Airbus A310

Service difficulty reports · 606

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A310'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 02FDEA00512Seal · leakingNR 1 ENGINE, STARTER DRIVE SHAFT OIL LEAKAGE. REMOVED AND REPLACED SEAL PER AMM.Jul 9, 2002 · N446FE · Airbus A310 · Turbine Engine Oil SystemSDR 02FDEA00466Bearing · wornELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 7 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. REMOVED AND REPLACED BEARINGS & HINGE ARM PER AMM 55-10-43-4.Jul 9, 2002 · N446FE · Airbus A310 · Elevator StructureSDR 02FDEA00467Pin · rotatedVERTICAL STABILIZER LEFT MID ATTACH FITTING PIN INDICATOR LINE SHOWS PIN ROTATED. REMOVED AND REPLACED PIN PER AMM 55-36-39-6.Jul 9, 2002 · N446FE · Airbus A310 · Vertical Stabilizer, Attach FittingsSDR 02FDEA00468Bearing · wornELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 1 LT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. REMOVED AND REPLACED BEARINGS & HINGE ARM PER AMM 55-16-43-4.Jul 9, 2002 · N446FE · Airbus A310 · Elevator StructureSDR 02FDEA00469Bearing · wornELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 5 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. REMOVED AND REPLACED BEARING AND HINGE ARM PER AMM 55-16-45.Jul 9, 2002 · N446FE · Airbus A310 · Elevator StructureSDR 02FDEA00470Hinge · wornELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 6 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. REMOVED AND REPLACED HINGE ARM PER AMM 55-22-13.Jul 9, 2002 · N446FE · Airbus A310 · Elevator StructureSDR 02FDEA00471Hinge · wornELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 1 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. REMOVED AND REPLACED BEARINGS PER AMM 55-16-43-4.Jul 9, 2002 · N446FE · Airbus A310 · Elevator StructureSDR 02FDEA00483Structure · damagedLT PYLON AFT BRACKET WHERE HYD LINES PASSES THROUGH FROM WING TO PYLON FOUND HOLES ELONGATED. REMOVED AND REPLACED HOLES PER IAW EA 26-5210-64291.Jul 8, 2002 · N446FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00482Structure · damagedNR 2 RT PYLON AFT FAIRING UPPER SIDE HYDRAULIC LINES HOLE ELONGATED ON THE FAIRING SIDE. REMOVED AND REPLACED HYD LINE HOLES PER EA 6-5710-64292.Jul 8, 2002 · N446FE · Airbus A310 · Wing Miscellaneous StructureSDR 02FDEA00499Stringer · corrodedN 108 STRINGER 56R AT CONNECTOR AFT OF FRAME 72. R&R STRINGER PER SRM 53-10-14.Jul 8, 2002 · N446FE · Airbus A310 · Fuselage Structure (General)SDR 02FDEA00462Proximity Sensor · malfunctionedCOULD NOT RETRACT GEAR ON POSITION 1 SELECTED POSITION 2 THE GEAR CAME UP (REPEAT WRITEUP) SUBSEQUENT INDICATIONS WERE PITCH TRIM INOP, ATS 2 OFF CAPT TAT INOP, (HEAT FAILURE) & CABIN PRESS REG 1 FAIL & NR 1 TRANSPONDER, NO ALTITUDE READOUT. REMOVED AND REPJul 5, 2002 · N402FE · Airbus A310 · Landing Gear Position and WarningSDR 02FDEA00449Compressor · stalledIMMEDIATELY AFTER LEVEL OFF AT FL350, NR 2 ENG EXPERIENCED SEVERE COMPRESSOR STALLS. PWR WAS REDUCED, WHEN PWR WAS INCREASED STALL RETURNED. F/F & EGT FLUX WAS EVIDENT AND N1 & 2 MOVED ACCORD. QRH PROC WAS ACCOMPL DURING DESCENT AND RETURNED TO ABQ. WHEN HJul 1, 2002 · N405FE · Airbus A310 · Turbine Engine Compressor SectionSDR 02FDEA00408Pylon · crackedCRACK FOUND ON HOLE #7 AND #6 ON OVERWING REFUEL APARTURE. ** S/D ** COMINGJun 18, 2002 · N421FE · Airbus A310 · Nacelle/Pylon StructureSDR 02FDEA00409Skin · corrodedWIDESPREAD CORROSION ON FUSELAGE SKIN ON THE OUTBOARD SIDES OF THE VERTICAL STAB LT & RT ATTACHMENT. R/R ALL TRACES OF CORROSION.Jun 18, 2002 · N421FE · Airbus A310 · Vertical Stabilizer, Plate/SkinSDR CA020617006Manifold · cracked(CAN) FOUND CRACK ON NR 1 ENGINE LPT AIR MANIFOLD SLEEVE BETWEEN 6-7 OCLOCK POSITION. A TEMPORARY REPAIR TO THE MANIFOLD SLEEVE WAS CARRIED OUT. A FLUID PENETRANT INSPECTION WAS CARRIED OUT; NO EVIDENCE OF CRACK FOUND. A DEFERRED MAINTENANCE ITEM WAS RAISEJun 13, 2002 · Airbus A310 · Turbine SectionSDR 02FDEA00404Fitting · corrodedRT WING PYLON SPIGOT BALL JOINT FOUND WITH BROWN STAIN ALL AROUND THE CIRCUMFERENCE OF FITTING. CLEARED IAW EA 6-5450-59029.Jun 12, 2002 · N421FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00406Fitting · corrodedLT WING PYLON AFT FITTING BALL JOINT ASSY FACE FOUND WITH BROWN STAIN. CONFIRMED CORROSION ON 12 JUNE 2002. INSTALLED NEW FITTING ASSY PER S/B A310-54-2021 EA. 6-5150-59026.Jun 12, 2002 · N421FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00405Nut · corrodedRT WING PYLON AFT FITTING BALL JOINT ASSY NUT FOUND WITH GREENISH STAIN. CONFIRMED CORROSION ON 12 JUNE 2002. INSTALLED NEW FITTING ASSY PER AIRBUS S/B A310-54-2021.Jun 12, 2002 · N421FE · Airbus A310 · FastenersSDR 02FDEA0404Fitting · corrodedRT WING PYLON SPIGOT BALL JOINT FOUND WITH BROWN STAIN ALL AROUND THE CIRCUMFERENCE OF FITTING.Jun 12, 2002 · N421FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00403Fitting · corrodedLT WING PYLON FWD SPIGOT BALL JOINT FOUND WITH BROWN STAINS ALL ROUND THE CIRCUMFERENCE OF FITTING. CONFIRMED CORROSION ON 12 JUNE 2002.Jun 12, 2002 · N421FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00384Controller · failedAIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 SYSTEM CONTROLLER CONTINUOUSLY SHOWS THE AIRCRAFT AT AN ELEVATION OF 400 FT WHEN IT SHOULD READ AJun 8, 2002 · N412FE · Airbus A310 · Cabin Pressure ControllerSDR 02FDEA00380Outflow Valve · damagedOVBD VALVE FAULT PLACED SWITCH TO OFF PER ECAM A/C WOULD NOT PRESSURIZE MEL 04JUN02 23:17 MEM R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-23-06 EQUIPMENT COOLING OVERBOARD VALVE FAULT LIGHT - INOP. VALVE MANUALLY SET PARTIALLY OPEN. FACT 05JUN02Jun 4, 2002 · N423FE · Airbus A310 · Air Distribution SystemSDR 02FDEA00378Pitot Line · obstructedMDIS- FIRST OFFICERS AIRSPEED IND INOP ON ELECTRONIC FLT INSTRUMENT SYSTEM. DISCONNECTED FIRST OFFICERS PITOT CONNECTION FOUND BLOCKAGE, CLEANED PITOT LINE AND RECONNECTED. BLEW PITOT NR 2 SYSTEM AIR LINES OUT AND RECONNECTED PITOT LINES. OPS CHECK GOOD.Jun 4, 2002 · N443FE · Airbus A310 · Pitot/Static SystemSDR 02FDEA00372Thrust Reverser · unlockedPDIS- AFTER TAKEOFF FROM TULSA HAD IND OF NR 1 REVERSER UNLOCKED, UPON SLAT RETRACTION HAD YAW COMMENSURATE WITH UNLOCKED REVERSER. R/R LT THRUST REVERSER CDU SWITCH.Jun 1, 2002 · N414FE · Airbus A310 · Engine Thrust ReverserSDR CA020528007Shutoff Valve · corroded(CAN) FUEL SHUTOFF VALVE, DURING 8C CHECK RT ENGINE LOWERED TO ALLOW FOR MOUNT BOLT REPLACEMENT & CORROSION REPAIR. ON REINSTALLED ENGINE INTERNAL & EXTERNAL LEAK CHECK OF LP FUEL FIRE SHUTOFF VALVE REQUIRED PER J/C 71-400-001-2. FUNCTION CHECK REVEALED THATMay 27, 2002 · Airbus A310 · Fuel Selector/Shut-Off ValveSDR 02FDEA00Sequence Valve · malfunctionedAFTER T/O FROM LGB THE GEAR WAS RAISED AND WAS CONFIRMED UP AND LOCKED UNTIL SLATS WERE RETRACTED AT WHICH TIME A THUMP AND SLIGHT SHUDDER WAS FELT AND L MAIN GEAR INDICATED UNSAFE. GEAR HANDLE WAS PLACED IN THE DOWN POSITION WITH ALL GEAR INDICATING DOWN ANDMay 17, 2002 · N442FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 02FDEA00312Bleed Valve · malfunctionedCRUISE IN WX AT 350 MACH 80 A/I ON, EXPERIENCED ENGINE COMPRESSOR STALL ON NR 2 ENGINE. REMOVED EVBC.May 4, 2002 · N456FE · Airbus A310 · Compressor Bleed ValveSDR CA020514001Tube · cracked(CAN) PRESENCE OF FUEL WAS DETECTED IN APU FUEL FEED LINE SHROUD, BENEATH CABIN FLOOR BETWEEN FRAMES 46 & 79. AFTER REMOVING A SECTION OF SHROUD FROM DRAIN TO FRAME 46 & GOING AFT, FUEL SHROUD AFT OF FRAME 79 STOPPED SHOWING PRESENCE OF FUEL. APU FUEL FEED TUBMay 3, 2002 · Airbus A310 · APU Engine Fuel and ControlSDR 02FDEA00250Line · kinkedNR 1 THROTTLE SPLIT 12 DEG TA MORE THAN NR 2, NR 1 NACELLE TEMP 35-45 DEG HOTTER THAN NR 2. REMOVED AND REPLACED PT2/TT2 SENSOR AND THE TT2 SENSOR. REMOVED AND REPLACED KINKED PT7 LINE AND RESEALED 1, 2, 3, 12, 13, 14 AND 16 FUEL NOZZLE PAD AIR LEAKS ALL ON Apr 11, 2002 · N447FE · Airbus A310 · Engine Pressure Ratio (EPR)SDR 02FDEA00231Compressor · stalledSEVERAL COMPRESSOR STALLS ON NR 1 ENGINE FL350. NO OTHER PARAMETERS NOTED. BLED ENG AND SLOWLY BROUGHT POWER BACK IN. REMOVED AND REPLACED NR 1 ENGINE AFTER NUMEROUS PARTS REPLACED.Apr 6, 2002 · N419FE · Airbus A310 · Turbine Engine Compressor SectionSDR 02FDEA00230Regulator · faultyON TAKEOFF THROTTLE WERE 2 KNOB WIDTHS APART. NR 1 ENG W/N REACH FULL CLIMB PWR. DURING DESCENT NR 1 ENG IDG ADVISORY ILLUMINATED & TEMP REACHED 144 DEG. REMOVED AND REPLACED PRESS REGULATOR & SHUTOFF VALVE. TRIMMED HEATSHIELD, LEAK CHECK GOOD.Apr 5, 2002 · N447FE · Airbus A310 · Compressor Bleed ControlSDR CA020405028Throttle Cable · contaminated(CAN) ENGINE NR 2 THROTTLE JAMMED IN DESCENT , IN IDLE POSITION. MAINTENANCE FOUND THE THROTTLE CONTROL CABLE ASSEMBLY WATER SOAKED AND ALSO FOUND THE ELASTOMER SLEEVE RIPPED OPENED. BOTH PARTS WERE REPLACED ; THE THROTTLE CONTROL CABLE ASSY.REPLACED I.A.W. Mar 31, 2002 · Airbus A310 · Power LeverSDR CA020308003Valve · unserviceable(CAN) FLT 757, LOST OF BLUE HYDRAULIC SYSTEM FLUID IN FLIGHT. HYDRAULIC LEAK WAS FOUND COMING FROM NR 3 RT SPOILER VALVE GROUP AT THE FILTER HOUSING CAP PACKING. AFFECTED SPOILER VALVE GROUP WAS REPLACED AND A/C WAS RETURNED TO SERVICE.Mar 8, 2002 · Airbus A310 · Drag Control ActuatorSDR 02FDEA00067Compressor · stalledNR 1 ENGINE COMPRESSOR STALL AT FL 350. THIS WAS FOLLOWED BY COMPLETE LOSS OF OIL PRESS, FOLLOWED ECAM PREC ENGINE SHUTDOWN. ENG WIND MILLED FOR ABOUT 30 MIN. REMOVED AND REPLACED NR 1 ENGINE.Jan 25, 2002 · N447FE · Airbus A310 · Turbine Engine Compressor SectionSDR CA020117017Door · missing(CAN) FOUND REFUELING PANEL DOOR MISSING ON ARRIVAL TO "VRA". REFUELING DOOR AND AN AIR INLET PANEL WERE REPLACED.Dec 10, 2001 · Airbus A310 · Service DoorsSDR 01FDEA00907Warning System · activatedAS SOON AS MLG BROKE OFF GROUND ECAM IND LG RETRACT FAULT.Oct 23, 2001 · N424FE · Airbus A310 · Landing Gear Position and WarningSDR 01FDEA00902Indicator · out of positionUNABLE TO RAISE LG IN POS 1. SWITCH TO POS 2, NO SUCCESS. RESET LT MLG PITCH DAMPER PRESS DROP IND. CHECK OK.Oct 23, 2001 · N424FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR CA011211027Pump · leaking(CAN) AIRCRAFT ARRIVED WITH NR 1 ENGINEHI VIBRATION DURING TAXI. TROUBLESHOOTING WAS CARRIED OUT IAW MM 72-31-00 AND FOUND GREEN HYDRAULIC PUMP SHAKING & LEAKING. THE PUMP WAS REPLACED & CHECKED SERVICEABLE.Sep 21, 2001 · Airbus A310 · Hydraulic Pump (Electric/Engine), MainSDR 01FDEA00769Controller · malfunctionedPDIS WRI 26-12-5025 AT ABOUT 1500 AFT MAIN DECK CARGO LOOP-A ILLUMINATED, FOLLOWED BY LOOP-B AND RED SMOKE LIGHT & ECAM FIRE WARNING. DECLARED EMER AND RETURNED TO LAND. REMOVED AND REPLACED AFT UPPER CARGO SMOKE DETECTION CONTROLLER AND TESTED PER MM 26-19-Aug 24, 2001 · N408FE · Airbus A310 · Detection SystemSDR 01FDEA00671Hydraulic System · failedON CLIMB LOST YELLOW SYS HYD QTY WENT TO RED DOT. PERF EMERGENCY CHECKLIST PER ECAM AND RED TABS.Aug 10, 2001 · N410FE · Airbus A310 · Hydraulic System, AuxiliarySDR 01FDEA00570Fire Warning · malfunctionedON CLIMBOUT NR 1 ENG FIRE WARNING. COMPLETED ECAM FIRE PROC, SHUTDOWN ENG. FIRED BOTTLES. REMOVED BOTH FIRE BOTTLES AND SQUIBS. RAN ENG AT HIGH POWER CK DUCTS, NO LEAKS NOTED.Jul 17, 2001 · N416FE · Airbus A310 · Fire DetectionSDR CA010723043Valve · failed(CAN) ETOP REQUIRED REPORTING. AIRCRAFT COULD NOT TRANSFER ALL THE FUEL FROM CENTER TANK. FQIS RESET AND BITE CHECKED SERVICEABLE. THIS IS A RECURRING DEFECT WHERE THE FQIS IS REST AND THE DEFECT RETURND A COUPLE OF FLIGHTS LATER ADDITIONAL TROUBLE SHOOTING REJul 16, 2001 · Airbus A310 · Fuel Transfer ValveSDR 01FDEA00163Panel · faultyNR 1 ENG AGENT NR 2 DISCHARGE LIGHT CAME ON IN FLT. REMOVED AND REPLACED NR 1 ENG OVERHEAD FIRE SHUTOFF PNL. RECHECK GOOD. OPS CK PER A300 AMM 26-12-20-4.Feb 24, 2001 · N680FE · Airbus A310 · Fire DetectionSDR 98FDEA00567Csd · failedDURING CRUISE, IDG OIL OUTLET FLASHING ADVISORY CAME ON NR 2 DISCONN START TEMP AROUND 135 DEG CELSIUS. AIR/OIL COOLER INOP. SECURE OPEN RAN ENG AT 85 PERCENT N1 TEMP AT 48C, DEFERRED OIL COOLER VALVE PER MEL 75-1B. *S/D* REMOVED AND REPLACED AIR/OIL HEAT Sep 10, 1998 · N417FE · Airbus A310* · Alternator-Generator DriveSDR 97FDEA00635Fuel Pump · malfunctionDURING T/O ROLL WITH T/O POWER SET, NR 2 ENG POWER STARTED FLUCTUATING. EEC OFF DUE NR 2 ENG EPR DEFERRED. REPLACED NR 2 ENG FUEL PUMP, FUEL CONTROL AND ENGINE VANE AND BLEED CONTROLLER. ENGINE RUN-UP CHECK OK.Sep 4, 1997 · N417FE · Airbus A310* · Engine Fuel PumpSDR 97FDEA00452Doubler · corrodedCORROSION ON INNER DOUBLER BETWEEN FRAMES 39 AND 40 BOTTOM CENTERLINE OF FUSE. THINNEST AREA MEASURED .085 THICK. REPAIRED PER EA 6-5310-29140 DATED, 7-11-97. REMOVED CORROSION, FABRICATED STRAP FROM .003 2024.73 LENGTH WAS AREA PLUS 3 FASTENERS EACH END. Jul 17, 1997 · N401FE · Airbus A310* · Fuselage Miscellaneous StructureSDR 97FDEA00453Plate · crackedCRACK IN LT WING L/E NOSE SKIN REINFORCING PLATE, (P/N A57243292200), BELOW SLAT TRACK NR 6. REPAIRED PER EA 6-5710-29135 DATED 7-11-97, BY REMOVING CRACKED PLATE. FABRICATING NEW PLATE FROM .063 STRINGERS HEAT TREATED TO 1050 AND INSTALLED WET WITH 1422 SEAJul 11, 1997 · N401FE · Airbus A310* · Wing, Plate/SkinSDR 97FDEA00454Plate · crackedWING L/E SKIN REINFORCING PLATES WERE FOUND CRACKED, ABOVE SLAT TRACKS SEVERAL LOCATIONS. REPAIRED PER EA 6571029129 DATED JULY 7, 1997 AND SRM BY INSTALLING NEW PLATES.Jul 7, 1997 · N401FE · Airbus A310* · Wing, Plate/SkinSDR 97FDEA00451Support · corrodedCORROSION ON RBL 20, FRAME 66 FLOOR SUPPORT. REMOVED CORROSION PER SRM AND INSTALLED DOUBLERS PER EA NR 6532129138 DATED JULY 14, 1997.Jul 7, 1997 · N401FE · Airbus A310* · Fuselage Miscellaneous StructureSDR 97FDEA00450Floorbeam · crackedFLOORBEAM FRAMES 33, 34, 35 AND 36 CRACKED FORM MAIN DECK CARGO. REPAIRED PER SRM 53-10-15 FIG 206, SHEET 3 AND EA 6-5321-29128 DATED JULY 7, 1997,Jul 7, 1997 · N401FE · Airbus A310* · Fuselage Main, Floor Beam
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