N657AW

Part: EPSU — NO TEST (ZONE 200) · airframe 83,898 hrs · 34,997 cycles

AIRCRAFT WAS NOT GROUNDED: LH EPSU NOT WORKING. MAINTENANCE REPLACED LH EPSU IAW AMM 33-51-38.

Part: BOTTLE — READS LOW (ZONE 800) · airframe 83,574 hrs · 34,768 cycles

AIRCRAFT WAS GROUNDED: RH OVERWING EMER EXIT INFLATION RESERVOIR FOUND BAD FROM STOCK. MAINTENANCE REMOVED BOTTLE IAW AMM 25-62-46.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 SLIDE) · airframe 83,574 hrs · 34,768 cycles

AIRCRAFT WAS GROUNDED: RH OVERWING EMER EXIT INFLATION RESERVOIR REQUIRES REPLACEMENT. MAINTENANCE REPLACED BOTTLE IAW AMM 25-62-46.

Part: POWER SUPPLY — NO TEST (ZONE 800) · airframe 83,574 hrs · 34,768 cycles

AIRCRAFT WAS GROUNDED: FWD L EPSU BATTERY FAILED OPS CHECK FOUND DURING MIC 1602637. MAINTENANCE REPLACEDFWD L/H EPSU BATTERY PER M/M 33-51-38.

Part: SLIDE — UNRAVELED (ZONE 800) · airframe 83,574 hrs · 34,768 cycles

AIRCRAFT WAS GROUNDED: RIGHT OFFWING SLIDE UNRAVELED WHILE ACCOMPLISHING INSTALLATION OF INFLATION RESERVOIR FOR THE OFF WING SLIDE. MAINTENANCE REPLACED SLIDE PER M/M 25-62-42.

Part: SIGN — FAULTED (ZONE 200) · airframe 82,843 hrs · 34,321 cycles

AIRCRAFT WAS NOT GROUNDED: FWD EMERGENCY EXIT LIGHT SIGN PARTIALLY ON. MAINTENANCE REPLACED EMERGENCY EXIT LOCATION SIGN AT FWD ENTRY DOOR, CENTER AISLE ABOVE AFT LAVATORY IAW AMM 33-51-16, 33-51-17.

Part: SIGN — FAULTED (ZONE 200) · airframe 82,843 hrs · 34,321 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EMERGENCY EXIT LIGHT SIGN PARTIALLY ON. MAINTENANCE REPLACED EMERGENCY EXIT LOCATION SIGNS AT AFT ENTRY DOOR, CENTER AISLE ABOVE AFT LAVATORY IAW AMM 33-51-16, 33-51-17.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 82,647 hrs · 34,217 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY OPERATION ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED R1 DOOR ACCUMULATOR BOTTLE IAW AMM 52-10-00.

Part: LAMP — BURNED OUT (ZONE 200) · airframe 82,235 hrs · 33,980 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT FOR L/H OVER WING EXIT HAS BURNED OUT LAMPS. MAINTENANCE REPLACED LAMPS IN L/H OVER WING EMERGENCY EXIT SIGN REF AMM 33-51-15.OPS NORMAL.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 81,994 hrs · 33,865 cycles

AIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND SEAT 26C FLOOR POXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM INOP. MAINTENANCE REPLACED EPSU 11WL AND BATTERY ASSY IAW AMM 33-51-38.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 81,340 hrs · 33,471 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 3 EMERGENCY LIGHT INOP. IAW TSM 33-51-00-810-801A FOUND EMERGENCY POWER SUPPLY UNIT 11WLFAULTED. REPLACED EMERGENCY LIGHTS AND UNIT TESTS OK.

Part: TARGET — LOOSE (ZONE 800) · airframe 81,215 hrs · 33,415 cycles

AIRCRAFT WAS GROUNDED: DUE TO REPEATS OF LANDING GEAR DISAGREE ECAM,AND TO AVOID FUTURE DELAYS, CANCELLATION ,AND LENGTHY OTS EVENTS ACCOMPLISH TSM 32-31-00-810-888-A. MAINTENANCE FOUND MISSING SCREW THAT HOLDS TARGET. REPLACED TARGET AND SCREW INSIDE UPLOCK ACTUATOR FOR 27GA PER AMM 32-31-14. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 81,212 hrs · 33,413 cycles

AIRCRAFT WAS GROUNDED: AFTER GEAR EXTENSION ON FINAL. L/G DOORS NOT CLOSED CAUTION. PERFORMED GO AROUND COMPLETED ECAM AND CHECKLIST. LEFT MAIN GEAR DOOR ON WHEEL PAGE SHOWS PARTIALLY OPEN. ARFF VISUAL SHOWED CLOSED. DECLARED EMERGENCY AND LANDED WITHOU INCIDENT. MAINTENANCE REPLACED L/H MLG PROX SENSOR 27GA IAW AMM 32-31-73.

Part: PROXIMITY SENSOR — FAULTED (LG DOORS) · airframe 81,215 hrs · 33,415 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT WAS GROUNDED: AFTER GEAR EXTENSION ON FINAL. L/G DOORS NOT CLOSED CAUTION. PERFORMED GO AROUND COMPLETED ECAM AND CHECKLIST. LEFT MAIN GEAR DOOR ON WHEEL PAGE SHOWS PARTIALLY OPEN. ARFF VISUAL SHOWED CLOSED. DECLARED EMERGENCY AND LANDED WITHOU INCIDENT. MAINTENANCE REPLACED L/H MLG PROX SENSOR 29GA IAW AMM 32-31-73.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 81,155 hrs · 33,385 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EPSU FAULTED DURING SLIDE CHANGE OPS CHECK. MAINTENANCE REPLACED AFT EPSU PER AMM 33-51-58.

Part: ACCESS PANEL — BENT (ZONE 200) · airframe 80,896 hrs · 33,239 cycles

AIRCRAFT WAS GROUNDED: PANEL CORNER BENT OUTWARD BEHIND LEFT WING ON FUSELAGE ACCESS PANEL 2 FEET AFT OF TRAILING EDGE. MAINTENANCE REPAIRED SLIDE CONTAINER PANEL PER EA 359015 AND REPLACED LH OVERWING SLIDE.

Part: CONTACT — FAILED (FUEL PUMP) · airframe 80,646 hrs · 33,040 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA202409111684: MAINTENANCE REPLACED #1 CENTER FUEL PUMP, REPLACED SDAC 1 (AALA202409231856) AND SDAC 2 (AALA202409236181) AND REPLACED GFI 69QA (AALA202409239557). A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PUMP — INOPERATIVE (CENTER FUEL) · airframe 80,646 hrs · 33,040 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. (OPEN)

Part: PUMP — INOPERATIVE (ZONE 100) · airframe 80,646 hrs · 33,040 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA202409111684: MAINTENANCE REPLACED #1 CENTER FUEL PUMP, REPLACED SDAC 1 (AALA202409231856) AND SDAC 2 (AALA202409236181) AND REPLACED GFI 69QA (AALA202409239557). A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PUMP — INOPERATIVE (ZONE 100) · airframe 80,646 hrs · 33,040 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **SUPPLEMENTAL REPORT FOR AALA202409111684: MAINTENANCE REPLACED #1 CENTER FUEL PUMP, REPLACED SDAC 1 (AALA202409231856) AND SDAC 2 (AALA202409236181) AND REPLACED GFI 69QA (AALA202409239557). A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: PUMP — INOPERATIVE (ZONE 100) · airframe 80,646 hrs · 33,040 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA202409111684: MAINTENANCE REPLACED #1 CENTER FUEL PUMP, REPLACED SDAC 1 (AALA202409231856) AND SDAC 2 (AALA202409236181) AND REPLACED GFI 69QA (AALA202409239557). A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SCREW — MISSING (ZONE 700) · airframe 80,611 hrs · 33,009 cycles

AIRCRAFT WAS GOUNDED: ECAM - LANDING GEAR DOOR NOT CLOSED. MAINTENANCE FOUND LEFT HAND MAIN LANDING GEAR DOOR UPLOCK SENSOR 27GA TARGET MISSING ATTACH SCREW AND INSTALLED IT PER AMM 32-31-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LGCIU — FAULTED (ZONE 700) · airframe 80,611 hrs · 33,009 cycles

AIRCRAFT WAS GROUNDED: LEFT MAIN LANDING GEAR DOOR FAILED TO CLOSE ON RETRACT. DOOR SUCCESSFULLY CLOSED FOLLOWING LANDING GEAR CYCLE IN ACCORDANCE WITH ECAM PROCEDURE. FLIGHT CREW ALSO REPORTED A LANDING GEAR DOOR NOT CLOSED ECAM MESSAGE ON GEAR EXTENSION FOR LANDING AT DESTINATION CITY. MAINTENANCE REPLACED #1 LGCIU (AALA202409031926) AND # 2 LGCIU (AALA202409034012) PER AMM 32-31-71. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: LGCIU — FAULTED (ZONE 700) · airframe 80,611 hrs · 33,009 cycles

AIRCRAFT WAS GROUNDED: LEFT MAIN LANDING GEAR DOOR FAILED TO CLOSE ON RETRACT. DOOR SUCCESSFULLY CLOSED FOLLOWING LANDING GEAR CYCLE IN ACCORDANCE WITH ECAM PROCEDURE. FLIGHT CREW ALSO REPORTED A LANDING GEAR DOOR NOT CLOSED ECAM MESSAGE ON GEAR EXTENSION FOR LANDING AT DESTINATION CITY. MAINTENANCE REPLACED #1 LGCIU (AALA202409031926) AND # 2 LGCIU (AALA202409034012) PER AMM 32-31-71. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: PROXIMITY SWITCH — LOOSE (ZONE 700) · airframe 80,401 hrs · 32,879 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR DOORS NOT CLOSED. ON APPROACH AFTER LOWERING THE GEAR THE LEFT MAIN GEAR DOOR FAILED TO CLOSE. MAINTENANCE FOUND BOLT ON UPLOCK PROXIMITY SWITCH LOOSE AND TIGHTENED BOLT PER AMM 20-21-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: UPLOCK — WARNING MESSAGE (ZONE 100) · airframe 80,350 hrs · 32,851 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT MAIN GEAR DOORS NOT CLOSED ECAM ON TAKEOFF. FLIGHT CREW CYCLED GEAR, DID NOT CLOSE AGAIN ON EXTENSION, DID CLOSE PROPERLY ON SECOND RETRACTION. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR UPLOCK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-31-33.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 800) · airframe 80,304 hrs · 32,825 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS THAT THE AFT LEFT SERVICE DOOR WILL NOT LOCK INTO POSITION WHEN OPENED. ADJUSTED AFT L/H PASSENGER CREW DOOR IAW AMM 52-13-00-820-001-A.OPS CHECK GOOD.

Part: BOLT — MISSING (PROX TARGET) · airframe 80,223 hrs · 32,783 cycles

AIRCRAFT WAS NOT GROUNDED: UPON LANDING GEAR EXTENSION, THE LEFT MAIN DOOR DID NOT CLOSE. LANDING GEAR DOORS NOT CLOSED ECAM DISPLAYED. FOUND PROX SENSOR (27GA) SWITCH-TARGET PROXIMITY HAD A MISSING LOWER MOUNT BOLT AND A LOOSE UPPER MOUNT BOLT CAUSING ERRATIC INDICATION. REINSTALLED A NEW LOWER MOUNT BOLT AND TIGHTENED UPPER

Part: LATCH — OUT OF ADJUST (COCKPIT DOOR) · airframe 80,158 hrs · 32,748 cycles

AIRCRAFT WAS NOT GROUNDED: UNABLE TO OPEN COCKPIT DOOR. ADJUSTED FLIGHT DECK LATCH MECHANISM.

Part: TARGET — LOOSE (MLG) · airframe 79,978 hrs · 32,639 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED 7 MINUTES PRIOR TO LANDING AT CLT DUE TO THE FLIGHT CREW REPORTING A LANDING GEAR DOOR NOT CLOSED ECAM WITH LEFT MAIN LANDING GEAR DOOR AMBER. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND FORWARD TARGET LOOSE ON LEFT HAND MAIN LANDING GEAR DOOR UPLOCK AND SECURED IT PER AMM 32-31-33. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 79,653 hrs · 32,417 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERATIVE UNDER SEAT 7 AND 17. INSPECTED AND FOUND BROKEN SPLICES AT BOTH SEATS, REMOVED AND REPLACED BROKEN SPLICES AT SEAT 7 AND 17 (AALA202405024687).

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 79,653 hrs · 32,417 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERATIVE UNDER SEAT 7 AND 17. INSPECTED AND FOUND BROKEN SPLICES AT BOTH SEATS, REMOVED AND REPLACED BROKEN SPLICES AT SEAT 7 (AALA202405021635) AND 17.

Part: CHECK VALVE — DEFECTIVE (HYD SYSTEM) · airframe 78,979 hrs · 32,008 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO CLT DUE TO A GREEN HYDRAULIC SYSTEM RESERVOIR OVERHEAT ECAM MESSAGE DISPLAYING DURING CRUISE. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURE WHICH RESULTED IN A LOSS OF GREEN HYDRAULIC SYSTEM PRESSURE. DURING FINAL APPROACH THE GREEN HYDRAULIC SYSTEM RESERVOIR OVERHEAT ECAM MESSAGE WENT OUT AND THE FLIGHT CREW WAS ABLE TO RESTORE THE GREEN HYDRAULIC SYSTEM PRESSURE WHICH ALLOWED THE FLIGHT CREW TO LAND NORMALLY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED HIGH PRESSURE MANIFIOLD CHECK VALVE 1022GM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 78,734 hrs · 31,854 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAILED SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202401038002) AND BATTERY (AALA202401037963). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 78,734 hrs · 31,854 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 12WL BATTERY FAILED SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 78,734 hrs · 31,854 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAILED SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202401038002) AND BATTERY (AALA202401037963). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 78,734 hrs · 31,854 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL BATTERY FAILED SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 78,734 hrs · 31,854 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAILED SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: TARGET — LOOSE (ZONE 700 - GEARS) · airframe 78,705 hrs · 31,841 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO ATL DUE TO AFTER LANDING GEAR RETRACTION, LANDING GEAR DOORS NOT CLOSED MESSAGE ON ECAM. FLIGHT CREW CYCLED GEAR AS PER PROCEDURE LEFT GEAR #1 INDICATED AMBER AND OPEN. STAYED BELOW ALL AIRSPEED RESTRICTIONS DURING FLIGHT. MAINTENANCE FOUND PROXIMITY SENSOR 29GA TARGET BOTTOM BOLT TAB WASHER UNLOCKED ALLOWING THE BOLT TO BACK OUT. MAINTENANCE INSTALLED BOLT AND LOCKED THE TAB WASHER ON THE TARGET PER CMM 32-31-33. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PTU — LEAKING (ZONE 100 - FUSE) · airframe 78,492 hrs · 31,692 cycles

AIRCRAFT WAS GROUNDED: MUSTY SMELL REPORTED BY FLIGHT ATTENDANT IN BACK AFTER TAKEOFF. MAINTENANCE FOUND THE POWER TRANSFER UNIT (PTU) LEAKING HYDRAULIC FLUID INTO THE APU INLET AND REPLACED IT PER AMM 29-23-41. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROBE — DEFECTIVE (ZONE 400 - NAC/P) · airframe 78,305 hrs · 31,564 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO STL. FLIGHT CREW REPORTED THAT DURING CRUISE AT FL 350 THEY LOST #2 ENGINE EPR AND N1 DEGRADED MESSAGE OCCURED. CREW ACCOMPLISHED QRH PROCEDURES AND THE AIRCRFT LANDED SAFELY AT STL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE P2/T2 PROBE PER TASK CARD 26L40073005.

Part: PRIORITY VALVE — LEAKING (ZONE 100 - FUSE) · airframe 77,709 hrs · 31,238 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DURING DESCENT INTO CLT DUE TO A GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL AND GREEN HYDRAULIC SYSTEM ENGINE #1 LOW PERSSURE ECAM MESSAGES. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PRIORITY VALVE 1064GM LEAKING AND REPLACED IT PER AMM 29-11-33. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: MEGAPHONE — INOPERATIVE (ZONE 200 - FUSE) · airframe 77,405 hrs · 31,041 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS CABIN MEGAPHONE INOPERATIVE. REMOVED AND REPLACED FORWARD L1 DOOR MEGAPHONE PER AMM 25-63-00.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 77,396 hrs · 31,035 cycles

AIRCRAFT WAS GROUNDED: FORWARD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED MEGAPHONE BATTERIES PER AMM 25-65-51-920-001-A.

Part: HINGE — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 77,230 hrs · 30,922 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS, VERY HARD TO OPEN FROM OUTSIDE. MAINTENANCE RE-ADJUSTED SHIMMING OF THE LAVATORY DOOR FORWARD HINGE PER AMM 25-45-19-400 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,230 hrs · 30,922 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS, VERY HARD TO OPEN FROM OUTSIDE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 77,209 hrs · 30,909 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE IN FLIGHT. DOOR JAMS ON BUT DOOR DOES NOT JAM ON GROUND. MAINTENACE INSPECTED DOOR AND FOUND THAT IT DOES NOT JAM ON FLOOR TRIM. MAINTENANCE ADJUSTED THE LAVATORY DOOR AS REQUIRED.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 77,190 hrs · 30,900 cycles

AIRCRAFT WAS NOT GROUNDED: THERE HAVE BEEN MULTIPLE REPORTS OF THE FORWARD LAVATORY DOOR BEING DIFFICULT TO OPEN BUT ONLY WHILE IN FLIGHT. MAINTENANCE ADJUSTED LAVATORY DOOR.

Part: THRESHOLD — LOOSE (ZONE 900 - LAV/G) · airframe 77,165 hrs · 30,884 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY (L1) ENTRY DOOR DIFFICULT TO OPEN IN FLIGHT ONLY. TIGHTENED THRESHOLD SCREWS AS REQUIRED. DOOR OPENS AND CLOSES EASILY.

Part: PIN — LOOSE (ZONE 900 - LAV/G) · airframe 77,148 hrs · 30,875 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR KEEPS GETTING STUCK WHEN CLOSED. TIGHTENED DOOR GUIDE PIN AS REQUIRED.

Part: BULB — INOPERATIVE (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCAFT IN BASE MAINTENANCE: SEAT 11D EMERGENCY EXIT LIGHT NEEDS RELAMP. REPLACED EMERGENCY EXIT LIGHT BULB ON SEAT 11D.

Part: WIRE — CUT (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER COMPARTMENT CELING AREA LEFT HAND EMERGENCY EXIT LIGHT CONNECTOR 7261VC2-A HAS WIRE CUT. MAINTENANCE REPAIRED WIRE PER ESPM 20-43-10 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM33-51-00.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 13WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACCESS PANEL — WORN (ZONE 500 - LH WI) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL TANK ACCESS PANEL 540LB HAS ELONGATED FASTENER HOLE. REPLACED ACCESS PANEL PER SRM 51-72-11.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST RIGHT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 342932

Part: PIN — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON AFT ATTACH FITTING UPPER BOLT / PIN AT PYLON RIB 10. REPLACED BOLT / PIN PER TASK CARD 26C42554028.

Part: SLEEVE — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON AFT ATTACH FITTING UPPER BOLT/PIN SLEEVE AT PYLON RIB 10. REPLACED BOLT / PIN SLEEVE PER TASK CARD 26C42554028.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 10 LOWER FORWARD BOLT BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #10 LOWER AFT BOLT BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #9 UPPER BOLT AT RIB 19. REPLACED BOLT PER AMM 27-84-66.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 LOWER FORWARD BOLT AT RIB 17. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 7 FORWARD BOLT AT RIB 15. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 UPPER AFT BOLT AT RIB 17. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #7 LOWER BOLT BETWEEN RIBS 14 AND 15. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #7 UPPER BOLT BETWEEN RIBS 14 AND 15. REPLACED BOLT PER AMM 27-84-65.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.

Part: ANCHOR FITTING — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIB 2 AND 3. REPAIRED ANCHORAGE FITTING PER EA 343866 AND SRM 57-26-13-300-008.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK # 8 LOWER AFT BOLT BETWEEN RIBS 15 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #8 LOWER MIDDLE BOLT. REPLACED BOLT PER TASK CARD 26C61057005.

Part: ANCHOR FITTING — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIB 2 AND 3. REPAIRED ANCHORAGE FITTING PER EA 343866 AND SRM 57-26-13-300-008.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #4 UPPER BOLT BETWEEN RIBS 5 AND 6. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 FORWARD BOLT AT RIB 9. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #6 LOWER AFT BOLT BETWEEN RIBS 12 AND 13. REPLACED BOLT PER AMM 27-84-64.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK # 4 LOWER BOLT BETWEEN RIBS 5 AND 6. REPLACED BOLT PER AMM 27-84-63.

Part: ATTACH FITTING — WORN (ZONE 100 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD ATTACH FITTING HAS MIGRATED BUSHING ON THE FORWARD LUG AT FR 43 AND Y254. REPLACED LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING PER EA 344171

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK # 5 LOWER BOLT AT RIB 9. REPLACED BOLT PER AMM 27-84-64.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 6 LOWER FORWARD BOLT AT RIB 12. REPLACED BOLT PER AMM 27-84-64.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER AFT BOLT. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #4 UPPER BOLT. REPLACED BOLT PER TASK CARD 26C61057005.

Part: STRUCTURE — CRACKED (ZONE 100 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN CENTER FUSELAGE SIDE SHELL AFT LOWER FASTENER HOLE #2 AT FR 35 AND S30L REPAIRED SIDE SHELL PER EA 343127.

Part: GAUGE — BROKEN (ZONE 800 - DOORS) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER GUAGE BROKEN. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: ATTACH FITTING — WORN (ZONE 600 - RH WI) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTION STRUT AFT ATTACH FITTING BEARING HAS EXCESSIVE PLAY AT RIB 24. REPLACED ATTACH FITTING PER SRM 51-42-11.

Part: ATTACH FITTING — WORN (ZONE 600 - RH WI) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY BEARING ON THE INBOARD FLAP END AT RIB 14. REPLACED ATTACH FITTING PER SRM 51-42-11.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: FRAME AFT FACE WEB ON THE HORIZONTAL FLANGE LOWER RADII CRACKED AT FR 68 AND S22L. REPAIRED FRAME PER EA 343126.

Part: UNKNOWN — CRACKED (ZONE 800 - DOORS) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 DOOR FRAME, EDGE CURVED LOWER CRACKED AT FR 38. REPLACED DOOR FRAME, EDGE CURVED LOWER PER SRM 51-42-11.

Part: UNKNOWN — CRACKED (ZONE 800 - DOORS) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENACNE: EMERGENCY EXIT DOOR 834 INTERNAL SEGMENT ANGLE CRACKED BETWEEN DOOR BEAM 2 AND BEAM 3. REPLACED SEGMENT PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 77,122 hrs · 30,855 cycles

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

Part: UNKNOWN — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

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

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 64 AND FR 66 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: UNKNOWN — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND -Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: WEB — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB AT FR 20 AND S23R. REPLACED WEB PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON LEFT HAND FRAME DOOR STOP FITTING #1 INBOARD LOWER FASTENER HOLE AT FR 66. REPAIRED FRAME PER SRM 53-41-12-300-011.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: RUDDER — UNKNOWN (ZONE 300 - STABS) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: TRAPPED WATER INDICATION FOUND ON RUDDER SIDE PANEL LEFT HAND HONEYCOMB CORE STRUCTURE BETWEEN RIB 6 AND RIB 7 AND 4.75 INCH FROM RIB 7 AND FASTENER 27 TO 28 AND 2.88 INCH FROM THE TRAILING EDGE. MAINTENANCE REPAIRED RUDDER PER SRM SRM 55-41-13-300-024.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 342932

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 77,122 hrs · 30,855 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND FRAME UPPER RADII UPPER FASTENER HOLE CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 342932

Part: BULB — BURNED OUT (ZONE 200 - FUSE) · airframe 77,021 hrs · 30,799 cycles

AIRCRAFT WAS NOT GROUNDED: MULTIPLE BULBS OUT IN EXIT SIGN OVER ENTRY AND SERVICE DOORS. MAINTENANCE REPLACED EXIT SIGN BULBS AS REQUIRED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: MECHANISM — DEFECTIVE (ZONE 700 - GEARS) · airframe 76,964 hrs · 30,767 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SFO DUE TO THE LANDING GEAR WOUND NOT RETRACT AND SHOCK ABSORBER FAULT. THE AIRCRAFT LANDED AT SFO SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR FLIGHT / GROUND SENSING MECHANISM PER AMM 32-31-73 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: TRANSFER VALVE — FAULTED (FUEL SYSTEM) · airframe 76,667 hrs · 30,600 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FUEL TRANSFER VALVE DID NOT OPEN ON DESCENT INTO PHX. OPENED AFTER LANDING. OPEN

Part: TRANSFER VALVE — FAULTED (LT WING TANK) · airframe 76,667 hrs · 30,600 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FUEL TRANSFER VALVE DID NOT OPEN ON DESCENT INTO PHX. OPENED AFTER LANDING. **SUPPLEMENTAL REPORT FOR AALA202212201145: MAINTENANCE ACCOMPLISHED TSM 28-15-00-810-801-A AND FOUND NO FAULTS OR ISSUES NOTED. ** (CLOSED)

Part: TIRE — BLOWN (ZONE 700 - GEARS) · airframe 75,948 hrs · 30,203 cycles

AIRCRAFT WAS GROUNDED: # 4 MAIN LANDING GEAR TIRE BLOWN ON LANDING. MAINTENANCE REPLACED THE #4 MAIN LANDING GEAR WHEEL ASSEMBLY PER AMM 32-41-12.

Part: TIRE — BLOWN (ZONE 700 - GEARS) · airframe 75,948 hrs · 30,203 cycles

AIRCRAFT WAS GROUNDED: # 3 TIRE BLEW ON LANDING . NORMAL LANDING 200-300 FPM ON TOUCH DOWN. MAINTENANCE REPLACED THE #3 MAIN LANDING GEAR WHEEL ASSEMBLY PER AMM 32-41-11.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 75,818 hrs · 30,140 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT FLOOR ROW 11 ABC HAS BATTERY FAULT WHEN TESTED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT FLOOR ROW 11 ABC. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS. REFERENCE AMM 33-51-38.

Part: WIRE HARNESS — DEFECTIVE (ZONE 200 - FUSE) · airframe 75,814 hrs · 30,139 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT SEAT 11ABC. REPLACED SIDE WALL CONNECTOR ELECTRICAL HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 75,349 hrs · 29,853 cycles

AIRCRAFT WAS NOT GROUNDED: AT ROW 7ABC EMERGENCY LIGHT WIRES ARE BROKEN UNDER THE SEAT. SPLICED EMERGENCY LIGHT WIRES ON SEAT 7ABC PER ESPM 20-53-29 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900 - LAV/G) · airframe 75,349 hrs · 29,853 cycles

AIRCRAFT WAS NOT GROUNDED: AT CRUISE LAVATORY SMOKE ECAM DISPLAYED BRIEFLY. NO SIGNS OF TAMPERING WITH DETECTOR OR SMOKE/ODOR. MAINTENANCE ACCOMPLISHED TSM 26-17-00 AND AMM 26-17-00 WITH NO FAULTS BEING NOTED ON LAVATORY D SMOKE DETECTION SYSTEM.

Part: ACTUATOR — TRIPPED (ZONE 500 - LH WI) · airframe 74,907 hrs · 29,615 cycles

AIRCRAFT WAS GROUNDED: FLAPS FAILED TO EXTEND WHEN CONFIGURING FOR LANDING. ECAM PROCEDURE FAILED TO FIX PROBLEM. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT HAND #1 FLAP ACTUATOR TRIPPED AND REPLACED IT PER AMM 27-54-49. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: ACTUATOR — FAULTY (ZONE 400 - NAC/P) · airframe 74,480 hrs · 29,359 cycles

AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT 80 KNOTS DUE TO #2 ENGINE COMPRESSOR VANE ECAM FAULT. SAFELY RETURNED TO GATE. **SUPPLEMENTAL REPORT FOR AALA202202026955: REPLACED #2 ENGINE VSV ACTUATOR PER JOB CARD 26T40075005. ACCOMPLISHED SATISFACTORY LEAK AND OPERATIONAL CHECKS.** (CLOSED)

Part: NONE — NONE · airframe 74,480 hrs · 29,359 cycles

AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT 80 KNOTS DUE TO #2 ENGINE COMPRESSOR VANE ECAM FAULT. SAFELY RETURNED TO GATE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: POWER SUPPLY — FAULT MESSAGE (ZONE 200 - FUSE) · airframe 74,269 hrs · 29,240 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT OVERWING EMERGENCY BATTERY PACK 11WL SHOWS EXTERNAL LIGHTS FAULT. REMOVED AND REPLACED LEFT CENTER EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 OPERATIONS CHECK GOOD AND REMOVED AND REPLACED WING EXIT MARKER (AALA202201030678) OVER WING PER AMM 33-51-15 OPERATIONS CHECK GOOD.

Part: SIGN — INOPERATIVE (ZONE 200 - FUSE) · airframe 74,269 hrs · 29,240 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT OVERWING EMERGENCY BATTERY PACK 11WL SHOWS EXTERNAL LIGHTS FAULT. REMOVED AND REPLACED LEFT CENTER EMERGENCY POWER SUPPLY UNIT (AALA202201037035) PER AMM 33-51-38 OPERATIONS CHECK GOOD AND REMOVED AND REPLACED WING EXIT MARKER OVER WING PER AMM 33-51-15 OPERATIONS CHECK GOOD.

Part: NONE — NONE · airframe 74,269 hrs · 29,240 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED 19 LEFT EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: HARNESS — INOPERATIVE (ZONE 200 - FUSE) · airframe 74,269 hrs · 29,240 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED 19 LEFT EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202201055244: REMOVED AND REPLACED HARNESS 5409V PER ESPM 20-33-11 OPERATIONS CHECK GOOD** (CLOSED)

Part: TRANSMITTER — FAULT MESSAGE (ZONE 200 - FUSE) · airframe 73,913 hrs · 29,041 cycles

AIRCRAFT WAS GROUNDED: ON TAKE OFF BRAKE SYSTEM 2 FAULT MESSAGE, TAKEOFF WAS ABORTED BELOW 20 KNOTS. REPLACED BRAKE PEDAL TRANSMITTER 9GG AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-42-47.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,552 hrs · 28,840 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT EXIT LOAD EMERGENCY LEFT. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-38.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 73,227 hrs · 28,644 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT ROW 19 WILL NOT ILLUMINATE. REPAIRED DAMAGED WIRING PER AFMM 20-18-1.

Part: TIRE — FAILED (MLG) · airframe 71,040 hrs · 27,491 cycles

AIRCRAFT WAS GROUNDED: DURING POST ARRIVAL WALKAROUND, MAINTENANCE FOUND THE NR 1 AND 2 MAIN LANDING GEAR TIRES BLOWN. AFTER APPLYING POWER TO THE AIRCRAFT IT WAS NOTED THAT THE ECAM WHEEL PAGE REFLECTED BRAKE TEMPS AS FOLLOWS: NR 1 (655), NR 2 (620), NR 3 (420) AND NR 4 (465). BOTH TIRES WERE REPLACED PER AMM 32-41-11 DUE TO THE FUSE PLUG BEING BLOWN DUE TO BEING OVER HEATED. THE NR 1 AND NR 2 BRAKE ASSEMBLIES WERE REPLACED DUE TO OVER HEATING PER AMM 32-42-27.

Part: BRAKE — OVERHEATED (MLG) · airframe 71,040 hrs · 27,491 cycles

AIRCRAFT WAS GROUNDED: DURING POST ARRIVAL WALKAROUND, MAINTENANCE FOUND THE NR 1 AND 2 MAIN LANDING GEAR TIRES BLOWN. AFTER APPLYING POWER TO THE AIRCRAFT IT WAS NOTED THAT THE ECAM WHEEL PAGE REFLECTED BRAKE TEMPS AS FOLLOWS: NR 1 (655), NR 2 (620), NR 3 (420) AND NR 4 (465). BOTH TIRES WERE REPLACED PER AMM 32-41-11 DUE TO THE FUSE PLUG BEING BLOWN DUE TO BEING OVER HEATED. THE NR 1 AND NR 2 BRAKE ASSEMBLIES WERE REPLACED DUE TO OVER HEATING PER AMM 32-42-27.

Part: TIRE — FAILED (MLG) · airframe 71,040 hrs · 27,491 cycles

AIRCRAFT WAS GROUNDED: DURING POST ARRIVAL WALKAROUND, MAINTENANCE FOUND THE NR 1 AND 2 MAIN LANDING GEAR TIRES BLOWN. AFTER APPLYING POWER TO THE AIRCRAFT IT WAS NOTED THAT THE ECAM WHEEL PAGE REFLECTED BRAKE TEMPS AS FOLLOWS: NR 1 (655), NR 2 (620), NR 3 (420) AND NR 4 (465). BOTH TIRES WERE REPLACED PER AMM 32-41-11 DUE TO THE FUSE PLUG BEING BLOWN DUE TO BEING OVER HEATED. THE NR 1 AND 2 BRAKE ASSEMBLIES WERE REPLACED DUE TO OVER HEATING PER AMM 32-42-27.

Part: BRAKE — OVERHEATED (MLG) · airframe 71,040 hrs · 27,491 cycles

AIRCRAFT WAS GROUNDED: DURING POST ARRIVAL WALKAROUND, MAINTENANCE FOUND THE NR 1 AND 2 MAIN LANDING GEAR TIRES BLOWN. AFTER APPLYING POWER TO THE AIRCRAFT IT WAS NOTED THAT THE ECAM WHEEL PAGE REFLECTED BRAKE TEMPS AS FOLLOWS: NR 1 (655), NR 2 (620), NR 3 (420) AND NR 4 (465). BOTH TIRES WERE REPLACED PER AMM 32-41-11 DUE TO THE FUSE PLUG BEING BLOWN DUE TO BEING OVER HEATED. THE NR 1 AND 2 BRAKE ASSEMBLIES WERE REPLACED DUE TO OVER HEATING PER AMM 32-42-27.

Part: INTERCOSTAL — CRACKED (FRAME 20) · airframe 70,847 hrs · 27,377 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION IN INTERCOSTAL AT UPPER INBD HOLE OF DOOR STOP #7 ATTACHMENT, MEASURING L=0.080 IN. REPLACED INTERCOSTAL WITH MODIFIED PART IAW SRM 51-72-11 AND EA 307247.

Part: FITTING — CRACKED (ZONE 200) · airframe 70,847 hrs · 27,377 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION AT UPPER IB HOLE IN INTERCOSTAL FITTING AT DOOR STOP #7 ATTACHMENT, FR16 BETWEEN STR10R AND STR11R, MEASURING 0.080 IN. REMOVED AND REPLACED FITTING WITH MODIFIED PART IAW SRM 51-72-11, EA 307245, AND DRAWING D53114097.

Part: ACTUATOR — FAULTY (NR 2 VSV) · airframe 69,972 hrs · 26,861 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS APPLIED T/O POWER ENG 2 COMPRESSOR VANE FAULT. EXIT RWY AND SHUTDOWN. CLASS 2 MESSAGE, ENGINE 2 FADEC. MAINTENANCE PERFORMED REMOVAL AND INSTALLATION OF ENGINE 2 VSV ACTUATOR IAW JOB CARD 26T40075005 AND 26L00071014. OKAY FOR SERVICE.

Part: ACTUATOR — UNRELIABLE (TE FLAP SYS) · airframe 69,811 hrs · 26,777 cycles

AIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO EWR ON ACCOUNT OF FLAPS FAULT INDICATION WHEN FLAPS TWO WAS SELECTED. LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TSM 27-51-00-810-810A AND REPLACED BOTH ROTARY #1 ACTUATORS IAW AMM 27-544-41-400-001A. ALL CHECKS GOOD, NO FAULTS. A/C OK FOR SERVICE. (SEE SDR # AALA201911139013)

Part: ACTUATOR — UNRELIABLE (TE FLAPS SYSTEM) · airframe 69,811 hrs · 26,777 cycles

AIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO EWR ON ACCOUNT OF FLAPS FAULT INDICATION WHEN FLAPS TWO WAS SELECTED. LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TSM 27-51-00-810-810A AND REPLACED BOTH ROTARY #1 ACTUATORS IAW AMM 27-544-41-400-001A. ALL CHECKS GOOD, NO FAULTS. A/C OK FOR SERVICE. (SEE SDR # AALA201911149019)

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 69,341 hrs · 26,485 cycles

AIRCRAFT NOT GROUNDED: LAVATORY SMOKE ALARM WENT ON BRIEFLY DURING CRUISE. F/A'S REPORT INDICATION FROM AFT RIGHT LAV. NO SMOKE NOTED. EXAMINED LAV DETECTORS, OK AT THIS TIME. ACCOMPLISHED GRD SCAN AND TEST OF LAV SMOKE DETECTORS. OPS CHECK NORMAL IAW AMM 26-17-00.

Part: HINGE — WORN (NLG DOOR) · airframe 69,019 hrs · 26,291 cycles

AIRCRAFT WAS GROUNDED: NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD HINGE WORN. REPLACED HINGE PER AMM 32-22-13.

Part: WEDGE — DEBONDED (RT WING TE FLAP) · airframe 67,996 hrs · 25,729 cycles

RIGHT WING OTBD TRAILING EDGE FLAP, TRAILING EDGE WEDGE LOWER SKIN WAS DEBONDED AND SEPERATED. THE AIRCRAFT WAS GROUNDED. REPLACED TRAILING EDGE WEDGE IAW SRM 57-53-00-283-013 AND EA 290728.

Part: LIGHT — DAMAGED (CABIN) · airframe 67,879 hrs · 25,673 cycles

AIRCRAFT NOT GROUNDED: SEAT 26 ABC EMERGENCY LIGHT IS DAMAGE. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26ABC; OPS CHECK IS GOOD IAW AMM 33-51-19.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 65,285 hrs · 24,452 cycles

EMERGENCY LIGHT TEST FAULTED ON THE FORWARD POWER SUPPLY UNIT. REPLACED THE POWER SUPPLY IAW AMM 35-51-38.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 64,060 hrs · 23,900 cycles

R2 DOOR EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS IAW AMM.

Part: OVEN — FAULTY (GALLEY) · airframe 63,335 hrs · 23,563 cycles

AIRCRAFT WAS NOT GROUNDED. DURING FLIGHT THE FORWARD GALLEY NR 2 OVEN OVERHEATED AND BURNT FOOD. REMOVED AND REPLACED GALLEY OVEN IAW CMM 25-35-53. OPERATIONAL CHECK GOOD.

Part: FAIRING — DAMAGED (LT WING) · airframe 63,139 hrs · 23,463 cycles

LEFT WING UPPER FAIRING AT THE LEADING EDGE IS MISSING. ALL FLIGHT INDICATIONS NORMAL. REPLACED LEFT WING TO FUSELAGE PANEL 191DT PER 53-35-11. AIRCRAFT WAS GROUNDED.

Part: LIGHT — DAMAGED (LT OVERWING) · airframe 63,139 hrs · 23,463 cycles

AFT LEFT OVERWING EMERGENCY LIGHT ASSY DAMAGED. REMOVED & REPLACED THE LIGHT ASSEMBLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,667 hrs · 23,249 cycles

ODOR REPORTED IN THE FOWARD CABIN DURING DESCENT. ODOR DESCRIBED OF MUSTY, DIRTY, BURNING PLASTIC. FOUND OVERHEAD AND RIGHT SIDEWALL LIGHTING AT ROWS 4, 8, 9, 13, 14, 18, 19, 24, 25 ON HIGH SETTING UNABLE TO DIM. SUSPECT CAUSE OF FAINT ODOR FROM BALLAST. PERFORMED CIDS RESET IAW AMM 23-73-00. CHECKS GOOD. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — CRACKED (FRAME 36) · airframe 62,331 hrs · 23,075 cycles

CRACK INDICATIONS ON LEFT SIDE FLOOR PRESSURE DECK PANEL FASTENER HOLES 1, 2, 3, 4, 5 AND 8 AT Y1400 AND FRAME 36, OUTBOARD END. REPAIRED THE FLOOR PANEL IAW EA 267147.

Part: FLOOR PANEL — CRACKED (FRAME 36) · airframe 62,331 hrs · 23,075 cycles

CRACK INDICATIONS ON RIGHT SIDE FLOOR PRESSURE DECK PANEL FASTENER HOLES 1, 3, 4, AND 5, OUTBOARD END AT -Y1400 AND FRAME 36. REPAIRED THE FLOOR PANEL IAW EA 267147.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM, FORWARD OUTBOARD MOUNT LAVATORY E, AT Y-1292 AND FR 66. REPLACED FLOORBEAM PER SRM 51-72-11 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND SILL FLOORBEAM AT FR 66 AND -Y1732. REPLACED FLOORBEAM PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM, FORWARD AND AFT G-5 GALLEY MOUNTS, AT -Y1292 AND FR 68. REPLACE FLOORBEAM PER SRM 51-72-11 AND 51-42-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON FORWARD CORNER UPPER SURFACE OF SHEAR PLATE AT STRINGER 23R BETWEEN FR 68 AND FR 69. REPLACED SHEAR PLATE PER SRM 51-42-11 AND SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

CORROSION ON AFT OUTBOARD MOUNT TOP SURFACE OF FLOORBEAM, LAVATORY D AT Y1292 BETWEEN FRAMES 64 AND 66. REPLACED FLOORBEAM IAW SRM 51-74-00, 51-42-11, AND 51-23-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

CORROSION ON FLOOR SUPPORT AT Y1292 BETWEEN FRAMES 68 AND 69. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, 51-42-11, AND 51-23-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

CORROSION ON AFT INBOARD TOP SURFACE MOUNT FOR LAVATORY D, CABIN FLOORBEAM AT Y765 AND FRAME 66. REPLACED FLOORBEAM IAW SRM 51-72-11 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

CORROSION ON G-5 GALLEY AFT MOUNT (TOP SURFACE ), CABIN FLOORBEAM AT Y765 AND FRAME 70. REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT AFT MOUNT FOR G-5 GALLEY FLOORBEAM AT -Y160 AND 6 INCHES FORWARD OF FR70. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON TOP SURFACE AFT MOUNT FOR G-5 GALLEY FLOORBEAM AT -Y765 BETWEEN FR 66 AND FR 70. REPLACED FLOORBEAM PER SRM 52-41-11.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 62,331 hrs · 23,075 cycles

DELAMINATION ON LEFT ELEVATOR UPPER SURFACE 55 INCHES FROM OUTER TIP AND 4 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 55-21-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON STRINGER 41L AT 3 INCHES FORWARD AND 4 INCHES AFT OF FR 26. REPAIRED STRINGER PER SRM 53-21-13.

Part: DOOR SILL — CORRODED (FRAME 55) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

CORROSION ON AFT CARGO DOOR SILL AT STRINGER 38R AND FRAME 55. REPLACED DOOR SILL IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON R2 DOOR OPENING, AFT LOWER CORNER SHAPES, AROUND SILL PLATE AT STRINGER 23R AND FR 68. REPLACED R2 DOOR AFT CORNER SILL SHAPE PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT -Y1292 BETWEEN FR 64 AND FR 69. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TOP SURFACE FLOORBEAM AT -Y765 BETWEEN FR 67 AND FR 68. REPLACED FLOORBEAM PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON TOP SURFACE OF FLOORBEAM AT Y1292 BETWEEN FR 66 AND FR 68. REPLACED FLOORBEAM PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L2 DOOR OPENING, INBOARD AT FORWARD EDGE OF SILL PLATE AT Y1589 BETWEEN FR 66 AND FR 68. REPAIRED SILL PLATE PER SRM 53-41-14.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON R-2 DOOR SILL PLATE (BOX) AT STRINGER 23R AND -Y1400, BETWEEN FR 66 AND FR 69. REPLACED R-2 DOOR SILL PLATE (BOX) PER SRM 53-42-11 AND DRAWING D53480019.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON PASSENGER FLOORBEAM AT -Y254 AND FR 66. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT OUTBOARD BOLT OF R1 DOOR SILL (GIRT BAR FITTING) AT -Y1589 AND FR 20. REPAIRED DOOR SILL PER SRM 51-75-12

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT -Y1292 BETWEEN FR 18 AND FR 20. REPLACED FLOORBEAM PER SRM 53-11-15.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD OUTBOARD BOLT ON R1 DOOR SILL (FORWARD GIRT BAR FITTING)AT -Y1589 AND FR 16. REPAIRED DOOR SILL PER SRM 51-75-15.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L-2 AFT DOOR SILL (GIRT BAR FITTING) AT Y1589 AND FR 20. REPAIRED DOOR SILL PER SRM 51-75-15.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND SIDE SHEAR PLATE AT Y1300 BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-42-01 AND SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,331 hrs · 23,075 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND SIDE SHEAR PLATE AT STRINGER 23R BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: CONTROL HANDLE — LACK OF LUBE (R1 DOOR) · airframe 62,005 hrs · 22,932 cycles

R1 EMERGENCY CONTROL HANDLE WILL NOT ARM. MAINTENANCE FOUND NO DEFECTS. AIRCRAFT WAS GROUNDED. LUBED THE MECHANISM IAW AMM 12-00-00.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 62,005 hrs · 22,932 cycles

FORWARD R1 DOOR WILL NOT ARM. LUBED R1 DOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE SLIDE IAW TASK 26L00025010.

Part: PROXIMITY SWITCH — LACK OF LUBE (SERVICE DOOR) · airframe 60,774 hrs · 22,380 cycles

AFTER SETTING TO THRUST ECAM, FLIGHT CREW RECIEVED AN AVIONICS DOOR ECAM WARNING DURING TAKEOFF ROLL. THE FLIGHT CREW ACCOMPLISHED A LOW SPEED ABORTED TAKEOFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBED THE AVIONICS DOOR PROXIMITY SWITCHES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,759 hrs · 22,375 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241JF DELAMINATED. REPLACED FLOOR PANEL 241JF IAW AMM 53-32-12.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,759 hrs · 22,375 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241LF DELAMINATED. REPLACED FLOOR PANEL 241LF IAW AMM 53-32-12.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 60,759 hrs · 22,375 cycles

AIRCRAFT IN BASE MAINTENACE, RT BOX BEAM UPPER FLANGE HAS 2 FASTENER HOLES WITH CRCK INDICATIONS, 3RD FASTENER HOLE FROM FORWARD AND THE AFT FASTENER HOLE, AT FRAME 43 AND -Y16.50. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,432 hrs · 22,224 cycles

EMERGENCY LIGHT COVER IS BROKEN & THE INSIDE HOUSING IS COMING OUT AT THE LAST SEAT ROW ON THE LT SIDE OF THE ACFT. REPLACED THE LENS COVER AT THE LAST SEAT ROW ON THE LT SIDE OF THE ACFT.

Part: LENS — BROKEN (R1 DOOR) · airframe 59,640 hrs · 21,893 cycles

AIRCRAFT IS NOT GNDED. EXIT LIGHT COVER AT BOTTOM OF 1R DOOR BROKEN. REPLACED EXIT LIGHT LENS AT 1R DOOR.

Part: RECEPTACLE — ARCED (EXTERNAL POWER) · airframe 59,564 hrs · 21,861 cycles

AIRCRAFT WAS NOT GNDED. RAMP REPORTS EXTERNAL POWER RECEPTACLE DAMAGED WITH SIGNS OF ARCING. REPLACED EXTERNAL POWER RECEPTACLE IAW AMM 24-41-51-000-001-A & 24-41-51-400-001-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: APU — ODOR (ZONE 100) · airframe 59,285 hrs · 21,743 cycles

AFTER LANDNG USED APU BLEED, HAD A BURNED FUEL SMELL OR DIRTY SOCK SMELL. REPLACED APU & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW TASK CARD 26L31049005.

Part: HYDRAULIC LINE — LEAKING (ZONE 400) · airframe 58,562 hrs · 21,432 cycles

FLIGHT 0627 DIVERTED DUE TO A GREEN HYD FAILURE. IT WAS VERIFIED THROUGH MX THAT THE SYS HAD FAILED COMPLETELY. THE CREW DID DECLARE AN EMER WITH ATC & THE FLIGHT LANDED & TAXIED IN SAFELY. R & R GREEN PRESS LINE LOCATED IN THE LT PYLON IAW AMM 29-11-49-000-013-A & 29-11-49-400-013-A. ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 58,499 hrs · 21,406 cycles

SEAT MOUNTED EMER LIGHT AT ROW 26L INOPERATIVE, WIRES BROKEN. REPLACED WIRES, REWIRED SEAT MOUNTED EMER LIGHT AT ROW 26LIN IAW TO ESPM 20-33-11. OPERATIONS CHECKED GOOD.

Part: COVER — LOOSE (ENGINE) · airframe 58,309 hrs · 21,316 cycles

FLIGHT 574 NOTIFIED DISPATCH THAT THEY BEGAN TO LOSE OIL QTY WHILE EN-ROUTE. THEY STATED THAT IT WAS OK TO CONTINUE & RECEIVED NO ECAM MSGS RELATED. ON APPROACH, THE CREW ASKED FOR NO UNDUE DELAYS DUE TO OIL QTY BEING LOW. ATC DECLARED AN EMER FOR THE FLIGHT. THE CAPTAIN SPECIFICALLY TOLD ATC THAT IT WAS NOT AN EMER SITUATION. THE FLIGHT SAFELY LANDED WITHOUT ISSUE. FOUND THE GEAR BOX CRANK COVER LOOSE. RE-INSTALLED COVER, SERVICED OIL & ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: LENS — MISSING (CABIN) · airframe 56,581 hrs · 20,653 cycles

EXIT LIGHT LENS AT SEAT 13C MISSING. REPLACED EXIT LIGHT LENS ON 13C.

Part: LIGHT — CRACKED (CABIN) · airframe 54,515 hrs · 19,858 cycles

AFT DOOR EMERGENCY EXIT LIGHT IN AISLE CRACKED. REPLACED EMERGENCY LIGHT HOUSING ASSEMBLY 52WL IAW AMM 33-51-17-0401.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,464 hrs · 19,491 cycles

EMERGENCY EXIT LIGHT AT ROW 10 LT INOPERATIVE. REPLACED LIGHT ASSEMBLY EMERGENCY EXIT LIGHT AT ROW 10 LT.

Part: LENS — MISSING (CABIN) · airframe 53,162 hrs · 19,392 cycles

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

Part: CONNECTOR — BROKEN (CABIN) · airframe 52,845 hrs · 19,301 cycles

ROW 24 EMERGENCY PATHWAY LIGHT INOPERATIVE. REPAIRED BROKEN CONNECTOR AT LOWER SIDEWALL ROW 24. REPLACED WIRE SEGMENT FROM SIDEWALL TO SEAT.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 52,631 hrs · 19,226 cycles

RETURNED TO GATE FOR LAVATORY D SMOKE DETECTOR FAULT. REPLACED LAVATORY D SMOKE DETECTOR IAW A320 AMM 28-17-15-401.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 52,567 hrs · 19,206 cycles

EMERGENCY LIGHT POWER SUPPLY UNIT AIRCRAFT LT HAS AN INTERNAL FAULT. REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT AIRCRAFT LT IAW A320 AMM 33-51-38-0401.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,195 hrs · 19,078 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS COVER MISSING AT 24C. MAINTENANCE REPLACED EMERGENCY LIGHT LENS COVER AT 24C.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 51,588 hrs · 18,849 cycles

FWD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FWD EMERGENCY FLASHLIGHT.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 51,244 hrs · 18,742 cycles

SEAT MOUNTED EMERGENCY LIGHT LENS IS MISSING AT ROW 24L. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT AT ROW 24L.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 51,064 hrs · 18,687 cycles

AFT F/A STATION , EMERGENCY FLASHLIGHT RED LED CHARGING LIGHT NOT FLASHING. REPLACED BATTERY PACK FOR FLASHLIGHT OPS CHECKED GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 49,433 hrs · 18,203 cycles

LEFT SIDE EMERGENCY LIGHT POWER SUPPLY UNIT FAULT ON SELF TEST. REPLACED POWER SUPPLY UNIT PER A/M/M 33-51-38, OPERATIONAL CHECK OK.

Part: CONTROL UNIT — DEFECTIVE (SMOKE DETECTOR) · airframe 49,333 hrs · 18,172 cycles

AFT LAVS FAILED SMOKE DETECTOR TEST. REMOVED AND REPLACED SMOKE DETECTOR CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 26-13-00.

Part: LENS — MISSING (CABIN) · airframe 47,755 hrs · 17,616 cycles

EMERGENCY EXIT LIGHT COVER AT 2L MISSING. REPLACED LIGHT LENS AT 2L DOOR.

Part: GEARBOX — LEAKING (APU) · airframe 46,325 hrs · 17,165 cycles

STRONG ODOR REPORTED ON INBOUND FLIGHT AND AGAIN AT GATE DURING BOARDING. MAINTENANCE FOUND OIL LEAKING INTO APU PLENUM ASSEMBLY AT CASE SPLIT SEAL AND SEVERAL EXTERNAL LEAKS. REMOVED AND REPLACED THE APU. CONFIRMED LEAK AT GEARBOX LIP SEAL.

Part: PACKING — LEAKING (APU) · airframe 46,257 hrs · 17,139 cycles

DIRTY SOCK ODOR IN CABIN WITH APU PROVIDING BLEED AIR. ODOR DISSIPATED IN FLIGHT. MAINTENANCE FOUND OIL LEAK AT APU TURBINE AREA. REPLACED TURBINE BEARING CAVITY VENT O-RINGS AND PERFORMED APU WASH IAW MM 49-00-00-100-001.

Part: O-RING — LEAKING (APU) · airframe 46,182 hrs · 17,116 cycles

PACKS WERE EMITTING A PUNGENT, ACRID ODOR, MAINTENANCE FOUND EXTERNAL LEAK AT APU STARTER ADAPTER PAD. REPLACED ADAPTER PAD O-RING IAW AIRBUS MAINTENANCE MANUAL 49-42-51. LEAK CHECK GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 45,938 hrs · 17,034 cycles

FORWARD ESPU FAILED TEST (MESSAGE: INTERIOR LIGHTS FAULT). REMOVED AND REPLACED EPSU AS REQUIRED PER AMM 33-51-38.

Part: FITTING — LEAKING (APU) · airframe 44,894 hrs · 16,655 cycles

CREW REPORTED A DIRTY SOCK ODOR IN CABIN AND FLIGHT DECK OUT OF 10'000 FEET. MAINTENANCE FOUND OIL LEAKS AT APU OIL TANK QUICK DISCONNECTS AND APU OIL SCAVENGE TUBES. REPLACED QUICK DISCONNECT FITTINGS AND PACKINGS ON OIL SCAVENGE TUBES.

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 44,540 hrs · 16,536 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 9 RIGHT. REPLACED CONNECTOR.

Part: FLEX HOSE — BURST (HYDRAULIC SYS) · airframe 44,247 hrs · 16,425 cycles

IN CRUISE, GREEN HYDRAULIC SYSTEM LOST, FLUID LEVEL INDICATES EMPTY. DIVERTED TO SEA AND DECLARED EMERGENCY LANDING. FOUND A BURST (EDP) ENGINE DRIVEN PUMP PRESSURE TRANSMITTER FLEX HOSE CAUSING POSSIBLE EDP CAVITATION. REMOVED AND REPLACED PRESSURE TRANSMITTER FLEX HOSE. REMOVED AND REPLACED NR 1 EDP AS PRECAUTION. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 43,470 hrs · 16,183 cycles

ROW 11 EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED EMERGENCY LENS ON WALL AT ROW 11AC.

Part: ACCESS PANEL — NOT SEATED (CABIN) · airframe 43,017 hrs · 16,040 cycles

PHX - EEL - LEFT OVERWING DOOR LIGHT INTERMITTENT. MAINTENANCE RE-SEATED FORWARD EMERGENCY EXIT ACCESS PANEL. OPS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,000 hrs · 16,034 cycles

PHX - EEL - AFT FLASHLIGHT (2) NOT BLINKING. MAINTENANCE REPLACED AFT RIGHT FLASHLIGHT BATTERY AS REQUIRED.

Part: SKIN — CRACKED (ELEVATOR)

LEFT ELEVATOR AREA CRACKED 91 INCHES FROM OUTBOARD EDGE. REPAIRED LEFT ELEVATOR AREA 91 INCHES FROM OUTBOARD EDGE IAW A320 SRM 55-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,987 hrs · 16,028 cycles

MIA - S5 - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR65, LBL 48. REPLACED FLOOR SUPPORT BEAM AT FR65, LBL48 IAW A320 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,987 hrs · 16,028 cycles

MIA - S5 - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR16, LBL 22. REPLACED FLOOR SUPPORT AT FR16, LBL 22 IAW A320 SRM 53-11-14 & 51-42-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,987 hrs · 16,028 cycles

MIA - S5 - CORROSION ON FUSELAGE EXTERNAL SKIN AT FR28, S38L, LBL 45. REPAIRED FUSELAGE EXTERNAL SKIN AT FR28, S38L, LBL45 IAW A320 SRM 53-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,987 hrs · 16,048 cycles

MIA - S5 - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR68, Y31. REPLACED FLOOR SUPPORT AT FR68, Y31 IAW A320 SRM 51-40-00 & 51-72-11.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 42,744 hrs · 15,936 cycles

FLT 70 - SEA - EEL - EMERGENCY LIGHT AT SEAT 3C AISLE LIGHT IS INOPERATIVE. MAINTENANCE INSPECTED LIGHT ASSEMBLY AND FOUND CONNECTOR AT SIDEWALL DISCONNECTED. RECONNECTED AND OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,624 hrs · 15,897 cycles

FLT 191 PHX - EEL - AFT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN AFT FLASHLIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 42,432 hrs · 15,826 cycles

FLT 174 PHX - EEL - ROW 19 FLOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMP WAS NO HELP. MAINTENANCE REPAIRED WIRING AT SEAT EMERGENCY LIGHT AT ROW 19 LEFT.

Part: LENS — BROKEN (L1 DOOR) · airframe 42,316 hrs · 15,781 cycles

LOG PAGE 7280599 - FLT#454-PHX - EEL - EMERGENCY LIGHT COVER NEAR FRONT ENTRY DOOR BROKEN OFF. MAINTENANCE REPLACED LENS AT L1 DOOR.

Part: EPSU — FAULTY (CABIN) · airframe 41,570 hrs · 15,511 cycles

FLT 148 - PHX - EEL - EMERGENCY LIGHTS FLASHED FOR APPROX 5 MINUTES ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT 11WL AIRCRAFT LEFT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-400-001.

Part: SMOKE DETECTOR — DEFECTIVE (E/E BAY) · airframe 40,624 hrs · 15,168 cycles

FLT 84 - RTF - DURING INITIAL TAKEOFF AND CLIMB, HAD AVIONICS SMOKE ECAM WARNING. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PHL. MAINTENANCE FOUND DOOR TO AIR FILTER OPEN. CHANGED FILTER AND SECURED DOOR CLOSED; ALSO REPLACED THE SMOKE DETECTOR FOR PRECAUTIONARY PURPOSES. SMOKE DETECTOR, MPN CG7G0, IS BEING REPLACED ON ATTRITION BY MPN CGDU2000-00.

Part: CYLINDER — LEAKING (L1 DOOR) · airframe 40,171 hrs · 15,030 cycles

PHL - EES - L-1 DOOR ASSIST DAMPER CYLINDER LEAKING. MAINTENANCE REMOVED AND REPLACED L-1 DOOR CYLINDER.

Part: BOTTLE — LOW PRESSURE (ENTRY DOOR) · airframe 38,961 hrs · 14,621 cycles

FLT 73 - SEA - EES - FORWARD ENTRY DOOR EMERGENCY ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED FORWARD ENTRY DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 38,635 hrs · 14,501 cycles

FLT 69 - LAS - EES - L1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED L1 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 38,384 hrs · 14,415 cycles

FLT 493 - DEN - EES - DOOR L-2 ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED L-2 DOOR ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: LENS — DETACHED (CABIN) · airframe 37,962 hrs · 14,258 cycles

FLT 230 - PHX - EEL - EMERGENCY EXIT LIGHT COVER AT 15C FELL OFF. MAINTENANCE RE-INSTALLED COVER.

Part: HINGE FITTING — EXCESS PLAY (LT MLG DOOR) · airframe 37,306 hrs · 14,019 cycles

SAL - TRIPLE GEAR CHANGE - MAJOR REPAIR - EXCESSIVE PLAY AND CORROSION ON FORWARD HINGE ASSEMBLY OF LEFT MAIN LANDING GEAR DOOR. REPLACED HINGE ASSEMBLY OF LEFT MAIN LANDING GEAR DOOR IAW A320 CMM 52-81-18.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 37,306 hrs · 14,019 cycles

SAL - TRIPLE GEAR CHANGE - MAJOR REPAIR - EXCESSIVE PLAY ON NOSE LANDING GEAR AFT DOOR AT RIGHT OUTBOARD SIDE. REPLACED NOSE LANDING GEAR AFT DOOR AT RIGHT OUTBOARD SIDE IAW A320 SRM 51-72-11.

Part: CONNECTOR — LOOSE (CABIN) · airframe 35,989 hrs · 13,552 cycles

FLT 147 - CMH-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 9 RIGHT. RECONNECTED LOOSE EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (R1 DOOR) · airframe 35,915 hrs · 13,531 cycles

FLT 614 - PHX - EES - R1 DOOR SLIDE WILL NOT ARM. ADJUSTED PROXIMITY SENSOR 4WN2 (R1 DOOR) PER AIRBUS MAINTENANCE MANUAL 52-71-00-820-002-01.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 34,917 hrs · 13,179 cycles

LOGPAGE: 8355428 - FLT 371 - CLT-PHX - EEL - FLIGHT ATTENDANT DIRECT VIEW JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE CHECKED FLASHLIGHT CHARGE AND ILLUMINATION AND FOUND OPERATIONAL WITH NO DEFECTS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,234 hrs · 12,934 cycles

FLT NR 71 ATL-PHX EMERGENCY EQUIPMENT. FLASHLIGHT AT FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. MX R&R THE FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK GOOD.

Part: APU — ODOR (APU BAY) · airframe 31,657 hrs · 12,011 cycles

LOG PAGE 7869922 - FLT NR 430 - CLT-PHX - ODOR - "DIRTY SOCKS" ODOR IS VERY STRONG IN CABIN CAUSING SEVERAL ALLERGIC REACTIONS FROM CREW MEMBERS AND PASSENGERS. MAINTENANCE CLEANED THE APU INLET IAW TASK CARD Z6D49302. RAN PACKS AND OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,085 hrs · 11,801 cycles

FLT 158 - PHX - STL - EEL - FAA RAMP CHECK, ROW 9 DEF EMERGENCY LIGHT INOP. MAINTENANCE RECONNECTED EMERGENCY LIGHT CONNECTOR 5157VC AT ROW 9DEF. SYSTEM OPS CHECKED GOOD.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - BC6 CHECK - RUDDER HINGE FITTING NR 4 WORN, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 55-36-41.

Part: FITTING — CORRODED (ZONE 200) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - C3 CHECK - CORROSION ON L2 DOOR CUTOUT LOWER CORNER FITTING, BS 808 / FR 20, S23L. REPLACED L2 DOOR CUTOUT LOWER CORNER FITTING, BS 808 / FR 20, S23 IAW A320 SRM 51-72-11.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - BC6 CHECK - RUDDER HINGE FITTING NR 1 WORN, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUDDER HINGE FITTING NR 1, VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 55-36-41.

Part: HINGE FITTING — WORN (R2 DOOR) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - BC6 CHECK - R2 DOOR LOWER HINGE FITTING WORN ALLOWING THE BEARING TO MIGRATE. REPLACED THE R2 DOOR LOWER HINGE FITTING, BEAM 2-3 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - BC6 CHECK - CORROSION ON THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3207 /FR 67. REPLACED THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3207 /FR 67 IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 30,856 hrs · 11,714 cycles

SAL - MAJOR REPAIR - BC6 CHECK - CORROSION ON CABIN FLOORBOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y1292 TO +Y1732. REPLACED CABIN FLOORBOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y1292 TO +Y1732 IAW A320 SRM 51-72-11.

Part: RESERVOIR — FAILED (ESCAPE SLIDE) · airframe 22,014 hrs · 8,411 cycles

BOS - EES - INBOUND WRITE UP INTO BOS, CREW REPORTED CIDS PANEL CAUTION LIGHT ON POST FLT MX REPORT INDICATES SLIDE BOTTLE EMER R. MAINTENANCE FERRIED AIRCRAFT TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OVERWING ESCAPE SLIDE RESERVOIR IAW AIRBUS MM 25-62-46-04.

Part: WIRE — BROKEN (NR 1 GENERATOR) · airframe 21,680 hrs · 8,283 cycles

AIR TURN BACK. DURING FLIGHT LOST APU WITH NR 1 GENERATOR ALREADY ON MEL. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 IDG IAW AMERICA WEST AIRLINES TASK CARD R5M24301. OPERATIONAL CHECKS WERE GOOD. PLACED THE APU ON MEL. TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UPON TEAR DOWN, FOUND TWO LEAD WIRES BROKEN ON THE EXCITER ROTOR. THIS STOPPED RESISTANCE FLOW AND OUTPUT TO THE CORRESPONDING PHASES, TRIGGERING THE IDG OFFLINE. UNIT WAS REPAIRED IAW CMM 24-11-79 REV. 18.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 222FF IAW T/C C1D25306.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF DUMMY RAIL Y503, AT FR 16. MAINTENANCE REMOVED DUMMY RAIL Y503, AT FR 16; INSTALLED A NEW REPLACEMENT RAIL IAW A320 SRM 51-42-1, FIG. 9-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472133; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 3 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-15, FIG. 203, PG. 219-220.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND AT NUT PLATE HOLE ON FORWARD INBOARD CORNER OF R-2 DOOR SILL AT FS 66. MAINTENANCE CUTOUT CORRODED NUT PLATE HOLE ON R-2 DOOR SILL AT FS 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW ER 26-5341-04279-RC2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472092; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D534-72172; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 262FF IAW T/C C1D25310.

Part: BEAM — CORRODED (CARGO DOOR SILL) · corrosion level 2 · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT BULK CARGO DOOR SILL BEAM Y1500 RT, BETWEEN FS 60 AND FS 62. MAINTENANCE CUTOUT DAMAGED AREAS OF AFT BULK CARGO DOOR SILL BEAM Y1500 RT AT FS 60, FS 61, AND FS 62; FABRICATED 3 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW ER 26-5341-04278-RC1.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,901 hrs · 7,192 cycles

DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 261FF IAW T/C C1D25310.

Part: TRANSDUCER — INOPERATIVE (NR 2 ENGINE) · airframe 17,430 hrs · 6,639 cycles

ON CLIMB OUT, EN ROUTE, RECEIVED ECAM MESSAGE (AIR ENG 2 BLEED ABNORMAL PRESSURE), BLEED VALVE INDICATED CLOSED WITH (0) PSI, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 2 ENG BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) IAW AMM, AND BLEED REGULATED PRESSURE TRANSDUCER (8HA2) IAW AMM, OPS & LEAK CHECKS GOOD. TEST OF TEMPERATURE LIMITATION SOLENOID THERMOSTAT S/N 2652 CONFIRMED FAILURE OF UNIT FOR LEAKAGE OUT OF TOLERANCE. SOLENOID WAS FOUND LEAKING & STICKING OPEN AND THE DIAPHRAGM HOLES WHERE ENLARGED. REPLACED BASE, SOLENOID CORE, DIAPHRAGM, SOLENOID SEAT, AND CLAPPER. UNIT TESTED GOOD IAW CMM 36-11-43.

Part: ENGINE — OVERTEMP (NR 2) · airframe 16,850 hrs · 6,417 cycles

ON APPROACH, NR 2 ENG EGT 890 DEGREES, FUEL FLOW 1300 LBS & OIL PRESS & TEMP NORM. DISCONN AUTOTHROT & MOVED POWER LEVER, EGT REMAINED ABOVE 800 DEGREES FOR 4 MIN, SHUTDOWN ENG & DECLARED EMERGENCY. MX FOUND ENG 4TH STAGE VARIABLE STATOR VAIN ACT LINKAGE BRACKET BROKEN WITH BOLT MISSING. R & R NR 2 ENG IAW T/C. INVEST REPORT OF ENG, FOUND UPPER BOLT ATTACH 4TH STAGE VSV BRACKET IN UNISON RING & MATING DOWEL MISSING, OTHER BOLT STILL IN PLACE. VSV ACT LOADS APPLIED TO BRACKET CAUSED IT TO BEND & CRACK. BOLT MAY HAVE WORKED LOOSE DUE TO DAMAGED HELICOIL. TORQUE CHECK PERFORMED ON HELICOILS, HELICOIL THAT HAD MISSING BOLT HAD TORQUE OF LESS THAN 1 FT LB PER INCH, WHILE OTHER HAD TORQUE OF 2 FT LBS PER INCH.

Part: ENGINE — OVERHEATED (NR 1) · airframe 14,381 hrs · 5,487 cycles

DURING TAKEOFF AT LAS EN ROUTE FOR SEA, AT TAKEOFF POWER NR 1 ENGINE TEMPERATURE REACHED APPROXIMATELY 620 DEGREE'S FOR LESS THAN 2 SECONDS. FLIGHT CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE INLET AND EXHAUST SYSTEM WITH NO FINDINGS PER AMM TASK 71-00-00-710-014. NO ADDITIONAL INSPECTIONS REQUIRED DUE TO ENGINE DID NOT REACH THE 635 DEGREE THRESHOLD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,901 hrs · 4,556 cycles

LAS - EEL - DURING INSPECTION THE CABIN EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES AT EMERGENCY POWER SUPPLY UNITS 10WL, 11WL, AND 13WL, OPERATIONAL TEST WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 11,009 hrs · 4,214 cycles

PHX - EEL - EMERGENCY LIGHTS SYSTEM WILL NOT TEST ON PRESS AND TEST PANEL (110RT). MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.

Part: FLOW DIVIDER — LEAKING (APU) · airframe 9,136 hrs · 3,502 cycles

CMH - APU TAILPIPE FIRE - S - WHILE AIRCRAFT WAS ON GROUND FOR RON AT CMH AUXILIARY POWER UNIT WAS PREMATURELY SHUTDOWN AND FLAMES WERE REPORTED COMING FROM THE TAILPIPE AREA, THERE WERE NO FIRE WARNINGS, EGT PROBLEMS, OR ECAM MESSAGES. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE APU COMPARTMENT, APU INLET, AND APU EXHAUST AREAS WITH NO ABNORMALITIES NOTED. SYSTEM WAS PLACED ON MEL. PHX MAINTENANCE TROUBLESHOT THE APU PER TSM 49-00-00-810-817, AND PERFORMED AN OPERATIONAL TEST IAW AMM TASK 49-00-00-710-004; FUEL WAS OBSERVED DRIPPING FROM THE DRAIN MAST AND A FUEL FLOW DIVIDER WAS REPLACED TO CORRECT THIS PROBLEM; OPERATIONAL TEST WAS REACCOMPLISHED AND CHECKED GOOD.

Part: LIGHT — BURNED OUT (ROW 14) · airframe 9,090 hrs · 3,486 cycles

WHILE ENROUTE FROM PHX TO LAX A FLIGHT ATTENDANT REPORTED A BURNING ODOR THAT SMELLED LIKE BURNING WIRES AT SEAT ROWS 14 OR 15. AT LAX MAINTENANCE OPENED THE PANELS ON BOTH SIDES OF ROW 14 AND 15 AND PERFORMED A DETAILED INSPECTION LOOKING FOR ANY ABNORMALITIES, NONE WERE NOTED WITH THE EXCEPTION OF A BURNED OUT LIGHT BULB AT SEAT STATION 14 LT, THE BULB WAS REPLACED AND THE PANELS WERE RESECURED. A DETAILED INSPECTION OF BOTH THE LT AND RT MAIN LANDING GEAR WHEEL WELLS WAS ALSO PERFORMED WITH NO DEFECTS NOTED. MAINTENANCE RAN BOTH ENGINES WITH BOTH AIR CONDITIONING PACKS ON TRYING TO DUPLICATE THE BURNING SMELL BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (PRESS CONTROL) · airframe 2,026 hrs · 769 cycles

ON CLIMB OUT THROUGH 4000 FT MSL AIRCRAFT WOULD NOT PRESSURIZE, ACCOMPLISHED ECAM ACTION (FAULT WAS DUPLICATED BY SHAKING WIRING AT MODE SELECT SWITCH)CORRECTIVE ACTION: REPLACED FAULT PIN AT CABIN PRESSURE MODE SELECT SWITCH CABIN PRESSURE CHECKED GOOD. RECOMMENDATION: REMAIN OPEN MONITOR