N831AW

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN LATERAL EMERGENCY EXIT LIGHT ON LOWER DOOR FRAME 841 AT FWD GAL LEY AREA (1EA). MAINTENANCE REPLACED LATERAL EMERGENCY EXIT LIGHT ON LOWER DOOR FRAME 841 AT FWD GALLEY AREA (1EA) IAW A320FAM 33-51-13-000-001-A.

Part: HINGE FITTING — CRACKED (ZONE 700) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON MLG FWD HINGE FITTING RH SIDE, AFT LUG POSITION. CRACK LENGTH IS L= 0.180 INCH. MAINTENANCE REPLACED MLG FWD HINGE FITTING RH SIDE IAW EA 369995 AND REPAIR DWG R53370500 ISSUE F, A319 SRM 51-42-11-801 AND SRM 51-72-11-911-001.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: WINDSHIELD FRAMING AT LH CENTER POST WAS FOUND CRACKED IN AREA A (UPPER POCKET). MAINTENANCE REPLACED CONTINUITY FITTING LH SIDE ON WINDSHIELD LOWER ATTACHMENT PER EA 369300.

Part: ATTACH FITTING — EXCESS PLAY (ZONE 600 FLAP) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-72-11.

Part: ATTACH FITTING — EXCESS PLAY (ZONE 500) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-72-11.

Part: SPIGOT — CORRODED (ZONE 400) · corrosion level 2 · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LT PYLON L= 4.340 INCH, W= 1.547 INCH D= 0.005 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE OF LT PYLON IAW A319 SRM 54-51-12-300-002.

Part: PLATE — CORRODED (ZONE 400) · corrosion level 2 · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING RETAINING PLATE PER SRM 54-51-12-300-002.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING HINGE FITTING #3 ON HORIZONTAL STABILIZER RH. MAINTENANCE REPLACED HINGE ARM 3 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING HINGE FITTING #5 ON HORIZONTAL STABILIZER RH. MAINTENANCE REPLACED HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING HINGE FITTING #6 ON HORIZONTAL STABILIZER RH. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING HINGE FITTING #2 ON HORIZONTAL STABILIZER RH. MAINTENANCE REPLACED HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION THRESHOLD SHEET IN AFT CARGO COMPARTMENT MEASURE OF CORROSION ARE: L=10.00INCH W=4.34INCH ,D= 0.050INCH. MAINTENANCE REPLACED THRESHOLD SHEET IN AFT CARGO COMPARTMENT IAW A319 SRM 51-72-11-911-001, DWG D53475500 AND DWG E53476320.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING HINGE FITTING #4 ON HORIZONTAL STABILIZER RH. MAINTENANCE REPLACED HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L LOC. BTW FR 69 TO FR 70. CRACK L:1.56 INCH AT GALLEY AREA. MAINTENANCE REPLACED SHEAR PLATE STR 23 L LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001 AND DWG D53474180.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE OF CRACK L= 0.890 INCH. MAINTENANCE REPLACED SHEAR PLATE STR 23 R LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001 AND DWG D53474180.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L LOC. BTW FR 69 TO FR 70. CRACK L:1.56 INCH AT GALLEY AREA. MAINTENANCE REPLACED SHEAR PLATE STR 23 L LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001 AND DWG D53474180.

Part: LIGHT — BROKEN (ZONE 800) · airframe 70,716 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN LATERAL EMERGENCY EXIT LIGHT ON LOWER DOOR FRAME 832 AT AFT GAL LEY AREA (1EA). REPLACED LATERAL EMERGENCY EXIT LIGHT ON LOWER DOOR FRAME 832 ATAFT GALLEY AREA (1EA) I.A.W A320FAM AMM 33-51-13-000-001-A STEP 1 THRU 4.A (1) AND A320FAM AMM 33-51-13-400-001-A STEP 1 THRU 4.A (1) THRU (3), 4.D AND 4.F TEST IS OK. ATTACHED FORM ME 0470.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER TENSION BOLT POSITION LH, CRACK LENGTH 0.127 INCH APPROX AND CRACK DIRECTION 1 C LOCK LOOKING INBOARD. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOCATED ON CENTER WINDSHIELD FRAMING POCKET AREA RH SIDE MIRROR FITTING REPAIR IAW EA 369300.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 70,715 hrs · 34,055 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER TENSION BOLT POSITION LH, CRACK LENGTH 0.127 INCH APPROX AND CRACK DIRECTION 1 C LOCK LOOKING INBOARD. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOCATED ON CENTER WINDSHIELD FRAMING POCKET AREA LH SIDE MIRROR FITTING REPAIR IAW EA 369300.

Part: BULB — BURNED OUT (ZONE 200) · airframe 70,486 hrs · 33,909 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY EXIT LIGHT HAS A BULB BURNT OUT. MAINTENANCE RE-LAMPED AS REQUIRED FUNCTIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 69,762 hrs · 33,433 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FA JUMPSEAT FLASHLIGHT BROKEN. MAINTENANCE REPLACED FLASHLIGHT BATTERIES REF IPC 25-63-53-01.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 69,621 hrs · 33,340 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU INT LOAD FWD L FAULT DURING OPS CHECK OF EPSU BY BITE TEST. MAINTENANCE REPLACED EPSU 11WL PER AMM33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 69,621 hrs · 33,340 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU INT LOAD FWD L FAULT DURING OPS CHECK OF EPSU BY BITE TEST. MAINTENANCE REPLACED EPSU 10WL PER AMM33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 69,621 hrs · 33,340 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU INT LOAD FWD L FAULT DURING OPS CHECK OF EPSU BY BITE TEST. MAINTENANCE REPLACED EPSU 10WL PER AMM33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 69,621 hrs · 33,340 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU INT LOAD FWD L FAULT DURING OPS CHECK OF EPSU BY BITE TEST. MAINTENANCE REPLACED EPSU 11WL PER AMM33-51-38.

Part: LIGHT — NO TEST (ZONE 200) · airframe 69,508 hrs · 33,265 cycles

AIRCRAFT WAS GROUNDED: SEAT 1C EMERGENCY LIGHT INOP. MAINTENANCE REPLACED FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT PER AMM 33-51-00 AND CMM 25-20-85.

Part: BRAKE SYS — DEFECTIVE (ZONE 700 - GEARS) · airframe 65,757 hrs · 30,853 cycles

AIRCRAFT WAS NOT GROUNDED: ON TAKE OFF ROLL AIRCRAFT PULLED TO THE RIGHT. AIRCRAFT PULLS TO THE RIGHT AT HIGH SPEEDS. MAINTENANCE BLEED THE RIGHT MAIN LANDING GEAR BRAKES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PRESSURE SWITCH — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 65,549 hrs · 30,713 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DURING APPROACH INTO DFW DUE TO A GREEN HYDRAULIC SYSTEM RESERVOIR LOW AIR PRESSURE ECAM MESSAGE. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 29-11-00-810-816-A AND REPLACED PRESSURE SWITCH 1151GN PER AMM 29-32-12. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SAFETY VALVE — WARNING MESSAGE (ZONE 700 - GEARS) · airframe 65,244 hrs · 30,516 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO RDU: LANDING GEAR DID NOT EXTEND ON FIRST ATTEMPT. ECAM ADVISED TO RECYCLE AND WAIT 120 SECONDS, BUT GEAR STILL DID NOT EXTEND. CREW FOLLOWED ECAM INSTRUCTIONS AND ACCOMPLISHED A GRAVITY EXTENTION OF THE LANDING GEAR. THE AIRCRAFT LANDED SAFELEY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SAFETY VALVE 49GA PER AMM 32-31-17 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: SLIDING WINDOW — CRACKED (ZONE 200 - FUSE) · airframe 65,206 hrs · 30,484 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK LEFT HAND SLIDING WINDOW CRACKED ON TAXI. MAINTENANCE REPLACED SLIDING WINDOW PER AMM 56-12-11.

Part: WIRE — MISROUTED (ZONE 900 - LAV/G) · airframe 64,788 hrs · 30,223 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLT. DURING CRUISE FLIGHT ATTENDANT REPORTED ACRID MUSTY SMELL FROM AFT LEFT LAVATORY. NO ODOR IN FLIGHT DECK. THE AIRCRAFT LANDED SAFELY AT CLT AND AFTER LANDING FIRE CREW DETERMINED IT TO POSSIBLY BE LAVATORY WATER PUMP. MAINTENANCE ACCOMPLISHED THE SMOKE / ODOR / FUME TROUBLESHOOTING TASK CARD AND NO ARCING WAS FOUND AT ANY ELECTRICAL COMPONENTS, ISOLATION ENGINE RUNS FOUND TO BE GOOD WITH NO ODORS NOTED. MAINTENANCE FOUND WIRE ON BACK OF COFFEE MAKER TOUCHING HEATER AND RE-ROUTED WIRES AS REQUIRED.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 64,145 hrs · 29,812 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE FITTING BORE WORN. MAINTENANCE REPLACED HINGE FITTING PER SRM 51-42-11.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 63,883 hrs · 29,646 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN ABOVE R1DOOR HAS BURNED OUT LIGHT BULBS MAINTENANCE REPLACED EXIT SIGN LIGHT AT R1 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: RELAY — DEFECTIVE (FUEL PUMP) · airframe 63,695 hrs · 29,519 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP LEFT HAND SIDE LOW PRESSURE ECAM MESSAGE. MAINTENANCE REPLACED RELAY 41QA PER AMM 28-46-15 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PRESSURE SWITCH — FAULTED (BOOST PUMP) · airframe 63,640 hrs · 29,476 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL LEFT CENTER TANK LOW PRESSURE MESSAGE, CREW TURNED PUMP # 1 CENTER TANK OFF PER ECAM PROCEDURE. MAINTENANCE REPLACED CENTER TANK #1 FUEL PUMP PRESSURE SWITCH PER AMM 28-21-15-40-001-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DEFECTIVE (ZONE 200 - FUSE) · airframe 63,050 hrs · 29,067 cycles

AIRCRAFT WAS NOT GROUNDED: 1L EMERGENCY EXIT LIGHT NEEDS SOME NEW LIGHT BULBS. MAINTENANCE REPLACED L1 DOOR EMERGENCY LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: BATTERY — DISCHARGED (ZONE 200 - FUSE) · airframe 60,960 hrs · 27,817 cycles

AIRCRAFT WAS NOT GROUNDED: COLD AIRCRAFT. WHEN AIRCRAFT POWER APPLIED, EMERGENCY EXIT LIGHTS ARE ON WITH SWITCH OFF. POWER SWITCH LEFT IN ON POSITION ON FLIGHT ATTENDANT PANEL. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 60,111 hrs · 27,338 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SYSTEM TEST FAULTING EMERGENCY POWER SUPPLY UNIT INT LOAD EMERGENCY RIGHT OFF WING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERIES 10WL AND 13WL (AALA202108238145) PER AMM 33-51-38-400-001-A OPERATIONS CHECK'S NORMAL, REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT POWER SUPPLY UNIT (AALA202108236095) PER AMM 33-51-38-400-001-A.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 60,111 hrs · 27,338 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SYSTEM TEST FAULTING EMERGENCY POWER SUPPLY UNIT INT LOAD EMERGENCY RIGHT OFF WING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERIES 10WL (AALA202108227337) AND 13WL PER AMM 33-51-38-400-001-A OPERATIONS CHECK'S NORMAL, REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT POWER SUPPLY UNIT (AALA202108236095) PER AMM 33-51-38-400-001-A.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 60,111 hrs · 27,338 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SYSTEM TEST FAULTING EMERGENCY POWER SUPPLY UNIT INT LOAD EMERGENCY RIGHT OFF WING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERIES 10WL (AALA202108227337) AND 13WL (AALA202108238145) PER AMM 33-51-38-400-001-A OPERATIONS CHECK'S NORMAL, REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT POWER SUPPLY UNIT PER AMM 33-51-38-400-001-A.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT RIGHT OVERWING LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT RIGHT OVERWING PER A320 AMM 33-51-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT FORWARD CABIN OVERHEAD LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT FORWARD CABIN OVERHEAD PER A320 AMM 33-51-16.

Part: SIGN — INOPERATIVE (LT OVERWING) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT LEFT OVERWING LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT LEFT OVERWING PER A320 33-51-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT R1 DOOR LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT R1 DOOR PER A320 AMM 33-51-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT RIGHT MID CABIN LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT RIGHT MID CABIN PER A320 AMM 33-51-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT AFT OVERHEAD LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT AFT OVERHEAD PER A320 AMM 33-51-16.

Part: SIGN — INOPERATIVE (LT CABIN) · airframe 59,941 hrs · 27,267 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN AT LEFT MID CABIN, LAMP NOT ILLUMINATED. REMOVED AND REPLACED EXIT SIGN AT LEFT MID CABIN PER A320 AMM 33-51-16.

Part: O-RING — LEAKING (ZONE 100 - FUSE) · airframe 59,519 hrs · 27,023 cycles

AIRCRAFT WAS GROUNDED: STRONG FUMES/ODOR OF OIL IN CABIN AND COCKPIT ON CLIMB OUT THEN DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTION. FUMES/ODOR RETURNED ON DESCENT, DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTION. EMERGENCY WAS NOT DECLARED. REPLACED SIGHT GLASS (AALA202105119013) AND O-RING PER CMM 49-25-69. RE SERVICED OIL. LEAK CHECK GOOD.

Part: SIGHT GLASS — LEAKING (ZONE 100 - FUSE) · airframe 59,519 hrs · 27,023 cycles

AIRCRAFT WAS GROUNDED: STRONG FUMES/ODOR OF OIL IN CABIN AND COCKPIT ON CLIMB OUT THEN DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTION. FUMES/ODOR RETURNED ON DESCENT, DISSIPATES WITHOUT FLIGHT OR CABIN CREW ACTION. EMERGENCY WAS NOT DECLARED. REPLACED SIGHT GLASS AND O-RING (AALA202105119001) PER CMM 49-25-69. RE SERVICED OIL. LEAK CHECK GOOD.

Part: SUPPORT ANGLE — CORRODED (CARGO DOOR SILL) · airframe 59,398 hrs · 26,955 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO DOOR SILL THRESHOLD FORWARD OF FR 59 SUPPORT ANGLE CORRODED ABOVE AFT LATCH ROLLER. REPLACED SUPPORT ANGLE PER SRM 51-42-11.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 59,398 hrs · 26,955 cycles

AIRCRAFT WAS GROUNDED: RIGHT WING OUT BOARD FLAP OUT BOARD TRAILING EDGE WEDGE LOWER SURFACE IN BOARD END IS DELAMINATED AND SPLIT ON THE TRAILING EDGE. **SUPPLEMENTAL REPORT: REPLACED FLAP TRAILING EDGE WEDGE PER EA 326641

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 59,398 hrs · 26,955 cycles

AIRCRAFT WAS GROUNDED: RIGHT WING OUT BOARD FLAP INBOARD TRAILING EDGE WEDGE LOWER SURFACE OUT BOARD END IS DELAMINATED AND SPLIT ON THE TRAILING EDGE. ** SUPPLEMENTAL REPORT: REPLACED FLAP TRAILING EDGE WEDGE PER EA 326641

Part: HYDRAULIC LINE — CRACKED (RT MLG BRAKE)

AIRCRAFT WAS GROUNDED: FOUND HYD LEAK COMINGFROM R/H BRAKE MANIFOLD ASSY. BRAKE PRESSURE LINE CRACKED NEEDSTO BE REPLACED. REMOVED AND REPLACED RT MLG BRAKE MANIFOLD ASSY PRESSURE LINE IAW AMM 32-42-16.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD LOWER LEFT HAND CONTINUITY FITTING CRACKED. REPACED CONTINUITY FITTING PER EA 300387.

Part: SKIN — DEBONDED (RT WING AILERON) · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON UPPER SKIN DISBONDED. REPLACED AILERON PER AMM 27-14-41.

Part: SLIDE — FAULTY (OVERWING) · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE MAINTENANCE: WORN CLAMP ON RIGHT HAND OFF WING RAMP SLIDE. REPLACED RIGHT HAND OFF WING RAMP SLIDE PER TASK CARD 26C19053012.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE VISIT: CORROSION ON SEAT TRACK AT Y765, 2IN. FWD OF FR16. REMOVED AND REPLACED SEAT TRACK IAW SRM51-42-11AND DRAWING D53112813002.

Part: SEAT TRACK — CORRODED (FRAME 64) · corrosion level 2 · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 64 AND +Y765. REPLACED SEAT TRACK PER AIRBUS DRAWING D5347200000.

Part: SEAT TRACK — CORRODED (FRAME 65) · corrosion level 2 · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 65 AND -Y765. REPLACED SEAT TRACK PER SRM 51-44-11.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,395 hrs · 26,408 cycles

AIRCRAFT IN BASE VISIT: CORROSION AT 2 FLOORBOARD SCREW HOLES ON L2 DOOR SILL PLATE, INBD OF AFT GIRT BAR FITTING LOCATION AT FR68 MINUS 2IN. INSTALLED INTERNAL DOUBLER REPAIR IAW SRM 53-41-15.

Part: GUSSET — CRACKED (LT NACELLE) · airframe 57,919 hrs · 26,130 cycles

AIRCRAFT WAS GROUNDED: LEFT WING PYLON INBOARD GUSSET CRACKED AT RIB 6. REPAIRED GUSSET PER SRM 54-52-12-300-036.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 55,917 hrs · 24,987 cycles

DURING CRUISE, ALL CABIN DOOR EMERGENCY EXIT LIGHTS ILLUMINATED. EMERGENCY EXIT LIGHT SWITCH MOVED TO OFF POSITION HAD NO EFFECT. RESET EMERGENCY EXIT LIGHT SYSTEM IAW AMM 33-50-02. PERFORMED OPS TEST. TESTED OK.

Part: CONTROL VALVE — FAULTED (BRAKE SYS) · airframe 55,495 hrs · 24,732 cycles

REJECTED TAKEOFF FOR MASTER WARNING FULL POWER SET. PARKING BRAKE SET INDICATION. THE AIRCRAFT WAS GROUNDED. REPLACED THE PARKING BRAKE ELECTRICAL CONTROL VALVE PER AMM 32-45-51. OPERATIONS LEAK CHECK GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 54,599 hrs · 24,270 cycles

THE R2 DOOR EMERGENCY EXIT SIGN COVER WAS BROKEN. REPLACED THE SIGN COVER. OK FOR SERVICE IAW AMM 33-51-11.

Part: LAMP — BURNED OUT (HANDLE LIGHT) · airframe 52,463 hrs · 22,992 cycles

EMERGENCY WINDOW HANDLE LIGHT INOPERATIVE ON BOTH SIDE. REPLACED THE LAMP. ACFT OK FOR SERVICE IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,674 hrs · 22,519 cycles

EXIT LIGHT LENS AT THE R2 DOOR IS BROKEN. REPLACED THE LENS.

Part: GCU — FAILED (ZONE 100)

AIRCRAFT WAS GROUNDED, FLIGHT CREW REPORTED ECAM FAULT MESSAGE FOR THE NR 2 ELECTRIC GENERATOR. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO MYR WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE IDG AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 24-21-51-400-810-A; AND REPLACED GCU PER AMM 24-23-34. (SEE AALA201701239014).

Part: IDG — FAILED (NR 2 ENGINE) · airframe 50,784 hrs · 22,059 cycles

AIRCRAFT WAS GROUNDED, FLIGHT CREW REPORTED ECAM FAULT MESSAGE FOR THE NR 2 ELECTRIC GENERATOR. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO MYR WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE IDG AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 24-21-51-400-810-A; AND REPLACED GCU PER AMM 24-23-34. (SEE AALA201701249004).

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 49,940 hrs · 21,576 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT 18A EMERGENCY LIGHT PLUG MISSING. REPLACED WIRING HARNESS AT SEAT ROW ABC FOR EMERGENCY LIGHTING IAW AMM 25-21-41.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 49,933 hrs · 21,574 cycles

AFT CARGO FLOOR PANEL 151ZG DELAMINATED. REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 151ZG IAW AMM 53-42-14.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 47,162 hrs · 20,115 cycles

1L DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,632 hrs · 19,821 cycles

DURING OVERNIGHT INSPECTION FOUND SEAT MOUNTED EMER LIGHTS INOPERATIVE ROWS 5, 7, 12, 15 & 20. R & R EMER LIGHT POWER SUPPLY 11WL TWICE IAW AMM 33-51-38-400. ALSO REPINED EMER LIGHT SEAT ROW 20L IAW AWM 33-51-08. OPERATIONS CHECKED ALL EMERGENCY LIGHTS.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 46,605 hrs · 19,809 cycles

MID LT EMER BATTERY PACK FAILS EMER LIGHT TEST. R & R LT MID EMER LIGHT POWER SUPPLY IAW AMM.33-5138-400-002. SYS OPERATIONAL TESTED GOOD.

Part: APU — LEAKING (APU BAY) · airframe 45,775 hrs · 19,343 cycles

ODOR IN FWD CABIN FROM APU START TO 25000. ODOR REAPPEARS DURING DESCENT THROUGH 10,0000 TILL AT GATE. R & R APU IAW CARD 26L31049005. OPERATIONS CHECKED GOOD.

Part: PACKING — LEAKING (APU) · airframe 45,712 hrs · 19,314 cycles

STRONG OIL MIST ODOR AFTER APU START. FLIGHT SWAPPED TO ANOTHER ACFT FOUND APU THE SOURCE OF CABIN ODOR. REPLACED NR 4 TURBINE CAVITY VENT TUBES PACKINGS IAW JC 26L00021001, 26L00021002 & 26L00021004. ACFT OK FOR SERVICE.

Part: BYPASS VALVE — FAULTY (AC BAY) · airframe 44,378 hrs · 18,565 cycles

EN ROUTE DURING CRUISE, AN AIR PACK 2 REGULATOR FAULT WHILE PACK 1 IS CURRENTLY ON MEL. FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. REMOVED & INSTALLED SERVICEABLE PACK 2 BYPASS VLV IAW AMM 21-61-53-400-001A. LEAK CHECK & OPERATIONS TEST CHECKED GOOD. NO FAULTS NOTED. REMOVED MEL ON PACK 1 WITH THE REPLACEMENT OF ENG 1 10HA1 THERMOSTAT, APU LOAD CONTROL VLV & PACK 1 FLOW CONTROL VLV. ACFT OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 43,508 hrs · 18,040 cycles

EMERGENCY EXIT LIGHT LENS AT SEAT 1C MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS AT SEAT 1C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,036 hrs · 17,398 cycles

THE EMERGENCY LIGHT AT LAVATORY D INOPERATIVE. REPLACED THE EMERGENCY LIGHT AT LAVATORY D IAW MM 33-51-19, OPERATIONS NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 41,720 hrs · 17,264 cycles

DURING CRUISE, CREW RECEIVED A SMOKE DETECTOR FAULT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R LAV "A" SMOKE DETECTOR IAW TSM 23-17-00-810. OPS CHECKED GOOD IAW 26-21-00.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 41,696 hrs · 17,256 cycles

2S CHECK -LOW PRESSURE ON DOOR DAMPER AT PASSENGER/CREW DOOR 831. PERFORMED THE SERVICE OF THE DOOR DAMPER AT PASSENGER/CREW DOOR 831 IAW AMM 52-10-00-614-001-A & PERFORMED LEAK TEST ON DOOR DAMPER, NO LEAK FOUND IAW AMM 52-10-00-790-001-A.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 41,696 hrs · 17,256 cycles

2S CHECK -LOW PRESSURE ON DOOR DAMPER AT PASSENGER/CREW DOOR 832. PERFORMED THE SERVICE OF THE DOOR DAMPER AT PASSENGER/CREW DOOR 832 IAW AMM 52-10-00-614-001-A & PERFORMED LEAK TEST ON DOOR DAMPER, NO LEAK FOUND IAW AMM 52-10-00-790-001-A.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, LOW PRESSURE ON DOOR DAMPER AT PASSENGER/CREW DOOR 841. PERFORMED THE SERVICE OF THE DOOR DAMPER AT PASSENGER/CREW DOOR 841 IAW AMM 52-10-00-614-001-A & PERFORMED LEAK TEST ON DOOR DAMPER, NO FOUND LEAK IAW AMM 52-10-00-790-001-A.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, LOW PRESSURE ON DOOR DAMPER AT PASSENGER/CREW DOOR 842. PERFORMED THE SERVICE OF THE DOOR DAMPER AT PASSENGER/CREW DOOR 842 IAW AMM 52-10-00-614-001-A & PERFORMED LEAK TEST ON DOOR DAMPER, NO LEAK FOUND IAW AMM 52-10-00-790-001-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 222EF BETWEEN FRAMES 16 TO 20 & -Y1292 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-12-00.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON SEATS TRACK BETWEEM FRAMES 36 TO 41, Y765. REPLACED SEATS TRACK IAW SRM 51-72-11 & DWG D57130300.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION ON RT DOOR SILL AT FRAME 66, S23R. REPLACED SILL IAW SRM 51-72-11, DWG D53480505 & EA 504379.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 41 - 46+15", -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53371112 & EA 504381.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON SEATS TRACK BETWEEM FRAMES 41 TO 46+15, Y765. REPLACED SEATS TRACK IAW SRM 51-72-11 & DWG D53371000.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION FOUND ON SEATS TRACK BETWEEM FRAME 36 TO 41, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D57130300.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 24 AND 35, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, PAGE 1-2 AND DWG D53233450.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 36 TO 41, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON LOWER SILL FITTING AT FRAME 19+3.5", S23L. REPLACED LOWER SILL FITTING IAW SRM 51-72-11 & DWG D53110339.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION ON SEAT TRACK AT FRAME 52+5, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53476977 & D53472079.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 24 TO 35, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53374003 & D53110920.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEM FRAMES 41 TO 46+15, Y765. REPLACED SEATS TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON SEATS TRACK BETWEEM FRAMES 36 TO 41, Y1292. REPLACED SEATS TRACK IAW SRM 51-72-11 & DWG D57130147.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON SEATS TRACK BETWEEM FRAMES 41 TO 46+15, Y1292. REPLACED SEATS TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR64, Y765. REPLACED SEAT TRACK BETWEEN FR47/51 TO FR64, Y765 IAW SRM 51-72-11 & DWG D53476977.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, A CRACK FOUND ON FRAME SEGMENT OF LT EMERGENCY EXIT DOOR 834 BETWEEN FRAMES 40 - 41 & BETWEEN BEAMS 1 TO 3. REPLACED FRAME IAW EO 5210Y228.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 161NF BETWEEN FRAMES 59 TO 61 & -Y623 TO Y623. REPLACED FLOOR PANEL IAW SRM 53-12-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 67+15" TO 69", Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53472780.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 162CF BETWEEN FRAMES 59 TO 63 BETWEEN -Y1328 TO -Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 SUP: 53-02-00-201 & IRM 9701, REV G.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, A CRACK FOUND ON FRAME SEGMENT OF RT EMERGENCY EXIT DOOR 844 BETWEEN FRAMES 40-41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME IAW EO 5210Y228.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 161CF BETWEEN FRAMES 59 TO 63 & Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 SUP: 53-02-00-201 & IRM 9701, REV G.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,696 hrs · 17,256 cycles

2S CHECK, CORROSION ON FLOORBEAM COUPLING AT FRAME 67+15", Y1162. REPLACED FLOORBEAM COUPLING IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FRAMES 66-68) · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, DELAMINATION ON FLOOR PANEL 261DF BETWEEN FRAMES 66 TO 68 & -Y765 TO Y765. REPAIRED FLOOR PANEL IAW EA 504378.

Part: HINGE FITTING — WORN (RUDDER) · airframe 41,696 hrs · 17,256 cycles

DURING 2S CHECK, EXCESSIVE PLAY ON RUDDER HINGE BEARING NR 7 AT RUDDER STA 561, RIB 11. REPLACED RUDDER HINGE ARM FITTING NR 7 AT RUDDER STA 561, RIB 11 IAW A319 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 262BG BETWEEN FRAMES 64 TO 66 & -Y1732 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 242DF BETWEEN FRAMES 35 TO 36 & -Y1732 TO -Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, TABLE 103, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251SF BETWEEN FRAMES 58 TO 53 & Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251LF BETWEEN FRAMES 54 TO 58 & Y254 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 241FF BETWEEN FRAMES 36 TO 42 & Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 261BG BETWEEN FRAMES 64 TO 66 & Y765 TO Y1732. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 261AG BETWEEN FRAMES 64 TO 66 & -Y765 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 242FF BETWEEN FRAMES 36 TO 42 & -Y254 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251FF BETWEEN FRAMES 51 TO 54 & -Y254 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 132EG BETWEEN FRAMES 28 TO 34 & Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8H, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,696 hrs · 17,256 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 131EG BETWEEN FRAMES 28 TO 34 & BETWEEN Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00 PAR 8H, FIG 209 & IRM 9701, REV G.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 41,223 hrs · 17,035 cycles

CREW REPORTED THE EMERGENCY FLOOR LIGHTING COVER MISSING AT ROW 10, ACFT RT. MX REPLACED EMERGENCY FLOOR LIGHT LENS COVER AT ROW 10, ACFT RIGHT.

Part: COVER — UNSECURE (CABIN) · airframe 39,977 hrs · 16,454 cycles

CREW REPORTED THE TRIM COVER AT OVERWING AIRCRAFT LEFT NEAR FLOOR NEEDS TO BE RE-ATTACHED. MAINTENANCE RE-SECURED EMERGENCY LIGHT COVER AT LEFT OVERWING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 232FF AT FR21, Z-500, -Y1178. REPLACED FLOOR PANEL 232FF IAW IRM 9701 REV 3.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SHEAR PLATE SUPPORT BETWEEN FR69 TO FR70, Z-500, -Y1162.5. REPLACED RIGHT SHEAR PLATE SUPPORT BETWEEN FR69 TO FR70, Z-500, -Y1162.5 IAW TYPICAL REPAIR TR320-2528-10-0011F & AIRBUS DRAWING 10D53470100.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69, Z-500, Y1169. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, Z-500, Y1169 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16, Z-500, Y765. REPLACED FLOORBEAM AT FR16, Z-500, Y765 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL AT FR67, Z-500, -Y1160. REPAIRED R2 DOOR SILL AT FR67, Z-500, -Y1160 IAW A319 SRM 53-41-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHEAR TIE BETWEEN FR69 TO FR70, Z-500, Y1169. REPLACED LEFT SHEAR TIE BETWEEN FR69 TO FR70, Z-500, Y1169 IAW TYPICAL REPAIR TR320-2528-10-001F.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16, Z-500, Y503.2. REPLACED FLOORBEAM AT FR16, Z-500, Y503.2 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Z-500, -Y765. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Z-500, -Y765 IAW A319 SRM 51-72-11.

Part: SHEAR PIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,821 hrs · 16,384 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1732 IAW TYPICAL REPAIR TR 320-2528-10-001F.

Part: COVER — BROKEN (CABIN) · airframe 39,620 hrs · 16,290 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS COVER BROKEN AT 20L. MAINTENANCE REPLACED LIGHT LENS COVER.

Part: LENS — BROKEN (CABIN) · airframe 39,590 hrs · 16,275 cycles

CREW REPORTED THE EMERGENCY LIGHT COVER AT SEAT 4C BROKEN. MAINTENANCE REPLACED LIGHT LENS COVER AT SEAT 4C. OK FOR SERVICE.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 38,202 hrs · 15,638 cycles

EMERGENCY ESCAPE PATH LIGHT AT 3L INOPERATIVE. REMOVED AND REPLACED HARNESS FROM WALL DISCONNECT TO SEAT DISCONNECT. OPS CHECKED GOOD.

Part: FAN — MALFUNCTIONED (NR 1) · airframe 37,363 hrs · 15,251 cycles

WHILE RETURNING TO FIELD AT PHX DUE TO IECAS (LAV/CARGO SMOKE DETECTOR FAULT), SMELLED ELECTRICAL SMOKE / FUMES IN THE COCKPIT AND THEY WERE DIVERTING TO TUS. FOUND NR 1 CABIN RECIRCULATION FAN CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 RECIRCULATION FAN PER AMM 21-21-50-400-001-1. TESTED NORMAL WITH NO ELECTRICAL SMELL IN CABIN OR FLIGHT DECK AREA.

Part: FLOORBOARD — SEPARATED (CARGO BAY) · airframe 37,283 hrs · 15,209 cycles

RON VISIT - AFT CARGO COMPARTMENT FLOORBOARD SKIN COMING LOOSE AT FR53 TO FR55. REPLACED AFT CARGO COMPARTMENT FLOORBOARD AT FR53 TO FR55 IAW A319 AMM 53-42-12.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 37,171 hrs · 15,151 cycles

LAVATORY E EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: SHEAR PIN — BROKEN (R2 DOOR) · airframe 35,242 hrs · 14,248 cycles

TRIPLE GEAR CHANGE - R2 DOOR HAS BROKEN SHEAR PIN ON DOOR DAMPER PRECUSSION MECHANSIM. REMOVED AND REPLACED SHEAR PIN ON R2 DOOR DAMPER PRECUSSION MECHANISM IAW A319 AMM TASK 52-10-00-610-001 STEP 4B(4).

Part: SHEAR PIN — BROKEN (L2 DOOR) · airframe 35,242 hrs · 14,248 cycles

TRIPLE GEAR CHANGE - L-2 DOOR HAS BROKEN SHEAR PIN ON DOOR DAMPER PRECUSSION MECHANISM. REMOVED AND REPLACED SHEAR PIN ON L-2 DOOR DAMPER PRECUSSION MECHANISM IAW A319 AMM 52-10-00-610-001 STEP 4B(4).

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 34,744 hrs · 14,021 cycles

FLT 630 - PHX-PIT - ODOR - SHORTLY AFTER TAKEOFF, CAPTAIN REPORTED "OILY RAG" SMELL IN COCKPIT. FLIGHT ATTENDANT IN FRONT OF AIRCRAFT ALSO REPORTED SAME SMELL CREW WENT ON OXYGEN AND LANDED SAFELY. FIRST OFFICER EXPERIENCED SLIGHT BURNING SENSATION IN NOSE. PER JOBCARD 4736548, LEFT AIR CYCLE MACHINE (ACM) REPLACEMENT REQUIRED. REMOVED AND REPLACED LEFT ACM PER AMM 21-52-21-400-001-0. OPERATIONAL CHECK GOOD.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 34,444 hrs · 13,888 cycles

FLT 112 - LAS-LAX - EMERGENCY EGRESS SYSTEM - L1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE PER JOBCARD 26L00025010.

Part: EPSU — INOPERATIVE (CABIN) · airframe 34,301 hrs · 13,827 cycles

FLT 396 - LAS-PHX - ABOUT HALF OF EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. REMOVED AND REPLACED LEFT MIDDLE EMERGENCY POWER SUPPLY UNIT (EPSU) AND REPAIRED SHORTED WIRE AT ROW 20 LEFT. OPERATIONAL CHECK WAS GOOD REF AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,058 hrs · 13,725 cycles

FLT 209 - SJC-PHX - EMERGENCY LIGHTS - SEVERAL ROWS OF EMERGENCY SEAT LIGHTS ARE INOPERATIVE AIRCRAFT LEFT. REMOVED AND REPLACED LEFT (MID CABIN) EMERGENCY POWER SUPPLY UNIT (EPSU). REF AMM 33-51-38; FUNCTIONAL TEST GOOD.

Part: LENS — MISSING (CABIN) · airframe 32,597 hrs · 13,108 cycles

FLT 224 - PHX-BOS - EMERGENCY LIGHTS - ROW 8 LEFT SEAT EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT LENS AT ROW 8 LEFT SEAT PER AMM 33-51-18.

Part: LENS — MISSING (CABIN) · airframe 31,875 hrs · 12,782 cycles

FLT 450 - MSY - PHX - EMERGENCY LIGHTS - AT ROW 9 EMERGENCY EXIT LIGHT LENS ON RIGHT SIDEWALL MISSING. REPLACED EMERGENCY LIGHT LENS AT ROW 9 RIGHT SIDEWALL.

Part: SLIDE — READS HIGH (L1 DOOR) · airframe 31,625 hrs · 12,665 cycles

SAL - C6 - EES - OVER PRESSURE SLIDE PACK AT L-1 DOOR. REPLACED SLIDE PACK AT L-1 DOOR IAW JOB CARD R1C25305.

Part: FITTING — WORN (RUDDER HINGE) · airframe 31,625 hrs · 12,665 cycles

SAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 3 RUDDER HINGE ARM FITTING. REPLACED NR 3 RUDDER HINGE ARM FITTING IAW A319 SRM 51-72-11 & AMM 55-36-41.

Part: FITTING — WORN (RUDDER HINGE) · airframe 31,625 hrs · 12,665 cycles

SAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 4 RUDDER HINGE ARM FITTING. REPLACED NR 4 RUDDER HINGE ARM FITTING IAW A319 SRM 51-72-11 & AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,625 hrs · 12,665 cycles

SAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 RUDDER HINGE ARM FITTING. REPLACED NR 1 RUDDER HINGE ARM FITTING IAW A319 SRM 51-72-11 & AMM 55-36-41.

Part: FILTER — DIRTY (CABIN) · airframe 31,577 hrs · 12,642 cycles

FLT 458 - DEN-PHL - ODOR - UPON RECEIVING AIRCRAFT, STRONG DIRTY SOCK SMELL. COMPLIED WITH JOB CARD 26L00021002. NO OIL LEAKS FOUND IN APU. CHECKED DUCT, NO LIQUIDS FOUND. REMOVED AND REPLACED AIR RECIRCULATION FILTERS PER AMM 21-21-41. NO FURTHER ODOR INCIDENTS FOLLOWED.

Part: ACM — MALFUNCTIONED (NR 2) · airframe 30,735 hrs · 12,273 cycles

FLT 400 - PHX-SFO - BURNING SMELL - GRINDING SOUND FOLLOWED BY THE SMELL OF RUBBER / ELECTRICAL SMOKE, 1 HOUR INTO A 2 HOUR FLIGHT. SMELL ONLY LASTED A SHORT TIME. CONFIRMED NR 2 PACK OVERHEAT. REMOVED AND REPLACED PACK NR 2 AIR CYCLE MACHINE (ACM) PER AMM21-52-21, LEAK & OPERATIONAL CHECK WAS GOOD.

Part: CYLINDER — OUT OF ADJUST (R1 DOOR) · airframe 30,704 hrs · 12,262 cycles

CHK - PHX - EMERGENCY EQUIPMENT/EMERGENCY EGRESS SYSTEM. WHILE PERFORMING TASK CARD F1C25305 EVACUATION DOOR SLIDE DEPLOYMENT, R1 DOOR ASSIST BOTTLE DID NOT OPERATE. FOUND TO BE IMPROPERLY ARMED. REMOVED AND REPLACED SHEAR PIN AND BURST DISC (DIAPHRAGM). SERVICED DOOR ASSIST BOTTLE TO 1600 PSI PER ASK CARD R1C25305. OPERATIONAL CHECK WAS GOOD.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 30,704 hrs · 12,262 cycles

CHK-PHX - EMERGENCY EQUIPMENT - DEPLOYED R1 SLIDE PER TC F1C25305 AND SLIDE DID NOT DEPLOY (FAILED TO INFLATE PROPERLY). REPLACED R1 DOOR SLIDE PER TASK CARD R1C25305. FOUND THAT THE R1 DOOR ASSIST BOTTLE WAS IMPROPERLY ARMED THAT LEAD TO THE FAILED DEPLOYMENT OF THE SLIDE. REFER TO SDR USAA2010030190466.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 28,304 hrs · 11,182 cycles

LOGPAGE:4520693 - FLT 528 - IAD-PHX - EMERGENCY EQUIPMENT - EMERGENCY LIGHTS FAIL SYSTEM TEST. REMOVED AND REPLACED L2 DOOR SLIDE PER JOBCARD R1C25305.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 26,353 hrs · 10,290 cycles

LOG PAGE 4427795 FLT NR 363 PHX-SMF EMERGENCY LIGHT AT 18 LT SEAT MOUNTED IS INOPERATIVE. FOUND SEAT HARNESS DISCONNECTED. SECURED AND RECONNECTED HARNESS. OPS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,677 hrs · 9,999 cycles

FLT 0220-ANC-PHX- EMERGENCY EQUIPMENT - FLASHLIGHT INOPERATIVE AT F/A. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S)

Part: HINGE PIN — WORN (ZONE 600) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN WORN. REPLACED RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN IAW AWA TASK CARD C3R57323.

Part: HINGE PIN — WORN (ZONE 500) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND LEFT WING NR 2 SPOILER HINGE PIN WORN. REPLACED LEFT WING NR 2 SPOILER HINGE PIN IAW AWA TASK CARD C3L57322.

Part: HINGE PIN — WORN (ZONE 500) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND LEFT WING NR 4 SPOILER CENTER HINGE PIN WORN. REPLACED LEFT WING NR 4 SPOILER CENTER HINGE PIN IAW AWA TASK CARD C3L57322.

Part: FLOORBEAM — CORRODED (ZONE 200 - FUSEL) · airframe 20,150 hrs · 7,664 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, +Y1292, FR65+19". REPLACED MAIN CABIN FLOORBEAM, +Y1292, FR 64 - FR 66 IAW A319 SRM 51-72-11.

Part: FLOORBOARD — CORRODED · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD, 261 FF, FR 66 - FR 68, +Y1292. REPLACED MAIN CABIN FLOORBOARD, 261 FF, FR 66 - FR 68, +Y1292 IAW A319 SRM 53-12-12.

Part: FITTING — CORRODED (ZONE 200) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23R. REPLACED R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23R IAW A319 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,150 hrs · 7,664 cycles

SAL - CORROSION ON MAIN CABIN FLOOR SUPPORT BEAM,+ Y503, F15+2". REPLACED MAIN CABIN FLOOR SUPPORT BEAM,+ Y503, FR 12 - FR 16 IAW A319 SRM 51-72-11.

Part: SUPPORT ANGLE — CRACKED (NR 2 NACELLE) · airframe 20,150 hrs · 7,664 cycles

SAL - NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSION) CRACKED, RIB 8. REPLACED NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSION), RIB 8 IAW A319 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 262 FF, FR 66 - FR 68, -Y1292. REPLACED MAIN CABIN FLOORBOARD 262 FF, FR 66 - FR 68, - Y1292 IAW A319 SRM 53-12-12.

Part: FITTING — CORRODED (ZONE 200) · airframe 20,150 hrs · 7,664 cycles

SAL - FOUND CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23L. REPLACED L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23L IAW A319 SRM 51-72-11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,410 hrs · 6,486 cycles

LAS - EEL - CREW REPORTED THAT THE FORWARD GALLEY EMERGENCY EXIT LIGHTS WERE INOPERATIVE OVER DOORS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY, 10WL IAW AWA TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD.

Part: FAN — VIBRATION (CABIN) · airframe 15,944 hrs · 5,882 cycles

CREW REPORTED THAT DURING CRUISE FLIGHT, AT FL 350, AN UNUSUAL VIBRATION IN THE COCKPIT AND FORWARD GALLEY. THEN REPORTED GETTING SMOKE ODOR IN THE COCKPIT. CREW USED THE O2 MASKS AND DIVERTED TO ABQ. LANDED WITHOUT FURTHER INCIDENT. MX R & R AVIONICS BLOWER FAN, 20HQ, IAW AIRBUS MM 21-26-51. OPERATIONAL CHECKS WERE GOOD. CONFIRMED FAILURE. UPON TEARDOWN VENDOR FOUND FRONT BEARING SHATTERED AND FRONT FLANGE WORN OUT. VENDOR CLEANED UNIT. VENDOR REPLACED BEARINGS, FRONT FLANGE AND CONSUMABLES, BALANCED ROTOR AND MOTOR, AND MODIFIED TO EVT3454HC. VENDOR TESTED UNIT IAW CMM 21-26-42 REV. 7.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,878 hrs · 5,117 cycles

PHX - EEL - DURING PHASE 8 CHECK, AFT EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING STEP 11 OF PHASE GENERAL TASK CARD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,563 hrs · 4,662 cycles

EMERGENCY EQUIPMENT - MAINTENANCE FOUND THE AFT EMERGENCY FLASHLIGHT INOPERATIVE. MX REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD.

Part: ADIRU — FAULTY (NR 1) · airframe 9,312 hrs · 3,539 cycles

ON TAKEOFF ROLL AT APPROX 90 KTS ATTITUDE & MAP NOT AVAILABLE, DISPLAYED ON CAPTS PRIMARY FLT DISPLAY & NAVIGATION DISPLAY, & NR 1 IR FAULT LIGHT ON, REJECTED TAKEOFF HIGH SPEED. AFTER REJECTED TAKEOFF BRAKE TEMP REACHED 990 DEG ON ALL FOUR BRAKES, AND NR 1 & 2 TIRES WENT FLAT WITH POSSIBLE LEAKS ON NR 3 & 4 TIRES. MX R & R NR 1 ADIRU IAW T/C R2A34304, OPS CHK GOOD. PERFORMED OVERTEMP INSP OF BOTH MLG AXLES, & R & R ALL FOUR MLG TIRES & BRAKE ASSY. BENCH TEST OF ADIRU COULD NOT VERIFY REASON FOR REMOVAL. SUSPECT PROBLEM WITH JFK RUNWAY 31L INDUCED FAULT OF Z QUANTIZER DC AMP FAILURE. THIS IS A KNOWN PROBLEM WITH JFK RUNWAY.

Part: POWER SUPPLY — DISCHARGED (ZONE 221) · airframe 8,809 hrs · 3,383 cycles

MCN - EEL - DURING B-02 CHECK THE EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 1, 4 AND 20 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE L-1 DOOR, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (ZONE 900) · airframe 6,253 hrs · 2,447 cycles

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

Part: BATTERY — INOPERATIVE (CABIN) · airframe 6,288 hrs · 2,577 cycles

DURING CLIMB, THE EMERGENCY EXIT SIGN LOCATED AT OVERHEAD AISLE MID-CABIN POSITION BECAME INOPERATIVE, FOLLOWED BY THE EXIT SIGN AT THE R/H OVER WING EXIT. THE AIRCRAFT CABIN R/H SIDE EMERGENCY ESCAPE PATH LIGHTING WAS ALSO INTERMITTENTLY ILLUMINATING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE R/H MID CABIN EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT 12WL IAW AMM TASK 33-51-38-400-002; OPERATIONAL CHECK WAS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 813 hrs · 356 cycles

PHX - EMERGENCY LANDING - C - DURING DESCENT INTO PHX FROM SEA FLIGHT CREW RECEIVED ECAM MESSAGES FOR 3 CLASS 1 FAULTS (1) NR 2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) (2) NR 2 BRAKE ANTISKID AND NOSE WHEEL STEERING, (3) LAVATORY/CARGO SMOKE DETECTION. MAINTENANCE CONTROL ADVISED FLIGHT CREW TO RESET CIRCUIT BREAKER WHICH HAD NO EFFECT. EMERGENCY LANDING WAS DECLARED AND AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 LGCIU IAW AMM 32-31-71-000-001, AND OPERATIONAL CHECKED GOOD IAW 32-69-00-740-001. THE 3-POLE CONTACTOR WAS ALSO REPLACED IAW AMM 24-51-55-000-001.