N976UY

Part: HANDLE — LOOSE (ZONE 800) · airframe 41,686 hrs · 17,083 cycles

AIRCRAFT WAS GROUNDED: R3 DOOR ARMING LEVER LOOSE. MAINTENANCE SECURED DOOR ARMING HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 40,917 hrs · 16,768 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 40,917 hrs · 16,768 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: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 40,258 hrs · 16,493 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DFW DUE TO THE FLIGHT ATTENDANTS REPORTING THAT THE 2L DOOR SLIDE BOTTLE PRESSURE DECREASED TO ZERO AFTER TAKEOFF ALONG WITH A CHECK SLIDE PRESSURE 2L MESSAGE ON THE FORWARD GALLEY SERVICE PANEL. THE FLIGHT CREW REPORTED THAT AS THE AIRCRAFT DESCENDED THE BOTTLE PRESSURE INCREASED. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE INFLATION RESERVOIR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-49.

Part: LANYARD — UNSECURE (ZONE 800) · airframe 40,228 hrs · 16,482 cycles

AIRCRAFT WAS NOT GROUNDED: A WARNING LANYARD IS VISIBLE BETWEEN THE SLIDE BUSTLE AND THE HINGE COVER AT 4R. IT APPEARS TO HAVE FALLEN FROM BEHIND THE HINGE COVER. MAINTENANE SECURED WARNING LANYARD PER AMM 25-62-00.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 39,440 hrs · 16,141 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 15WL FAILED SYSTEM TEST PER TASK CARD 2600025010. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL AND ACCOMPLISHED A SATSISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: SLIDE — NO TEST (ZONE 800) · airframe 39,294 hrs · 16,077 cycles

AIRCRAFT WAS GROUNDED: DURING A SCHEDULED REPLACEMENT OF THE L1 DOOR SLIDE, THE REPLACEMENT SLIDE FAILED THE OPERATIONAL CHECK PER TASK CARD 26L00025010 AND WAS REMOVED TO BE SENT OUT FOR REPAIR. THE ORIGINAL SLIDE WAS RE-INSTALLED PER TASK CARD 26L00025010.

Part: ELEC CONNECTOR — LOOSE (ZONE 200) · airframe 39,130 hrs · 16,012 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY CEILING LIGHT AT ROW 28 IS INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR LOOSE AND PLUGGED IT BACK IN PER AMM 33-51-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LEVER — LOOSE (ZONE 800) · airframe 39,034 hrs · 15,975 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS REPORTED THAT THE 3R DOOR ARMING LEVER ON 3R JIGGLES WHEN IN THE DISARMED POSITION. MAINTENANCE FOUND THE R3 DOOR YELLOW GRAB ADAPTOR ON THE ARMING LEVER LOOSE AND SECURED IT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — FAULTED (ZONE 800) · airframe 38,781 hrs · 15,860 cycles

AIRCRAFT WAS GROUNDED: DURING A FUNCTIONAL CHECK OF THE L1 DOOR, MAINTENANCE FOUND THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DAMPING FUNCTION FAULTY WHICH RESULTED IN REQUIRING EXCESSIVE FORCE TO MANEUVER THE DOOR INTO THE OPEN POSITION AND CAUSING THE DOOR TO CONTACT THE FUSELAGE. MAINTENANCE REPLACED THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 800) · airframe 37,891 hrs · 15,468 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN IN FLIGHT. MAINTENANCE ADJUSTED THE FLIGHT DECK DOOR CENTER LATCH AND ACCOMPLISHED ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-00.

Part: SCREW — LOOSE (ZONE 800) · airframe 37,886 hrs · 15,466 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER SHUT DOWN, FLIGHT ATTENDANT ADVISED THAT THE ARMING LEVER WAS LOOSE WHILE DISARMING THE R3 DOOR. APPEARED TO BE A LOOSE SCREW. TIGHTENED ARM PADDLE SCREW.

Part: DOOR — BINDING (ZONE 800) · airframe 37,785 hrs · 15,415 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN IN FLIGHT USING MECHANICAL D-RING HANDLE. FLIGHT CREW HAD TO USE THE TOGGLE SWITCH ON THE FLIGHT DECK DOOR HANDLE LOCATED ON CENTER PEDESTAL TO ASSIST OPENING THE DOOR. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: HANDLE — STICKING (ZONE 800) · airframe 37,785 hrs · 15,415 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN IN FLIGHT USING MECHANICAL D-RING HANDLE. FLIGHT CREW HAD TO USE THE TOGGLE SWITCH ON THE FLIGHT DECK DOOR HANDLE LOCATED ON CENTER PEDESTAL TO ASSIST OPENING THE DOOR. **SUPPLEMENTAL REPORT FOR AALA202409187896: MAINTENANCE PERFORMED INSPECTION OF DOOR ASSEMBLY AND COULD NOT FIND ANY EVIDENCE OF STICKING. MAINTENANCE PERFORMED AN OPERATIONAL TEST WITH NO ISSUES NOTED.** (CLOSED)

Part: DOOR LATCH — LACK OF LUBE (ZONE 800) · airframe 37,776 hrs · 15,411 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR HANDLE IS DIFFICULT TO TURN/OPEN. DOOR FEELS LIKE IT'S RUBBING/STICKING ON DOOR FRAME. LUBED DOOR LATCH PLUNGERS.

Part: COOLING FAN — SEIZED (ZONE 100) · airframe 37,595 hrs · 15,343 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE HEARD A SOUND POSSIBLY ASSOCIATED WITH A BAD BEARING ALONG WITH MOMENTARY BURNING ELECTRICAL SMELL. PURSER REPORTS THESAME ALONG WITH A SLIGHT VIBRATION IN GALLEY. APPEARS TO HAVE COME FROM BEHIND AND BELOW FLIGHT DECK. NO ECAM AND NO CB TRIP. ALL INDICATIONS APPEAR NORMAL.LOUD NOISE VIBRATION ASSOCIATED WITH PREVIOUS WRITE UP PROGRESSED NEGATIVELY UNTIL A LOUD POP AND ECAM VENT EXTRACT FAN. A BRIEF ELECTRICAL BURNING SMELL ONCE AGAIN PRESENTED. NOISE AND VIBRATION IMMEDIATELY STOPPED AND SMELL DISSIPATED ONCE THE ECAM MESSAGE APPEARED. FOLLOWING ECAM PROCEDURES THE EXTRACT OVRD PB ON THE OVERHEAD VENTILATION PANEL WAS SELECTED. IT IS ALSO LIKELY THE EXTRACT FAN FAILED AND IS NOT OPERATING DUE TO TACTILE CLUES. FOUND AVIONICS VENT EXTRACT FAN SEIZED, R/R FAN PER AMM 21-26-51 OPS/LEAK CHECK GOOD.

Part: BULKHEAD — OUT OF ADJUST (ZONE 200) · airframe 37,396 hrs · 15,251 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR DIFFICULT TO OPEN IN FLIGHT. ADJUSTED UPPER COCKPIT WALL BETWEEN GALLEY AND FORWARD LAVATORY.

Part: SCREW — LOOSE (R3 ARMING LEVER) · airframe 37,203 hrs · 15,165 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER/ PLATE LOOSE. RE-SECURED SCREW AT DOOR 3R ARMING LEVER PER AMM 52-20-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 37,110 hrs · 15,130 cycles

AIRCRAFT WAS GROUNDED: RIGHT-HAND AFT DOOR DAMPER PRESSURE IS LOW PER PS CHECK. SERVICED RIGHT-HAND AFT DOOR CYLINDER BOTTLE PER AMM 52-10-00.

Part: DOOR LATCH — LACK OF LUBE (COCKPIT) · airframe 37,096 hrs · 15,127 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR HARD TO OPEN FROM THE INSIDE. LUBRICATED DOOR LATCH AND LOCK ASSEMBLY.

Part: CONNECTOR — MISINSTALLED (PROXIMITY SWITCH) · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: ECAM PAGE DOOR SHOWN DOOR AFT CARGO, DOOR BULK CARGO, DOOR LEFT AFT CABIN, DOOR, LEFT FORWARD EMERGENCY EXIT, DOOR LEFT AFT EMERGENCY EXIT FAULT MESSAGES. MAINTENANCE FOUND ELECTRICAL CONNECTOR FOR THE AFT LEFT DOOR HOOK PROXIMITY SWTICH NOT CONNECTED PROPERLY AND PROPERLY CONNECTED THE CONNECTOR PER AMM 52-71-13. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: FITTING — CORRODED (FRMS 66-68 S23L) · corrosion level 2 · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER FITTING LOCATED ON STR 23L BETWEEN FR 66 AND FR 68. REPLACED CENTER FITTING PER SRM 53-41-79-02.

Part: SHEAR PLATE — CRACKED (FRS69-70 S23L) · airframe 36,999 hrs · 15,080 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: DUMMY RAIL — CORRODED (FRMS 12-16) · corrosion level 2 · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY DUMMY RAIL BETWEEN FR 12 AND FR 16 AT Y503.2. REPLACED DUMMY RAIL PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FRS 69-70 S23R) · airframe 36,999 hrs · 15,080 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: FORK — WORN (FRS 23-24 S32L) · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN ALLOWING CONTACT BETWEEN FITTING BOLT AND STRUCTURE, BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 354516.

Part: WEB — CRACKED (FR 23-24 S32-33L) · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL PYRAMID STRUCTURE WEB CRACKED BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL PYRAMID STRUCTURE WEB PER EA 354516.

Part: ANGLE — CRACKED (FR 23-24 S32-33L) · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL PYRAMID STRUCTURE ANGLE FITTING CRACKED BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL PYRAMID STRUCTURE ANGLE FITTING PER EA 354516.

Part: FORK — NONE (ZONE 100 - FUSE) · airframe 36,999 hrs · 15,080 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTINGBETWEEN FR 23 AND FR 24 AT-Y1292, BETWEEN S32R AND S33R REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIRS BEING ACCOMPLISHED PER EA 354516. REPLACED RIGHT HAND LATERAL FORK END FITTING PER EA 354516.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 36,537 hrs · 14,878 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT AFT FLASHLIGHT NOT BLINKING. REPLACED BATTERY.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 36,255 hrs · 14,745 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 25 EMERGENCY LIGHT INOPERATIVE. FOUND WIRE TO CONNECTOR 7261VC7-A BROKEN. REPAIRED CONNECTOR PER AWM 33-51-08.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 36,255 hrs · 14,745 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 26 EMERGENCY LIGHT INOPERATIVE. FOUND WIRE 7261VC7-A TO CONNECTOR BROKEN. REPINNED CONNECTOR PER AWM 33-51-08.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 35,783 hrs · 14,527 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR DISARM HANDLE LOOSE. MAINTENANCE FOUND HANDLE PLATE LOOSE AND SECURED IT PER AMM 25-23-46.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 35,715 hrs · 14,487 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE ARMING HANDLE ON DOOR 3R IS LOOSE. SECURED AND ADJUSTED SLIDE ARMING HANDLE ON DOOR 3R PER AMM 20-00-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900 - LAV/G) · airframe 35,463 hrs · 14,366 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY SMOKE DETECTOR ECAM AND AURAL ALERT DURING CLIIMB. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL TEST OF THE LAVATORY SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED.

Part: LOCK — STICKING (ZONE 900 - LAV/G) · airframe 34,764 hrs · 14,060 cycles

AIRCRAFT WAS NOT GROUNDED: BACK LEFT LAVATORY DOOR LOCK GETS STUCK WITH PASSENGER INSIDE LAVATORY. MAINTENANCE LUBRICATD THE DOOR LOCK.

Part: FLOOR PANEL — UNKNOWN (ZONE 100 - FUSE) · airframe 34,429 hrs · 13,899 cycles

AIRCRAFT WAS GROUNDED: FORWARD GALLEY FLOOR PANEL 222EF HAS A SOFT SPOT IN MIDDLE OF THE PANEL. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 34,085 hrs · 13,757 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAULT DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 34,085 hrs · 13,757 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL BATTERY FAULT DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: APU — LEAKING (ZONE 100 - FUSE) · airframe 33,529 hrs · 13,501 cycles

AIRCRAFT WAS GROUNDED: A DIRTY SOCKS SMELL THAT STARTED DURING TAKEOFF AND CONTINUED THRU THE ENTIRE FLIGHT WAS REPORTED. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU AND REPLACED IT PER TASK CARD 26L31049003. A SATISFACTORY LEAK/OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TOILET — LEAKING (ZONE 900 - LAV/G) · airframe 33,170 hrs · 13,333 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT ODOR, SOURCE UNKNOWN, STRONGEST MID TO AFT CABIN. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE MID LAVATORY TOILET ASSEMBLY THAT WAS LEAKING AND REPLACED IT PER AMM 38-31-41. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: HANDLE — WORN (ZONE 800 - DOORS) · airframe 33,166 hrs · 13,331 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING PLATE LOOSE. MAINTENANCE REPLACED WORN SLIDE ARM HANDLE PER AMM 52-22-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LEVER — LOOSE (R3 DOOR) · airframe 32,325 hrs · 12,968 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARMING LEVER IS LOOSE. MAINTENANCE TIGHTENED 3R DOOR ARMING LEVER AS REQUIRED.

Part: NONE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 31,530 hrs · 12,604 cycles

AIRCRAFT WAS NOT GROUNDED: MIDDLE LAVATORY DOOR WILL NOT OPEN OR CLOSE. MAINTENANCE ADJUSTED LAVATORY DOOR STOP PER AMM 25-40-00.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 30,145 hrs · 11,978 cycles

AIRCRAFT WAS NOT GROUNDED: 3L ARM/DISARM DOOR LEVER LOOSE. TIGHTENED ARM / DISARM LEVER AS REQUIRED.

Part: CONTROL HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 29,695 hrs · 11,793 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING LEVER AT DOOR 3R NEEDS TIGHTENING. TIGHTENED 3R DOOR ARMING SLIDE CONTROL HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-00.

Part: SCREW — LOOSE (ZONE 800 - DOORS) · airframe 29,300 hrs · 11,643 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R SLIDE ARMING LEVER LOOSE. TIGHTENED LOOSE SCREW ON 3R DOOR ARMING HANDLE.

Part: RECEPTACLE — LACK OF LUBE (ZONE 800 - DOORS) · airframe 29,151 hrs · 11,581 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4R ARMING LEVER TOUGH TO MOVE. CLEANED AND LUBRICATED GIRT BAR RECEPTACLES PER AMM 52-10-00.

Part: SENSOR — DEFECTIVE (ZONE 700 - GEARS) · airframe 28,873 hrs · 11,460 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF #3 BRAKE SHOWED HOT UP CLIMBING TO 995 C GEAR EXTENDED AT FIRST INDICATION OF HOT BRAKE TO COOL BRAKES, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202110155346: REPLACED #3 BRAKE TEMPERATURE SENSOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER A.M.M. 32-47-15. **(CLOSED)

Part: NONE — NONE · airframe 28,873 hrs · 11,460 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF #3 BRAKE SHOWED HOT UP CLIMBING TO 995 C GEAR EXTENDED AT FIRST INDICATION OF HOT BRAKE TO COOL BRAKES, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LATCH — STICKING (COCKPIT DOOR) · airframe 28,630 hrs · 11,364 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR WILL NOT OPEN MANUALLY FROM INSIDE OF COCKPIT. REMOVED AND REPLACED DOOR LATCH MECHANISM PER AMM 52-51-21.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 28,509 hrs · 11,305 cycles

AIRCRAFT WAS GROUNDED: CLIMBING THROUGH FL 270 WE STARTED FEELING VIBRATION WORSE IN BACK OF AIRPLANE SPEED 305 SLOWED TO 280 AND VIBRATION DISSIPATED. MAINTENANCE ACCOMPLISHED ELEVATOR FREE PLAY CHECK AND FOUND THE LEFT HAND ELEVATOR #3 HINGE FITTING TO HAVE EXCESSIVE PLAY. REPLACED HINGE FITTING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-34-41.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 28,509 hrs · 11,305 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY DOOR ASSIST BOTTLE CYLINDER ACCUMULATOR NEEDS SERVICED. SERVICED L1 DOOR EMERGENCY DOOR ASSIST BOTTLE CYLINDER ACCUMULATOR PER AMM 52-10-00.

Part: BATTERY — FAILED (ZONE 200 - FUSE) · airframe 28,434 hrs · 11,271 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT (11WL) EXIT RIGHT FAILED TEST. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY (11WL) PER A321 AMM 33-51-38-000-00.

Part: BATTERY — FAILED (ZONE 200 - FUSE) · airframe 28,434 hrs · 11,271 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT (13WL) AFT LEFT FAILED TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY (13WL) PER A321 AMM 33-51-38-000-003.

Part: SEAT TRACK — CORRODED (FRM 20) · airframe 28,434 hrs · 11,271 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND SEAT TRACK LOCATED AT FR20 AND RBL -Y1292. REPAIRED SEAT TRACK PER SRM 53-11-15-300-008.

Part: LEVER — LOOSE (L3 DOOR) · airframe 28,167 hrs · 11,165 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER LOOSE. SECURED 3L DOOR ARMING LEVER AS NEEDED, OK FOR SERVICE.

Part: APU — LEAKING (ZONE 300 - STABS) · airframe 28,081 hrs · 11,130 cycles

AIRCRAFT WAS GROUNDED: CABIN ODOR NOTICED DURING CLIMB OUT FOR 15 MIN AND DURING TAXING IN. TURNED ON APU BLEED DURING TAXI IN AND ODOR INCREASED. ACCOMPLISHED JOB CARDS 26L00021001, 26L00021002, AND 26L00021004. REPLACED APU PER JOB CARD 26L31049003.

Part: REHEATER — INOPERATIVE (CABIN AIR) · airframe 27,661 hrs · 10,964 cycles

AIRCRAFT WAS GROUNDED: ON TAKE-OFF, SMELL OF FUMES IN COCKPIT AND CABIN APU WAS OFF. SMELLED LIKE DEICE/BURNT OIL. RETURNED TO PHL. PERFORMED J/C'S 26L00021001, 26L00021003, 26L00021004. SUCCESSFUL DECONTAMINATION ACCOMPLISHED, LEFT PACK. REPLACED CONDENSER (AALA202103099006), REHEATER (AALA202103099013), OZONE FILTER (AALA202103099014) AND FLOW CONTROL VALVE (AALA202103099015).

Part: CONTROL VALVE — ODOR (CABIN AIR) · airframe 27,661 hrs · 10,964 cycles

AIRCRAFT WAS GROUNDED: ON TAKE-OFF, SMELL OF FUMES IN COCKPIT AND CABIN APU WAS OFF. SMELLED LIKE DEICE/BURNT OIL. RETURNED TO PHL. PERFORMED J/C'S 26L00021001, 26L00021003, 26L00021004. SUCCESSFUL DECONTAMINATION ACCOMPLISHED, LEFT PACK. REPLACED CONDENSER (AALA202103099006), REHEATER (AALA202103099013), OZONE FILTER (AALA202103099014) AND FLOW CONTROL VALVE (AALA202103099015).

Part: FILTER — ODOR (CABIN AIR) · airframe 27,661 hrs · 10,964 cycles

AIRCRAFT WAS GROUNDED: ON TAKE-OFF, SMELL OF FUMES IN COCKPIT AND CABIN APU WAS OFF. SMELLED LIKE DEICE/BURNT OIL. RETURNED TO PHL. PERFORMED J/C'S 26L00021001, 26L00021003, 26L00021004. SUCCESSFUL DECONTAMINATION ACCOMPLISHED, LEFT PACK. REPLACED CONDENSER (AALA202103099006), REHEATER (AALA202103099013), OZONE FILTER (AALA202103099014) AND FLOW CONTROL VALVE (AALA202103099015).

Part: CONDENSER — ODOR (A/C PACK) · airframe 27,661 hrs · 10,964 cycles

AIRCRAFT WAS GROUNDED: ON TAKE-OFF, SMELL OF FUMES IN COCKPIT AND CABIN APU WAS OFF. SMELLED LIKE DEICE/BURNT OIL. RETURNED TO PHL. PERFORMED J/C'S 26L00021001, 26L00021003, 26L00021004. SUCCESSFUL DECONTAMINATION ACCOMPLISHED, LEFT PACK. REPLACED CONDENSER (AALA202103099006), REHEATER (AALA202103099013), OZONE FILTER (AALA202103099014) AND FLOW CONTROL VALVE (AALA202103099015).

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 26,806 hrs · 10,598 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN INTERCOMMUNICATION DATA SYSTEM PANEL INDICATES THAT SLIDE PRESSURE NEEDS TO BE CHECKED AT 1L DOOR. FOUND 1L DOOR DAMPER CYLINDER PRESSURE LOW. CHARGED DOOR DAMPER CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 26,581 hrs · 10,506 cycles

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

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 26,459 hrs · 10,457 cycles

AIRCRAFT WAS NOT GROUNDED:CHECK DOOR PRESSURE ON CIDS PANEL DOOR 1L. SERVICED L1 DOOR DAMPER & EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00. LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,288 hrs · 10,388 cycles

AIRCRAFT NOT GROUNDED - L3 DOOR, EMERGENCY FLASHLIGHT INOPREMOVED AND REPLACED EMERGENCY FLASHLIGHT, L3 DOOR, PER AMM 25-63-53, OPERATIONAL CHECK OKAY.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 25,406 hrs · 10,010 cycles

AIRCRAFT WAS GROUNDED: 15WL BATTERY FAULT IN SMOKE CLASS 2. MAINTENANCE REPLACED 15WL POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,406 hrs · 10,010 cycles

AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT BREAK AWAY FLASHLIGHT DISCHARGED. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER GPM 02-01-2.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 25,320 hrs · 9,976 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT CRUISE FL 320 INITIAL INDICATION ENG #2 SENSOR AND ENG #2 FADEC B ECAM. A FEW SECONDS LATER AUTO-THRUST DISCONNECTED. NEXT ECAM START VALVE #2 NOT CLOSED. NEXT ENG SURGE -PULLED BACK TO IDLE, DECLARED EMERGENCY AND DIVERTED TO KBNA. #2 ENG REMAINED AT IDLE REST OF FLT. ALL ECAM PROCEDURES WERE FOLLOWED. MAINTENANCE REPORTS IAW TSM 71-00-00-810-809A, EXAMINED #2 ENGINE FOR FOD OR DAMAGE, NONE NOTED. PERFORMED BORESCOPE. READ AND DISTRIBUTED FAULT CODES FROM #2 ENGINE FADEC CHANNELS 2A AND 2B. REMOVED AND INSTALLED SERVICEABLE EEC IAW AMM 73-22-34-400-010A. OPS TEST OF EEC GOOD, NO FAULTS NOTED. IDLE ENGINE RUN AND HIGH POWER ASSURANCE RUN ACCOMPLISHED IAW AMM 71-00-00-710-013C. NO FAULTS NOTED, NO UNUSUAL INDICATIONS, OK FOR SERVICE.

Part: ACCUMULATOR — LOW PRESSURE (HYD SYSTEM) · airframe 25,211 hrs · 9,935 cycles

AIRCRAFT WAS GROUNDED: RETUEN TO GATE BRAKES PARK BRK LO PRE AFTER STARTING ENGINE 1 ACCUM PRESSURE DROPS TO BELOW GREEN ARC, AND BRAKE PRESS @1000 PSIW/ ACCOMPANYING ECAM. MAINTENANCE FILLED ACCUMULATOR YELLOW SYS IAW AMM 12-14-29-001-614 PERFROMED FUNCTIONAL CHECK OF BRAKING SYS IAW AMM 32-44-11-200-001A. MSG CLEARED. AIRCRAFT TAXIED TO DE- ICEPAD WITH OUT ANY PROBLEMS/ OK TO CONTINUE SERVICE.

Part: BRAKE — DRAGGING (MLG) · airframe 23,793 hrs · 9,373 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO MCO ON ACCOUNT OF BRAKE OVERHEAT INDICATION. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND #2 BRAKE DRAGGING & PIECES OF BRAKE DISC IN WHEEL COVER. REPLACED #2 BRAKE ASSEMBLY AND #2 MAIN WHEEL ASSEMBLY IAW AMM 32-42-27 AND AMM 32-41-11. BRAKE FAN OPS CHECKED SATISFACTORY IAW AMM 32-48-00.

Part: UNKNOWN — MALFUNCTIONED (ENGINES) · airframe 23,607 hrs · 9,288 cycles

AIRCRAFT NOT GROUNDED: PILOT REJECTED TAKE OFF. FLEX SELECTED, NO 1 WENT TOGA NO 2 WENT FLEX. MAINTENANCE ACCOMPLISHED OPS TEST OF THROTTLE CONTROL UNIT IAW AMM 76-11-00-710-040, NO FAULTS FOUND. NO DEFECTS NOTED IN PFR, AIRMAN, OR CMS. NO RECENT HISTORY OF DISCREPANCY. ACCOMPLISHED SUCCESSFUL HIGH POWER RUNS IAW AMM 71-00-00-710-013 & AMM 71-00 00-860-010. BOTH ENGINES STAYED @ FLEX WHEN THRUST LEVERS WERE SET TO FLEX / MCT DETENT. OK FOR SVC.

Part: LATCH — OUT OF ADJUST (COCKPIT DOOR) · airframe 22,862 hrs · 8,992 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR WAS DIFFICULT TO OPEN FROM INSIDE. MAINTENANCE ADJUSTED CENTER LATCH AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-21.

Part: LENS — MISSING (R1 DOOR) · airframe 20,341 hrs · 8,016 cycles

AIRCRAFT WAS NOT GROUNDED. SLIDE ARMED LIGHT MISSING LENS AT DOOR R1. INSTALLED LENS COVER ON R1 DOOR PER AMM 52-70-00.

Part: SHEAR WEB — CRACKED (FRAME 69) · airframe 19,833 hrs · 7,821 cycles

CRACK INDICATION FOUND ON THE SHEAR WEB, CRACK IN JOGGLE AT FRAME 69, FLOOR LEVEL. REPLACED THE SHEAR WEB IAW SRM 51-75-12, AND DRAWING D53474180.

Part: FITTING — CORRODED (FRAME 68) · airframe 19,833 hrs · 7,821 cycles

CORROSION ON L4 DOOR CUTOUT LOWER SILL AFT CORNER FITTING AT FRAME 68, STRINGER 17L, REPLACED THE FITTING IAW SRM 51-42-11

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 19,833 hrs · 7,821 cycles

CORROSION ON THE SUPPORT AT STRINGER 17R, -Y1732. REPAIRED IAW SRM 53-41-14-300-001, REPAIR PRINCIPLE 7, FIGURE 20101.

Part: BEAM — CORRODED (FRAME 65) · airframe 19,833 hrs · 7,821 cycles

CORROSION FOUND ON THE L4 DOOR SILL BEAM. REPLACED THE SILL BEAM IAW DRAWING D53480505, AND SRM 51-42-11.

Part: SPLICE — CORRODED (FRAME 66) · airframe 19,833 hrs · 7,821 cycles

CORROSION FOUND ON THE SPLICE ANGLE AT FRAME 66, -Y1450. REPLACED THE SPLICE ANGLE IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,833 hrs · 7,821 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON SILL. FABRICATED REPAIR ANGLE (SILL) AND FILLER FROM FORMED SECTION ANGLE PER SRM 53-41-14-300-001. PRINCIPLE 7 FIG 20101.

Part: DECODER — FAULTY (R3 DOOR) · airframe 19,163 hrs · 7,566 cycles

R3 DOOR PRESSURE, SLIDE LIGHT CHECK. REPLACED DECODER/ENCODER UNIT B (300RH6) SYSTEM CHECKS OK IAW AMM 23-73-42-400-001-A.

Part: DECODER — FAULTY (L3 DOOR) · airframe 19,163 hrs · 7,566 cycles

L3 DOOR PRESSURE SLIDE LIGHT CHECK. REPLACED DECODER/ENCODER UNIT B (300RH6) SYSTEM CHECKS OK PER AMM 23-73-42-400-001-A. (SEE CONTROL #AALA201802269076)

Part: CIDS — MALFUNCTIONED · airframe 19,062 hrs · 7,529 cycles

LT AND RT HANDSET INOPERATIVE. LT AND RT SLIDES WILL NOT PRESSURIZE. RESET CIDS SYSTEM IAW TSM 24-00-00.

Part: FLOOR PANEL — DAMAGED (GALLEY) · airframe 18,204 hrs · 7,199 cycles

FLIGHT ATTENDANT REPORTED A SOFT SPOT IN FORWARD GALLEY FLOOR. MAINTENANCE REPAIRED THE FLOOR PANEL 221DF IAW EA 275103. AIRCRAFT WAS GROUNDED.

Part: HANDLE — BROKEN (DOOR ASSIST) · airframe 17,900 hrs · 7,082 cycles

L1 DOOR ASSIST HANDLE BROKEN. REPLACED THE HANDLE IAW AMM 52-10-00.

Part: CONNECTOR — CORRODED (OVERHEAT DETECT) · airframe 17,086 hrs · 6,798 cycles

DURING CRUISE, INTERMITTENT ECAM ADVISORY NAC TEMP HIGH, FLASHING, MAX 385 DEG C. RAN THE NR 1 ENGINE, NO AIR LEAKS. FOUND CORRODED DETECTOR CONNECTOR. REMOVED AND REPLACED DETECTOR IAW AMM 26-12-17 AND ACCOMPISHED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED

Part: LENS — MISSING (CABIN) · airframe 16,966 hrs · 6,752 cycles

L4 DOOR LOWER LEFT EXIT LIGHT LENS MISSING. INSTALLED A NEW LENS.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 16,124 hrs · 6,439 cycles

ECAM DISPLAYED FOR RIGHT WING FUEL TANK PUMP NR 1, LOW PRESSURE. TURNED PUMP OFF PER SCAM PROCEDURES. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 28-21-00-710-007-A. AIRCRAFT WAS GROUNDED.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 15,678 hrs · 6,271 cycles

FLIGHT ATTENDANT AND PASSENGER REPORTED A CABIN ODOR THAT BEGAN DURING APPROACH. DISSIAPTED AFTER RUNNING ENGINE. MAINTENANCE FOUND APU OIL OVERSERVICED. DRAINED TO WITHIN LIMITS IAW 49-90-00/301 AIRCRAFT WAS GROUNDED.

Part: LIGHT — BROKEN (CABIN) · airframe 15,300 hrs · 6,122 cycles

BROKEN RED AISLE EMERGENCY LIGHT AT 10C. REPLACED THE EMERGENCY LIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — DETACHED (CABIN) · airframe 15,192 hrs · 6,080 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4R EXIT LIGHT LENS FELL OFF. MAINTENANCE REPLACED EXIT LIGHT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,794 hrs · 5,931 cycles

MISSING EXIT LIGHT LENS. REPLACED THE LIGHT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,115 hrs · 5,652 cycles

SEAT 1L EMERGENCY LIGHT COVER MISSING. REPLACED LIGHT ASSEMBLY PER AMM 33-51-19.

Part: LENS — MISSING (ZONE 800) · airframe 13,127 hrs · 5,298 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT COVER LENS MISSING FROM DOOR 4L. INSTALLED EMERGENCY EXIT LIGHT COVER LENS ON DOOR 4L AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 12,610 hrs · 5,103 cycles

AIRCRAFT WAS GNDED. FWD CARGO FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-22-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 12,610 hrs · 5,103 cycles

AIRCRAFT WAS GNDED. AFT CARGO FLOOR PANEL 151MK DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-22-14-400-001-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 12,610 hrs · 5,103 cycles

AIRCRAFT WAS GNDED. AFT CARGO FLOOR PANEL 151 LF DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-42-14-000-001-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 12,610 hrs · 5,103 cycles

AIRCRAFT WAS GNDED. AFT CARGO FLOOR PANEL 151GF DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-22-14-400-001-A.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 12,293 hrs · 4,980 cycles

AIRCRAFT WAS GNDED. CABIN FLOOR PANEL 221EF HAS SOFT SPOT. REPLACED FLOOR PANEL IAW AMM 53-12-12-400-003-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,028 hrs · 4,879 cycles

AIRCRAFT WAS GNDED. BELOW 10000' FLIGHT ATTENDANT REPORTED VERY STRONG ODOR IN REAR OF ACFT. CHECKED ACFT FOR ODOR & NONE DETECTED. ACCOMPLISHED JC 26L00021001, NO ODOR NOTED. ACFT RETURNED TO SERVICE.

Part: LENS — BROKEN (CABIN) · airframe 11,569 hrs · 4,703 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT REPORTS 4R DOOR EMER LIGHT LENS BROKEN. REPLACED 4R DOOR EMER LIGHT LENS. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.