Airbus A310-324
Service difficulty reports · 1,439
Newest first. General aviation reporting is voluntary.
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 = 'A310324' 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 = 'A310324' 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 07FDEA04110Skin Panel · failedFOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AFT OF FRAME 78 BETWEEN STRG 1LH - 1RH, NOT CONFORM TO SRM. OLD REPAIR REMOVED AND RENEWED IAW SRM 53-10-12/FIG 226.SDR 07FDEA04107Skin Panel · corrodedCORROSION ON UPPER SIDE (FRAME 14, STRG 11) ) OF THE FWD RT PAX DOOR FAIL/SAFE RING. REPAIR PERFORMED BY SMOOTH REWORK, HFEC/ROTOTEST INSPECTION AND OVERSIZING HOLES IN CORRODED AREA IAW EA 6-5312-82879 AND RAS/AS/151/2005 ISSUE A.SDR 07FDEA04105Skin Panel · corrodedCORROSION ON FWD DOOR FRAME PANEL, RT FWD PAX DOOR, BETWEEN FRAME 13-14C, STRG 9-14, SOME AREAS OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH REWORK AND HFEC/ROTOTEST INSPECTION IAW EA 6-5312-82923 AND RAS 037817/008/2005 ISSUE A.SDR 07FDEA04102Skin · chafedCHAFING MARK ON INBOARD FLAP VANE LT, CAUSED BY NOT INSTALLED PROTECTIVE PLATE AT VANE-NOSE-SKIN FOR JAM RETRACTED MICROSWITCH STRIKER, RIB 2-22. REPAIR PERFORMED BY SMOOTH BLEND OUT CHAFING MARK IAW EA 6-5752-82885 AND RAS/DABRE/7005373/2005 ISSUE B AND INSTSDR 07FDEA04100Fitting · crackedCRACKED FITTING BETWEEN STRG 45-47 RT AT FRAME 67, CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF FITTING IAW SRM 51-72-10.SDR 07FDEA04099Skin · chafedFOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK NR 5 AND 6 LT WING. REPLACEMENT OF DAMAGED NOSE SKIN IAW SRM 51-72-10.SDR 07FDEA04096Fitting · unknownOLD REPAIR, FRAME 17, STR 44 LT WITH NO OLD RECORDS FOR RUN OUT FITTING REPLACEMENT OR PERMANENT REPAIR. STRUCTURE REPAIR PERFORMED IAW INSTRUCTION R536-10440 ISSUE C.SDR 07FDEA04093Skin Panel · corrodedCORROSION ON FAIL/SAFE RING, LT FWD PAX DOOR, SOME AREAS OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH REWORK AND HFEC/ROTOTEST INSPECTION IAW EA 6-5312-82878 AND RAS 037837/015/2005 ISSUE A.SDR 07FDEA04091Skin Panel · corrodedCORROSION ON FAIL/SAFE RING, LT FWD PAX DOOR, SOME AREAS OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH REWORK AND HFEC/ROTOTEST INSPECTION IAW EA 6-5312-82878 AND RAS 037837/015/2005 ISSUE A.SDR 07FDEA04088Box Beam · crackedTWO CRACKS IN HOLE (EACH 10MM) FOUND IN THE UPPER TORSION BOX IN BEAM AT FRAME 75, STRG 11 LT. REPAIR PERFORMED BY CUT OUT OF DAMAGED AREA, INSTALLATION OF FILLER AND REPAIR ANGLE IAW EA 6-5318-82894 AND RAS/DAHAM/4019625/2005 ISSUE A.SDR 07FDEA04084Panel · damagedFOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLERS AT INBOARD AND OUTBOARD SIDEWALL PANEL, PYLON NR 1 LT. REPAIR PERFORMED BY INSTALLING NEW DOUBLERS ON SIDEWALL PANELS IAW SRM 54-51-31/FIG 201.SDR 07FDEA04082Panel · damagedFOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLER AT INBOARD SIDEWALL PANEL, PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLING NEW DOUBLER ON SIDEWALL PANEL IAW SRM 54-51-31/FIG 201.SDR 07FDEA04078Skin · misrepairedFOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN AT BUTT-JOINT FRAME 18 BETWEEN STRG 22-26 LT, NOT CONFORM TO SRM (RIVET SIZE). FOUND CORROSION AFTER REMOVAL. NEW DOUBLER REPAIR PERFORMED IAW DRW R536-11046 ISSUE B, HFEC AND ROTOTEST INSPECTION PERFORMED. SDR 07FDEA04076Skin · delaminatedFOUND SEVERAL DELAMINATIONS TO TRAILING EDGE ON UPPER AND LOWER SKIN OF INBOARD FLAP LT. REPLACEMENT OF LT INBOARD FLAP TRAILING EDGE PER DRW A579-70868, SOLID FASTENERS ARE REPLACED BY BLIND FASTENERS. REPAIR APPROVED BY EA 6-5752-92147 AND RAS/DABRE/7005SDR 07FDEA04074Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 2 RT, LOWER SKIN (100 BY 30 MM). REPAIR PERFORMED IAW SRM 57-70-00/201/PARA 12.SDR 07FDEA04073Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 2 LT, LOWER SKIN (100 BY 30 MM). REPAIR PERFORMED IAW SRM 57-70-00/201/PARA 12.SDR 07FDEA04067Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 1 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A.SDR 07FDEA04065Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 2 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A.SDR 07FDEA04063Skin · delaminatedFOUND DELAMINATION AROUND OLD REPAIR ON TRAILING EDGE OF INNER FLAP RT, UPPER AND LOWER SKIN. REPLACEMENT OF RT INBOARD FLAP TRAILING EDGE PER DRW A579-70868, SOLID FASTENERS ARE REPLACED BY BLIND FASTENERS. REPAIR APPROVED BY EA 6-5752-92147 AND RAS/DABRE/7SDR 07FDEA04050Skin Panel · damagedFOUND GROOVES ON OUTER SKIN PANEL, AFT LOWER CORNER AT AFT PAX DOOR LT, ZONE 833 AND ON SKIN PANEL, LOWER EDGE AREA AT AFT PAX DOOR RT, ZONE 843. REPAIR PERFORMED BY INSTALLING EXTERNAL DOUBLER AS PER SRM 52-11-00/PB 235/PAR 5F/FIG 206 ON LT PAX DOOR AND IAW SDR 07FDEA04044Hinge Fitting · corrodedNEW CORROSION ON OLD REPAIR, FOUND ON FWD PAX DOOR RT ON DOOR HINGE FITTING (LOWER ARM WEB - BOTTOM SIDE). CORROSION REMOVED (TOTAL OF 53 PERCENT REMOVED), FILLER AND OLD REPAIR DOUBLER INSTALLED IAW EA 6-5211-82884 AND RAS/AS/115/2005 ISSUE A.SDR 07FDEA04039Skin · misrepairedOLD EXTERNAL DOUBLER REPAIR ON INBOARD FLAP RT ON LOWER SIDE BETWEEN RIB 10-11, NOT CONFORM TO OLD RECORDS AS PER SRM 57-52-12/FIG 204: EXTERNAL DOUBLER IS ON LOWER SURFACE INSTEAD OF UPPER SURFACE, NO FILLER ON UPPER SURFACE INSTALLED AND NO RIVETS ON TRAILINSDR 07FDEA04037Door Frame · damagedDURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPAIR PERFORMED BY CUT OUT OF LOWER BEAM WEB IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE A.SDR 07FDEA04036Door Frame · damagedDURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPLACEMENT OF STRINGER 26 COUPLING BY NEW ONE IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE ASDR 07FDEA04034Skin Panel · misrepairedFOUND OLD DOUBLER REPAIR BETWEEN FRAME 11-11A, STRG 27-28 LT, NOT CONFORM TO REPAIR REFERENCE AS PER SRM 53-12-12/FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-12-12/FIG 201.SDR 07FDEA04033Rib · noneOLD REPAIR ON RT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.SDR 07FDEA04032Rib · noneOLD REPAIR ON LT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.SDR 07FDEA04029Stringer · corrodedDURING NON ROUTINE DR0115, FOUND CORROSION ON STRINGER 51 LT, BETWEEN FRAME 54.1-54.2. PARTIAL STRINGER REPLACEMENT WITH SPLICE REPAIR PERFORMED, BETWEEN FRAME 54.1-54.2 IAW SRM 53-10-14/FIG 201 AND 54.2-54.3 (DR0115).SDR 07FDEA04026Stringer Splice · corrodedCORROSION ON CONNECTING SEGMENT STRG 51 LT, BETWEEN FRAME 54.2-54.3. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10.SDR 07FDEA04024Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 63 RT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.SDR 07FDEA04022Floor Support · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 AD, BULK CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10.SDR 07FDEA04021Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 69 LT, BULK CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.SDR 07FDEA04019Frame · damagedOLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED AND AFTER REWORK OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING NEW REPAIR ANGLE AT OLD REPAIR AS PER PRINCIPLE IN SRM 53-10-13.SDR 07FDEA04015Shear Plate · crackedCRACKED SHEAR PLATE AT STR 26 LT, BETWEEN FRAME 79-80. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.SDR 07FDEA04014Stringer · corrodedCORROSION ON STRINGER 42 RT, BETWEEN FRAME 72-73. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.SDR 07FDEA04013Stringer · damagedOLD DAMAGE ON STRINGER 30 RT, BETWEEN FRAME 54.2-54.3. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.SDR 07FDEA04011Beam · corrodedCORROSION ON TOP SURFACE OF AFT CARGO COMP SILL BEAM FLANGE BETWEEN FRAME 59-59A AROUND A RIVET NUT. REMAINING THICKNESS AFTER REWORK IS 0,8MM, NOMINAL: 2,0MM. REPAIR PERFORMED BY CUT OUT AFFECTED AREA AND INSTALLING FILLER AND REPAIR ANGLE IAW ENG-STATEMENTSDR 07FDEA04006Stringer Clip · failedFOUND FRAME-STRINGER-CONNECTING ANGLES WITH LESS EDGE MARGIN AT STRINGER 26 RT BETWEEN FRAME 67-68, 69-70 AND 71-72 AND ON STRG 26 LT BETWEEN FRAME 70-71 AND 71-72. REPLACEMENT WITH FABRICATED ENLARGED REPAIR ANGLES IAW SRM 51-72-10.SDR 07FDEA04003Support · failedFOUND SUPPORT STRUT WITH LESS EDGE MARGIN BETWEEN FRAME 71-72, STRG 26 RT. REPLACEMENT OF STRUT IAW SRM 51-72-10.SDR 07FDEA04001Frame · damagedFOUND OLD ENLARGED HOLE (DIA 6MM) AT CONNECTING SEGMENT FRAME 55/58, STRG 25 LT. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10.SDR 07FDEA04000Stringer · damagedFOUND SEVERAL MISDRILLED HOLES ON T-STRINGER 26 RT, AT FRAME 71. REPAIR PERFORMED BY INSTALLING NEW PARTIAL STRINGER PROFILE FABRICATED WITH COUPLINGS IAW ENG-STATEMENT: REA 0492-009.SDR 07FDEA03997Stringer · damagedSEVERAL OLD MISDRILLED HOLES ON STRINGER 15 LT, BETWEEN FRAME 35-36. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.SDR 07FDEA03995Skin Panel · crackedCRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON RT ZONE 675CB ONE HOLE WITH CRACK IN SKIN. FOR LOCATION SEE EA 6-5710-81091/PG 4 (CRACK LENGTH IN HOLE ABOUT 3MM). DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW DRW R573-49237 AND EA 6-5710-81091.SDR 07FDEA03994Crossbeam · corrodedFOUND CORROSION AT CROSS BEAM C 63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10SDR 07FDEA03993Skin Panel · crackedCRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON LT ZONE 575CB TWO HOLES WITH CRACKS IN SKIN. FOR LOCATION SEE EA 6-5710-81091/PG 3 CRACK LENGTH IN HOLES ABOUT 2 AND 4MM. DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW. DRW. R573-49237 AND EA 6-5710- 8109SDR 07FDEA03990Stiffener · crackedFOUND CRACK ON STIFFENER AT FRAME 12A LT, STRG 27. REPLACEMENT OF STIFFENER AS PER DWG A536-10318/SH 05.SDR 07FDEA03988Floor Support · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 LHS, Y805 OF BULK CARGO COMPARTMENT FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10.SDR 07FDEA03987Longeron · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 LHS, Y140 OF BULK CARGO COMPARTMENT FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10.SDR 07FDEA03984Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 67. CROSSBEAM REPLACED IAW SRM 51-72-10.SDR 07FDEA03983Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 55/58. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.
Back to Airbus A310-324