Airbus A310-322
Service difficulty reports · 42
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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 = 'A310322' 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.
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 = 'A310322' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA200903161405Floorbeam · corrodedAREA 100 - PREVIOUS REPAIR AT FLOORBEAM FOUND LOCATED AT FR 63 BTW Y420 AND Y-420. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS REMOVED BECAUSE THE FLOORBEAM WAS REPLACED DUE TO SSDR FDEA200902250721Smoke Warning · false activationJUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP FAULT, BOTH A AND B ON AFT DECK, MAIN DECK CARGO SMOKE ILLUMINATED AND REMAINED ON. JUST PRIOR TSDR FDEA200901080081Frame · corrodedAFT CARGO DOOR CUTOUT FRAME 59A CORROSION AT LOWER END OF DOOR FRAME. PERFORMED REPAIR PER SRM 53-17 FIG 201 AND 202A AND EA NR 6-5320-125509.SDR 08FDEA00563Fitting · crackedLT WING, THREE CRACKS AT CENTRAL FITTING ATTACHMENT TO ACTUATOR AT NUMBER 4 LT SPOILER REPLACED FITTING IN ACCORDANCE WITH EA 6-5750-115315, SB A310-57-2057, IPC 57-73-11-01 AND SRM 57-73-11.SDR 07FDEA04554Stringer Splice · misrepairedAFT PIT STRINGER SPLICE REPAIR AT STRINGER 52L FRAME 60/61 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND THAT STGR COUPLING MATERIAL TYPE AND MATERIAL TEMPER DID NOT CONFORM TO A310 SRM REQUIRESDR 07FDEA04475Floor Support · corrodedFOUND BETWEEN FRAME 67 AND FRAME 64 RBL44 FLOOR SUPPORT STRUCTURE IS CORRODED. 10-22-07 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00; REMOVED AND REPLACED SUPPORT STRAP IAW A310 SRM 53-17-14 ITEM 1 FIG 9, AND 51-40-44 AND 51-40-21.SDR 07FDEA04433Mount · gougedNR 2 PYLON TO ENGINE FWD MOUNT PLATE, AFT INBD HOLE GOUGED. BLENDED AREA IAW A310-200 SRM 54-51-81. HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. CADMIUM PLATED IAW A310-200 SRM 51-21-10. ADHESION TEST PASSED IAW FEDEX A310-200 SRM 51-21-10.SDR 07FDEA04248Spar · failedLEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 4/5 REPAIR STRAP IN WRONG MATERIAL TYPE. REMOVE AND REPLACE AS REQUIRED REMOVED STRAP IAW A310-200 FX SRM 55-11-21. FABRICATED NEW STRAP IAW FX A310-200 SRM 55-11-21 FIG 214 AND PG 285. INSTALLED NEW STSDR 07FDEA04251Spar · damagedLEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 10 AND 11 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP IAW A310-200 SRM 55-11-21 PG 202. FABRICATED NEW STRAP IAW A310-200 SRM 55-11-21 FIG 214 AND PG 285. INSTALLED NEW STRAPSDR 07FDEA03727Strap · crackedAREA IS RT FWD PAX/CREW DOOR CUTOUT, 3 5/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF AFT CORNER STRAP, BEGINNING 1" FROM FWD EDGE OF CORNER STRAP. (LOWER, AFT CORNER OF DOOR CUTOUT BEHIND FAIL/SAFE RING) AREA MARKED IN RED. SEE SDR 07FDEA04012Door Frame · corrodedAFT CARGO COMPARTMENT DOOR FRAME FOUND CORRODED, FR59A, BETWEEN STRG27 RT AND 36 RT. THE AFFECTED FRAME WAS REPAIRED BETWEEN STRG 27-36RT.SDR 07FDEA03716Seat Track · corrodedAFT SEAT TRACK AT Y 1390 WITH CORROSION OUT OF SRM ALLOWABLE VALUES NEXT TO FR68. SEAT TRACK REPAIRED IAW SRM 53-16-10, FIG 202.SDR 07FDEA01880None · nonePREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS207-270 RIB4-5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-8181SDR 07FDEA01890Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 3 WS 1835-1868 RIB 30-31. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM SDR 06FDEA04307Skin · misrepairedPREVIOUS REPAIR, FUSELAGE SKIN RT SIDE HAS EXTERNAL REPAIR DOUBLE BETWEEN FR 54.1 TO 54.2, BETWEEN STR 38 RT TO STR 40 RT, MEASURES 6.3" BY 6.2" PREVIOUSLY INSTALLED REPAIR LOCATED AT RT SIDE FUSELAGE SKIN BETWEEN FRAMES 54.1- 54.2 STRINGERS 38 TO 40 RT DETERMSDR 06FDEA04301Hinge Fitting · corrodedVERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.SDR 06FDEA04300Skin · delaminatedRT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN IAW A310-200 SRM 57-52-12 FIG 204. THE REPAIR IS FOUND TO BE MAJOR IAW FED EX GMM 6-2-100.SDR 06FDEA1864None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 3938-3956, FS 73 AND STR 53-54, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1837None · noneCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR FOUND LOCATED RT FS 1340-1370, FS 18 AND STR 40-41, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATSDR 06FDEA1435Skin · corrodedBELLY OF A/C EXTERIOR SKIN AT FS 82 20 SQ IN OF CORROSION AROUND FASTENER. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND OUT OF LIMITS REPAIRED IAW EA 6- 5330-97550.SDR 06FDEA1434Bulkhead · corrodedREAR PRESSURE BULKHEAD INTERIOR SIDE STRG 27 TO 27 FS 80/82 HAS 6 AREAS OF CORROSION AT APPROX STRG 27R, 33-34R, 43R AND 23L AND 31R ON THE INNER RIM ANGLE. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND ALL AREAS OUT OF LIMITS. REPAIRED IAW EA 6-5330SDR 06FDEA1432Pressure Panel · corrodedFOUND MAIN WHEEL WELL LT SIDE FS 48-54 WEB HAS 50 SQ IN OF CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND 3 SPOTS OUT OF LIMITS. REPAIRED IAW EA 6-5315-98983.SDR 06FDEA1431Skin · corrodedRT A/C BAY BETWEEN FS 43-44 FROM STRG 37 AND BETWEEN STRG 41 TO STRG 51 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS FASTENERS ADJACENT AREAS. REMOVED CORROSION IAW A310-200 SRM FOUND 5 AREAS OUT OF LIMITS. REPAIRED IAW EA 6-5315-98992.SDR 06FDEA1430Stringer · corrodedRT A/C BAY STRG 40 BETWEEN FS 44-47 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS AND ON TOP OF VERTICAL FLANGE REF N00733. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND 1 AREA OUT OF LIMITS, REPAIRED IAW EA 6-5315-98992.SDR 06FDEA1295Skin · corrodedFOUND RIGHT WING T/E LOWER SKIN AT T/E OF NR 2 PYLON HAS 3 AREAS OF EXFOLIATED CORROSION. COMPLIED WITH EA 6-5730-99016 PART 1.SDR 06FDEA1294Access Panel · damagedVERTICAL STAB L/E FRONT SPAR ACCESS PNL ON RT SIDE HAS 2 HOLES DOUBLE DRILLED. COMPLIED WITH EA 6-5530-97607 PART 1.SDR 06FDEA1293Frame · corrodedFOUND NOSE LANDING GEAR WHEEL WELL FWD WALL HAS NUMEROUS SPOTS OF CORROSION ON FR 11. COMPLIED WITH EA 6-5310-97511 PART 1 AND PART 2.SDR 06FDEA1292Skin · corrodedLT A/C BAY BETWEEN FS 39-41 HAS NUMEROUS SPOTS OF CORROSION ON SKIN FS STRG 37- 47. REMOVED CORROSION IAW A310-200 SRM 51-74-10, ALL AREAS WITHIN LIMITS IAW A310-200 SRM 53-15-12. ALODINED PRIMED AND TOP COATED ALL AREAS IAW A310-200 SRM 51-75-10.SDR 06FDEA1291Skin · corrodedFWD OF LT AIR COND CUT OUT EXTERNAL DOUBLER HAS NUMEROUS SPOTS OF CORROSION ON SKIN AND AROUND FASTENERS. REMOVED CORROSION IAW A310-200SRM 51-74-10 ALL AREAS FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-15-12 PROTECTED ALL AREAS IAW A310-200 SRM 51-75-10.SDR 06FDEA1290Structure · damagedFOUND VERTICAL LEADING EDGE RIGHT SIDE ATTACH LANDING HAS ELONGATED FASTENER HOLE AT APPROXIMATELY RIB 14. COMPLIED WITH EA 6-5530-97607 PART 1.SDR 06FDEA1289Repair · unknownREPAIR LOC, ON LT O/B FLAP UPPER SURFACE 48 INCH FROM I/B END REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5750-97513 PART 1.SDR 06FDEA1288Floor Support · crackedFOUND BULK CARGO BAY LEFT SIDE FLOOR SUPPORT BETWEEN FS 65 AND 66 IS CRACKED. REMOVED AND REPLACED SUPPORT SECTION IAW A310-200 SRM 51-72-10.SDR 06FDEA1287Repair · unknownREPAIR LOC, ON R1 DOOR UPPER EDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5210-97507.SDR 06FDEA1286Repair · unknownREPAIR LOC, AT FS 87 STRG 34R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5330-97506 PART 1.SDR 06FDEA1285Floorbeam · corrodedBULK CARGO FLOOR STRUCTURE BEAM AT FR. 66 CENTER TOP BEAM HAS EXFOLIATED CORROSION MEASURING 2 INCH BY 3 IN. REMOVED AND REPLACED FLOORBEAM IAW A310-200 SRM 51-72-10SDR 06FDEA1284Repair · unknownREPAIR LOC, LT HORIZ STAB REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED IAW EA 6-5510-97564 DUE TO EXISTING REPAIR MATERIAL NOT PER A310-200 55-12-12.SDR 06FDEA1283Skin · corrodedRT A/C BAY BETWEEN FS 45-46 BETWEEN STRG 37- 45 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS FASTENERS AND SIDE OF 3 ANGLE WEB. REMOVED CORROSION IAW A310-200 SRM 51-74-10 MATERIAL LOSS WITHIN LIMITS EXCEPT 1. PICKUP ANGLE IAW A310-200 SRM 310-200 5SDR 06FDEA1282Skin · corrodedBELLY OF A/C EXTERIOR SKIN FROM FS 86 TO 90 HAS 25 SQ IN OF CORROSION AROUND FASTENERS. REMOVED CORROSION IAW A310-200 SRM 51-74-10 MATERIAL WITHIN LIMITS IAW A310-200 SRM 1. AREA OUT OF LIMITS IAW SRM A310-200 53-10-00 NOTED AS NR 1 STEP 5 OF JPF. REPAIRSDR 06FDEA1268Unknown · warning messageDURING CLIMB-OUT FROM PEN MID2 'A' FAULT ILLUMINATED, FOLLOWED SHORTLY BY MID1 CARGO SMOKE LOOP FAULT. PERFORMED ECAM AND QRH PROCEDURES NO HELP. ECAM ADVISORY FOR NR 1 BLEED TEMP HIGH BEGAN FLASHING WITH TEMPERATURE CYCLING ERRATICALLY. CARGO SMOKE LIGHTSDR 04FDEA03448Display · intermittentREJECTED TAKEOFF IND DUE TO F/O PFD & ND BLANKING AT ABOUT 95 KTS. DISPLAYS RETURNED BY THE TIME THE A/C STARTED SLOWING. BACK TO RAMP TO ALLOW BRAKES TEMPS TO COOL NO OTHER PROBLEM DEVELOPED WITH PFD/ND APPEARED NORMAL. SECOND TAKEOFF NORMAL. MALFUNCTION SDR 20000911SH009Structure · corrodedWHILE C/W A DETAILED VISUAL INSPECTION OF THE LEFT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSION REMOVAL, THE SPIGOT BALL JOINT HOLE EXCEEDED THE ALLOWABLE LIMITS SPECIFIED IN SB A310-54-2019. SDR 20000911SH008Structure · corrodedWHILE C/W A DETAILED VISUAL INSPECTION OF THE RIGHT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSION REMOVAL, THE SPIGOT BALL JOINT HOLE EXCEEDED THE ALLOWABLE LIMITS AS SPECIFIED IN SB A310-54-201
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