BUT RETURNED THE REMAINDER OF THE FLIGHT AND AT GATE. AIRCRAFT WAS GROUNDED. REPLACED AVIONICS FAN 20HQ IAW AMM 21-26-51.

Part: LEVER — LACK OF LUBE (L1 DOOR) · airframe 53,535 hrs · 22,900 cycles

ARMING LEVER FOR DOOR 1L IS DIFFICULT TO OPEN OR CLOSE. LUBED 1L DOOR PER 52-20-00 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 53,190 hrs · 22,727 cycles

AIRCRAFT WAS NOT GROUNDED. 1L ARMING DOOR IS STICKING. CLEANED DEBRIS FROM GIRT BAR HOOKS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CAM — DIRTY (L1 DOOR) · airframe 53,190 hrs · 22,727 cycles

AIRCRAFT WAS NOT GROUNDED. 1L ARMING LEVER VERY STIFF. CLEANED AND LUBED GIRT BAR LOCKS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CONTROL SERVO — FAULTED (NLG STEERING) · airframe 52,381 hrs · 22,272 cycles

FLIGHT CREW REPORTED RECIEVEING AN ECAM NOSE WHEEL STEERING FAULT MESSAGE DURING DESCENT AND DECLARED AN EMERGENCY. THE AIRCRAFT LANED AT LAX SAFELY, TAXIED OFF THE RUNWAY UNDER IT'S OWN POWER AND THEN WAS TOWED TO THE GATE. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE NOSE WHEEL STEERING CONTROL SERVO PER AMM 32-51-51. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 51,919 hrs · 22,048 cycles

AIRCRAFT WAS NOT GNDED. FOUND LT OFF WING SLIDE INFLATION RESERVOIR LOW PRESS. CIDS CAUTION LIGHT ON. REPLACED LT OFF WING SLIDE INFLATION RESERVOIR IAW AMM 25-62-46.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 51,796 hrs · 21,984 cycles

AIRCRAFT WAS GNDED. INFLIGHT THE WHEELS PAGE SHOWED AMBER XX'S FOR THE NOSE GEAR DOORS. CREW REPORTED LOUD NOISE COMING FROM THE FRONT OF THE ACFT & A SLIGHT VIBRATION WAS ALSO FELT. THE FLIGHT CREW DECLARED AN EMER & WHEN GEAR LOWERED IT WAS UNEVENTFUL WITH NO ABNORMAL INDICATION, NO MORE AMBER XX'S. THE ACFT LANDED SAFELY & TAXIED TO THE GATE WITH NO FURTHER INCIDENTS. PERFORMED VISUAL INSPECTION OF NLG & NLG DOORS, NO DEFECTS NOTED. PERFORMED NUMEROUS SATISFACTORY OPERATIONAL CHECKS OF NLG DOORS IAW AMM 32-22-00. CHECKED GOOD. PERFORMED BITE CHECK OF LGCIU 1 & 2 NO FAULTS.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,614 hrs · 21,884 cycles

AIRCRAFT IN BASE MX. THE LT ELEVATOR UPPER SURFACE HAD 3 AREAS WHERE THERE WAS AN INDICATION OF WATER INGRESS. AREA 1 5" FROM THE TE & 18" FROM THE OTBD END, AREA 2 5.25" FROM THE TE & 58" FROM THE OTBD END & AREA 3 25.75" FROM THE TE & 24" FROM THE OTBD END. ELEVATOR UPPER SURFACE REPAIRED IAW SRM 55-21-11-201-1 PARAGRAPH 5E.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 51,084 hrs · 21,601 cycles

DOOR 1L ARMING MECHANISM STIFF. PERFORMED VISUAL INSPECTION OF GIRT BAR & ARMING MECHANISM. CLEANED & LUBED GIRT BAR FITTINGS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-11-22-220-001.

Part: MODULE — BROKEN (CABIN) · airframe 50,968 hrs · 21,533 cycles

AIRCRAFT WAS NOT GNDED. AFT RED EMER EXIT PATH LIGHT ON LAVATORY D IS BROKEN. INSTALLED NEW LAMP MODULE ON EXTERIOR OF LAVATORY D. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-1.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 50,570 hrs · 21,257 cycles

AIRCRAFT WAS GNDED. BURNING PLASTIC SMELL IN COCKPIT & CABIN, NO SMOKE VISIBLE. DISSIPATED SOME DURING APPROACH. ACCOMPLISHED TASK CARD 26L00021001, NO ODORS DETECTED.

Part: FILTER — DIRTY (AC BAY) · airframe 50,519 hrs · 21,219 cycles

DESCENDING, APPROX 10,000 FT TO TOUCH DOWN, NOXIOUS ODORS & STRANGE FOUL FUMES. ACCOMPLISHED TASK CARDS 26L00021001 & 26L00021003. REPLACED HEPA FILTERS. SECURED HYD DOOR LINE. ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK. SEE AALA201511259002 FOR ADDITIONAL INFORMATION.

Part: HYDRAULIC LINE — LEAKING (ZONE 800) · airframe 50,519 hrs · 21,219 cycles

DESCENDING, APPROX 10,000 FT TO TOUCH DOWN, NOXIOUS ODORS & STRANGE FOUL FUMES. ACCOMPLISHED TASK CARDS 26L00021001 & 26L00021003. REPLACED HEPA FILTERS. SECURED HYD DOOR LINE. ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK. SEE AALA201511259005 FOR ADDITIONAL INFORMATION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,556 hrs · 20,706 cycles

EMERGENCY LIGHTS ROW 14, 18, 22 LAVATORY D, L2 DOOR, R2 DOOR, ROW 14 OVERHEAD INOPERATIVE. REPLACED 13WL EPSU IAW 33-51-38. OPERATIONAL TEST NORMAL. SEE ALSO AALA201507319001.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 49,556 hrs · 20,706 cycles

EMERGENCY LIGHTS ROW 14, 18, 22 LAVATORY D, L2 DOOR, R2 DOOR, ROW 14 OVERHEAD INOPERATIVE. REPLACED 22L SEAT HARNESS & LIGHT ASSEMBLY FROM 5751VC-A, IAW ASM 33-51-04. SEE ALSO AALA201507319019.

Part: FLOORBOARD — DEBONDED (CABIN) · airframe 49,072 hrs · 20,425 cycles

AFT GALLEY FLOORBOARD 261PF FOUND TO BE DISBONDED ON LT & RT SIDES. REPLACED AFT GALLEY FLOORBOARD 261PF.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,372 hrs · 20,098 cycles

STRONG SMELL OF SMOKE IN AFT GALLEY. INSPECTED AFT GALLEY COFFEEMAKERS, LIGHTS, ELEC PANEL & OUTLETS. NO SIGNS OF DAMAGE OR SMIELL NOTED. ACFT OK FOR SERVICE.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 48,281 hrs · 20,045 cycles

PASSENGER DOOR L1 IS HARD TO ARM OR DISARM. CLEANED DE-ICING AGENT FROM GIRT BAR FLOOR ATTACH MOUNTS. ARMING & DISARMING OPERATION SMOOTH & NORMAL. OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 47,976 hrs · 19,887 cycles

DOOR 1L ARMING LEVER HARD TO OPERATE. REMOVED DEBRIS FROM DOOR 1L DOOR FRAME AREA, OPERATIONS NORMALLY.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 47,882 hrs · 19,849 cycles

DOOR L1 EMER SLIDE WILL NOT STAY ARMED. CLEARED DEBRIS FROM DOOR L1 GIRT BAR BRACKET. OPERATIONS CHECKED GOOD. NO FURTHER FAULTS NOTED.

Part: WIRE — DAMAGED (CABIN) · airframe 47,802 hrs · 19,814 cycles

SEAT ROWS 14,18 & 22, EMER SEAT LIGHTS INOPERATIVE. FOUND WIRE 2109 AT 7222VT FAULTING. RELIEVED STRAIN & REINSTALLED IAW AWM 33-51-08, PAGE 77, SHEET 2 & ESPM 20-33-44. OPERATIONS CHECKED IAW AMM 33-51-00-710-001A OK.

Part: HANDLE — BINDING (ENTRY DOOR) · airframe 47,525 hrs · 19,635 cycles

FORWARD ENTRY DOOR ESCAPE SLIDE ARMING HANDLE IS TIGHT & NEEDS LUBE. ACCOMPLISHED AMM TASK 52-10-00-720-005-A. CHECKED OK AT THIS TIME.

Part: LENS — MISSING (CABIN) · airframe 47,079 hrs · 19,349 cycles

THE EMER EXIT LIGHT LENS MISSING AT ROW 1L. INSTALLED MISSING ROW 1 EMER LIGHT LENS COVER. NO DEFECTS NOTED AT THIS TIME IAW AMM 33-50-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,940 hrs · 19,259 cycles

THE FWD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPERATIONS CHECKED GOOD ON GND AT THIS TIME.

Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 46,771 hrs · 19,166 cycles

A SMOKE DETECTOR FAULT ECAM. CLEANED FILTERS IN ALL THREE LAVATORY SMOKE DETECTORS & RESET THE SDCU IAW TSM TASK 26-17-00-810-802-A. TESTED OK, FAULT CLEARED. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 46,583 hrs · 19,049 cycles

THE L3 DOOR ASSIST BOTTLE LOW. SERVICED L3 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001A.

Part: LENS — BROKEN (CABIN) · airframe 46,541 hrs · 19,017 cycles

PASSENGER SEAT 1 C EMER LIGHT LENS BROKEN. REPLACED SEAT 1 C EMER LIGHT LENS AS REQUIRED, CHECKED OK.

Part: THRESHOLD — DIRTY (FUSELAGE) · airframe 46,438 hrs · 18,955 cycles

FLIGHT ATTENDANT REPORTED THE FWD ENTRY DOOR SLIDE ARMING LEVER TO TIGHT. REMOVED DEBRIS & CLEANED THRESHOLD SILL. OPERATIONS CHECKED GOOD, NO FAULTS NOTED. OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (THRUST REVERSER) · airframe 46,282 hrs · 18,887 cycles

ON TAXI TO GATE COMPANY CREW BEHIND US REPORTED SMOKE FROM OUR NR 1 ENG, OIL DROPLETS ON WINDSCREEN & SMELL OF OILY SMOKE ON THEIR ACFT. FIRST OFFICER DISCOVERED LARGE AMOUNT OF LIQUID LEAKING FROM NR 1PYLON ON POST FLIGHT. REPLACED NR 1 TR HCU RETURN HOSE IAW AMM 29-11-49.

Part: LIGHT — LOOSE (CABIN) · airframe 45,631 hrs · 18,596 cycles

CREW REPORTED 3C EMERGENCY LIGHT EXIT PATH SMASHED LOOSE IN BRACKET. SECURED EMERGENCY LIGHT IAW AMM 33-51-19-400-003-A, OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 45,442 hrs · 18,522 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT COVER MISSING ON SEAT 3C. REPLACED LIGHT LENS IAW AMM 33-51-13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,413 hrs · 18,511 cycles

MAINTENANCE REPORTED THE WHITE EMERGENCY FLOOR PROXIMITY LIGHT AT 12 LT INOPERATIVE. R & R LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-51-19.

Part: LENS — MISSING (CABIN) · airframe 45,413 hrs · 18,511 cycles

CREW REPORTED SEAT 14D, EMERGENCY EXIT LIGHT LENS COVER MISSING. MX REPLACED EMERGENCY FLOOR PROXIMITY LIGHT LENS AT 14D.

Part: PAD — LACK OF LUBE (L1 DOOR) · airframe 45,269 hrs · 18,455 cycles

CREW REPORTED DOOR L1 IS HARD TO DISARM SLIDE. LUBRICATED L1 DOOR SLIDE PADS, OPERATIONS OK.

Part: MOUNT — DIRTY (GIRT BAR) · airframe 44,333 hrs · 18,053 cycles

CREW REPORTED L1 DOOR ARM-DISARM LEVER VERY STIFF, HARD TO OPEN. MAINTENANCE REMOVED DEBRIS FROM L1 DOOR GIRT BAR FLOOR MOUNTS. OPS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,316 hrs · 18,043 cycles

CREW REPORTED THE EMERGENCY FLASHLIGHT IN AFT CABIN, RED LIGHT NOT FLASHING. MAINTENANCE REPLACED FWD FACING EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD. OK FOR SERVICE.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 44,062 hrs · 17,939 cycles

CREW REPORTED THE L1 DOOR NOT ARMING. MX REMOVED DEBRIS FROM GIRT BAR. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 43,770 hrs · 17,816 cycles

MX REPORTED THE L2 DOOR ASSIST BOTTLE PRESSURE LOW. MX SERVICED BOTTLE TO FULL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 43,597 hrs · 17,745 cycles

MX REPORTED ROW 10R EMERGENCY LIGHT LENS (RED) MISSING. MX REPLACED ROW 10R EMERGENCY LIGHT LENS.

Part: LENS — MISSING (ZONE 200) · airframe 43,597 hrs · 17,745 cycles

MX REPORTED ROW 4 RT EMERGENCY LIGHT LENS (CLEAR) MISSING. MX REPLACED 4 RT EMERGENCY LIGHT LENS.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 43,512 hrs · 17,704 cycles

CREW REPORTED ROW 1C EMERGENCY LIGHT COVER IS MISSING FROM SIDE OF SEAT. MX REPLACED COVER. OPS CHECKED GOOD.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 42,897 hrs · 17,426 cycles

CREW REPORTED DOOR 2L IS DIFFICULT TO ARM. MAINTENANCE CLEANED GIRT BAR AND LUBED. OPS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 42,720 hrs · 17,340 cycles

CREW REPORTED THE EMERGENCY EXIT LIGHT COVER MISSING, ROW 1 A/C LEFT. MAINTENANCE REPLACED LENS AS REQUIRED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (L2 DOOR) · airframe 42,668 hrs · 17,314 cycles

CREW REPORTED DOOR 2L SLIDE ARMED INDICATION DOES NOT SHOW ARMED IN FLIGHT UNLESS HANDLE IS HELD BY FLIGHT ATTENDANT. MAINTENANCE ADJUSTED DOOR 2L SLIDE ARMED PROX SWITCH PER 52-71-00-820-002-A-01. OPS CHECK GOOD.

Part: CONNECTOR — DAMAGED (EVAC SLIDE) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - DAMAGED ELECTRICAL CONNECTOR ON SLIDE PACK ASSEMBLY AFT LEFT. REPLACED ELECTRICAL CONNECTOR ON SLIDE PACK ASSY AFT LEFT IAW A320 ESPM 20-44-11. PERFORMED OPERATIONAL TEST IAW A320 AMM 25-62-44-400-006-A, TEST IS OK. PERFORMED OPERATIONAL TEST IAW A320 AMM 33-51-00-710-001-A, TEST IS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - INOPERATIVE EPSU AT EMERGENCY RIGHT AREA. REPLACED EPSU AT EMERGENCY EXIT RIGHT IAW AMM33-51-38-400-001-A. PERFORMED BITE TEST IAW AMM 33-51-38-400-001-A OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - INOPERATIVE EPSU AT EMERGENCY EXIT LEFT AREA. REPLACED EPSU AT EMERGENCY EXIT LEFT IAW AMM33-51-38-400-001-A.

Part: SLIDE — CRACKED (CABIN) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CRACK ON ENCLOSURE OF OFFWING ESCAPE SLIDE ON RIGHT SIDE. REPLACED OFF WING ESCAPE SLIDE RIGHT SIDE IAW A319 AMM 25-62-42-000-001-A.

Part: STRUT — CORRODED (RT WING) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4862 & WS 5512 & BETWEEN RIB 9 TO RIB 10. REPLACED RIGHT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44.

Part: STRUT — CORRODED (LT WING) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4862 & WS 5512 & BETWEEN RIB 9 TO RIB 10. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT CORNER FITTING AT FR68, S23L. REPLACED LEFT CORNER FITTING AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR ASSEMBLY 640NB BETWEEN RIB 13 TO RIB 21 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR ASSEMBLY 640NB IAW A319 AMM 57-27-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 211KF BETWEEN FR6 TO FR12 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 211KF IAW A319 SRM 53-12-00 FIG 206 & IRM 9701, REV G.

Part: HINGE FITTING — WORN (LT SPOILER) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - WEAR AREA ON CENTER HINGE OF LEFT WING 4 SPOILER BETWEEN WS 924 TO WS 970 & BETWEEN RIB 18 TO RIB 19. REPLACED LEFT WING 4 SPOILER CENTER HINGE FITTING IAW A319 SRM 57-70-00, FIGURE 201.

Part: HINGE FITTING — WORN (RT SPOILER) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - WEAR AREA ON CENTER HINGE OF RIGHT WING 2 SPOILER BETWEEN WS 613 TO WS 670 & BETWEEN RIB 11 TO RIB 12. REPLACED RIGHT WING 2 SPOILER CENTER HINGE FITTING IAW A319 SRM 57-70-00, FIGURE 201.

Part: HINGE FITTING — WORN (LT WING) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - WEAR AREA ON CENTER HINGE OF LEFT WING 3 SPOILER BETWEEN WS 779 TO WS 827 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING 3 SPOILER CENTER HINGE FITTING IAW A319 SRM 57-70-00, FIGURE 201.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CRACK ON RIGHT EMERGENCY EXIT DOOR 844 SEGMENT ANGLE FRAME BETWEEN FR40 TO FR41 & BETWEEN S13L TO S20L. REPLACED RIGHT EMERGENCY EXIT DOOR 844 SEGMENT ANGLE FRAME IAW EO 5210Y228.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CRACK ON LEFT EMERGENCY EXIT DOOR 834 SEGMENT ANGLE FRAME BETWEEN FR40 TO FR41 & BETWEEN S13L TO S20L. REPLACED LEFT EMERGENCY EXIT DOOR 834 SEGMENT ANGLE FRAME IAW EO 5210Y228.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CRACK ON RIGHT EMERGENCY EXIT DOOR 844 SEGMENT ANGLE FRAME BETWEEN FR40 TO FR41 & BETWEEN S13L TO S20L. REPLACED RIGHT EMERGENCY EXIT DOOR 844 SEGMENT ANGLE FRAME IAW EO 5210Y228.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - CRACK ON LEFT EMERGENCY EXIT DOOR 834 SEGMENT ANGLE FRAME BETWEEN FR40 TO FR41 & BETWEEN S13L TO S20L. REPLACED LEFT EMERGENCY EXIT DOOR 834 SEGMENT ANGLE FRAME IAW EO 5210Y228.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL LOWER SURFACE AT FR63+2 INCHES, S23R, -Y765. REPAIRED SEAT RAIL AT FR63+2 INCHES, S23R, -Y765 IAW A319 SRM 53-41-15, PAGE 207/208, FIG 202.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR47/51 TO FR64, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 42,656 hrs · 17,307 cycles

2S CHECK - ELONGATED HOLE ON SEAT TRACK COUPLING AT FR64, -Y765. REPLACED SEAT TRACK COUPLING AT FR64, -Y765 IAW A319 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66 Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66 Y765 IAW A319 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53472831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR58 TO FR59, Y765. REPLACED SEAT TRACK BETWEEN FR58 TO FR59, Y765 IAW A319 SRM 53-00-15, FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112828.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT LOWER SILL BETWEEN FR66 TO FR68, S23R. REPLACED RIGHT LOWER SILL BETWEEN FR66 TO FR68, S23R IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503948.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,656 hrs · 17,307 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT LOWER SILL BETWEEN FR66 TO FR68, S23L. REPLACED LEFT LOWER SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 41,606 hrs · 16,834 cycles

RUDDER DISBOND VISIT - DELAMINATION ON LEFT ELEVATOR UPPER SURFACE. REPLACED LEFT ELEVATOR IAW A319 AMM 27-34-41C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION FOUND ON FLOOR SUPPORT AT FR14, Y254. REPLACED FLOOR SUPPORT AT FR14, Y254 IAW A319 SRM 51-74-00, 53-11-14, 53-00-14 & 51-42-11.

Part: LENS — MISSING (CABIN) · airframe 41,194 hrs · 16,623 cycles

SY6 CHECK - EMERGENCY EXIT LIGHT, SEAT 18C, MISSING LENS. REMOVED, REPLACED AND OPS CHECKED EMERGENCY EXIT LIGHT AT SEAT 18C IAW A319 AMM 33-51-19 AND 33-51-00.

Part: DIAPHRAGM — LEAKING (L1 DOOR) · airframe 41,194 hrs · 16,623 cycles

SY6 CHECK - L-1 DOOR DAMPER CYLINDER PRESSURE SHOWS ZERO. REMOVED AND REPLACED L1 DOOR DAMPER CYLINDER DIAPHRAM, SERVICED DAMPER, OPS AND LEAK CHECK OK IAW A319 AMM 52-10-00 AND 52-10-00-614.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR67, -Y1292. REPLACED FLOOR SUPPORT AT FR67, -Y1292 IAW A319 SRM 51-74-00, 53-00-14, 51-42-11, & DRAWING # D5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - CORROSION ON FLOORBEAM AT FR68-2 INCHES, Y1292. REPLACED FLOORBEAM AT FR68-2 INCHES, Y1292 IAW A319 SRM 51-74-00, 53-00-14, 51-44-11 & 51-42-11.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 9 INCHES FROM OUTBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 9 INCHES FROM OUTBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 69.5 INCHES FROM OUTBOARD EDGE AND 6.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 69.5 INCHES FROM OUTBOARD EDGE AND 6.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 18.5 INCHES FROM INBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 18.5 INCHES FROM INBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 27 INCHES FROM OUTBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 27 INCHES FROM OUTBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 5.5 INCHES FROM INBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 5.5 INCHES FROM INBOARD EDGE AND 5.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (LT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON LEFT ELEVATOR ON UPPER PANEL 54 INCHES FROM OUTBOARD EDGE AND 16.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR ON UPPER PANEL 54 INCHES FROM OUTBOARD EDGE AND 16.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON RIGHT ELEVATOR ON UPPER PANEL 27.5 INCHES FROM OUTBOARD EDGE AND 8.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR ON UPPER PANEL 27.5 INCHES FROM OUTBOARD EDGE AND 8.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SKIN PANEL — SATURATED (LT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON LEFT ELEVATOR ON UPPER PANEL 71 INCHES FROM INBOARD EDGE AND 7 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR ON UPPER PANEL 71 INCHES FROM INBOARD EDGE AND 7 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BEAM AT FR67+15 INCHES, Y1292. REPLACED FLOOR SUPPORT BEAM AT FR67+15 INCHES, Y1292 IAW A319 SRM 51-00-14, 51-74-00, 51-44-11 & 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1160. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1160 IAW A319 SRM 51-42-11, ESPM 20-33-22.

Part: SKIN PANEL — SATURATED (LT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON LEFT ELEVATOR ON UPPER PANEL 76 INCHES FROM OUTBOARD EDGE AND 20.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR ON UPPER PANEL 76 INCHES FROM OUTBOARD EDGE AND 20.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR68, -Y165. REPLACED FLOOR SUPPORT AT FR68, -Y165 IAW A319 SRM 51-74-00, 51-73-00, 51-42-11 & AIRBUS DRAWING 18-D534-7278.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR70, -Y160. REPLACED FLOOR SUPPORT AT FR70, -Y160 IAW A319 SRM 51-74-00, 51-10-04, 51-42-11, DRAWING 18.

Part: SKIN PANEL — SATURATED (LT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON LEFT ELEVATOR ON UPPER PANEL BETWEEN 87 TO 104 INCHES FROM INBOARD EDGE AND 10 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR ON UPPER PANEL BETWEEN 87 TO 104 INCHES FROM INBOARD EDGE AND 10 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1160. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1160 IAW A319 SRM 51-42-11, ESPM 20-33-222 & AMM 34-55-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR16, -Y254. REPLACED FLOOR SUPPORT AT FR16, -Y254 IAW A319 SRM 53-11-14, 51-42-11 & AMM 27-41-44-0401.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - WATER INGRESS ON LEFT ELEVATOR ON UPPER PANEL 33 INCHES FROM INBOARD EDGE AND 20 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR 33 INCHES FROM INBOARD EDGE AND 20 INCHES FROM TRAILING EDGE IAW A319 SRM 55-20-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 16,622 cycles

SY6 CHECK - LEVEL 2 SURFACE CORROSION ON FLOOR SUPPORT AT FR67, -Y1292. REPLACED FLOOR SUPPORT AT FR67, -Y1292 IAW A319 SRM 51-42-11, 51-74-00, 51-10-04 & 53-00-14.

Part: FMU — SURGES (NR 1 ENGINE) · airframe 40,775 hrs · 16,435 cycles

PRIOR TO 1,000 AGL ENGINE 1 SHUT DOWN - ECAM ACTIONS COMPLETED DURING DOWN WIND - POPPING SOUND COMPRESSOR STALL. COMPLIED WITH TROUBLESHOOTING AND ENGINEERING REQUEST. REMOVED AND REPLACED FMU, FUEL PUMP, AND EEC. COMPLIED WITH FUNCTIONAL CHECK OF BLEED VALVES, SOLENOIDS, AND IP CHECK VALVE. COMPLETED WINDMILL INSPECTION. HIGH POWER ASSURANCE RUN ACCOMPLISHED. NO SYSTEM FAULTS AND OPS CHECKED GOOD.

Part: EEC — SURGES (NR 1 ENGINE) · airframe 40,775 hrs · 16,435 cycles

PRIOR TO 1,000 AGL ENGINE 1 SHUT DOWN - ECAM ACTIONS COMPLETED DURING DOWN WIND - POPPING SOUND COMPRESSOR STALL. COMPLIED WITH TROUBLESHOOTING AND ENGINEERING REQUEST. REMOVED AND REPLACED FMU, FUEL PUMP, AND EEC. COMPLIED WITH FUNCTIONAL CHECK OF BLEED VALVES, SOLENOIDS, AND IP CHECK VALVE. COMPLETED WINDMILL INSPECTION. HIGH POWER ASSURANCE RUN ACCOMPLISHED. NO SYSTEM FAULTS AND OPS CHECKED GOOD.

Part: CYLINDER — DAMAGED (R2 DOOR) · airframe 40,457 hrs · 16,296 cycles

R2 DOOR CYLINDER DAMPER SHEER PIN STUCK IN HOUSING. REMOVED AND REPLACED R2 DOOR DAMPER CYLINDER IAW AMM 52-13-14-0401. OPS CHECKED GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,117 hrs · 16,147 cycles

AT FL 360 FIRST OFFICER FORWARD WINDSHIELD CRACKED. COMPLIED WITH QRH DESCENT TO FL200. DECLARED EMERGENCY. REMOVED AND REPLACED FIRST OFFICER FORWARD WINDSHIELD IAW JOB CARD 26L21056001. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,498 hrs · 15,865 cycles

R1 DOOR MISSING EMERGENCY EXIT LIGHT LENS COVER. REPLACED R1 DOOR EMERGENCY EXIT LIGHT LENS COVER.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 37,612 hrs · 15,002 cycles

SLIDE R1 NOT ARMING PROPERLY. RESECURED AND STOWED SLIDE AT BOTTOM. OPERATIONAL CHECK GOOD.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 37,425 hrs · 14,908 cycles

DFW-PHX - ELECTRICAL SMELL - NR 1 FORWARD COFFEEMAKER HAS ELECTRICAL SMELL, ALL LIGHTS ON. REMOVED AND REPLACED FORWARD NR 1 COFFEEMAKER. PERFORMED OPERATIONAL CHECK PER AMM 25-35-15. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 35,400 hrs · 14,012 cycles

FLT 185 - FLL - EEL - EMERGENCY EXIT SIGN COVER IS BROKEN AT ROW 9 LEFT FORWARD BOTTOM SIDE OF EMERGENCY DOOR. MAINTENANCE REPLACED EMERGENCY EXIT SIGN COVER AT ROW 9 LEFT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,333 hrs · 13,980 cycles

FLT 396 - DFW-LAS - EMERGENCY LIGHTS - L2 EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED L2 EMERGENCY FLASHLIGHT.

Part: LENS — BROKEN (CABIN) · airframe 32,327 hrs · 12,722 cycles

SAL - BC6 - EEL - BROKEN UPPER "EXIT" LIGHT LENS ON LEFT & RIGHT EMERGENCY EXIT DOORS. REPLACED UPPER "EXIT" LIGHT LENS ON LEFT & RIGHT EMERGENCY EXIT DOORS IAW A319 AMM 33-57-16.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 32,327 hrs · 12,722 cycles

SAL - BC6 - EES - LOW PRESSURE DAMPER AT R-1 DOOR. CHARGED DAMPER AT R-1 DOOR & PERFORMED LEAK TEST IAW A319 AMM 52-10-00.

Part: SUPPORT — WORN (TE FLAP) · airframe 32,327 hrs · 12,722 cycles

SAL - BC6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY AT INBOARD END OF LEFT INBOARD FLAP AT RIB 1. REPLACED TORSION SUPPORT ASSEMBLY AT INBOARD END OF LEFT INBOARD FLAP AT RIB 1 IAW CMM 57-52-21.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 32,327 hrs · 12,722 cycles

SAL - BC6 - EES - LOW PRESSURE DAMPER AT DOOR 842. CHARGED DAMPER AT DOOR 842 & PERFORMED LEAK TEST IAW A319 AMM 52-10-00.

Part: SUPPORT — WORN (TE FLAP) · airframe 32,327 hrs · 12,722 cycles

SAL - BC6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY AT INBOARD END OF RIGHT INBOARD FLAP AT RIB 1. REPLACED TORSION SUPPORT ASSEMBLY AT INBOARD END OF RIGHT INBOARD FLAP AT RIB 1 IAW CMM 57-52-21.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,256 hrs · 12,171 cycles

FLT 679 - PHX-BOI - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT ON SEAT 1C IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) IN FORWARD GALLEY PER MAINTENANCE MANUAL 33-51-38-401. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 30,962 hrs · 12,051 cycles

LOGPAGE:4501176 - FLT 321 - LAS-ORD - EMERGENCY LIGHTS - FLOOR LEVEL LIGHT AT 20ABC FOR EMERGENCY LIGHT IS INOPERATIVE. FOUND ONE WIRE PULLED FROM WALL CONNECTOR AT SEAT 20ABC. REMOVED AND REPLACED CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (CABIN) · airframe 30,845 hrs · 11,993 cycles

LOGPGE:8444354 - FLT 486 - PHX-DEN - EMERGENCY LIGHTS - EMERGENCY EXIT SIGN LENS MISSING OVERHEAD CENTER AISLE ROW 9. REPLACED LENS COVER EMERGENCY EXIT SIGN OVERHEAD CENTER AISLE, ROW 9. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 29,031 hrs · 11,186 cycles

LOG PAGE 4329007 FLT NR 536 SEA-PHX EMERGENCY LIGHTS AT 18L ARE INOPERATIVE. FOUND BULKHEAD CONNECTOR DISCONNECTED. RECONNECTED CANNON PLUG. OPS CHECK WAS GOOD.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 28,223 hrs · 10,815 cycles

FLT 350 PHX-LAX - BURNING SMELL - COFFEEMAKER WILL NOT BREW. COFFEEMAKER WENT OFF AND THERE WAS A SMELL OF WIRE BURNING. NO SMOKE WAS DETECTED. MAINTENANCE REMOVED AND REPLACED THE COFFEEMAKER. OPERATIONAL CHECK WAS GOOD. (A)

Part: EPSU — FAULTED (EMERGENCY LIGHTS)

PHX - THE LEFT, MID-CABIN, EMERGENCY POWER SUPPLY UNIT FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED THE LEFT, MID-CABIN, EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK.

Part: CONTROL UNIT — FAILED (SMOKE DETECTION) · airframe 25,055 hrs · 9,520 cycles

PHX - OTH - LOG NR 7809886 - MX REPORTED SMOKE LAV AND CARGO DET FAULT ON ECAM. MX REPLACED THE SDCU, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 23,029 hrs · 8,691 cycles

ATL - EEL - FOUND EMERGENCY POWER SUPPLY UNIT FWD LEFT INOP. MX REMOVED AND REPLACED EPSU AND BATTERY IAW REF AMM 33-51-38-000-001, 33-51-38-400-001 AND 33-51-38-400-2, OPERATIONAL CHECK WAS NORMAL.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 21,598 hrs · 8,085 cycles

LAX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE AFT ESCAPE PATH LIGHT WAS INOP. MX RESECURED THE WIRE FOR THE AFT EMERGENCY ESCAPE PATH LIGHTS. OPS CHECK WAS GOOD.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B - 04. NR 5944831. FLOOR PANEL NR 162 EF AFT. CARGO COMPARTMENT WAS FOUND WITH DELAMINATION. FLOOR PANEL NR 162 EF WAS REPLACED IAW IRM 9701 REV 8 SRM 53 - 02 - 00 PAR 8 G,H.

Part: FLOOR PANEL — PERFORATED (CARGO BAY) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 151 GE OF THE AFT CC WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 GE OF THE AFT CC WAS REPAIRED IAW SRM 53-02-00 PAR 8C.

Part: FLOOR PANEL — PERFORATED · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 151 HE OF THE AFT CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 151 WAS REPAIRED IAW SRM 53 - 02 - 00.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 131 BF OF FWD CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 BF OF FWD CC WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

TEMPORARY REPAIR ON FWD CC FLOOR PANEL NR 131 CG. FLOOR PANEL NR 131 CG WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B-04. NR 5944856. THE FLOOR PANEL NR 151 BE ON THE AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 BE IN AFT. CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (CARGO BAY) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 132 EG OF FWD CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 132 EG OF FWD CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (CARGO BAY) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 132 DG IN FWD CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 132 DG IN FWD CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 152 XE IN AFT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 152 XE IN AFT WAS REPAIRED IAW SRM 53-02-00 PAR 8C C21.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 151 PE WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 PE WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 151 VG IN AFT CARGO COMPARTMENT WAS FOUND WITH DISBONDED DOUBLER. THE FLOOR PANEL NR 151 VG WAS REPLACED IAW SRM 53 - 02 - 00 PAR 8G, 8H, AND IRM 9701 REV F PROTECTIVE DOUBLER WAS BONDED IAW ER NS 26 - 5326 - 05209 - RC1C PAR 1G AND AWA CARD M2M53301 REV B.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 131 EG IN FWD CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 EG WAS REPAIRED IAW SRM 53 - 02 - 00 PARA 8 C. (2).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4 NO NR. 5945288. CORROSION LOCATED ON FLOORBEAM - Y 765 PASSENGER CABIN FRAME 64 + 10". FLOORBEAM WAS REPLACED IAW SRM A319 51 - 42 - 11 AND 51 - 72 - 11 LOCATED BETWEEN FR 64 TO FR 66 - Y 765 PASSENGER CABIN FLOOR STRUCTURE.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

DENT IN A/C LEFT BEHIND BOARDING DOOR. PERFORMED PERMANENT REPAIR LOCATED FS 23 + 2.5 ", STRINGER 23L IAW SRM A319 53-00-11 PAGE 219 - 220 FIG 204, MEASURED OF DOUBLER L = 9.5 " W = 8. 25 ".

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

FOUND CORROSION ON FLOORBEAM Y 765 FS 16 PAX CABIN. SEATTRACK LDC ON PAX CABIN Y 765 FROM FS 12 TO FS 24 WAS REMOVED AND REPLACED IAW SRM A319 51-42-11 AND SRM A319 51-72-11. BECAUSE AFTER IT HAD BEEN REWORKED AND WAS FOUND OUT OF LIMITS IAW SRM A319 53-11-15 FIG 102 PAGES 105/ 106.

Part: PLATE — LIGHTNING STRIKE (FUSLAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5945020. LIGHTNING STRIKE ON BLANKING PLATE OF STATIC PORT EXTERNAL FUSELAGE AT FRAME 4 - 0.5" , Z + 67CM. REWORKED AREA ON BLANKING PLATE OF STATIC PORT, FRAME 4 - 0.5" L/H SIDE IAW ER NO. 25 - 5311 - 06184 - 553 (Z + 67 CM APPROX.) GRAY DOT APPLIED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945123. CORROSION ON FLOORBEAM Y - 1292 FR 20 PASSENGER CABIN. SEAT TRACK LOCATED Y - 1292 BETWEEN FR 12 TO FR 24 REPLACED IAW SRM A319 51 - 72 - 11 SEAT TRACK CORRODED WAS EVALUATED AND FOUND OUT OF LIMITS IAW SRM A319 53 - 11 - 15 FIG 102 PAGES 105 - 106.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 151 Z6 WAS FOUND WITH MISSING MATERIAL. FLOOR PANEL NR 151, Z6 WAS REPLACED IAW IRM 9701 REV F AND SRM 53-02-00 PAR 86, 8H.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 151 DE WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 DE WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.

Part: PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FOUND LIGHTNING STRIKE ON RIVER EXTERNAL FUSELAGE AT FRAME 5L Z55 CM APPROX. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE FRAME 5L Z55 CM APPROX IAW SRM A319 53-00-11 PNG 353 TO 362 FIG 223 SHEET 2 AND FASTENER REPLACED IAW SRM A319 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,624 cycles

FOUND CORROSION LOCATED ON FLOORBEAM - Y 1292 PASSENGER CABIN FRAME 66. REWORKED AREA FOUND OUT OF LIMITS IAW SRM A319 53-00-14 FIG 102 PAGE 106 AND FLOORBEAM - Y 1292 BETWEEN FS 64 TO FS 66 WS REPLACED IAW SRM A319 51-72-11 PAGE 1 AND PAGE 2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NO. B-04. NR NO. 5944842. FLOOR PANEL NO. 151 CE WAS FOUND WITH PERFORATION IN AFT. CARGO COMPARTMENT. FLOOR PANEL NO. 151 CE WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945286. CORROSION LOCATED ON FLOORBEAM - Y 1292 PASSENGER CABIN FR 67 + 17" FRAME 68" , AND FRAME 68 + 2" (3 POINT). REWORKED AREAS FOUND OUT OF LIMITS IAW SRM A319 53 - 00 - 14 FIG 102 PAG 106 AND FLOORBEAM - Y 1292 BETWEEN 67 + 10 TO FR 69 WAS REPLACED IAW SRM A319 51 - 72 - 11 PAG 1/2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 151 FE WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 FE WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 200,623 hrs · 7,674 cycles

FOUND LIGHTNING STRIKE, FLOOR PANEL ON RIVET EXTERNAL FUSELAGE AT FRAME 2L 2171 CM APPROX. PERFORMED PERMANENT REPAIRS ON EXTERNAL FUSELAGE FRAME 2L Z + 71 CM APPROX IAW SRM A319 53-00-11 PAGE 353 TO 362 FIG 223 SHEET 2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B-04. NR 5945421. FLOOR PANEL NR 131 DG WAS FOUND WITH PERFORATION IN FWD. CARGO COMPARTMENT. FLOOR PANEL NR 131 WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FOUND FLOOR PANEL NR 131 DF WAS FOUND WITH PERFORATION IN FWD CC. FLOOR PANEL NR 131 WAS REPAIRED IAW SRM 53-02-00 PARA 8C 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

CORROSION LOCATED ON SEAT TRACK - Y 765 FROM FS 41 + 5" FS 45 + 16". REPLACED SEAT TRACK ON - Y 765 FROM FS 41 FS 47 IAW SRM A319 51 - 72 - 11 AND SRM A319 51 - 42 - 11 PAR 7 EVALUATED AND WAS FOUND OUT OF LIMITS IAW SRM A319 53 - 31 - 75 PAGE 107 FIG 103.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B-04. NR 5944833. THE FLOOR PANEL NR. 161 FF OF AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NR 161 FF AFT. CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 161 BF OF AFT CC WAS FOUND WITH PERFORATION. THE PANEL NR 161 BF IN 2FT CC WAS REPAIRED IAW SRM 53-02-00 PARA 8C 2 FIG 204.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - NR NR 5944810. DURING B - 04 CHECK THE FLOOR PANEL NR 131 CF OF FWD. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 CF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C 2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

THE FLOOR PANEL NR 162 FF OF AFT CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 162 FF WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2 FIG 204.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 152 WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 152 WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B - 04. NR 5944858. FLOOR PANEL NR 151 TG OF THE AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NO. 151 TG WAS REPLACED IAW IRM 9701 REV. I AND SRM 53 - 02 - 00 PAR 8H - 8G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B-04. NR 5944859. THE FLOOR PANEL NR 152 TG OF THE AFT. CARGO COMPARTMENT WAS FOUND WITH DELAMINATION. THE FLOOR PANEL NR 152 TG WAS REPLACED IAW IRM 9701 REV. F AND SRM 53 - 02 - 00 PAR 8G, 8H.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC - 4. NR 5945409. CORROSION LOCATED ON PLATE SHEAR PASSENGER CABIN BETWEEN FRAME 69 TO FR 70 STRINGER 23R. SHEAR PLATE LOCATED ON PASSENGER CABIN BETWEEN FR 69 TO FR 70 STRINGER 23R WAS REPLACED AND INSTALLED IAW SRM A 319 51 - 72 - 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC - 4. NR 5945287. CORROSION LOCATED ON FLOORBEAM Y 1292 PASSENGER CABIN FR 68. (1 POINT). MAINTENANCE REWORKED AREA AND FOUND OUT OF LIMITS IAW SRM A 319 53 - 00 - 14 FIG 102 PAG 106 AND FLOORBEAM Y 1292 BETWEEN FR 68 TO FR 69 WAS REPLACED IAW SRM A319 51 - 72 - 11 PAG 1/2.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,624 cycles

THE FLOOR PANEL NR 161 EF OF AFT CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 161 EF OF AFT CC WAS FOUND WITH PERFORATION, WAS REPAIRED.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - FLOOR PANEL NR 151 UG WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 UG WAS REPAIRED IAW SRM 53-02 -00 PAR 8C 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 206,230 hrs · 76,740 cycles

SAL - MAJOR REPAIR - CHECK NO. BC-4. NR NR 5945290. CORROSION LOCATED ON FLOORBEAM Y 1292 PASSENGER CABIN FR 67, FR 67 + 4", FR 67 + 8" (3 POINT). REWORKED AREA FOUND OUT OF LIMITS IAW SRM A319 53 - 00 - 14 FIG 102 PAG 106 AND FLOOR BEAM Y 1292 BETWEEM FR 66 TO FR 68 WAS REPLACED IAW SRM 51 - 72 - 11 PAG 1/2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

FOUND CORROSION LOCATED ON FLOORBEAM - Y 1292 PAX CABIN FRAME 66 + 13 " AND FRAME 67 + 11 ". CORROSION LOCATED ON FLOORBEAM - Y 1292 PAX CABIN FRAME 66 + 13 " AND FRAME 67 + 11 " WAS REPLACED IAW SRM A379 51-72-11.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FLOOR PANEL NR 161 CF WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 161 CF WAS REPAIRED IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 76,740 cycles

SAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5944998. CORROSION LOCATED ON SEAT TRACK FRAME 43 + 3" AND FRAME 46-4" (2 POINT). SEAT TRACK LOCATED BTW FR 41 TO FR 47 OUTBOARD Y 1292 WAS REPLACED IAW SRM A379 51 - 72 - 11 PAG 42 AND IAW SRM A319 53 - 31 - 75 FIG 103.

Part: FLOOR PANEL — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC - 4. NR NO. 5945214. CORROSION ON FLOOR PANEL OF FWD PASSENGER CABIN ON LOWER RIGHT CREW DOOR. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 222 FF BETWEEN FR 16 TO FR 20 AND WAS INSTALLED WITH AWA CARD CID25306. JOG 89.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR- CHECK NR BC-4. NR 5945412. CORROSION LOCATED ON FLOOR PANEL NR 261 FF BETWEEN FRAME 66 TO FRAME 68 LEFT SIDE PASSENGER CABIN. REMOVED AND REPLACED FLOOR PANEL 261 FF BETWEEN FR 66 TO FR 68 AND WAS INSTALLED WITH AWA CARD CID 255318. SEQ 97.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR B-04. NR 5944836. FLOOR PANEL NR 161 CF WAS FOUND WITH PERFORATION IN AFT. CARGO COMPARTMENT. FLOOR PANEL NR 161 CF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).

Part: PLATE — LIGHTNING STRIKE (NACELLE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC - 4. RN NR 5945019. LIGHTNING STRIKE ON BLANKING PLATE ON STATIC PORT EXTERNAL FUSELAGE AT FRAME 4 - 0.5 Z + 62 CM. REVLORED AREA ON BLANKING PLATE OF STATIC PORT FRAME 4 - 0.5 + Z + 62 CM. APPROXIMATELY SIDE LH ER NO. 25 - 5311 - 06189 - 353.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - FOUND CORROSION LOCATED ON FLOOR PANEL NR 261 FF BETWEEN FRAME 66 TO FRAME 68 LEFT SIDE PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261 FF BETWEEN FS 66 TO FS 68 AND INSTALLED WITH AWA CARD CID25318 SEQ 97.

Part: PLATE — CORRODED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FOUND CORROSION LOCATED ON SHEAR PLATE PASSENGER CABIN BETWEEN FS 69 TO FS 70 STRINGER 23 L. CORROSION LOCATED ON SHEAR PLATE PASSENGER CABIN BETWEEN FS 69 TO FS 70 STRINGER 23 L WAS REPLACED AND INSTALLED IAW SRM A319 51-72-11, PAGE 1 - 2.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945413. CORROSION ON FLOOR PANEL NR 262 FF BETWEEN FRAME 66 TO FRAME 68 RIGHT SIDE PASSENGER CABIN. MAINTENANCE REMOVED AND REPAIRED FLOOR PANEL 262 F BETWEEN FR 66 TO FR 68 AND INSTALLED WITH AWA CARD CID 25318 SEQ 97.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945415. DELAMINATION LOCATED FLOOR PANEL NR 251 SF BETWEEN FRAME 58 TO FRAME 62 PASSENGER CABIN. FLOOR PANEL NR 251 SF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 3.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

DELAMINATION LOCATED FLOOR PANEL NR 251 SF BETWEEN FRAME 58 TO FRAME 62 PASSENGER CABIN. FLOOR PANEL NR 251 SF WAS REPAIRED IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5945414. DELAMINATION LOCATED ON FLOOR PANEL LOWER SILL DOOR L2 FR 68 LEFT SIDE. REMOVED AND REPLACED FLOOR PANEL LOWER SILL DOOR FR 68 LEFT SIDE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC-4. NR 5944992. CORROSION LOCATED ON SEAT TRACK - Y 1292 (3 POINT) FRAME 42 + 8" - FR 42 + 16.5" - FR 44 + 8". SEAT TRACK - Y 1292 BETWEEN FR 41 TO FR 51 REPLACED IAW SRM A319 51 - 72 - 11 PAG 1 AND PAG 2, SEAT TRACK EVALUATED AND IS OUT OF LIMIT IAW SRM 53 - 31 - 15 PAG 107 FIG 103.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,623 hrs · 7,674 cycles

FOUND CORROSION LOCATED ON SEAT TRACK Y - 1292 FS 39 - 2 INS SEAT TRACK Y - 1292 BETWEEN FS 36 TO FS 41 REPLACED IAW SRM A319 51-72-11 PAX 1, 2, SEAT TRACK EVALUATED AND IS OUT LIMIT IAW SRM A319 53 - 31 - 15 PAX 102 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

FOUND CORROSION LOCATED ON SEAT TRACK - Y 1292 (3 POINT) FRAME 42 + 8 IN - FS 42 + 16.5 IN - FS 44 + 8 INCH SEAT TRACK - Y 1292 BETWEEN FS 41 TO FS 51 REPLACED IAW SRM A319 51 - 72 - 11 PAGE 1 AND SRM 53 - 31 - 15 PAGE 107 FIG 103.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,623 hrs · 7,674 cycles

SAL - MAJOR REPAIR - CHECK NR BC -4. NR 5945416. CORROSION LOCATED ON FLOOR PANEL LOWER SILL DOOR R2 FRAME 68 RIGHT SIDE PASSENGER CABIN. REMOVED AND REPLACED FLOOR PANEL LOWER SILL R2 DOOR FR 68 RIGHT SIDE PASSENGER CABIN IAW SRM 5/ 7211.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 20,223 hrs · 7,508 cycles

ATL - EEL - MAINTENANCE REPORTED THAT THE FORWARD GALLEY EMERGENCY LIGHT, POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY LIGHT EMERG LIGHT POWER SUPPLY IAW AWA TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD.

Part: FMU — MALFUNCTIONED (NR 1 ENGINE) · airframe 15,102 hrs · 5,531 cycles

BOS - ABORTED TAKEOFF - FLT 0068 - ON TAKEOFF AT BOS EN ROUTE FOR PHX RECEIVED ECAM INDICATIONS, ENG 1 FADEC, ENG 1 COMPRESSOR, ENG 1 FAIL, ENG 1 FUEL CTRL FAULT. REJECTED TAKEOFF AT LOW SPEED. MAINTENANCE TROUBLESHOT AND REPLACED NR 1 ENGINE FUEL METERING UNIT (FMU) IAW T/C R5M73308, LEAK AND OPERATIONAL CHECK WAS GOOD. TEAR DOWN REPORT CONFIRMED FAULT. TESTED UNIT IAW CMM BASIC. PERFORMANCE OF FMU CONSIDERED UNACCEPTABLE WITH DETERATION BEING ATTRIBUTED TO HEAVY FUEL LACQUER IN MAIN INLET FILTER. AFTER REPLACING MAIN INLET FILTER, PERFOMANCE OF THIS FMU RESTORED TO ACCEPTABLE LIMITS.

Part: ACTUATOR — FAILED (NR 1 ENGINE VSV) · airframe 14,320 hrs · 5,259 cycles

ON TAKEOFF AT EWR EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "ENG 1 COMPRESSOR VANE FAILURE", REJECTED TAKEOFF AT 68 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED HIGH POWER ASSURANCE TEST, NR 1 ENGINE CHECKED GOOD. FUNCTIONAL TEST OF VSV ACTUATOR CONFIRMED REASON FOR REMOVAL. TEST REVEALED FAULTS WITH LINEAR VARIABLE DISPLACEMENT TRANSMITTER BONDING RESISTANCE AND VOLTAGE, PISTON VELOCITIES, AND INTERNAL LEAKAGE. DISASSEMBLY FOUND A DEFECTIVE TORQUE MOTOR, LACQUER LEVEL 3 ON FILTER SCREENS, AND SEVERAL WORN SEALS. REPLACED ALL DEFECTIVE PARTS, CALIBRATED VOLTAGES, CLEANED THE PISTON AND SLEEVE ASSEMBLIES, AND PERFORMED FINAL TEST IAW CMM.

Part: SELECTOR VALVE — FAILED (ZONE 140) · airframe 11,741 hrs · 4,456 cycles

PHX - AIR TURNBACK - FLT 0251 - AFTER TAKEOFF FROM PHX EN ROUTE TO MSP RECEIVED ECAM MESSAGE LG LGCIU 2 FAULT, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL AND INTERFACE FACE UNIT (LGCIU) NR 2 (5GA2) IAW AMM 32-31-71. AIRMAN INDICATED A HARD FAULT FOR LANDING GEAR SELECTOR VALVE (40GA). REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-31-12. JACKED AIRCRAFT AND PERFORMED LANDING GEAR OPERATIONAL CHECK, CHECK WAS GOOD.

Part: ODOR — DETECTED (COCKPIT/CABIN) · airframe 11,483 hrs · 4,371 cycles

AN ELECTRICAL BURNING ODOR OBSERVED IN THE COCKPIT & CABIN NEAR SEAT ROW 4, DECLARED EMERGENCY, LANDED WITHOUT FURTHER DIFFICULTIES. MX REMOVED AFT WALL OF FWD BAG PIT & INSPECTED RECIRCULATION FANS & DUCTING FOR EVIDENCE OF OVERHEATING & ODOR, NO DEFECTS NOTED. DUE TO FAILURE HISTORY: REPLACED AVIONICS COOLING FAN (18HQ) IAW AMM 21-26-51-401, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF AVIONICS COOLING FAN CONFIRMED FAILURE, BEARING NOISE COULD BE HEARD DURING TEST. R & R WORN BEARINGS & BALANCED ROTOR & MOTOR IMPELLER IAW CMM. RE-TEST OF UNIT GOOD.

Part: FLASHLIGHT — INOPERATIVE (ZONE 900) · airframe 11,483 hrs · 4,371 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: BALLAST — OVERHEATED (SEAT ROW 16 LT) · airframe 9,458 hrs · 3,648 cycles

ON CLIMBOUT FROM SAN EN ROUTE FOR LAS AT 20,000 FT, FLT ATTENDANT REPORTED A STRONG ELECTRICAL BURNING ODOR IN MID TO AFT CABIN, DIVERTED TO LAX. MAINTENANCE FOUND CABIN LIGHTING BALLAST AT SEAT ROW 16 LT EXTREMELY HOT. REMOVED AND REPLACED BALLAST, PERFORMED ENGINE RUN OPERATING BOTH A/C PACKS, INSPECTED ALL LIGHTING AND ELECTRICAL BOXES, NO BURNING ODOR NOTED. OPERATIONAL TEST OF LIGHT BALLAST SEAT ROW 16 LT WAS GOOD.

Part: HOUSING — DEFECTIVE (RT OVERWING EXIT) · airframe 9,164 hrs · 3,534 cycles

EMERGENCY LIGHT FLASHING ON AND OFF AT RT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT HOUSING AT THE RT OVERWING EXIT, OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CORRODED (RT PYLON) · airframe 9,160 hrs · 3,532 cycles

MCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054; INSTALLED REPAIR PART IAW A319 SRM 54-50-00 PG 106 FIG 104.

Part: SKIN — CORRODED (LT PYLON) · airframe 9,160 hrs · 3,532 cycles

MCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 22-23.

Part: THERMOCOUPLE — DEFECTIVE (NR 2 ENGINE) · airframe 8,450 hrs · 3,269 cycles

ON DESCENT WITH AUTO THROTTLE ON 11,000 FT, NR 2 ENGINE SPOOLED NORMALLY TO MAINTAIN MANAGED SPEED, NR 1 ENGINE DID NOT SPOOL FOR 3 TO 4 SECONDS. NR 1 ENGINE WENT TO CLIMB THRUST RESULTING IN SUBSTANTIAL YAW (3 TO 5 DEG) ROLL OF 2 TO 3. ON IDLE DESCENT 6000 FT NR 1 ENGINE FUEL FLOW 800, NR 2 ENGINE 1450 WITH HIGH N1, N2 & EPR. TURNED OFF AUTO THROTTLES, APPROACH & LANDING NORMAL. MX TROUBLESHOT SYS USING TSM 73-00-00-810-877 AND FOUND NR 2 ENGINE IDLING HIGH. MX FOUND FADEC NR 2 A & B FAULTS FOR FUEL TEMP SENSOR (4017KS). REMOVE & REPLACED NR 2 ENGINE FUEL TEMP SENSOR. OPS & LEAK CHECK GOOD. AUTO FLT SYS & FADEC INDICATE NO FAULTS. PERFORMED HIGH POWER ASSURANCE TEST, OPS NORMAL & ALL PARAMETERS MATCH.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,133 hrs · 3,152 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS LEFT ON 2 HOURS AFTER CREW LEFT. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS, ZONES 221, 241, 242, AND 263. FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 5,673 hrs · 2,227 cycles

PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 14, 17, AND 20 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-04, OPERATIONAL CHECK WAS GOOD.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 3,438 hrs · 1,332 cycles

DEN - AIR TURNBACK -C - WHILE EN ROUTE ACFT RECEIVED ECAM MESSAGE FOR VENT SKIN FAULT. DURING TURN AT DEN DEACTIVATION OF THE VENT SKIN AIR VALVE WAS ACCOMPLISHED. UPON TAKEOFF FROM DEN TO LAS ECAM MESSAGE REAPPEARED AND ACFT WOULD NOT PRESSURIZE, ACFT TURNED BACK TO DEN AND MADE UNEVENTFUL LANDING. MX TROUBLESHOT SYSTEM & FOUND VENT SKIN AIR VALVE IN OPEN POSITION. DEACTIVATION OF VENT AIR SKIN VALVE IN CLOSED POSITION WAS CORRECTLY RE-ACCOMPLISHED AND CPC TEST 1 AND 2 WAS PERFORMED WITH NO DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE. REPLACED THE VENT SKIN AIR VALVE. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: RELIEF VALVE — RUPTURED (CENTER TANK) · airframe 566 hrs · 226 cycles

CMH - DIVERTED FLIGHT - 2/14/01 - EN ROUTE FROM PHL TO PHX THE CREW GOT AN ECAM AUTO FUEL FAULT. SELECTED MANUAL AND NOTICED FLASHING QUANTITY NR 2 MAIN AND OUTBOARD RESERVE AND DECREASING FUEL QUANTITY IN NR 1 MAIN; TRIED NR 1 FUEL PUMPS OFF, DECREASE CONTINUED; FLIGHT WAS DIVERTED TO CMH. IN CMH, MAINTENANCE FOUND THE CENTER TANK OVERPRESSURE PROTECTOR RUPTURED; IT WAS REPLACED AND CHECKS WERE GOOD.