N140AN

Part: CHILLER — ODOR (ZONE 900) · airframe 31,814 hrs · 12,430 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE ALTITUDE FLIGHT ATTENDANTS REPORTED A BURNING SMELL COMING FROM THE AFT GALLEY CENTER METAL STORAGE BOX AREA. FLIGHT ATTENDANTS TURNED OFF THE MASTER GALLEY SWITCH AND THE SMELL WAS ELIMINATED. MAINTENANCE FOUND AFT GALLEY CHILLER NO LONGER BLOWING COLD AIR AND HAD A STRANGE BURNING SMELL. MAINTENANCE REPLACED THE AFT GALLEY CHILLER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-34-51.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 30,813 hrs · 12,039 cycles

AIRCRAFT WAS NOT GROUNDED: MOMENTARY LAVATORY SMOKE WARNING ECAM AT CRUISE FL350. FLIGHT ATTENDANT COULD NOT IDENTIFY SOURCE OR ACTUAL SMOKE. MAINTENANCE ACCOMPLISHED MCDU TEST AND GROUND SCAN DETECTED NO FAULTS.

Part: SENSOR — FAULTED (ZONE 700) · airframe 30,367 hrs · 11,869 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND TO DFW DUE TO THE FLIGHT CREW REPORTING THAT AFTER TAKEOFF RECEIVED HOT BRAKES ECAM FOR NUMBER 4 BRAKE WITH TEMPERATURE OF 305C NUMBER 1 BRAKE: 75C NUMBER 2 BRAKE: 80C NUMBER 3 BRAKE: 65C NUMBER 4 BRAKE: 305C. LATER IN FLIGHT AT FL330 HOT BRAKES ECAM AGAIN FOR NUMBER 4 BRAKE AT 325C AND CLIMBING. AFTER DESCENDING WHEN WE PUT GEAR DOWN TO COOL THE BRAKE AND THE TEMPERATURE INSTANTLY DROPPED FROM 325C TO 30C. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE BRAKE TEMPERATURE SENSOR FOR THE #4 BRAKE PER AMM 32-47-15.

Part: TRANSCEIVER — FAULTED (WX RADAR) · airframe 30,350 hrs · 11,861 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ORD DUE TO THE FLIGHT CREW REPORTING THAT WEATHER RADAR NOT PICKING UP WEATHER TO DISPLAY. IN ADDITION RADAR WOULD PICK UP GROUND CLUTTER. THE AIRCRAFT LANDED SAFELY AT ORD AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCIEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 34-41-33.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 30,154 hrs · 11,777 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 29,587 hrs · 11,540 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL BATTERY PACK FAULTED DURING CIDS SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38,

Part: LIGHT — MISSING (ZONE 200) · airframe 29,360 hrs · 11,444 cycles

AIRCRAFT WAS GROUNDED: L3 DOOR EMERGENCY LIGHT COVER POPPED OFF DURING FLIGHT AND FLIGHT ATTENDANT DISCOVERED THE INTERIOR LIGHT ASSEMBLY IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900) · airframe 29,112 hrs · 11,347 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED A MOMENTARY - SMOKE LAVATORY SMOKE - ECAM MESSAGE WHICH SELF CLEARED. FLIGHT ATTENDANT REPORTS NO INDICATIONS OF SMOKE/FIRE AND/OR NO PASSENGER MISCONDUCT IN THE MID CABIN LAVATORY. MAINTENANCE ACCOMPLISHED BITE PER AMM 26-17-00 WITH NO FAULTS NOTED.

Part: WARNING MESSAGE — ILLUMINATED (ZONE 100) · airframe 28,838 hrs · 11,230 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO SEA DUE TO THE FLIGHT CREW REPORTING A LEFT WING BLEED AIR LEAK CAUTION MESSAGE. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY AT SEA WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SEAL — LEAKING (ZONE 500) · airframe 28,838 hrs · 11,230 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO SEA DUE TO THE FLIGHT CREW REPORTING A LEFT WING BLEED AIR LEAK CAUTION MESSAGE. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY AT SEA WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202412093057: MAINTENANCE FOUND THE WING ANTI ICE TAPPING COUPLING (CONNECTOR) SEALS ON THE PRE-COOLER DUCT LEAKING AND REPLACED THE SEALS PER AMM 20-26-00-910-002-A. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WIRE — LOOSE (ZONE 200) · airframe 28,640 hrs · 11,146 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LEFT HAND EMERGENCY EXIT DOOR AFT WALL EMERGENCY LIGHT (90WL3) BOTTOM INOPERATIVE. MAINTENANCE FOUND WIRE LOOSE, RECONNECTED WIRE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 28,640 hrs · 11,146 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. EPSU 10WL BATTERY FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HYDRAULIC SYSTEM — WARNING MESSAGE · airframe 28,619 hrs · 11,134 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ATL DUE TO THE FLIGHT CREW REPORTING YELLOW HYDRAULIC SYSTEM LOW LEVEL ECAM MESSAGE. THE FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY AT ATL WITHOUT FURTHER INCIDENT. ** SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 28,619 hrs · 11,134 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ATL DUE TO THE FLIGHT CREW REPORTING YELLOW HYDRAULIC SYSTEM LOW LEVEL ECAM MESSAGE. THE FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY AT ATL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC FLUID LEAKING FROM THE #2 ENGINE AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP PER AMM 29-13-51. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 28,432 hrs · 11,050 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT FLIGHT ATTENDANT SEAT LOWER FLASHLIGHT TEST BUTTON DOES NOT ILLUMINATE WHEN PRESSED. REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SENSE LINE — CONTAMINATED (NR 2 ENGINE) · airframe 28,351 hrs · 11,014 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THEY RECEIVED ENGINE 2 STALL ECAM BRIEFLY 9 TIMES DURING DESCENT BUT THE ENGINE SEEMED TO BE RUNNING NORMALLY. MAINTENANCE PERFORMED TSM 71-00-00-810-809-A AND FOUND MOISTURE IN THE PRESSURE SENSE LINE. MAINTENANCE CLEARED THE MOISTURE AND PERFORMED POWER ASSURANCE RUN WITH NO DEFECTS BEING NOTED ON THE POST FLIGHT REPORT.

Part: MEGAPHONE — BROKEN (ZONE 200) · airframe 27,848 hrs · 10,785 cycles

AIRCRAFT WAS NOT GROUNDED: AFT MEGAPHONE BROKEN. REPLACED MEGAPHONE PER TASK CARD 26L00005005.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 26,384 hrs · 10,173 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING PERIODIC SERVICE CHECK FOUND THE L2 EMERGENCY EXIT DOOR PRESSURE TO BE OUT OF LIMITS. SERVICED THE L2 EMERGENCY EXIT DOOR PRESSURE DAMPER CYLINDER.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 24,640 hrs · 9,464 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER NEEDS SERVICING. SERVICED DAMPER PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 24,640 hrs · 9,464 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER NEEDS SERVICING. SERVICED THE L4 DOOR DAMPER PER AMM 52-10-00.

Part: CONNECTOR — INOPERATIVE (ZONE 200 - FUSE) · airframe 24,418 hrs · 9,378 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 24 & 25 SEAT PATH EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PATH EMERGENCY LIGHT CANNON PLUG PER AWM 33-51-08.

Part: LOCK — STICKING (ZONE 900 - LAV/G) · airframe 23,570 hrs · 9,048 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY DOOR IS HARD TO OPEN OR CLOSE. MAINTENANCE REPLACED MID CABIN LAVATORY DOOR UPPER LOCK ASSEMBLY PER AMM 25-42-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SENSOR — DEFECTIVE (ZONE 700 - GEARS) · airframe 23,092 hrs · 8,827 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER 1+55 HOURS FLIGHT TIME, LEFT MAIN GEAR RED UNLOCK AND GREEN DOWN LOCK LIGHT ILLUMINATED INTERMITTENTLY FOR 3 MINUTES.WHEEL PAGE ALSO SHOWED LEFT GEAR LEFT GREEN TRIANGLE ILLUMINATED. MAINTENANCE REPLACED MAIN LANDING GEAR DOWN LOCK PROXIMITY SENSOR 15GA PER AMM 32-31-73-400-001-A.

Part: TAPE — LOOSE (ZONE 200 - FUSE) · airframe 23,047 hrs · 8,805 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE SPEED TAPE ON FIRST OFFICERS REAR WINDOW COMMING LOOSE, CAUSING EXTREMELY LOUD AIR LEAK FROM BEHIND THE FIRST OFFICERS SEAT. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE RE-APPLIED SPEED TAPE ON FIRST OFFICERS AFT SIDE WINDOW PER AFMM 20-11-33.

Part: DOOR LATCH — STICKS (ZONE 900 - LAV/G) · airframe 21,494 hrs · 8,159 cycles

AIRCRAFT WAS NOT GROUNDED: 1ST CLASS LAVATORY DOOR STICKS CLOSED. LUBED LAVATORY DOOR LATCH AS REQUIRED.

Part: LATCH — DIRTY (ZONE 900 - LAV/G) · airframe 20,103 hrs · 7,572 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR LOCK STICKS DIFFICULT TO UNLOCK. CLEANED AND LUBRICATED LATCH.

Part: SENSOR — DEFECTIVE (ZONE 400 - NAC/P) · airframe 20,073 hrs · 7,556 cycles

AIRCRAFT WAS GROUNDED: #1 ENGINE APPEARS NOT TO GO INTO APPROACH IDLE DURING DESCENT #1 N1 = 51.4%. #2 N1 = 36.6% AT IDLE. REPLACED FUEL TEMPERATURE SENSOR PER AMM 73-35-15 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LOCK — STICKING (ZONE 900 - LAV/G) · airframe 19,927 hrs · 7,492 cycles

AIRCRAFT WAS NOT GROUNDED: R2 LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. REPLACED LAVATORY BI-FOLD DOOR HOLD OPEN LOCK ASSEMBLY PER AMM 25-45-21.

Part: SCREW — LOOSE (ZONE 900 - LAV/G) · airframe 19,724 hrs · 7,407 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS DIFFICULT TO OPEN IN FLIGHT. SECURED ALL SCREWS ON FORWARD LAVATORY DOOR HINGE AND THRESHOLD PER AMM 25-40-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 19,635 hrs · 7,371 cycles

AIRCRAFT WAS NOT GROUNDED: 1L LAVATORY DOOR VERY DIFFICULT TO OPEN OR CLOSE IN FLIGHT. ON THE GROUND VERY EASY TO OPERATE. ADJUSTED LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — BINDING (MID LAVATORY) · airframe 18,339 hrs · 6,825 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR JAMMED. RE-INSTALLED MID LAVATORY DOOR PER AMM 25-45-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON LEFT HORIZONTAL STABILIZER (1 EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 3 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: RESERVOIR — LOW PRESSURE (DOOR SLIDE) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE EMERGENCY EXIT DOOR 843 ESCAPE SLIDE RESERVOIR IN PASSENGER CABIN (1EA). REMOVED AND REPLACED EMERGENCY EXIT DOOR 843 ESCAPE SLIDE RESERVOIR IN PASSENGER CABIN PER AMM 25-62-49-000-001-A AND AMM 25-62- 49-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 6 PER AMM 55-16-42-400-001-A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT FLASHLIGHT BY LAVATORY H INOPERATIVE. REPLACED FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: DOOR 2R FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT FLASHLIGHT BY LAVATORY D INOPERATIVE. REPLACED FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT FLASHLIGHT BY LAVATORY E INOPERATIVE. REPLACED FLASHLIGHT.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 2 PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON LEFT HORIZONTAL STABILIZER (1EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 5 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 1 PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LEFT HORIZONTAL STABILIZER (1EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 6 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON LEFT HORIZONTAL STABILIZER (1EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 4 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: HINGE — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LEFT HORIZONTAL STABILIZER (1EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 2 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: HINGE — EXCESS PLAY (LT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LEFT HORIZONTAL STABILIZER (1EA). REMOVED AND REPLACED ELEVATOR HINGE ARM 1 ON LEFT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 3 PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 5 PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 4 PER AMM 55-16-42-400-001-A.

Part: SUPPORT — CORRODED (FRM 68 S23L) · corrosion level 2 · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT LEVEL FR68 AND S23L. REPAIRED PER SRM 53-41-14-300-001.

Part: SHEAR PLATE — CRACKED (FRMS 69-70 S23R) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: L=0.765 INCH CRACK ON SHEAR PLATE AT FR69 + 4.5 INCHES AND STR 23R. REPLACED SHEAR PLATE IAW SRM A321 51-42-11-801 AND DRAWING D53474180.

Part: SHEAR PLATE — CRACKED (FRMS 69-70 S23L) · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENACE: L=0.828 INCH CRACK ON SHEAR PLATE AT FR69 + 4.5 INCHES AND STR 23L. REPLACED SHEAR PLATE IAW SRM A321 51-42-11-801 AND DRAWING D53474180.

Part: FITTING — CORRODED (FRMS 66-68 S23L) · corrosion level 2 · airframe 18,105 hrs · 6,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORRODED AREA, MEASURING L= 1.148 INCH, W= 0.360 INCH, D= 0.087 INCH, ON CENTER FITTING FROM FR66 TO FR68. AND STR 23L. REMOVED AND REPLACED CENTER FITTING AT AFT GALLEY AREA IAW A321 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53480009.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 17,952 hrs · 6,683 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAILED TEST. REPLACED BATTERY PER AMM 33-51-38.

Part: SERVO VALVE — FAULTED (MLG BRAKES) · airframe 14,760 hrs · 5,480 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY INTO MCO ON ACCOUNT OF PRIMARY BRAKE FAULT MESSAGE. FLIGHT DID A GO AROUND AND THEN LANDED USING ALTERNATE BRAKES. MAINTENANCE REMOVED AND REPLACED NORMAL BRAKE SERVO VALVE ON L/H MAIN GEAR STRUT IAW AMM 32-42-48. NORMAL BRAKING TEST BITE AND BSCU GROUND SCANNING BITE CHECKS GOOD IAW AMM 32-46-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR ASSIST) · airframe 13,461 hrs · 4,981 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS ACCUMULATOR PRESSURE LOW ON DOOR R4 PASSENGER/ CREW DOOR. SERVICED DOOR ASSIST BOTTLE PRESSURE IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 13,461 hrs · 4,981 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS ACCUMULATOR PRESSURE LOW ON DOOR L1. PASSENGER/ CREW DOOR. SERVICED DOOR ASSIST BOTTLE PRESSURE IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 13,461 hrs · 4,981 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS ACCUMULATOR PRESSURE LOW ON DOOR L4. PASSENGER/ CREW DOOR. SERVICED DOOR ASSIST BOTTLE PRESSURE IAW AMM 52-22-00.

Part: HANDLE — CRACKED (L1 DOOR) · airframe 10,251 hrs · 3,797 cycles

L1 DOOR ASSIST HANDLE CRACKED. MAINTENANCE REPLACED THE DOOR HANDLE COVER AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 9,614 hrs · 3,553 cycles

L1 DOOR WILL NOT RELEASE TOO CLOSE. LUBRICATED THE GUST LOCK MECHANISM. OPS CHECKED NORMAL IAW AMM 52-11-00.

Part: SLIDE — NONE (ZONE 800 - DOORS) · airframe 8,972 hrs · 3,323 cycles

**SUPPLEMENTAL REPORT FOR AALA201804039028 AS REQUESTED BY FAA SDR REJECTION LETTER DATED 7/7/2022** AIRCRAFT WAS GROUNDED. L2 DOOR SLIDE DUE SCHEDULED INSPECTION / OVERHAUL AND REQUIRES REPLACEMENT. MAINTENANCE REPLACED L2 DOOR SLIDE PER AMM 25-62-47-04 AND TASK CARD 25-94-02. SLIDE WAS SENT TO REPAIR VENDOR AND WAS OVERHAULED AS REQUIRED.

Part: COVER — DETACHED (DOOR HANDLE) · airframe 7,994 hrs · 2,956 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR ASSIST HANDLE TRIM COVER DETACHED. REPLACED HANDLE COVER PER AMM STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECKS.

Part: DOOR — MISSING (FUEL) · airframe 7,766 hrs · 2,862 cycles

DECLARED EMERGENCY, DUE TO A TIRE PRESSURE INDICATION. UNEVENTFUL LANDING AND TAXIED TO GATE. MAINTENANCE EVALUATED INDICATION ISSUE, NO PHYSICAL DAMAGE TO TIRE. MAINTENANCE INSPECTED AND FOUND SPEED TAPE COVERING MISSING FUEL PANEL. REPLACED FUEL DOOR ON RIGHT FUSELAGE IAW AMM 52-42-10.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 7,062 hrs · 2,589 cycles

R2 DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED R2 DOOR DAMPER CYLINDER TO CORRECT PRESSURE IAW AMM 52-22-00.

Part: CYLINDER — LOW PRESSURE (EMERGENCY EXIT) · airframe 6,901 hrs · 2,521 cycles

AIRCRAFT WAS NOT GROUNDED. R2 EMERGENCY EXIT DOOR DAMPNER PRESSURE LOW. SERVICED R2 EMERGENCY EXIT DOOR DAMPNER PER AMM 52-22-00.

Part: DOOR — LACK OF LUBE (R4) · airframe 6,807 hrs · 2,486 cycles

FLIGHT ATTENDANT REPORTED LOUD CRACK FROM THE R4 DOOR. LUBRICATED THE R4 DOOR IAW MM 12-22-52, OPERATIONAL CHECKED NORMAL.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 6,579 hrs · 2,407 cycles

AIRCRAFT WAS NOT GROUNDED. R2 EMERGENCY EXIT DOOR DAMPENER PRESSURE IS LOW. SERVICED R2 EMERGENCY DOOR DAMPENER PER AMM 52-22-00.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 6,580 hrs · 2,407 cycles

AIRCRAFT WAS NOT GROUNDED. R2 EMERGENCY EXIT DOOR DAMPENER PRESSURE IS LOW. SERVICED R2 EMERGENCY DOOR DAMPENER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 6,367 hrs · 2,322 cycles

R2 DOOR BOTTLE REQUIRES SERVICING. SERVICED R2 DOOR BOTTLE IAW MM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 6,292 hrs · 2,296 cycles

R2 DOOR DAMPER BELOW LIMITS. SERVICED R2 DOOR DAMPER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 5,927 hrs · 2,156 cycles

FOUND DURING AN EMERGENCY LIGHT TEST BATTERY, EMERGENCY POWER SUPPLY UNIT (12WL) EXIT RIGHT FAULT. REPLACED EPSU IAW AMM 33-51-38.

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 5,832 hrs · 2,122 cycles

AIRCRAFT WAS GROUNDED. R2 DOOR ACCUMULATOR PRESSURE LOW. SERVICED R2 DOOR DAMPER PER AMM 52-10-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 5,778 hrs · 2,101 cycles

R2 DOOR DAMPER PRESSURE FOUND IN LOWER RED ZONE. SERVICED THE R2 DOOR DAMPER TO GREEN ZONE, NO LEAKS FOUND IAW AMM 52-22-00. OK FOR SERVICE.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 5,652 hrs · 2,060 cycles

R1 DOOR WILL NOT ARM. MAINTENANCE REPOSITIONED LANYARD FROM UNDER GIRT BAR IAW AMM 25-62-44.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 5,652 hrs · 2,060 cycles

ECAM OPEN INDICATION ON THE R1 DOOR, DISPLAYED UNARMED ON LANDING ROLL OUT. MAINTENANCE ADJUSTED GIRT BAR ON R1 DOOR IAW AMM 25-62-44.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 5,652 hrs · 2,060 cycles

R1 DOOR WILL NOT ARM. MAINTENANCE REPOSITIONED LANYARD FROM UNDER GIRT BAR AND SERVICED DOOR PER MM 25-62-44.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 5,556 hrs · 2,026 cycles

R2 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED THE R2 DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: CYLINDER — READS LOW (R1 DOOR) · airframe 5,188 hrs · 1,892 cycles

AIRCRAFT WAS NOT GROUNDED. R1 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-22-00. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 4,733 hrs · 1,733 cycles

R2 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS BELOW LIMITS. SERVICED CYLINDER IAW AMM 52-22-00. OPERATIONAL CHECK GOOD.