Airbus A310

Service difficulty reports · 606

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Query with SQL
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 03FDEA00375Rib · damagedCOMPLY WITH EA 6-5740-68775 WINGS-RT SLAT NR 2-LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3 UNDER W/O NR 13350 FEDEX N/R NR S00005. *S/D* COMPLIED WITH EA 6-5740-68775 WINGS-RT SLAT NR 2 LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3. Apr 2, 2003 · N443FE · Airbus A310 · Leading Edge DevicesSDR 03FDEA00356Panel · crackedNR 2 ENG I/B TRANSLATING COWL UPPER T- TRACK SLIDER CRACKED OFF. INSTALLED NEW UPPER SLIDER WITH NEW TRANSLATING SLEEVE W/C NOO193Mar 28, 2003 · N443FE · Airbus A310 · Nacelle/Pylon, Main FrameSDR 03FDEA00355Panel · peelingNR 1 ENGINE OUTBOARD THRUST REVERSER TRANSLATING PANEL UPPER SLIDER TEFLON PEELING UP, AND SLIDER DAMAGED.Mar 28, 2003 · N443FE · Airbus A310 · Engine Thrust ReverserSDR 03FDEA00354Rib · crackedLT HORIZONTAL STAB. INTERIOR RIB 5 UPPER CHORD AT REAR SPAR IS CRACKED AT HOISTING POINT WRITTEN ON FEDEX N/R N00494 UNDER MAE W/O NR 13350 CUT OUT DAMAGED SECTION IAW/SRM 51-71-50 FABRICATED REPAIR ANGLE OF 7075T6 BATCH NR 7R00115001 IAW/SRM 51-71-50 Mar 28, 2003 · N443FE · Airbus A310 · Horizontal Stabilizer StructureSDR 03FDEA00353Panel · delaminatedVERTICAL STAB. LE PANEL 321AL DELAMINATEDMar 28, 2003 · N443FE · Airbus A310 · Vertical StabilizerSDR 03FDEA00357Spar Cap · corrodedLT HORIZONTAL UPPER AFT SPAR CAP CORRODED APPROX. 4FT. FROM FUSELAGE. UNDER MAE W/O NO. 13350. REPAIRED AFT SPAR CAP IAW SRM 55-13-11 AND SRM 51-41-01. Mar 21, 2003 · N443FE · Airbus A310 · Horizontal Stabilizer StructureSDR 03FDEA00340Solenoid Valve · failedAFTER TAKE OFF AT SIN, RECEIVED FLAPS SYS 1 FAULT. ALSO LOST AIRSPEED HOOK ON CAPT SIDE WITH RED SPEED LIMIT SHOWING. SFCC NR 1 BITE SHOWS FLAP RT WTB. R & R RT WTB SOLENOID VALVE PER MM 27-56-13-4 AND PERFORMED SFCC BITE TEST PER MM 27-51-00 TEST OK. Mar 20, 2003 · N422FE · Airbus A310 · Trailing Edge Flap Control SystemSDR 03FDEA00339Controller · failedON CLIMB OUT SIN. GOT "SLATS" LIGHT AND "SLATS" SYS 1 LIGHT ON OVERHEAD. DID PROCEDURE BUT NO CHANGE. RETURN TO SIN RAMP. SFCC 1 BITE SHOW SFCC FAULTED. R & R NR 1 SFCC PER MM 27-51-18-4. OPS CHECKED OK.Mar 20, 2003 · N422FE · Airbus A310 · Leading Edge Slat Control SystemSDR 03FDEA00312Bracket · corrodedLT HORZONTAL STABILIZER LEADING EDGE ATTACH APRON IS HEAVILY CORRODED AT AFT UPPER "L" ANGLE. REMOVED AND REPLACED WITH ON SITE FABBRICATED PARTS.Mar 13, 2003 · N445FE · Airbus A310 · Horizontal Stabilizer StructureSDR 03FDEA00231Access Panel · damagedLT WING, LOWER ACCESS CUTOUT FOR PANEL 550GB. TWO SCREW HOLES FOR PANEL HAVE DAMAGED EDGES. REMOVED ANCHOR NUTS TO ACCESS DAMAGED HOLES. REMOVED DAMAGED AREA AND REAMED HOLES TO 0.495 AND 0.467. ENSURED CLEANED HOLES ARE CRACK FREE BY HFEC IAW NTM 51-10-01. Mar 5, 2003 · N448FE · Airbus A310 · Wing, Plate/SkinSDR 03FDEA00281Structure · corrodedMLG DOOR, SKIN HAS CORROSION. REMOVED WITHIN LIMITS CORROSION IAW/SRM 51-74-10 ON OUTER SKIN INNER SURFACE. DOOR SKIN OUT OF LIMITS REPAIRED ON E.A.6-5281-6871.RESTORED DOOR IAW/SRM 51-40- 21 PREPPED AND PAINTED IAW/SRM 51-21-50.Feb 20, 2003 · N445FE · Airbus A310 · Landing Gear DoorsSDR 03FDEA00067Tailpipe · damagedSIGNIFICANT TAIL PIPE FIRE DAMAGE FOUND ON POSTFLIGHT WALKAROUND, ON INBOARD AILERON, AND BOTH CANOE FAIRINGS ADJACENT TO THE AILERON ON THE NR 2 ENGINE SIDE (INWORK) WORKING IN CONJUNCTION WITH WRI 73-10/4991, CHECKED COMBUSTER DRAIN VALVE IAW M/M. NO DEFECTJan 21, 2003 · N430FE · Airbus A310 · Engine Collector/Tailpipe/NozzleSDR 02FDEA00961Bulb · faultyLEVELED OFF AT FL330, OIL TEMPERATURE BEGAN INCREASING. INCREASED THRUST, ATTEMPTING TO DECREASE OIL TEMPERATURE, BUT IT CONTINUED TO CLIMB, TURNING AMBER, THEN RED UNTIL IT REACHED 165 DEGREES, SHUT DOWN NR 1 ENGINE AND DIVERTED. REMOVED AND REPLACED TEMP BDec 22, 2002 · N450FE · Airbus A310 · Engine Oil TemperatureSDR 02FDEA00870Attach Fitting · brokenRT WING NR 3 SPOILER, OUTBOARD ACTUATOR LUG BROKEN OFF. COMPLETELY MISSING. FOUND DURING C-CHECK INSPECTION BY MX TASK CARD 46C0510. REMOVED AND REPLACED NR 3 RT SPOILER IAW MM 27-61-51-4 RIG AND OPS CHECKS GOOD GOOD IAW/MM 27-61-51-4. SERVICE TAG NO.7Nov 19, 2002 · N404FE · Airbus A310 · Drag Control SystemSDR 02FDEA00837Wire · chafedON TAKEOFF ROLL GREATER 80 KNOTS TO POWER NOT ACHIEVED. NR 2 EGT FLUCTUATION +- 200C FOLLOWED BY ROLLBACK TO ZERO. DASHED LINES RTD ON TAXI OUT/IN OK. REPAIRED CHAFED WIRING TO NR 2 EGT INDICATOR IAW EA. COMPLIED WITH PART 2 EA. OPS CHECK NORMAL.Nov 14, 2002 · N419FE · Airbus A310 · Engine Indicating System WiringSDR 02FDEA00836Switch · failedGO-AROUND DUE TO ONLY 2 GREEN LANDING GEAR LIGHT ON FORWARD LANDING GEAR PANEL, OVERHEAD LANDING PANEL 3 GREEN AS NORMAL. DURING GO-AROUND FORWARD GREEN NOSE GEAR LIGHT CAME ON. NORMAL LANDING ON SECOND PASS. LANDING GEAR INDICATING PANELS SYSTEM NR 1 NOSE GNov 14, 2002 · N426FE · Airbus A310 · Landing Gear Position and WarningSDR 02FDEA00777Spar · corrodedRIGHT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED BETWEEN RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468.Oct 29, 2002 · N419FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 02FDEA00776Skin · corrodedFOUND CORROSION AT FWD CARGO DOOR INNER SKIN LWR SECTION AT FR 20. R&R SKIN PER EA 6-5230-66467.Oct 29, 2002 · N419FE · Airbus A310 · Cargo/Baggage DoorsSDR 02FDEA00775Spar · corrodedLEFT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED APPROX 280 MM FROM RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468.Oct 29, 2002 · N419FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 02FDEA00774Spar · corrodedRIGHT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED BETWEEN RIB 5 TO 9. R&R T CHORD PER EA 6-5100-66468.Oct 29, 2002 · N419FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 02FDEA00778Bulkhead · corrodedCORROSION ON NOSE LAND GEAR WHEEL WELL BULKHEAD AT LEFT TOP CORNER NEAR FRAME 16. R&R SKIN PER EA 6-5340-66864.Oct 29, 2002 · N419FE · Airbus A310 · Fuselage Main, BulkheadSDR 02FDEA00768Pivot Assy · seizedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. IN SYS 1 OR 2 TROUBLESHOT INTERLOCK SYSTEM. FOR NR 1 AND NR 2 SYSTEMS, FOUND ALL ELECTRICAL FUNCTIONS CHECK GOOD. CHECKS GOOD WITH GROUND ON RECEPTACLE OF PROX BOX AT PINS 44 AND 55. JACKED AIRCRAFT IAW M/M ANDOct 22, 2002 · N445FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 02FDEA00742Skin · corrodedLT WING T/E SKIN CRACKED AT 581AB ACCESS CUTOUT AT RIB 11. R&R SKIN PER EA 6-5710-65463.Oct 15, 2002 · N419FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00741Fitting · corrodedLT PYLON AFT THRUST AND SIDE LOAD FITTING CORRODED AT BEARING FACE. R&R FITTING PER EA 6-5450-66460.Oct 15, 2002 · N419FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00739Fitting · corrodedSIGNS OF CORROSION AT L/PYLON THRUST & SIDE LOAD FITTING SLEEVE. R&R FITTING PER EA 6-5450-66458.Oct 15, 2002 · N419FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00738Fitting · corrodedR/SING PYLON FWD THRUST AND SIDE LOAD FITTING AREA, FOUND BEARING AREAS WITH BROWNISH STAINS AT TOP & BOTTOM OF FITTING. R&R FITTING PER EA 6-5450-66461.Oct 15, 2002 · N419FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00740Fitting · corrodedRT WING PYLON AFT MOUNT FITTING ATTACHMENTS CORRODED. R&R FITTING PER EA 6-5450-66459.Oct 14, 2002 · N419FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00698Bearing · corrodedRIGHT WING ENGINE PYLON AFT MOUNT FITTING BEARING CORRODED. R&R FITTING PER EA 6-5450-65104.Oct 1, 2002 · N422FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00695Fitting · corrodedLT ENGINE PYLON SPIGOT FITTING ASSEMBLY FOUND CORRODED. R&R FITTING PER SB A310-54-2020.Oct 1, 2002 · N422FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00696Fitting · corrodedCORROSION ON RIGHT WING ENGINE PYLON THRUST AND SIDE LOAD FITTING. R&R FITTING PER EA 6-5450-65103.Oct 1, 2002 · N422FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00697Skin · damagedAFT PYLON HYD TUBES FITTING HOLES ON RIGHT WING UNDER SURFACE SKIN FOUND ELONGATED AFT OF PYLON RIB 21. R&R WING LWR SKIN PER EA 6-5710-65098.Oct 1, 2002 · N422FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00694Skin Panel · crackedLEFT WING LWR SKIN PANEL NR 2 FOUND WITH EDGE CRACK JUST OUTBOARD OF RIB 11, CRACKED 1 INCH. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65099.Oct 1, 2002 · N422FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00773Attach Fitting · broken#4 RH SPOILER ACTUATOR ATTACH FITTING IS BROKEN. FWD I/B SIDE OF FITTING IS MISSING. ** S/D ** COMINGSep 28, 2002 · N450FE · Airbus A310 · Flight Control SystemSDR 02FDEA00699Actuator · malfunctionedRUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, FAULTED PASSING 170KIAS. REPLACED NR 2 ADC PER A310 MM34-11-34. OPERATIONAL CHECK AND PITOT/STATIC LEAK TEST GOOD. R&R RUDDER VARIABLE STOP ACTUATOR AS PER A-310, MM 27-23-23-4. R&R NR 1 FEEL LIMITATION COMPUTER Sep 25, 2002 · N420FE · Airbus A310 · Rudder ActuatorSDR 02FDEA00684Relay · failedRUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, WOULD NOT RESET. RUDDER TRAVEL SYSTEM ONE ALREADY DEFERRED. CHECKED FAULT AT FLC NR 2 RUDDER TRAVEL POWER LOOP. PERFORMED T/S PER TSM 27-23-03 REPLACED 309 CY2 RELAY, BITE TEST FLC NR 2 PER MM 27-23-00. OK, NO FASep 24, 2002 · N420FE · Airbus A310 · Rudder Control SystemSDR 02FDEA00717Spar · corrodedBOTH L&R HORIZ STAB UPR & LWR CHORDS OF SPAR CORRODED ENTIRE LENGTH. R&R CHORD PER SRM 55-11-21.Sep 23, 2002 · N403FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 02FDEA00655Skin · corrodedFUSELAGE SKIN INNER SURFACE CORRODED IN AVIONICS COMPT ON RIGHT SIDE OF ENTRY HATCH BETWEEN 8 & 9. CORROSION BLENDOUT DEPTH IS BEYOND LIMITS OF SRM 53-10-00. R&R STIFFENER PER EA 6-5330-65-66446.Sep 19, 2002 · N422FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 02FDEA00641Doubler · corrodedFWD LAVATORY SERVICING PANEL DOUBLER AT LEFT SIDE OF FUSELAGE BETWEEN FRAME 12 AND 12A IS CORRODED ALONG LWR EDGE. R&R FRAME DOUBLER PER EA 6-5330-65-65906.Sep 13, 2002 · N422FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 02FDEA00642Fitting · corrodedLT PYLON AFT MOUNT FITTING FOUND CORRODED. R&R FITTING PER SB A310-54-2021 ON PYLON STRUCTURE.Sep 13, 2002 · N422FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 02FDEA00648Cable · corrodedELEVATOR CONTROL CABLES AZ737114000000 (E2R1) & A2731145000000 (E2RC) AT SUPPORT PULLIES BS 4467 - FR 84 SEVERELY CORRODED. ** S/D ** COMINGSep 13, 2002 · N451FE · Airbus A310 · Elevator Control SystemSDR 02FDEA00640Skin · crackedRIGHT WING OUTER LWR SKIN PANEL NR 2 AT TRAILING EDGE OF RIB 2 CRACK. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65100.Sep 12, 2002 · N422FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00639Doubler · corrodedDOUBLER ON INNER FACE OF FUSELAGE SKIN CORRODED IN AVIONIC COMPT BETWEEN FRAME 16A & 17, EXTENDING FWD OF FRAME 16A OUTBD OF STR 44L & FWD OF FRAME 17 INBD OF STR 44L. R&R SKIN DOUBLER PER EA 6-5330-65-65906.Sep 12, 2002 · N422FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 02FDEA00636Skin · corrodedINNER FACE OF FUSELAGE SKIN CORRODED IN AVIONICS COMPT BETWEEN FRAME 16, 16A AND 17 OUTBOARD OF STRINGER 44R AND BETWEEN FRAME 16A AND 17, INBD OF STR 44R. R&R SKIN DOUBLER PER EA 6-5330-65-65906.Sep 11, 2002 · N422FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 02FDEA00583Torque Box · corrodedCORROSION AROUND FASTENER HEADS IN AVIONICS COMPT NOSE GEAR WHEEL WELL TOP TORQUE BOX (FROM FRAME 13 TO 15A).Aug 13, 2002 · N420FE · Airbus A310 · Fuselage Main, StructureSDR 02FDEA00531Fitting · chafedLT WING PYLON THRUST & SIDE LOAD FITTING OUTBD TOP CORNER OF FITTING FOUND CHAFING.Jul 29, 2002 · N420FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00498ControllerCLIMBING OUT OF SEA, ECAM ALERT - "EXCESS CAB ALT". DONNED O2 MASKS AND TRIED TO TROUBLESHOOT PROBLEM. SWAPPED REGULATORS FOR PRESS. TRIED MANUALLY PRESS AIRPLANE. NO SUCCESS. RETURNED TO SEA FOR LANDING. UPON BLOCK-IN, COULD NOT TEST EITHER SYS 1 OR 2.Jul 17, 2002 · N448FE · Airbus A310 · Cabin Pressure Control SystemSDR 02FDEA00492Skin · corrodedRT WING LOWER SKIN CORRODED ON LWR SURFACE ON NR 2 PANEL AT AFT EDGE AT RIB 9. STRUCTURAL REPAIR PER E.A. 6-5710-64296.Jul 16, 2002 · N419FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00493Wing · corrodedINBD LT WING UNDER SURFACE TRAILING EDGE AT ZONE 575 FND CORRODED. TEMPORARY REPAIR PER E.A. 6-5710-64295.Jul 16, 2002 · N419FE · Airbus A310 · Wing StructureSDR 02FDEA00478Skin · corrodedRT ELEVATOR TRAILING EDGE LOWER SKIN IS CORRODED 40 CM OUTBD OF INBOARD EDGE. CLEANED CORROSION WITHIN LIMITS IN SRM 55-20-00.Jul 10, 2002 · N446FE · Airbus A310 · Elevator, Plate/SkinSDR 02FDEA00465Seal · leakingNR 1 ENG STARTER DRIVE SHAFT OIL LEAKAGE. REMOVED AND REPLACED SEAL PER AMM 72-65-07-4-A.Jul 9, 2002 · N446FE · Airbus A310 · Turbine Engine Oil System
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