N9010R

Part: OIL SYSTEM — LEAKING (APU) · airframe 32,112 hrs · 15,511 cycles

AIRCRAFT WAS GROUNDED: OIL ODOR CAN BE SMELLED THROUGHOUT CABIN AND COCKPIT. MAINTENANCE FOUND OIL LEAKING FROM APU DRAIN MAST REF MIC 1418556. ACCOMPLISHED WC/ 26L00021001 . CONFIRMED ODOR WAS FROM APU. BOTH ENGINE BLEEDS FOUND ODORLESS. APU DEFERED PER MIC 1418985. (OPEN)

Part: COFFEEMAKER — ODOR (ZONE 900) · airframe 31,876 hrs · 15,388 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW COMPLAINING OF ELECTRICAL ODOR IN AFT GALLEY. DURING PREFLIGHT. ACCOMPLISHED SOF JOB CARD 26L00021001 SUSPECT 5-7 AFT GALLEY COFFEE MAKER SOURCE OF SOF.MAINTENANCE REPLACED COFFEEMAKER.

Part: LIGHT — SHORTED (DOOR SLIDE) · airframe 31,761 hrs · 15,326 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT TEST FAILED DURING PS CHECK. FAULT EPSU(10WL) FWDL/DEU-B(300RH1) ATA 335138. AFTER TROUBLE SHOOTING FOUND WIRE FROM EPSU (10WL) TO R1 DOOR SLIDE OPEN. MAINTENANCE REPLACED R1 DOOR ESCAPE SLIDE IAW J/C 26L00025011.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,940 hrs · 14,863 cycles

AIRCRAFT WAS GROUNDED: FLT ATTENDANTS COMPLAINED OF AN ODOR IN THE CABIN DURING CRUISETHROUGH WEATHER AND IN THE DESCENT MOST PRONOUNCED IN AFT CABIN. (OPEN)

Part: APU — DIRTY (ZONE 200) · airframe 30,940 hrs · 14,863 cycles

AIRCRAFT WAS GROUNDED: FLT ATTENDANTS COMPLAINED OF AN ODOR IN THE CABIN DURING CRUISETHROUGH WEATHER AND IN THE DESCENT MOST PRONOUNCED IN AFT CABIN. **SUPPLEMENTAL REPORT FOR SDR AALA202502285271.** (CLOSED) MAINTENANCE PERFORMED DETAIL INSPECTION AND CLEANED APU AS REQUIRED IAW J/C 26L00021002 AND 26L00021014. LEAK CHECK AND OPS CHECK GOOD.

Part: LIGHT — NO TEST (ZONE 200) · airframe 30,811 hrs · 14,799 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT ROW 14ABC SIDEWALL LIGHT INOP. MAINTENANCE REPLACED LIGHT IAW AMM 33-21-11.

Part: MOTOR — INOPERATIVE (VBV) · airframe 30,152 hrs · 14,420 cycles

AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT TO IDLE AND ENGINE STABILIZED. PUSHED THROTTLE UP SLIGHTLY AND ENGINE STALLED AGAIN. LEFT THROTTLE OF ENG 2 AT IDLE AND DIVERTED TO CMH DUE TO STRONG THUNDERSTORMS OVER THE FIELD IN PIT. MAINTENACE PER TSM 75-30-00 FOUND #2 ENGINE VBV GEAR MOTOR BAD REPLACED GEAR MOTOR ASSEMBLY.

Part: ENGINE — STALLED (NR 2) · airframe 30,152 hrs · 14,420 cycles

AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT TO IDLE AND ENGINE STABILIZED. PUSHED THROTTLE UP SLIGHTLY AND ENGINE STALLED AGAIN. LEFT THROTTLE OF ENG 2 AT IDLE AND DIVERTED TO CMH DUE TO STRONG THUNDERSTORMS OVER THE FIELD IN PIT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: WIRE HARNESS — BROKEN (ZONE 200) · airframe 29,747 hrs · 14,182 cycles

AIRCRAFT WAS GROUNDED: EMER LTS WIRING DAMAGED AND DISLODGED FROM SIDEWALL. SEAT ROWS 9 AND 10 LTS INOP. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHTS WIRING HARNESS FOR ROWS 9 & 10.

Part: COOLING FAN — LEAKING (ZONE 100 - FUSE) · airframe 29,700 hrs · 14,157 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A STRONG MILDEW / DIRTY SWEAT SOCK ODOR IN CABIN AND FLIGHT DECK DURING ALL PHASES OF FLIGHT. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING OIL AND REPLACED IT. (AALA202408051354). MAINTENANCE ALSO REPLACED THE AIR OIL SEPERATOR (AALA202408058574). A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SEPARATOR — LEAKING (APU) · airframe 29,700 hrs · 14,157 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A STRONG MILDEW / DIRTY SWEAT SOCK ODOR IN CABIN AND FLIGHT DECK DURING ALL PHASES OF FLIGHT. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING OIL AND REPLACED IT. (AALA202408051354). MAINTENANCE ALSO REPLACED THE AIR OIL SEPERATOR (AALA202408058574). A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: VENT LINE — CLOGGED (APU) · airframe 29,477 hrs · 14,023 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A DIRTY SOCK SMELL WAS NOTED ON FLIGHT DECK BEGINNING IN DESCENT THROUGH 9000. STILL EVIDENT AT 6000. MAINTENANCE FOUND THE APU GEARBOX VENT LINE CLOGGED AND UNCLOGGED THE VENT LINE.

Part: LIFE VEST — OPEN (SEAT 15C) · airframe 28,854 hrs · 13,678 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT15C. REPLACED LIFE VEST PER AMM 25-66-52.

Part: LIFE VEST — OPEN (SEAT 13B) · airframe 28,854 hrs · 13,678 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT13B. REPLACED LIFE VEST PER AMM 25-66-52.

Part: LIFE VEST — OPEN (SEAT 27E) · airframe 28,854 hrs · 13,678 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT27E. REPLACED LIFE VEST PER AMM 25-66-52.

Part: TUBE — LEAKING (APU OIL) · airframe 28,334 hrs · 13,439 cycles

AIRCRAFT WAS GROUNDED: OIL SMELL ON DESCENT INTO DFW. STARTED AT FL250 THROUGH LANDING. MAINTENANCE FOUND THE APU TURBINE BEARING RETURN TUBE LEAKING AND REPLACED IT PER CMM 49-26-95. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS NOTED.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 27,793 hrs · 13,191 cycles

AIRCRAFT WAS NOT GROUNDED: L2 LAVATORY DOOR DIFFICULT TO OPEN. MAINTENANCE ADJUSTED THE LAVATORY DOOR PER CMM 25-47-01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 27,312 hrs · 12,899 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUL. DURING CRUISE ECAM MESSAGE FOR FUEL USED AND FUEL ON BOARD DISAGREE. FLIGHT CREW ACCOMPLISHED THE QRH FUEL LEAK PROCEDURES. DURING DESCENT INTO TUL, THE FIRST OFFICER TOOK A PICTURE OF ECAM AND IT REFLECTED FUEL OVERLAND AFTER CLEARING THE INITIAL ECAM. THE LEFT MAIN TANK WAS ABOUT 1000LBS LESS THEN THE RIGHT TANK. THE AIRCRAFT LANDED SAFELY AT TUL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 28-11-00-810-805-A AND THE FAULTS CLEARED WITH NO ADDITIONAL FAULTS OR ISSUES NOTED BY MAINTENANCE. NO SPECIFIC PART CAUSING THE DIFFICULTY WAS IDENTIFIED BY MAINTENANCE.

Part: DAMPER — UNDERSERVICED (ZONE 800 - DOORS) · airframe 27,278 hrs · 12,876 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR ASSIST BOTTLE NEEDS FULL SERVICE. SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: PIVOT — CRACKED (ZONE 400 - NAC/P) · airframe 26,212 hrs · 12,338 cycles

AIRCRAFT WAS NOT GROUNDED: #2 ENGINE THRUST REVERSER PIVOT FITTING CRACKED. REPLACED PIVOT FITTING PER CMM 78-32-36 REPAIR #71

Part: GARLOCK SEAL — LEAKING (ZONE 400 - NAC/P) · airframe 25,922 hrs · 12,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202303245540: MAINTENANCE FOUND THE LEFT ENGINE ACCESSORY DRIVE GEAR BOX GARLOCK SEALS FOR THE IDG AND THE HYDRAULIC PUMP LEAKING. REPLACED BOTH GARLOC SEALS AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO LEAKS NOTED. (ALSO SEE AALA202304048961) ** (CLOSED)

Part: GARLOCK SEAL — LEAKING (ZONE 400 - NAC/P) · airframe 25,922 hrs · 12,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202303245540** MAINTENANCE FOUND THE LEFT ENGINE ACCESSORY DRIVE GEAR BOX GARLOCK SEALS FOR THE IDG AND THE HYDRAULIC PUMP LEAKING. REPLACED BOTH GARLOC SEALS AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO LEAKS NOTED. (ALSO SEE AALA202304048961)

Part: ENGINE — LEAKING (ZONE 400 - NAC/P) · airframe 25,922 hrs · 12,205 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: HINGE ARM — WORN (RUDDER) · airframe 25,517 hrs · 12,034 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER # 4 BEARING HINGE ARM ASSEMBLY HAS ELONGATED FASTENER HOLE. MAINTENANCE REPAIRED THE HINGE ARM ASSEMBLY PER EA 341726.

Part: HINGE ARM — WORN (RUDDER) · airframe 25,517 hrs · 12,034 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER # 3 BEARING HINGE ARM ASSEMBLY HAS TWO EACH EXISTING FASTENER HOLES FOR PIVOT FITTINGS OVERSIZED AND ARE OBLONGED. MAINTENANCE REPLACED THE HINGE ARM ASSEMBLY PER SRM 51-42-11.

Part: LIGHT — INOPERATIVE (SEAT ROW 23) · airframe 25,518 hrs · 12,034 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN CEILING EMERGENCY LIGHT 205WL AT SEAT ROW 23 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY 205WL PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (SEAT ROW 19) · airframe 25,518 hrs · 12,034 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN CEILING EMERGENCY LIGHT 201WL AT SEAT ROW 19 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY 201WL PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GUST LOCK — STICKING (PAX DOOR) · airframe 25,131 hrs · 11,871 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR GUST LOCK JAMMING AND HARD TP PUSH. MAINTENANCE CLEANED AND LUBRICATED GUST LOCK MECHANISM PER AMM 52-10-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — LOW (ZONE 200 - FUSE) · airframe 24,996 hrs · 11,802 cycles

AIRCRAFT WAS NOT GROUNDED: DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, MAINTENANCE FOUND EMERGENCY POWER SUPPLY UNIT 10WL BATTERY CHARGE LOW. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT 10WL BATTERY PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — LOW (ZONE 200 - FUSE) · airframe 24,973 hrs · 11,788 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY EXIT LIGHT TEST, MAINTEANCE FOUND EMERGENCY EXIT LEFT HAND EMERGENCY POWER SUPPLY UNIT BATTERY WITH LOW CHARGE. MAINTENANCE REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: ACTUATOR — FAULTY (ZONE 100 - FUSE) · airframe 24,820 hrs · 11,700 cycles

AIRCRAFT WAS GROUNDED: AT ALTITUDE FL 230 CABIN PRESSURE EXCESSIVE FLUCTUATIONS. MAINTENANCE REPLACED RAM AIR INLET ACTUATOR FOR PACK 2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-61-51.

Part: BRAKE — STICKING (ZONE 700 - GEARS) · airframe 24,644 hrs · 11,613 cycles

AIRCRAFT WAS GROUNDED: #1 BRAKE GOT EXTREMELY HOT COMPARED TO #2, 3, AND 4 WHILE TAXING SLOW. BRAKE WAS STICKING AND PULLING TO LEFT IN JAC, TEMPERATURE GOT AS HIGH AS 550 DEGREES WHILE OTHERS WERE MID 200'S. MAINTENANCE REPLACED #1 MAIN LANDING GEAR BRAKE PER AMM 32-42-27.

Part: NONE — NONE · airframe 24,137 hrs · 11,376 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GUST LOCK IS DIFFICULT TO RELEASE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LATCH — DEFECTIVE (ZONE 800 - DOORS) · airframe 24,137 hrs · 11,376 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GUST LOCK IS DIFFICULT TO RELEASE. **SUPPLEMENTAL REPORT FOR AALA202207220244: REPLACED LATCH PER AMM 52-11-00. ** (CLOSED)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 23,843 hrs · 11,238 cycles

AIRCRAFT WAS GROUNDED: ACRID FUMES ON THE GROUND AND DURING THE DESCENT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 23,843 hrs · 11,238 cycles

AIRCRAFT WAS GROUNDED: ACRID FUMES ON THE GROUND AND DURING THE DESCENT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202206106084: MAINTENANCE FOUND OIL LEAKING FROM BETWEEN THE GEAR BOX AND APU. REPLACED APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L31049003 . ** (CLOSED)

Part: RELAY — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 22,657 hrs · 10,683 cycles

AIRCRAFT WAS GROUNDED: CENTER TANK 1 PUMP FAULT LIGHT ON FUEL PANEL .ECAM MESSAGE READS FUEL CENTER TANK PUMP 1 LOW PRESSURE. REPLACED RELAY 69QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TSM 28-21-00-810-817A.

Part: NONE — NONE · airframe 22,626 hrs · 10,671 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 01 LOW PRESSURE MESSAGE / CENTER TANK PUMP FAULT LIGHT ILLUMINATED / AMBER LOW INDICATION ( FUEL PAGE). **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN)

Part: RELAY — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 22,626 hrs · 10,671 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 01 LOW PRESSURE MESSAGE / CENTER TANK PUMP FAULT LIGHT ILLUMINATED / AMBER LOW INDICATION ( FUEL PAGE). **SUPPLEMENTAL REPORT FOR AALA202201042822: REPLACED RELAY 69QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TSM 28-21-00-810-817A.**(CLOSED)

Part: NONE — NONE · airframe 22,596 hrs · 10,660 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: HINGE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 22,596 hrs · 10,660 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202201036694: ADJUSTED DOOR HINGE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00** (CLOSED)

Part: NONE — NONE · airframe 22,213 hrs · 10,502 cycles

AIRCRAFT WAS NOT GROUNDED: 9C EMERGENCY LIGHT IS WRONG COLOR. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: LIGHT — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 22,213 hrs · 10,502 cycles

AIRCRAFT WAS NOT GROUNDED: 9C EMERGENCY LIGHT IS WRONG COLOR. **SUPPLEMENTAL REPORT FOR AALA202111193106: REMOVED AND REPLACED 9C EMERGENCY LIGHT COVER PER AMM 33-50-00.** (CLOSED)

Part: DOOR — FAULTED (ZONE 800 - DOORS) · airframe 21,751 hrs · 10,285 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, DOOR L EMERGENCY EXIT CAME ON, SHOWED LEFT OVERWING EXIT NOT LOCKED. FLIGHT DECLARED EMERGENCY RETURNED TO MIA. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. INSPECTED AND ACCOMPLISHED EMERGENCY EXIT DOOR PER TSM 52-21-00-810-806-A NO FAULTS NOTED OK FOR SERVICE.

Part: BRAKE ASSY — OVERTEMP (ZONE 700 - GEARS) · airframe 21,699 hrs · 10,263 cycles

AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.

Part: BRAKE ASSY — OVERTEMP (ZONE 700 - GEARS) · airframe 21,699 hrs · 10,263 cycles

AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY PER WORK CARD 26L70032008.

Part: WHEEL — OVERTEMP (ZONE 700 - GEARS) · airframe 21,699 hrs · 10,263 cycles

AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.

Part: MOTOR — OVERTEMP (ZONE 700 - GEARS) · airframe 21,699 hrs · 10,263 cycles

AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.

Part: PUMP — LOW PRESSURE (CENTER TANK) · airframe 21,277 hrs · 10,062 cycles

AIRCRAFT WAS NOT GROUNDED FUEL CENTER TANK PUMP 1 LOW PRESSURE: (OPEN)

Part: PRESSURE SWITCH — DEFECTIVE (CNTR FUEL PUMP) · airframe 21,277 hrs · 10,062 cycles

AIRCRAFT WAS NOT GROUNDED FUEL CENTER TANK PUMP 1 LOW PRESSURE: **SUPPLEMENTAL REPORT FOR AALA202107270783: REPLACED THE PRESSURE SWITCH FOR THE CENTER TANK #1 FUEL PUMP AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 28-21-15** (CLOSED)

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 19,357 hrs · 9,247 cycles

AIRCRAFT WAS NOT GROUNDED. R1 WINDSHIELD DELAMINATED. REPLACED WINDSHIELD, PER TASK CARD 56-94-01.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANEL 231FF CRACKED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AR FR 66 AND FR 23R. REPLACED LOWER SILL PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #6 HAS EXCESSIVE PLAY / WEAR AT RIB 9 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED SILL SHAPE FITTING PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,979 hrs · 8,074 cycles

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

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY / WEAR AT RIB 2 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER CENTER SILL SHAPE FITTING AT FR 67 AND S23L. REPLACED SILL SHAPE FITTING PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,979 hrs · 8,074 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 15,984 hrs · 7,607 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS AFTER PERFORMING OPS TEST OF THE ESCAPE-FACILITIES MSG SHOWS BAT/EPSU (10WL) FWD L. MAINTENANCE REMOVED AND REPLACED 10WL FWD L EPSU POWER SUPPLY IAW AMM 33-51-38. OPS TEST OKAY.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 14,223 hrs · 6,769 cycles

POWER SUPPLY 10WL FAULTED ON A CIDS TEST. REPLACED THE POWER SUPPLY IAW AMM 33-51-38. OPS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 14,126 hrs · 6,728 cycles

L1 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS DEAD. INSTALLED A NEW BATTERY, OPS CHECKED OK IAW AMM 25-65-00.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 14,126 hrs · 6,728 cycles

FOUND THE EPSU 10WL FAULTED AFTER A SYSTEM TEST. RESET EPSU AND OPS CHECKED NORMAL IAW AMM 33-51-38.

Part: LIGHT — CRACKED (CABIN) · airframe 9,935 hrs · 4,881 cycles

EMERGENCY EXIT LIGHT AT L2 DOOR IS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-57-13. OPERATIONAL CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 9,935 hrs · 4,881 cycles

EMERGENCY EXIT LIGHT AT R2 DOOR IS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-57-13. OPERATIONAL CHECK GOOD.

Part: OVEN — FAULTY (GALLEY) · airframe 9,032 hrs · 4,478 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-JAC FLIGHT DIVERTED TO OKC ACCOUNT METALLIC ODOR IN COCKPIT, FIRST CLASS GALLEY AND CABIN. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 GALLEY OVEN (AALA20161230025) AND NR 2 GALLEY OVEN IAW AMM 25-35-19. OPERATIONAL CHECK GOOD.

Part: OVEN — FAULTY (GALLEY) · airframe 9,013 hrs · 4,467 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-JAC FLIGHT DIVERTED TO OKC ACCOUNT METALLIC ODOR IN COCKPIT, FIRST CLASS GALLEY AND CABIN. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 GALLEY OVEN AND NR 2 GALLEY OVEN (AALA20170103005) IAW AMM 25-35-19. OPERATIONAL CHECK GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 8,667 hrs · 4,327 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. R1 DOOR EXIT MARKER IS DAMAGED. REMOVED AND REPLACED EXIT MARKER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: CONTROL UNIT — FAULTED (BRAKE/STEERING) · airframe 8,667 hrs · 4,327 cycles

DURING DESCENT, RECEIVED AN ECAM "BRAKE SYSTEM 1 FAULTY". EMERGENCY DECLARED. LANDING UNEVENTFUL. A SUCCESSFUL RESET WAS ACCOMPLISHED DURING FINAL APPROACH. REMOVED & REPLACED THE BRAKING AND STEERING CONTROL UNIT IAW AMM 32-42-34. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 8,581 hrs · 4,291 cycles

DURING CRUISE THE CREW REPORTED SMOKE IN THE FLIGHT DECK ACCOMPANIED BY AN ELECTRICAL ODOR. EMERGENCY DECLARED. LANDING UEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED TSM 05-50-00, MCM 05-96-84, INSPECTION OF ALL DEUS AND RADIO UNIT IN THE FLIGHT DECK AND ALL E&E COMPARTMENT COMPONENTS AND WIRING WITH NO DISCREPANCIES FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,147 hrs · 2,792 cycles

DURING TAKEOFF, RECEIVED MASTER CAUTION, VENT SKIN VLV FAULT, VENT BLOWER FAULT & VENT EXTRACT FAULT. ALSO AFTER SELECTING FLX TAKEOFF SETTING, RT ENG SPOOL UP LAGGED, COMPARED TO LT ENG CAUSING ACFT TO YAW FEET TO THE RT. TAKE OFF ABORTED AT APPROX 70 KNOTS. TROUBLE SHOT VENT SKIN, BLOWER VLV & VENT EXHAUST FAULTS IAW TSM 21-26-00-810-803-A WITH NO FAULTS FOUND. ACCOMPLISHED STEERING DEVIATION TEST IAW TSM 32-51-00-810-823-A WITH ALL INDICATIONS NORMAL.