# Service difficulty reports: Airbus A310-203 A list on [Airbus A310-203](https://openairdocs.org/model/airbus-a310-203.md). Newest first. General aviation reporting is voluntary. Page 1 of 48 · 2,392 reports - [SDR FDEA201511093525](https://openairdocs.org/sdr/FDEA201511093525.md): Battery · inoperative · Nov 9, 2015 · N426FE · Airbus A310203 · Door Warning System > DURING SERVICE CHECK, FOUND ASPSU FAULTED NR 2 BATTERY REASON CODE. R & R NR 2 BATTERY ON ASPSU IAW AMM 52-73-18-04. PERFORMED BITE TEST IAW AMM 52-73-00-05, SYS CHECKED GOOD. EMER POWER SUPPLY BATTERY PN AD-3214-30 & SN 42169. - [SDR FDEA201510293405](https://openairdocs.org/sdr/FDEA201510293405.md): Gearbox · lack of lube · Oct 29, 2015 · N429FE · Airbus A310203 · Trailing Edge Flap Control System > SELECTED FLAPS 15 DEGREES AT 200 KTS. FLAPS SYS 1 & 2 FAULT LIGHTS & ON ECAM. CYCLED HANDLE WITH SAME RESULT. FOLLOWED ECAM & QRH. LANDED SLATS 30, FLAPS 0 UNEVENTFULLY & CANCELLED EMERGENCY. LUBED & SERVICED RT ANGLE GEARBOX, TORGUE LIMITER & NR 1 GEARBO - [SDR FDEA201509042800](https://openairdocs.org/sdr/FDEA201509042800.md): Sensor · failed · Sep 4, 2015 · N429FE · Airbus A310203 · Auto Throttle System > AUTO THROTTLES OFF, SET N1 TO 107% ON BOTH ENGS. THERE WAS SIGNIFICANT THRUST DIFFERENCE CAUSING YAW ON CLIMB OUT. WE GOT ECAM ENG EXCEEDENCE WARNING & REDUCED POWER. NOTICED N1 ANALOG & DIGITAL INDICATIONS DISAGREED SIGNIFICANTLY. ON ATB MANUAL THROTTLES - [SDR FDEA201507202272](https://openairdocs.org/sdr/FDEA201507202272.md): Angle · corroded · Jul 20, 2015 · N443FE · Airbus A310203 · Passenger/Crew Doors > AFT UPPER CORNER OF L1 ENTRY DOOR CORNER ANGLE CORRODED. FABRICATED IAW EA 6-5210-T0318924 AND INSTALLED IAW SRM 51-40-20. - [SDR FDEA201506031688](https://openairdocs.org/sdr/FDEA201506031688.md): Unknown · malfunctioned · Jun 3, 2015 · N427FE · Airbus A310203 · Cabin Pressure Control System > LOST CABIN AT APPROX 18 - 210 FL, THE MAN PRESS VLV SHOWED OPEN & TRIED MANUAL CONTROL & IT DID NOT FIX PROBLEMS. NEITHER PRESSURIZATION SYS FAULTED. TROUBLESHOOTING ON THE PRESSURIZATION SYS IN PROGRESS. - [SDR FDEA201504141230](https://openairdocs.org/sdr/FDEA201504141230.md): Nut · lack of lube · Apr 14, 2015 · N427FE · Airbus A310203 · Trailing Edge Flap Control System > ON APPROACH, WHEN CONFIG FROM SLATS 15 TO FLAPS 15, RECEIVED FLAPS SYS 1 & SYS 2 FAULT. RECYCLED HANDLE TO SLATS 15 IAW PHASE ONES THEN RE-ATTEMPTED FLAPS 15, SAME RESULT FLAPS SYS 1 & SYS 2 FAULT. REVIEWED QRH, ELECTED TO DIVERT, ON APPROACH, CONFIGURED WHE - [SDR FDEA201503271107](https://openairdocs.org/sdr/FDEA201503271107.md): Control Unit · faulty · Mar 27, 2015 · N410FE · Airbus A310203 · Landing Gear Brake System > AUTO BRAKE FAIL LIGHT ILLUMINATED LATE ON TAKEOFF ROLL. IN ADDITION TO AUTO BRAKE FAIL LIGHT, ALL TRIPLE BAR LIGHTS ON MAX, MED & LOW, NO RELATED ECAM WARNING TILL LATER. WAS UNABLE TO PERFORM BITE TEST OF BSCU. BSCU BITE LIGHT & TEST SCREEN CONTINUALLY CYC - [SDR FDEA201502240588](https://openairdocs.org/sdr/FDEA201502240588.md): Valve · unknown · Feb 24, 2015 · N430FE · Airbus A310203 · Standard Practices/Structures > IAW MOCC REQUEST NEED TO R & R DEPRESSURIZATION VLV 93 HM. PART ON ORDER. R & R DEPRESSURIZATION VLV 93 HM IAW 21-31-15-04-01. - [SDR FDEA201410042967](https://openairdocs.org/sdr/FDEA201410042967.md): Warning Light · false activation · Oct 4, 2014 · N423FE · Airbus A310203 · Landing Gear Position and Warning > AFTER TAKEOFF WITH LANDING GEAR RETRACTION, NOSE GEAR DOOR INDICATED UNSAFE, AMBER ON BOTH INDICATORS. FELT FLUTTER INDICATING DOOR WAS IN FACT STILL OPEN. AIR TURN BACK. WORK INSPECTING NOSE GEAR DOOR OPERATION & GENERAL NOSE GEAR AREA. NO OBVIOUS FAULTS - [SDR FDEA201404260861](https://openairdocs.org/sdr/FDEA201404260861.md): Pressure Switch · malfunctioned · Apr 26, 2014 · N429FE · Airbus A310203 · Trailing Edge Flap Control System > ON APPROACH WHEN WE SELECTED, SLATS EXT, GOT ECAM SLATS SYS NR 1 & NR 2 FAULT. CYCLED & SLATS EXTENDED, WHEN SELECTING FLAPS 15, GOT FLAP SYS NR 1 & NR 2 FAULT. CYCLED WITH NO HELP. LANDED WITH 0 FLAPS. CYCLED FLAPS SEVERAL TIMES WITH NO HELP. TROUBLESHO - [SDR FDEA201402240394](https://openairdocs.org/sdr/FDEA201402240394.md): Coalescer Bag · dirty · Feb 24, 2014 · N403FE · Airbus A310203 · Humidity Control System > AS TAKEOFF POWER WAS APPLIED ACRID SMELL DETECTED BY FIRST OFFICER THEN CAPTAIN, NOT VISIBLE, LOW SPEED REJECT AT 50 - 60 KTS. SHUTDOWN ON RWY & TUGGED TO GATE. SMELL WENT AWAY WITHIN MINUTES OF REJECT. NO HEAT DETECTED BY CRASH CREW. NO CB IN FLIGHT DECK - [SDR FDEA201312283062](https://openairdocs.org/sdr/FDEA201312283062.md): Wire · broken · Dec 28, 2013 · N410FE · Airbus A310203 · Equipment/Furnishings Wiring > R1 DOOR SLIDE ARMING LIGHT ASSEMBLY HAS BROKEN WIRES. TERMINATED WIRES TO 8WN FWD RT DOOR ESCAPE SLIDE WARNING LIGHT ASSEMBLY IAW A310-200 AWM 52-73-01. TESTED GOOD IAW A310-200 AMM 52-73-11-04. - [SDR FDEA201312132980](https://openairdocs.org/sdr/FDEA201312132980.md): Valve · failed · Dec 13, 2013 · N427FE · Airbus A310203 · Pressure Regulator/Outflow Valve > ON DEPARTURE, CLIMBING THROUGH 10,000' CABIN ADVISORY HIGH RATE, THEN EXCESS CABIN ALTITUDE COMPLIED WITH ECAM & QRH. ACFT WOULD NOT PRESSURIZE. RETURNED TO A/P. PRESS PAGE SHOES MAN PRESS DOOR OPEN. TRIED REG 1 & 2, MANUAL PRESSURIZATION TO NO AVAIL. PER - [SDR FDEA201312102960](https://openairdocs.org/sdr/FDEA201312102960.md): Control Unit · faulty · Dec 10, 2013 · N410FE · Airbus A310203 · VHF Communications System > COMPLETE LOSS OF COMM ON VHF 1, 2 & 3 AT 1:15 INTO 2 HR FLIGHT. WE CHECKED QRH, NO HELP. CHECK 02 MASK DOORS & RESET. UNPLUGGED & PLUGGED IN AUXILIARY HEADSETS. TRIED COMM WITH CTR USING MASKS, AUXILIARY, NO HELP. RESET VHF 1, 2 & 3 BREAKERS & AFTER 12 - - [SDR FDEA201311282888](https://openairdocs.org/sdr/FDEA201311282888.md): Unknown · abnormal · Nov 28, 2013 · N436FE · Airbus A310203 · Auto Throttle System > WHEN TAKEOFF THRUST APPLIED & TOGA SELECTED ATS LEVER TRIPPED OFF. LOW SPEED REJECT ACCOMPLISHED ECAM ATTEMPTED NO HELP. REMOVED AND REPLACED THRUST CONTROL COMPUTER PRECAUTIONARY PER A310-200 M/M REF 22-35-34 -04-01. PERFORMED SUCCESSFUL AFS/LAND TEST PE - [SDR FDEA201311102720](https://openairdocs.org/sdr/FDEA201311102720.md): Tee Fitting · cracked · Nov 10, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > CENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING RT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521. - [SDR FDEA201311102719](https://openairdocs.org/sdr/FDEA201311102719.md): Tee Fitting · cracked · Nov 10, 2013 · N429FE · Airbus A310203 · Fuselage Main, Frame > CENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING LEFT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521. - [SDR FDEA201311052688](https://openairdocs.org/sdr/FDEA201311052688.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FRAME 40 RT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-0303103. - [SDR FDEA201311052687](https://openairdocs.org/sdr/FDEA201311052687.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FRAME 40 LT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-T0303103. - [SDR FDEA201311052686](https://openairdocs.org/sdr/FDEA201311052686.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FUSELAGE CENTER BOX FRAME 45 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124. - [SDR FDEA201311052685](https://openairdocs.org/sdr/FDEA201311052685.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FUSELAGE CENTER BOX FRAME 44 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKS AT H5 & H13. R & R THE SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311052684](https://openairdocs.org/sdr/FDEA201311052684.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FUSELAGE CENTER BOX FRAME 43 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H2. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311052683](https://openairdocs.org/sdr/FDEA201311052683.md): Fitting · cracked · Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FUSELAGE CENTER BOX FRAME 45, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124. - [SDR FDEA201311042676](https://openairdocs.org/sdr/FDEA201311042676.md): Fitting · cracked · Nov 4, 2013 · N429FE · Airbus A310203 · Fuselage Main, Structure > FUSELAGE CENTER BOX FRAME 43, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKED. R & R SUPPORT FITTING SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311042677](https://openairdocs.org/sdr/FDEA201311042677.md): Support Fitting · cracked · Nov 4, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach Fittings > FUSELAGE CENTER BOX, FRAME 44 LT UPPER FRAME SUPPORT FITTING FOUND CRACKED. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201310312659](https://openairdocs.org/sdr/FDEA201310312659.md): Skin · cracked · Oct 31, 2013 · N429FE · Airbus A310203 · Fuselage Main, Plate/Skin > FUSELAGE SKIN UNDER PICKUP ANGLE AT FRAME 40 LT, FASTER HOLE 14 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0303309. - [SDR FDEA201310202557](https://openairdocs.org/sdr/FDEA201310202557.md): Seat Track · corroded · Oct 20, 2013 · N429FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK FRAMES 47-48 -Y953, SEAT TRACK CORRODED. SPLICE REPAIRED SEAT TRACK IAW EA 6-5315-T0303255 & SRM 53-10-16. - [SDR FDEA201310182549](https://openairdocs.org/sdr/FDEA201310182549.md): Floor Support · corroded · Oct 18, 2013 · N429FE · Airbus A310203 · Fuselage Miscellaneous Structure > MAIN DECK FR 12A-14 Y770, FLOOR SUPPORT CORRODED REPLACED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21. - [SDR FDEA201310072434](https://openairdocs.org/sdr/FDEA201310072434.md): Engine · failed · Oct 7, 2013 · N426FE · Airbus A310203 · Engine (Turbine/Turboprop) > DURING CLIMBOUT, NR 1 ENGINE OVERTEMPED. HEARD A LOUD POP WITH A YAW TO THE LEFT. ALL ENG INDICATIONS WERE NORMAL EXCEPT EGT WHICH WAS 700 DEGREES HIGHER THEN NR 2 EGT, NR 1 EGT STAYED BEWTEEN 600 TO 700 DEGREES. DURING RETURN, MAX EGT 1000 FT. REMOVED AND - [SDR FDEA201309282335](https://openairdocs.org/sdr/FDEA201309282335.md): Engine · power loss · Sep 28, 2013 · N410FE · Airbus A310203 · Engine Controls > THROTTLE KNOBS STAYED WITH A HALF A KNOB. ON TAXI OUT ENG 1 LAGGED ENG NR 2 N1 UP TO 30 PERCENT ACCELARATION. FOR TAKEOFF, TRIED TO SET 40 PERCENT N1 AND ENG NR 1 N1 LAGGED ENG 2 N1 BY INITALLY 10 TO 20 PERCENT. WHEN TO GAD FOR TAKEOFF THE N 1 INITIALLY W - [SDR FDEA201309212274](https://openairdocs.org/sdr/FDEA201309212274.md): Jackscrew · worn · Sep 21, 2013 · N423FE · Airbus A310203 · Leading Edge Slat Control System > ON APPLICATION OF SLATS 1 & 2, FAULT LIGHT CAME ON. SLATS LESS THAN 15- CYCLED HANDLE & NO CHANGE. RAN CHECKLIST & MADE NO SLAT LANDING. AFTER LANDING TRIED SLATS AGAIN AND THEY CAME DOWN. PERFORMED BITE TEST ON NR 1 & 2 SFCC IAW FIM 27-80-01/101. ALL IN - [SDR FDEA201309042115](https://openairdocs.org/sdr/FDEA201309042115.md): Selector Valve · failed · Sep 4, 2013 · N435FE · Airbus A310203 · Landing Gear Retraction/Extension System > ON LANDING, NOSE TILLER COULD NOT BE MOVED. DIFFERENTIAL BRAKING USED TO CLEAR RWY. TROUBLESHOT IAW TSM 32-51-00 FIG 103 TO STEP 4. NOSE GEAR DOORS WILL NOT RAISE. SUSPECT LANDING GEAR SELECTOR VALVE. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-3 - [SDR FDEA201308242031](https://openairdocs.org/sdr/FDEA201308242031.md): Window · cracked · Aug 24, 2013 · N427FE · Airbus A310203 · Flight Compartment Windows > CAPTAIN'S FRONT FIXED WINDOW CRACKED AT FL 390. INSTALLED SERVICEABLE WINDSHIELD TO STEP 1.E.17, REF MM 56-11-11-04. WINDOW IS INSTALLED SEALED & TORQUED. - [SDR FDEA201308201962](https://openairdocs.org/sdr/FDEA201308201962.md): Fitting · cracked · Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach Fittings > FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826. - [SDR FDEA201308201961](https://openairdocs.org/sdr/FDEA201308201961.md): Fitting · cracked · Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach Fittings > FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826. - [SDR FDEA201308171919](https://openairdocs.org/sdr/FDEA201308171919.md): Spar · damaged · Aug 17, 2013 · N426FE · Airbus A310203 · Nacelle/Pylon, Main Frame > RT PYLON LWR SPAR BETWEEN RIBS 6 AND 7. REPAIRED IAW EA 6-5450-117917C, PART 2. COMPLIED WITH EA 6-5450-117917C PART2. REMOVED AND INSTALLED THE REPAIR DOUBLER FOR NDT INSPECTION. - [SDR FDEA201308171918](https://openairdocs.org/sdr/FDEA201308171918.md): Skin · corroded · Aug 17, 2013 · N426FE · Airbus A310203 · Fuselage Main, Plate/Skin > LT WING ROOT CENTER WING BOX BOTTOM SKIN LWR SURFACE FOUND CORRODED BETWEEN FR44-45. REMOVED CORROSION IAW SRM 51-74-10. REPAIRED EA 6-5710-T0301458. - [SDR FDEA201308161913](https://openairdocs.org/sdr/FDEA201308161913.md): Frame · cracked · Aug 16, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > FUSELAGE FRAME 40, UPPER CORNER FOUND CRACK IN RT NR 2 HOLE COMPLIED WITH EA 6-5710-T0301577. - [SDR FDEA201308131861](https://openairdocs.org/sdr/FDEA201308131861.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > RIGHT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131860](https://openairdocs.org/sdr/FDEA201308131860.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > RT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5330-T0301676. - [SDR FDEA201308131859](https://openairdocs.org/sdr/FDEA201308131859.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > RT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131858](https://openairdocs.org/sdr/FDEA201308131858.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > LEFT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131857](https://openairdocs.org/sdr/FDEA201308131857.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame > LEFT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131856](https://openairdocs.org/sdr/FDEA201308131856.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Structure > LEFT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308101829](https://openairdocs.org/sdr/FDEA201308101829.md): Engine · failed · Aug 10, 2013 · N428FE · Airbus A310203 · Turbine Engine Oil System > DURING CLIMB ENG NR 1 OIL LOW QTY ADVISORY CAME ON, SHOWED 2 QUARTS. ALL OTHER INDICATIONS NORMAL. IAW QRH, MONITORED QTY. ABOUT 15 MINUTES LATER, DECIDED TO DIVERT WITH POSSIBLE OIL PRESSURE FLUCTUATION. DID NOT SHUT NR 1 DOWN, PRESSURE STAYED ABOVE 40 P - [SDR FDEA201308091817](https://openairdocs.org/sdr/FDEA201308091817.md): Skin · delaminated · Aug 9, 2013 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin > LEFT FWD FUSELAGE TOILET SERVICE PANEL LOWER SKIN CUTOUT DELAMINATED. REPAIRED IAW EA 6-5330-T0301676. - [SDR FDEA201308061782](https://openairdocs.org/sdr/FDEA201308061782.md): Sill · corroded · Aug 6, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous Structure > BULK CARGO DOOR SILL FOUND CORROSION SURROUNDING FASTENER HOLES BETWEEN FR 68 & 69. REPLACED SILL IAW SRM 51-40-21. - [SDR FDEA201307261665](https://openairdocs.org/sdr/FDEA201307261665.md): Floor Support · corroded · Jul 26, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous Structure > MAIN DECK FR 14-14B, Y730, FLOOR SUPPORT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207. - [SDR FDEA201307261666](https://openairdocs.org/sdr/FDEA201307261666.md): Floor Support · corroded · Jul 26, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous Structure > MAIN DECK FR 12A-15A Y1456 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207. - [SDR FDEA201306181339](https://openairdocs.org/sdr/FDEA201306181339.md): Seal · leaking · Jun 18, 2013 · N423FE · Airbus A310203 · Pneumatic Distribution System > AFTER TAKE OFF, BLEED LEAK RT SIDE. REF QRH- LIGHT OUT IN FLIGHT. ON APPROACH LOWER ACCESS DOOR LIGHT CAME ON. FOUND LEAK TO BE COMING FROM THE UPPER RT CORNER OF PACK BAY BLEED SUPPLY LINE. REMOVED RT ENG BLEED DUCT SECTION IN FWD A/C BAY IAW MM 36-11-0 Next page: https://openairdocs.org/model/airbus-a310-203/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'A310203' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/airbus-a310-203/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.