N978UY

Part: LEVER — LOOSE (ZONE 800) · airframe 39,912 hrs · 16,422 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER LOOSE. MAINTENANCE RESECURED 3R ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22.

Part: LEVER — LOOSE (ZONE 800) · airframe 39,711 hrs · 16,335 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVEL LOOSE. MAINTENANCE RESECURED ARMING LEVER PER AMM 52-22-22.

Part: PLATE — LOOSE (ZONE 800) · airframe 39,527 hrs · 16,262 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ARM HANDLE DOOR 3R IS LOOSE. MAINTENANCE TIGHTENED ATTATCH BOLT FOR SLIDE ARM/DISARM YELLOW GRIP PLATE PER AMM 52-22-22.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 39,421 hrs · 16,215 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT 5C IS OUT. MAINTENANCE FOUND CONNECTOR ON HARNESS UNDER THE SEAT LOSE. INSTALLED CONNECTOR CORRECTLY IAW AMM 33-51-18.

Part: SCREW — LOOSE (DOOR LEVER) · airframe 39,141 hrs · 16,102 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER IS LOOSE. MAINTENANCE TIGHTENED LOOSEN SCREW ON DOOR 3R ARM LEVER PER AMM 20-21-11.

Part: DOOR LATCH — STICKING (ZONE 800) · airframe 39,121 hrs · 16,092 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR TOP LATCH WOULD NOT DISENGAGE AFTER ARRIVAL. MAINTENANCE REPLACED CENTER LATCH DOOR MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-21.

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 38,790 hrs · 15,968 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LEFT LAVATORY LOCK IS DIFFICULT TO LOCK AND UNLOCK. PASSENGERS KEEP GETTING LOCKED INSIDE. MAINTENANCE ADJUSTED MID CABIN LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00.

Part: LEVER — LOOSE (ZONE 800) · airframe 38,714 hrs · 15,932 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING LEVER FOR DOOR 2R LOOSE. MAINTENANCE SECURED ARMING HANDLE PER AMM 20-21-11.

Part: HANDLE — LOOSE (ZONE 800) · airframe 38,544 hrs · 15,863 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING LEVER AT 3R IS LOOSE. MAINTENANCE SECURED ARM/DISARM HANDLE TAB PER AMM 52-22-22.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 38,014 hrs · 15,633 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: LEVER — UNSECURE (ZONE 800) · airframe 37,927 hrs · 15,591 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER BROKEN. MAINTENANCE SECURED DOOR ARMING LEVER TAB AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 37,920 hrs · 15,585 cycles

AIRCRAFT WAS NOT GROUNDED: 3L CHECK SLIDE PRESSURE MESSAGE. MAINTENANCE SERVICED 3L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BULB — NO TEST (ZONE 200) · airframe 37,687 hrs · 15,484 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY LIGHTING FOUND INOPERATIVE ON SEAT 28C. REPLACED LED BULB PER AMM 33-51-18.

Part: LEVER — LOOSE (ZONE 800) · airframe 37,585 hrs · 15,442 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THE ARMED LATCH FOR SLIDE 3R IS LOOSE. MAINTENANCE RESECURED ARMING LEVER LATCHED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-00.

Part: WIRE — BROKEN (ZONE 200) · airframe 37,357 hrs · 15,328 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 15L HAS WIRING EXPOSED AND BROKEN. MAINTENANCE REPAIRED EMERGENCY LIGHTING WIRING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 37,292 hrs · 15,304 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND FORWARD DOOR 831, DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE IN THE YELLOW BAND. MAINTENANCE SERVICED DAMPER PER AMM 52-10-00-614-001.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 37,174 hrs · 15,256 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED 2 SPURIOUS LAVATORY SMOKE ECAMS FOR THE MID LAVATORY. THE FLIGHT ATTENDANTS INVESTIGATED AND FOUND NO EVIDENCE OF SMOKE OR AEROSOL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF MID LAVATORY SMOKE DETECTOR PER AMM 26-17-00-710-001-A WITH NO FAULTS FOUND.

Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 36,781 hrs · 15,074 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR WILL NOT ARM. MAINTENANCE FOUND ARMING GRIPBAR PACK PUSHING ON MECHANISM, MOVED AWAY AND SECURED IN PLACE IAW AMM 52-10-00 AND 52-11-22.

Part: SLIDE — DEFORMED (ZONE 800) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 SLIDE IS DEFORMED. REPLACED SLIDE PER TASK CARD 26C84152006.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 36,777 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,777 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,777 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA FLOOR BEAM LOCATED BETWEEN FR 12 AND FR 24 AT +Y1292 REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,777 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11.

Part: HOOK — WORN (ZONE 800) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 INNER CONTROL HANDLE HOOK WORN. REPLACED INNER CONTROL HANDLE HOOK PER CMM 52-13-15 AND AMM 52-13-21-400-001-A.

Part: HOOK — WORN (ZONE 800) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 INNER CONTROL HANDLE HOOK WORN. REPLACED INNER CONTROL HANDLE HOOK PER CMM 52-13-15 AND AMM 52-13-21-400-001-A.

Part: HOOK — WORN (ZONE 800) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 INNER CONTROL HANDLE HOOK WORN. REPLACED DOOR INNER CONTROL HANDLE HOOK PER CMM 52-11-15 AND AMM 52-11-21-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 36,778 hrs · 15,073 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: FLAP SYSTEM — WARNING MESSAGE (ZONE 500) · airframe 36,708 hrs · 15,040 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING A FLIGHT CONTROL FLAP SYSTEM 2 FAULT WHEN MOVING FLAPS FROM 2 TO 1 ON TAKEOFF. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 27-51-00-810-814 STEP A(5) SINGLE MOTOR OPERATIONAL TEST OF THE FLAP SYSTEM WITH NO FAULTS NOTED.

Part: HANDLE — LOOSE (R2 DOOR) · airframe 35,790 hrs · 14,615 cycles

AIRCRAFT WAS NOT GROUNDED: THE EXIT ROW DOOR 2R THE ARM SIGN ON THE DOOR IS LOOSE. MAINTENANCE TIGHTENED THE ARMED HANDLE ON THE R2 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LATCH — FAULTY (COCKPIT DOOR) · airframe 34,962 hrs · 14,236 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR WILL NOT OPEN NORMALLY. SEEMS LIKE THE BOTTOM LATCH ISN'T WORKING. HAD TO USE THE UNLOCK SWITCH TO OPEN THE DOOR. REMOVED AND REPLACED FLIGHT DECK DOOR LATCH MECHANISM PER AMM 52-51-21.

Part: TRANSFER VALVE — WARNING MESSAGE (LT WING) · airframe 34,583 hrs · 14,058 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUL DUE TO CENTER TANK LEFT TRANSFER FAULT IN FLIGHT. FLIGHT CREW FOLLOWED ECAM PROCEDURES. LEADING TO ENGINE 1 FUEL PUMPS OFF ALLOWING FUEL BURN FROM RIGHT TANK ONLY. THE AIRCRAFT LANDED SAFELY AT TUL. MAINTENANCE ACCOMPLISHED TSM 28-26-00-810-828-A AND FAULT COULD NOT BE DUPLICATED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 28-26-00-710-001.

Part: GUIDE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 34,048 hrs · 13,821 cycles

AIRCRAFT WAS NOT GROUNDED: MIDDLE LAVATORY DOOR IS HARD TO OPEN. MAINTENANCE ADJUSTED THE LAVATORY DOOR GUIDE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FAULTY (ZONE 900 - LAV/G) · airframe 32,930 hrs · 13,319 cycles

AIRCRAFT WAS GROUNDED: DURING CLIMBOUT LAVATORY SMOKE WARNING ON ELECTRONIC CENTRALIZED AIRCRAFT MONITOR WITH NO ONE IN LAVATORY. FLIGHT ATTENDENT REPORTS BURNT POPCORN SMELL IN FORWARD GALLEY, ELECTRONIC CENTRALIZED AIRCRAFT MONITOR WARNING AND SMELL WENT AWAY. CONTINUED TO DFW WITH DISPATCH CONCURENCE WHILE IN ROUTE 3 FLIGHT ATTENDENTS COMPLAINED OF BURNING EYES. ACCOMPLISHED SMOKE/ODOR/FUMES WORK CARD 26L00021001. FOUND BURNT FOOD IN FORWARD GALLEY OVEN, REMOVED TRAY FROM OVEN, ACOMPLISHED REMOVAL AND INSTALLATION FORWARD LAVATORY "A" SMOKE DETECTOR PER AMM 26-17-15.

Part: TRACK — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 32,793 hrs · 13,248 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT E LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBED LAVATORY E DOOR TRACK AND ACCOMPLISHED A SATISFACTROY OPERATIONAL CHECK.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 31,724 hrs · 12,742 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING HANDLE ON DOOR 3R IS LOOSE. MAINTENANCE TIGHTENED ARM/DISARM HANDLE PER AMM 52-22-22.

Part: LOCK — STICKING (ZONE 900 - LAV/G) · airframe 31,678 hrs · 12,720 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE. REPLACED MID LAVATORY DOOR LOCK PER CMM 25-43-24 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — UNKNOWN · airframe 31,577 hrs · 12,675 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY BIFOLD DOOR JAMMED, WILL NOT OPEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DOOR — JAMMED (ZONE 900 - LAV/G) · airframe 31,577 hrs · 12,675 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY BIFOLD DOOR JAMMED, WILL NOT OPEN. **SUPPLEMENTAL REPORT FOR AALA202303164088: REPLACED MID LAVATORY DOOR PER AMM 25-42-41 AND ACCOMPKISHED A SATISFACTORY OPERATIONAL CHECK.** (CLOSED)

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 31,432 hrs · 12,594 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED : AT 4000 FT MSL INTERCEPTING FINAL APPROACH AT VPS . RECEIVED RIGHT ENGINE COMPRESSOR VANE STALL ON ECAM. WITHIN 30 SECONDS RECEIVED ENGINE FAIL ECAM ACCOMPANIED BY AN AUDIBLE AND PHYSICAL THUMP, ACCOMPLISHED ECAM FOR ENGINE FAILURE AND LANDED IN APPROX, 10 MINUTES. NO RELIGHT ATTEMPTED. THE AIRCRAFT LANDED AT VPS SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 31,432 hrs · 12,594 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED : AT 4000 FT MSL INTERCEPTING FINAL APPROACH AT VPS . RECEIVED RIGHT ENGINE COMPRESSOR VANE STALL ON ECAM. WITHIN 30 SECONDS RECEIVED ENGINE FAIL ECAM ACCOMPANIED BY AN AUDIBLE AND PHYSICAL THUMP, ACCOMPLISHED ECAM FOR ENGINE FAILURE AND LANDED IN APPROX, 10 MINUTES. NO RELIGHT ATTEMPTED. THE AIRCRAFT LANDED AT VPS SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202302201409: MAINTENANCE REPLACED #2 ENGINE PER TASK CARD 26L40071004. ** (CLOSED)

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 30,422 hrs · 12,129 cycles

AIRCRAFT WAS NOT GROUNDED: 2R DOOR ARMING LEVER NEEDS TIGHTENED. MAINTENANCE TIGHTENED 2R DOOR ARMING LEVER PER AMM 52-22-22.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 30,176 hrs · 12,016 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARMING HANDLE IS LOOSE. MAINTENANCE RE-SECURED ARMING HANDLE ON EMERGENCY EXIT DOOR 3R AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — NONE (ZONE 500 - LH WI) · airframe 29,674 hrs · 11,808 cycles

AIRCRAFT WAS GROUNDED: LEFT TRANSFER FAULT-ECAM ACTION DID NOT CLEAR LEFT TANK -14000 AND STAYING CENTER 3800 RIGHT 12000 UNABLE TO GET FUEL OUT OF LEFT TANK. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FUEL CONTROL VALVE ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-26-43.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 29,605 hrs · 11,765 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR EMERGENCY EXIT ARMING HANDLE IS LOOSE. TIGHTENED R3 EXIT DOOR ARMING HANDLE AS REQUIRED.

Part: LOCK — STICKS (ZONE 900 - LAV/G) · airframe 29,141 hrs · 11,549 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY C DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED LOCK ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 28,842 hrs · 11,418 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN EMERGENCY EXIT LIGHT EMERGENCY POWER SUPPLY UNIT 15WL CHARGER ABOVE L2 DOOR IS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: LOCK — JAMMED (ZONE 900 - LAV/G) · airframe 28,471 hrs · 11,282 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR IS JAMMED OR DAMAGED. REPLACED UPPER DOOR LOCK ON MID LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-50-00.

Part: DOOR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 28,341 hrs · 11,224 cycles

AIRCRAFT WAS NOT GROUNDED: MAIN CABIN ENTRY DOOR DIFFICULT TO OPEN AFTER ARRIVAL AT THE GATE. LUBRICATED MAIN CABIN ENTRY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 12-22-520 AND AMM 52-10-00.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 28,289 hrs · 11,202 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR ARMING LEVER IS LOOSE. TIGHTENED ATTACHING HARDWARE ON R3 DOOR ARMING LEVER .

Part: POWER SUPPLY — ODOR (SEAT 26DEF) · airframe 27,649 hrs · 10,926 cycles

AIRCRAFT WAS GROUNDED: ODOR SMELL ACRID AT 1950Z FL 310 .NOTICED AROUND ROW 26, SMELL DISSIPATED AFTER 5 MINUTES. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE IN SEAT POWER SUPPLY AT SEAT ROW 26DEF AND ACCOMPLISHED A RESET OF THE SYSTEM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER THE VIASAT AMM 25-21-42.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 27,174 hrs · 10,735 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THAT THE DOOR 1L ARMING LEVER FEELS VERY TIGHT AND DIFFICULT TO ARM. CLEANED AND LUBRICATED GIRT BAR FITTINGS AND LINKAGE, INSPECTED DOOR 1L AND FUNCTIONAL CHECKED PER AMM 52-10-00.

Part: PUMP — LOW PRESSURE (LT FUEL BOOST) · airframe 27,146 hrs · 10,725 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM MESSAGE FUEL LEFT FUEL L TK PUMP 1 LO PR INDICATED DURING CLIMB FL 280. REPLACED LEFT HAND FUEL PUMP #1 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 28-21-51.

Part: HANDLE — LOOSE (R3 DOOR) · airframe 26,096 hrs · 10,285 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARM LEVER IS LOOSE. SECURED ARMING LEVER HANDLE PER AMM 52-22-22.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 25,811 hrs · 10,157 cycles

AIRCRAFT WAS NOT GROUNDED. 1L FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: GRIP — LOOSE (R3 DOOR LEVER) · airframe 25,710 hrs · 10,106 cycles

AIRCRAFT WAS NOT GROUNDED. LOOSE DISARM LEVER GRIP ON R3 DOOR. SECURED DISARM LEVER GRIP, IAW AMM 25-23-47, OPERATIONS CHECK GOOD.

Part: RELAY — INOPERATIVE (THRUST REVERSER) · airframe 25,309 hrs · 9,937 cycles

AIRCRAFT WAS GROUNDED. LOW SPEED REJECTED TAKEOFF AT 60 KTS. ENGINE REVERSER MASTER CAUTION LIGHT/ECAM INDICATION DISPLAYED. PERFORMED GROUND SCAN OF FADEC 1A, GROUND SCAN REPORTED T/R SOV/HCU/HC1. PERFORMED TSM TASK 78-37-00-810-809-A13. REMOVED AND REPLACED STATIC RELAY 3EG1, PER ESPM 20-46-50. OPERATIONAL CHECKS GOOD.

Part: LEVER — LOOSE (R3 DOOR) · airframe 25,267 hrs · 9,920 cycles

AIRCRAFT WAS NOT GROUNDED: 3 RIGHT EXIT DOOR ARMING LEVER IS LOOSE. TIGHTENED 3R ARMING LEVER HANDLE ATTACH BOLT CHECKS OK.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 25,233 hrs · 9,908 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4L EXIT LIGHT COVER FELL OFF. RESECURED LIGHT COVER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,920 hrs · 8,990 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT LENS MISSING AT ROW 1 LEFT. MAINTENANCE REPLACED LIGHT AT ROW 1 LEFT PER AMM 33-51-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,920 hrs · 8,990 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT LENS MISSING AT ROW 8 LEFT. MAINTENANCE REPLACED LIGHT AT ROW 8 LEFT PER AMM 33-51-11.

Part: SOLENOID VALVE — LEAKING (NR 1 ENGINE) · airframe 22,920 hrs · 8,990 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO LAX ON ACCOUNT POSSIBLE COMPRESSOR STALL ON #1 ENGINE. EMERGENCY DECLARED. MAINTENANCE ACCOMPLISHED FULL ENGINE BORESCOPE INSPECTION IAW AMM 72-00-00-200-012, AMM 72-00-00-200-013, AMM 72-00-00-200-014, AMM 72-00-00-200-015, AMM 72-00-00-200-016 & AMM 72-00-00-200-017, NO DEFECTS FOUND. WHILE ACCOMPLISHING WORKCARD 26T40075003, FOUND STAGE 10 AIR SOLENOID VALVE LEAKING. REPLACED STAGE 10 AIR SOLENOID VALVE IAW AMM 75-23-52. LEAK AND OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 50,000 hrs · 20,000 cycles

CORROSION FOUND ON THE L4 DOOR CUTOUT LOWER SILL AT FRAME 68, +Y1447.8. REPLACED THE DOOR SILL IAW SRM 51-42-11.

Part: BEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 20,260 hrs · 7,980 cycles

CORROSION ON THE BEAM, FR 68, RBL -Y1292. REPAIRED THE BEAM IAW SRM 53-41-14-300-001 NR 5.

Part: FITTING — CORRODED (BS 7599) · corrosion level 2 · airframe 20,260 hrs · 7,980 cycles

CORROSION ON L1 DOOR CUTOUT LOWER SILL SEAL SHAPE FITTING AT BS 7599 AND STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11-911-001.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 19,856 hrs · 7,823 cycles

AFT CARGO FLOOR PANEL 151QF WAS SPONGY. REPLACED THE FLOOR PANEL IAW AMM 53-42-14-04.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 19,676 hrs · 7,747 cycles

L1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,676 hrs · 7,747 cycles

EMERGENCY LIGHT AT SEAT 3L, THE LENS WAS BROKEN. REPLACED LIGHT ASSY IAW AMM 33-51-09.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 19,577 hrs · 7,712 cycles

EXIT LIGHT COVER AT THE L1 DOOR WAS DAMAGED. INSTALLED EXIT LIGHT COVER IAW AMM 52-20-00.

Part: CAP — MISSING (ELECT CONNECTOR) · airframe 19,015 hrs · 7,511 cycles

EMERGENCY LIGHT AT SEAT 30L CONNECTOR CAP MISSING. INSTALLED THE CAP.

Part: LIGHT — MISSING (CABIN) · airframe 18,223 hrs · 7,199 cycles

EXIT LIGHT AT THE LOWER L4 DOOR MISSING. INSTALLED THE EXIT LIGHT IAW AMM 33-50-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,832 hrs · 7,051 cycles

LENS MISSING FROM THE EMERGENCY LIGHT AT THE R1 DOOR. INSTALLED A NEW LENS.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 17,682 hrs · 6,995 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 25 MOUNTED EMERGENCY/ESCAPE PATH LIGHT INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR THAT HAD COME UNDONE PER AMM 33-51-19.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,682 hrs · 6,995 cycles

THE AIRCRAFT WAS NOT GROUNDED. CEILING LIGHT EMERGENCY LIGHT INOPERATIVE AT ROW 18. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IN CEILING PER AMM 33-51-11. OPERATIONS CHECK GOOD AT THIS TIME.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 17,682 hrs · 6,995 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: LENS — MISSING (DOOR ASSIST BOTT) · airframe 17,682 hrs · 6,995 cycles

R1 DOOR, ASSIST GAUGE VIEWING LENS MISSING. MAINTENANCE INSTALLED VIEWING LENS FOR DOOR ASSIST BOTTLE AT R1 DOOR PER AMM 25-23-46 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLOORBOARD — DELAMINATED (AFT CARGO) · airframe 17,371 hrs · 6,877 cycles

DELAMINATED FLOORBOARD 151MK IN THE AFT CARGO BAY. REPLACED THE FLOORBOARD IAW AMM 53-42-14.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 17,260 hrs · 6,831 cycles

FLIGHT ATTENDANT REPORTED A SOFT SPOT IN THE FLOOR PANEL, 6-7 INCHES WIDE IN FRONT OF 22C AND NR 3 JUMP SEAT. REPLACED THE FLOORBOARD 251BG IAW AMM 53-32-12. THE AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 17,260 hrs · 6,831 cycles

AIRCRAFT WAS NOT GROUNDED. SOFT SPOT LOCATED IN FWD GALLEY APPROX 12" FROM THRESHOLD STRIP. REMOVED AND REPLACED FLOOR PANEL 221 DF PER AMM 53-12-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,944 hrs · 6,703 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERABLE AT ROW 30 LEFT HAND. REPLACED EMERGENCY LIGHT PER AMM 33-51-19.

Part: LENS — MISSING (CABIN) · airframe 15,631 hrs · 6,215 cycles

AIRCRAFT WAS NOT GROUNDED. 4R EMERGENCY EXIT LIGHT COVER, MISSING. MAINTENANCE REPLACED EXIT LIGHT LENS COVER AT R4 DOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,542 hrs · 6,177 cycles

L1 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 15,440 hrs · 6,135 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4L ARMED LIGHT LENS BROKEN. REPLACED ARMED LIGHT LENS AT DOOR 4L AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,072 hrs · 5,987 cycles

EMERGENCY LIGHT LENS MISSING AT THE L4 DOOR. REPLACED THE LENS.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 14,496 hrs · 5,772 cycles

EMERGENCY LIGHT ON SEAT 34ABC INOPERATIVE. FOUND THE CONNECTOR LOOSE UNDER SEAT 34A. SECURED THE CONNECTOR.

Part: APU — LEAKING (ZONE 100) · airframe 13,667 hrs · 5,446 cycles

FUMES ODOR IN CABIN AT START OF DESCENT. MAINTENANCE DETERMINED THE APU WAS THE SOURCE OF THE ODOR DUE TO OIL LEAKS. REPLACED APU PER JOB CARD 26L31049003. ACCOMPLISHED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSYEM AND SATISFACTORY OPERATIONAL CHECK.

Part: OIL COOLER — LEAKING (APU) · airframe 13,585 hrs · 5,411 cycles

FLIGHT ATTENDANTS FLEW AIRCRAFT INBOUND AND ON LANDING NOTICED FOUL ODOR IN CABIN. AIRCRAFT WAS GROUNDED. REPLACED APU OIL COOLER PER AMM 49-91-44.

Part: PRIORITY VALVE — DEFECTIVE (ZONE 100) · airframe 12,699 hrs · 5,056 cycles

AIRCRAFT WAS GROUNDED: ON TAKEOFF RETRACTING THE LANDING GEAR ECAM GEAR DOORS NOT UP. RECYCLED THE GEAR GOT THE SAME ECAM. AIRCRAFT RETURNED TO DEPARTURE. R & R GREEN PRIORITY VALVE IAW AMM 29-11-33-401 LEAK AND OPS CHECKED GOOD. PERFORMED LANDING GEAR FUNCTIONAL TEST IAW AMM 32-31-00-720-002A WITH NO DEFECTS NOTED.

Part: SELECTOR VALVE — FAULTY (ZONE 100) · airframe 12,618 hrs · 5,023 cycles

AIRCRAFT WAS GROUNDED: APPROXIMATELY 2000 FT AFTER EXTENDING GEAR, HAD ECAM LANDING GEAR LEVER DISAGREE GEAR FINALLY EXTENDED AFTER 30 SECONDS THEN ECAM LANDING GEAR DOORS UNLOCKED THEN 30 SECONDS GEAR DOORS RETRACTED. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE MANIFOLD AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 32-31-31-401.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 12,521 hrs · 4,976 cycles

AIRCRAFT WAS GROUNDED: SOFT SPOT IN FORWARD GALLEY FLOOR PANEL 222EF. REPLACED FLOOR PANEL 222EF IAW AMM 53-12-12.

Part: LENS — BROKEN (L1 DOOR) · airframe 12,144 hrs · 4,839 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS AT THE L1 DOOR BROKEN. REPLACED EMERGENCY LIGHT LENS AT THE L1 DOOR.

Part: FAN — DEFECTIVE (ZONE 100) · airframe 11,454 hrs · 4,579 cycles

AIRCRAFT WAS GNDED. SLIGHT SMELL OF FUMES THEN BLOWER FAULT CAME ON, SWITCHED TO OVERRIDE. R & R BLOWER FAN 20HQ & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM TASK 21-26-51-400-001-A & AMM 21-26-51-710-001-A.

Part: PLATE — MISSING (EMERGENCY EXIT) · airframe 11,351 hrs · 4,543 cycles

AIRCRAFT WAS NOT GNDED. EMER EXIT 3R INSPECTION PLATE MISSING. REPLACED 3R SLIDE ARMING WARNING LIGHT ASSEMBLY.

Part: COMPUTER — MALFUNCTIONED (ZONE 100) · airframe 11,338 hrs · 4,539 cycles

AIRCRAFT WAS NOT GNDED. LOST PRESSURIZATION AT 3500, SELECTED MANUAL. EVALUATED & FOUND NO CABIN PRESS FAILURES ON POST FLIGHT. CABIN PRESS LDG ELEV FAULT CAUSED BY LOSS OF FLIGHT MANAGEMENT GUIDANCE COMPUTER, FMGC 1. RESET FMGC. OPERATIONAL CHECKED NORMAL IAW TSM 24-00-00-810-818-A & AMM 22-96-00.