Airbus Industrie A310-221

Service difficulty reports · 42

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A310221'
  ORDER BY difficulty_date DESC"

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SDR FDEA201009273752Controller · malfunctionedBEFORE DESCENT, NOTICED R INNER TANK QTY WAS DEPLEATING AT A MUCH HIGHER RATE THAN THE LT INNER TANK. SUSPECTED A FUEL LEAK AND CONSULTED THE QRH. IAW QRH PROCEDURE ACCOMPLISHED AN INFLIGHT SHUTDOWN. PERFORMED INSP ON NR 2 ENG FOR FUEL LEAK AND WET MOTORINSep 27, 2010 · N416FE · Airbus A310221 · Fuel Quantity IndicatorSDR FDEA201005111507Actuator · leakingLT WING NR 6 SPOILER ACTUATOR LEAK. PRESSURED THE HYD SYS CK LEAKAGE IAW AMM 29-10-00-3. REPLACED THE LT NR 6 SPOILER ACTUATOR IAW AMM 27-64-14-4, RESULT:10 DROPS/10MIN CARRIED OUT OPS TEST OF ROLL TEST IAW AMM27-11-00-5 AND LEAK CHECK. TEST OK AND NO LEMay 11, 2010 · N416FE · Airbus A310221 · Drag Control ActuatorSDR FDEA200911123938Actuator · wornLDG GEAR WOULD NOT RETRACT AFTER T/O. REMOVED AND REPLACED LT MLG BOGIE BEAM PITCH DAMPER ACTUATOR IAW AMM 32-11- PERFORMED JACKING FOR ACFT MX OPERATION FOR LANDING GEAR EXTENSION AND RETRACTION TEST ON SYS 1 AND SYS 2. RET/EXT SATISFACTORY IAW AMM 07-Nov 12, 2009 · N416FE · Airbus A310221 · Landing Gear ActuatorSDR FDEA200901300405Unknown · unknownLOST SPOILER NR 7 FOLLOWED BY BLUE HYD PRESSURE/FLUID LOSS ON INITIAL T/O ROLL. RTO AT 50KTS. ON BLOCK PERFORM INSPECTION FOR SIGN OF LEAKAGE, NO LEAK FOUND. COCKPIT CHK BLUE HYD INDICATION AT LOWER BAND OF SVC RANGE. SERVICE TO TOP HAT RANGE AS PER SMPJan 30, 2009 · N416FE · Airbus A310221 · Drag Control SystemSDR 08FDEA03220Adapter · wornMDCC BETWEEN SEAT TRACK 2R AND 3R FRAME 38 CARGO LOADING SYSTEM ADAPTER HAS 2 EACH AREAS OF WORN SCALLOPS. REMOVED WORN CLS ADAPTER AND INSTALLED NEW CLS ADAPTER BETWEEN SEAT TRACK 2R AND 3R FRAME 38 IAW A310-200 SRM 51-40-21 AND SRM 51-72-10.Aug 3, 2008 · N430FE · Airbus A310221 · Fuselage Main, StructureSDR 08FDEA00377Skin · chafedNR 1 ENGINE INBOARD THRUST REVERSER INTERIOR SKIN CHAFED JUST BELOW DEOILER EXHAUST PORT, NAC STATION 385 ,4:00 POSITION. REPAIRED PER EA NR 6-7800-113019 , EXHAUST, NR 1 ENGINE INBOARD T/R AFT BARREL SKIN DOUBLER, REPAIR.Feb 11, 2008 · N416FE · Airbus A310221 · Engine Thrust ReverserSDR 08FDEA00316Bracket · corrodedTHS LEFT LOWER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED LOWER SURFACE, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED LOWER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 SRM 51-40-21. REMOVJan 28, 2008 · N416FE · Airbus A310221 · Horizontal Stabilizer Miscellaneous StructureSDR 08FDEA00312Bracket · corrodedTHS LEFT UPPER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED UPPER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 51-40-21. REMOVED UPPER ATTACH PLATE Jan 28, 2008 · N416FE · Airbus A310221 · Horizontal Stabilizer Miscellaneous StructureSDR 08FDEA00303Seat Track · crackedNR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FEDEX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION.Jan 27, 2008 · N416FE · Airbus A310221 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00302Seat Track · crackedNR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FEDEX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION.Jan 27, 2008 · N416FE · Airbus A310221 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00263Heat Shield · crackedPYLON NR 1 FWD ENG MOUNT, HEAT SHIELD CRACKED (MKD). REMOVED HEAT SHIELD NR 1 ENG PYLON IAW FEDEX A310-200 SRM 51-40-21 PAGE 1. RECEIVED NEW HEAT SHIELD P/N A2611501200200 S/N IC673554 PO 605041.1 FROM SUPPLY. INSTALLED NEW HEAT SHIELD IAW FEDEX A310-200 SJan 24, 2008 · N416FE · Airbus A310221 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00244Skin · corrodedRT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED. REPAIRED RT ELEVATOR LWR SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 224.Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/SkinSDR 08FDEA00243Skin · corrodedRT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 2Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/SkinSDR 08FDEA00232Skin · corrodedRT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED.Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/SkinSDR 08FDEA00231Skin · corrodedRT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 224Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/SkinSDR 08FDEA00209Rib · crackedCRACKED, R/WING SPOILER NR 3 IBD BOX HINGE RIB. REMOVED PANEL IAW A310-200 SRM 51-40-21 PG 7. CUT AND REMOVED CRACKED END RIB IAW A310-200 SRM 57-51-11 PG 227 AND 228. LOCATED, DRILLED AND DEBURRED ITEM 1, ITEM 2, AND ITEM 3 IAW A310-200 SRM 57-51-11 PG 222Jan 21, 2008 · N416FE · Airbus A310221 · Wing, Rib/BulkheadSDR 08FDEA00202Sill · corrodedBULK CARGO DOOR CUTOUT LOWER SILL CORROSION AFT SECTION. MARKED REMOVED AND REPLACED LOWER SILL BEAM IAW A310-200 SRM 53-17-18 FIG 6 SHT 8 AND 51-40-21.Jan 18, 2008 · N416FE · Airbus A310221 · Fuselage Miscellaneous StructureSDR 08FDEA00119Skin · misrepairedEVALUATION OF FUSELAGE NOSE REPAIR (AERODYNAMIC BODY FILLER) BETWEEN FRAMES 3 AND 4 CENTERLINE, JUST AFT OF LOWER EDGE OF RADOME. EVALUATED REPAIR, FOUND REPAIR NOT TO CONFORM TO FEDEX SRM. REMOVED DAMAGED AREA IAW 53-11-12 FIG 201. FABRICATED AND INSTALLEDJan 13, 2008 · N416FE · Airbus A310221 · Fuselage Main, Plate/SkinSDR 08FDEA00027Beam · corrodedNR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT HAS SEVERE RUST ON BOTTOM FACE OF MOUNT. CLEANED BEAM ASSY. IAW AMM 54-51-00-6.5 B-1. REMOVED CORROSION FROM BEAM SURFACE IAW 54-51-00-6.5 B-1 & SRM 51-74-10 ITEM 7 B-2, ITEM 5 A-5 & PMS 01-01-14-1. POLISHED REWORKJan 3, 2008 · N416FE · Airbus A310221 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00026Beam · corrodedNR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT AFT SIDE , 2 PLACES, UPPER END EMITTING RUST. REMOVED & REPLACED NR 2 ENG. MOUNT SHIM REF AMM 54-54-86-4 2B-3. PRIMED SHIM REF AMM 54-51-00-6 PG. 5. MATCH DRILLED SHIM REF SRM 51-4-44. REMOVED & REINSTALLED PRE COOLJan 3, 2008 · N416FE · Airbus A310221 · Engine Mount SectionSDR 08FDEA00025Mount · corrodedNR 1 ENGINE PYLON AFT ENGINE MOUNT LOWER SURFACE LIGHT CORROSION AROUND LEFT AND RIGHT OUTBOARD SIDES. CLEANED ASSY IAW AMM 54-51-00 6.5 B.P1 REMOVED CORRSION FROM ASSY SURFACE IAW SRM 51-74-10 ITEM 7 B-2 & PMS 01-01-14-1, POLISHWED REWORK AREA IAW AMM 54-51-0Jan 3, 2008 · N416FE · Airbus A310221 · Engine Mount SectionSDR 08FDEA00022Support Angle · crackedLEFT WING UPPER SURFACE TRAILING EDGE PANEL NR 575BT CUTOUT SUPPORT ANGLE CRACKED AT STATION 490. CLEANED AREA IAW FEDEX A310-200 SRM 51-23-10 PG 1. ACCOM. HFEC INSP. PER A310 NTM 51-10-08. VERIFIED AREA IS CRACKED. USED TOOL TWS 8209A. UNABLE TO MARK END OFJan 3, 2008 · N416FE · Airbus A310221 · Wing Miscellaneous StructureSDR 06FDEA1306Selector Valve · malfunctionedSHORTLY AFTER T/O, NR 2 REVERSER UNLOCK LIGHT ILLUMINATED WITH ECAM WARNING LIGHT STAYED ON FOR APPROX 30 SEC, FLICKERED AND WENT OUT. THE LIGHT AND ECAM WARNING CAME ON AGAIN A FEW SECONDS LATER IT STAYED ILLUMINATED FOR SEVERAL MINUTES AND WENT OUT, AT NO TApr 4, 2006 · N416FE · Airbus A310221 · Engine Thrust ReverserSDR 01FDEA01000Warning System · activatedON CLIMBOUT NR 1 EGT PEGGED AT MAX GAUGE NOSE GEAR SHOW UNSAFE.Nov 17, 2001 · N416FE · Airbus A310221 · Engine EGT/TIT Indicating SystemSDR 00FDEA00625Elevator · malfunctionedAFT 20 MIN OF FLT A/C HAD A AIR TURNBACK DUE TO TOO MUCH PRESS NEEDED TO OPERATE ELEVATOR. AC RETURN TO LAX.Sep 5, 2000 · N448FE · Airbus A310221 · Elevator Control SystemSDR 00FDEA00464Controller · failedAIR TURNBACK, FOR MULTIPLE FAILURES. NR 1, 2 PITCH TRIM, NR 2 A.T.S, NR 1, 2 TRANSPONDERS, NR 1 CABIN PRESS, CAPT TAT WARNING, CAPT A.S. & PFD. *S/D* REMOVED AND REPLACED RLY 10XE, PROX DET UNIT, NR 2 TRANSFORMER RECTIFIER MM 24-32-00-/5, MM 32-61-00/501.Jul 19, 2000 · N446FE · Airbus A310221 · Cabin Pressure ControllerSDR 00FDEA00406Engine · failedAFT 20 MIN OF FLT, CREW HEARD LOUD BANG, NR 2 ENGINE FAILED. NO IND ON N1 OR N2 IND''S. AC RETURNED TO MEM.Jun 25, 2000 · N446FE · Airbus A310221 · Engine (Turbine/Turboprop)SDR 99FDEA00236Pitot System · dirty99-143 - NO AIRSPEED IND ON F/O SIDE PFD ON T/O. RTO AT 70 KNOTS. PERF ADC NR 2 OPS CK IAW MM 34-10-00 SYS CK GOOD. FLUSHED NR 2 PITOT SYS IAW 34-10-00, FOUND DEBRIS IN F/O PITOT TUBE, SYS OK FOR SERVICE.Jun 24, 1999 · N448FE · Airbus A310221 · Pitot/Static SystemSDR 99FDEA00233Adc · inoperativeNO AIRSPEED IND ON TAKEOFF ROLL. ALL PFD SYMBOLS WERE PRESENT BUT CAPT AIRSPEED TRIANGLE NEVER INCREASED FROM 0. REMOVED AND REPLACED NR 1 ADC IAW M/M 34-11-34, SYSTEM OK FOR SERVICE.Jun 23, 1999 · N448FE · Airbus A310221 · Air Data ComputerSDR 99FDEA00234Airspeed Ind · inoperativeCAPT HAD NO AIRSPEED INDICATION ON PFD DURING T/O. ABORTED AT 70 KNOTS. F/O AND STBY AIRSPEED INDICATE NORMAL.Jun 22, 1999 · N448FE · Airbus A310221 · Airspeed/Mach IndicatorSDR 98FDEA00480Control Handle · failed98-0188 STA-IND - AFTER T/O LANDING GEAR WOULD NOT RETRACT UNLOCK AND GREEN DIAMONDS ON ALL 6 INDICATORS. BOTH SYS 1 AND SYS 2 ON POSITION DETECTOR SWITCH TRIED MULTIPLE TIMES. REMOVED AND REPLACED LAND GEAR CONTROL HANDLE MODULE PER M/M 32-30. PERFORMED GJul 30, 1998 · N448FE · Airbus A310221 · Landing Gear SelectorSDR 97FDEA00808Engine · flamed outNR 1 ENGINE FLAMED OUT DURING CRUISE AT 5,000 FT, NO PRIOR INDICATIONS. CONT RELIGHT PLACED ON AND ENGINE RELIT IMMEDIATELY, N1 ROLLED BACK FROM APPROX 70 PERCENT TO 40 PERCENT BEFORE RELIGHT. FAILURE OCCURRED SHORTLY OR DURING AN AUTOTHROTTLE-COMMANDED POWENov 6, 1997 · N446FE · Airbus A310221 · Engine (Turbine/Turboprop)SDR 97FDEA00561Pitot Line · cloggedON DEPARTURE CAPTS AIRSPEED TAPE WAS SHOWING ERRONEOUS SPD IND. SWIT TO ALT SPD TAPE RETURNED TO OPERATION BUT SPD WAS 300 KTS WHEN F/O WAS 160 KTS. SWITCHED TO ALT EFIS NO CHANGE. AFTER FLAP/SLAT RETRACT NR 1 YAW DAMPER FAILED AUTO THROTTLE SYS FAILED WOULAug 16, 1997 · N448FE · Airbus A310221 · Pitot/Static SystemSDR 97FDEA00170Fuel Control · out of adjustON TAXI IN AT IDLE POWER, NR 1 ENG FLAMED OUT WITH CORRESPONDING ENG FAIL ECAM WARNINGS. FOR INFORMATION, 25-30 KT TAILWIND WAS PRESENT WHEN ENG FAILED. ENGINE RUN PERFORMED AND GROUND IDLE SPEED FOUND TO BE LOW. TEST NR 9 FUEL CONTROL TRIM PERFORMED IAW M/Mar 14, 1997 · N448FE · Airbus A310221 · Fuel Control/Turbine EnginesSDR 96FDEA01696Controller · malfunctionedCLIMBOUT APPROX 8,000 FT, RECEIVED RED ECAM WARNING LWR ACCESS DOOR NOT CLOSED, FOLLOWED BY EXCESSIVE CABIN RATE. ACCOMPLISHED ECAM. CABIN RATE CLIMBED AT SAME RATE AND ALTITUDE AS A/C DESCENDED TO 10,000 FT MADE PRECAUTIONARY LANDING KUL. LONG HISTORY OF PDec 5, 1996 · N419FE · Airbus A310221 · Cabin Pressure ControllerSDR 96FDEA01687Regulator · malfunctionedAFTER NR 2 ENG START CABIN AUTO PRESS NR 2 AND NR 2 REGULATOR FAIL, NR 1 SYS OK. AFTER TAKEOFF UNABLE TO PRESSURIZE CABIN IN AUTO OR MANUAL. THE OVERRIDE AND ECAM OUTFLOW VALVE POSITION INDICATED CLOSED. RESET NR 2 AUTO FLOW VALVE AND CONTROLLER C/B'S. ALSNov 21, 1996 · N419FE · Airbus A310221 · Pressure Regulator/Outflow ValveSDR 96FDEA01684Tr Cowl · damagedUPON ARRIVAL, DURING WALKAROUND FOUND APPROX 18 DIA HOLE ON AFT INBD EDGE OF NR 2 ENGINE FAN COWL. ALSO, NOTED SEVERE DISCOLORATION ON INBD REVERSER HALF WITH BURN STREAKS AND STRUCTURAL DAMAGE TO THE REVERSER. *S/D* REMOVED AND REPLACED GROUND THRUST REV CNov 20, 1996 · N448FE · Airbus A310221 · Engine Thrust ReverserSDR 96FDEA01634Actuator Rod · shearedREPORTED BY RAMP PERSONNEL. WHILE OPENING THE MDC DOOR. A LOUD SOUND WAS HEARD. MX DISCOVERED THAT THE MDC DOOR ACTUATOR ROD-END SHEARED. *S/D* REMOVED AND REPLACED MDC DOOR ACTUATOR PER M/M 52-36-27 AND TESTED PER M/M 52-36-00, CHECK OK.Oct 29, 1996 · N419FE · Airbus A310221 · Cargo/Baggage DoorsSDR 96FDEA01415O-Ring · failedSTA SFS - APPROX 1 HOUR INTO CRUISE, ECAM REPORTED GREEN HYD SYS RESERVOIR LOW OVERHEAD AND SYS PAGE AGREED. ACCOMPLISHED PROCEDURE, SHUT DOWN GREEN SYSTEM. MANUALLY EXTENDED GEAR. CHECKED AND FOUND HYD GREEN SYS GREEN ELECTRO HYD SELECTOR FITTING LEAKING.Aug 28, 1996 · N419FE · Airbus A310221 · Hydraulic System, MainSDR 96FDEA01391Gcu · malfunctionedNR 1 GENERATOR FAULT WITH INTERMITTENT NR 1 IDG FAULT. GENERATOR DID RESET BUT STILL HAD NR 1 IDG FLASHING. *S/D* PERFORMED OPS CHECK OF AIR/COOLER, CHECKS GOOD. REMOVED AND REPLACED NR 1 GCU, OPS CK'D GOOD.Aug 26, 1996 · N417FE · Airbus A310221 · AC RegulatorSDR 96FDEA01238Hyd Line · leakingSTA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THAN HAT ARC. T/S FOUND HYD FLUID LEAKING FROM LT INSIDE WING SPAR BETWEEN PYLON AND 1ST FLAP TRACK IT IS A RIDGID LINE FOR AILERON DROOP RUBBJul 11, 1996 · N418FE · Airbus A310221 · Hydraulic System, MainSDR 96FDEA00037Structure · vibrationAFTER TAKEOFF WITH GEAR UP, A/C STARTED VIBRATING. GEAR WAS CYC DOWN & UP WITH NO PROBLEMS. VIB CONTD. LEVEL OFF AT 5000 FEET. FLAPS/SLATS RETRACTED, VIBRATION STOPPED AT PWR REDUCTION (VIB WAS MOD). RETND FOR LANDING WITH NORMAL SLAT/FLAP EXTENSION & NO Jan 10, 1996 · N416FE · Airbus A310221 · Aircraft Structures
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