Airbus A310-304

Service difficulty reports · 238

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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 = 'A310304'
  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 07FDEA01110Bulkhead · gougedSOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049380/2007 ISS. AMar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, BulkheadSDR 07FDEA01103Skin Panel · gougedTWO MISDRILLED HOLES THROUGH THE SKIN PANEL, INTERNAL DOUBLER, C17 FLANGE AND CONNECTING FITTINGS AT P44 LT. REPAIR PERFORMED BY REPLACING CONNECTING FITTINGS P44 BY NEW ONES; INSTALLING STEEL REPAIR BUSHES IN SKIN PANEL, INTERNAL DOUBLER C17 FLANGE AND C17 FMar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA01053Frame · crackedDEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6-5710-106423 AND RAS/049817/013/2007 ISSUE "A".Mar 21, 2007 · N816FD · Airbus A310304 · Wing SparSDR 07FDEA01052Mount · chafedOLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANGLE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441.Mar 21, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01050Fitting · damagedMISDRILLED HOLES IN C17 AT P44 LT. REPAIR WAS PERFORMED BY BUSHING REPAIR AND NEW FITTING INSTALLATION (P/N A536-10607-206-93, A536- 10607-207-93) IAW EA 6-5312-106418 AND RAS/AS/006/2007 ISSUE "A".Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Attach FittingsSDR 07FDEA01036Skin · scratchedOLD SCRATCH REPAIR ON EXTERNAL SKIN BETWEEN C75/76, P27. REPAIR VERIFICATION, PERFORMED IAW SRM 53-18-12/FIG 102 EA FOR TRACKING: 6-5318-106413.Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00990Skin · chafedCHAFE MARKS ON C38.1, P14-15 LT SIDE. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-106417 AND RAS/DATLS/0003560/2007 ISS. BMar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00989Skin · damagedDOUBLE HOLE ON FUSELAGE SKIN AT C67, P35 RHS REPAIR WAS PERFORMED BY BUSH REPAIR IAW SRM 51-40-51, APPROVED BY EA 6-53176-106410 AND RAS/DAHAM/4021719/2007 ISS. AMar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00987Vane · damagedCHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED.Mar 19, 2007 · N816FD · Airbus A310304 · Trailing Edge FlapsSDR 07FDEA00955Attach Fitting · damagedV/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.)Mar 16, 2007 · N816FD · Airbus A310304 · Vertical StabilizerSDR 07FDEA00954Floor Support · corrodedCORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT, CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00. PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR 07FDEA00953Floor Support · corrodedFOUND CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT (CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00). PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR 07FDEA00952Crossbeam · corrodedFOUND CORRODED CROSSBEAM AT C67, Y-1070-1115. PART REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, StructureSDR 07FDEA00951Beam · damagedTWO LONGITUDINAL BEAMS BETWEEN C64-65, -Y 525 AND Y 805 WITH WRONG EXISTING HOLES. PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, StructureSDR 07FDEA00948Stiffener · damagedRT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER.Mar 16, 2007 · N816FD · Airbus A310304 · Wing Miscellaneous StructureSDR 07FDEA00947Skin · crackedRT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R572-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED).Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Plate/SkinSDR 07FDEA00946Rib · chafedKRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT.Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Rib/BulkheadSDR 07FDEA00945Web · chafedCHAFING MARK AT BACK WALL OF KRUEGER FLAP CHAMBER. REPAIR WAS PERFORMED BY BLEND OUT AND REPROTECT.Mar 16, 2007 · N816FD · Airbus A310304 · Leading Edge DevicesSDR 07FDEA00944Attach Fitting · chafedPYLON NR 2, CHAFING MARKS ON INBOARD SIDE OF PYLON-TO-ENGINE ATTACH FITTING. REPAIR WAS PERFORMED BY BLEND OUT AND RESTORE PROTECTION.Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Nacelle/Pylon Attach FittingsSDR 07FDEA00938Longeron · bentAPU ACCESS DOOR LT/RT LOWER LONGERON, OLD BENT REPAIR. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLATION OF NEW LONGERON SECTION.Mar 16, 2007 · N816FD · Airbus A310304 · APU Cowling/ContainmentSDR 07FDEA00936Floorbeam · corrodedAFT CARGO COMP FLOORBEAM AT C63 LT, Y 445 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207 BY LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Floor BeamSDR 07FDEA00933Stringer · chafedOLD CHAFING MARKS BETWEEN C44-45, P45 LT. REPAIR PERFORMED BY BLEND OUT IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Longeron/StringerSDR 07FDEA00932Skin · dentedOLD DENT REPAIR ON BULK CARGO DOOR OUTER SKIN BETWEEN BEAM 1-2 AND BEAM 4-5. REPAIR WAS PERFORMED BY INSTALLING EXTERNAL DOUBLER BETWEEN BEAM 4-5 AND BLEND OUT BETWEEN BEAM 1-2 IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage DoorsSDR 07FDEA00931Skin · chafedTWO OLD NICK/CHAFING MARKS AT THE INTERNAL SKIN OF FWD CARGO DOOR C20A-25A, LONGERON 4-5. REPAIR WAS PERFORMED BY INSTALLING A DOUBLER IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage DoorsSDR 07FDEA00930Shaft · chafedOLD CHAFING MARK ON PAX DOOR NR 1 RT AT LOCKING CONTROL SHAFT. REPAIR WAS PERFORMED BY BLEND OUT IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Passenger/Crew DoorsSDR 07FDEA00929Skin · delaminatedOLD REPAIR ON LT MLG DOOR, DELAMINATED SKIN. REPAIR WAS PERFORMED BY FILL OUT THE DELAMINATED AREA IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Landing Gear DoorsSDR 07FDEA00928Door Frame · damagedOLD MARKS ON FWD CARGO DOOR FRAME FWD LOWER CORNER. REPAIR WAS PERFORMED BY BLEND OUT WITH LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, StructureSDR 07FDEA00927Stringer · corrodedFOUND CORRODED STRINGER P52 AND P53, C65-66. REPAIR WAS PERFORMED IAW SRM 53-10-14.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Longeron/StringerSDR 07FDEA00851Skin · damagedELONGATED HOLES IN LT BOTTOM WING SKIN AT PYLON SUPPORT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5720-106422, DRAWING R572-49184 AND RAS/BAE/1004144/2007 ISSUE "A".Mar 15, 2007 · N816FD · Airbus A310304 · Wing, Plate/SkinSDR 07FDEA00850Hinge · misinstalledRT MLG FITTING BUSH, WRONG INSTALLATION. REPAIR WAS PERFORMED IAW EA 6-5281-106381 AND RAS/CASA/5328/2007 ISSUE "A" AND RAS/AS/228/95 ISSUE "A".Mar 15, 2007 · N816FD · Airbus A310304 · Fuselage, Door HingeSDR 07FDEA00151Slide · lowR1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25-61-22-4-01 AND A310 - 300 AMM 52-10-00-3.Jan 22, 2007 · N817FD · Airbus A310304 · Escape SlideSDR CA061121001Engine · failed(CAN) AFTER TAKE OFF AND DURING LEVEL AT 40,000 FT CREW GOT ECAM MESSAGE MIN EQUIPMENT SMOKE WITH OVERHEAD WITH OVERHEAD LIGHT ON AND ODOR IN THE CABIN AND COCKPIT. CREW DECIDED TO RETURN BACK TO THE AIRPORT. QRH PROCEDURES WERE FOLLOWED. BOROSCOPE CARRIED OUNov 19, 2006 · Airbus A310304 · Engine (Turbine/Turboprop)SDR CA061114006A/C Pack · odor(CAN) IN CLIMB OUT ECAM WARNING MIN EQUIPMENT BAY SMOKE CAME ON WITH BURNING ODOR AND A SMALL AMOUNT OF SMOKE IN THE FLIGHT DECK AND FWD CABIN. AIRCRAFT RETURNED TO THE STATION. MAINTENANCE INSPECTED THE MIN EQUIPMENT COMPARTMENT (NO FINDING). DURING ECS COMPANov 12, 2006 · Airbus A310304 · Cabin Cooling SystemSDR CA061114003Shutoff Valve · leaking(CAN) DURING TAKE OFF AT APPROXIMATELY 100 KNOTS NR 1 ENGINE THRUST REVERSER UNLOCKED LIGHT ILLUMINATED ACCOMPANIED WITH EAM MESSAGE NR 1 ENG REV UNLOCK¿. THE FLIGHT CREW REJECTED THE TAKE OFF ROLL, CYCLED THE REVERSER WITH NO FAULTS. CREW THEN ELECTED TO RETUNov 7, 2006 · Airbus A310304 · Engine Thrust ReverserSDR 06FDEA03799Smoke Detector · malfunctionedON TAKEOFF, AT 1000FT AVIONICS SMOKE INDICATION COMPLIED W/QRA. NO OBSERVED SMOKE NOTED FROM SNIFFER FAN. RETURNED TO MEMPHIS. SMOKE WARNING DID GO OUT AFTER APPROX 7 MINUTES. WAS NOT OVERWEIGHT ON LANDING. PERFORMED TEST REF 26-15-00. TESTED GOOD. FOUNOct 27, 2006 · N803FD · Airbus A310304 · Smoke DetectionSDR 06FDEA03588Fitting · corrodedCOMPLY WITH AGING 9-AGING-INSP, FOUND CORROSION AND WEAR LOCATED IN RT FITTING BETWEEN FS 16A/ FS 17 IN HOLE AT ATTACHMENT FITTING OF AFT DOOR.Oct 4, 2006 · N817FD · Airbus A310304 · Fuselage Main, Attach FittingsSDR 06FDEA03400Skin · damagedRT MLG-STRUT DOOR W/SKIN SURFACE DAMAGED AND REPAIR AT LOWER AREA THE STRUT DOOR WAS REPAIRED PER FEDEX EA 6-5280-99721 EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".Sep 22, 2006 · N817FD · Airbus A310304 · Landing Gear DoorsSDR CA060906006Warning System · multiple ind(CAN) AT 50 KNOTS, FLIGHT CREW REJECTED TAKE OFF DUE TO NAV ADC, GPS DISAGREE WARNING. DURING TAXI TO THE GATE, FAULT CLEARED IT`S SELF. FMS WAS RESET IAW MM, GPS, IRS AND FM POSITIONAL FOUND MATCHING. AUTO FLIGHT SYSTEMS TESTED AND FOUND SERVICEABLE. AIRCRAFTSep 3, 2006 · Airbus A310304 · Central WarningSDR 06FDEA03054Skin · damagedFOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO ANAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03053Skin · damagedFOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTBD LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR W/W DOOR PER SRM 52-81-12. REPAIR EVALUATED PER GMM Aug 22, 2006 · N817FD · Airbus A310304 · Landing Gear DoorsSDR 06FDEA03052Skin · damagedFOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-2Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/SkinSDR 06FDEA03051Skin · damagedFOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-21-12 FIG 204. Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/SkinSDR 06FDEA03050Skin · damagedFOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR, DISCREPANCY REPORT 43000001-391Aug 22, 2006 · N817FD · Airbus A310304 · Leading Edge DevicesSDR 06FDEA03049Skin · damagedFOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS REF : RAS /DA/BRE/1642/97, REPAIR EVALUATEAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03048Skin · damagedFOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03047Skin · damagedFOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03046Skin · damagedFOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03045Structure · unknownFOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OUTB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THIS REPAIR WAS REMOVED AND REPLACED A NEW TRAILING EDGE PAug 22, 2006 · N817FD · Airbus A310304 · Wing Miscellaneous StructureSDR 06FDEA03044Door · misrepairedFOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA, REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03043Door · misrepairedFOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN EXISTING SRM REPAIR . NEW REPAIR ACCOMPLISHEDAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
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