Airbus A310-324

Service difficulty reports · 1,439

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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"

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SDR 07FDEA03863Stringer · corrodedHEAVY CORROSION ON STRINGER 56 LT AND RT BETWEEN FRAME 55/58-65. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14 / FIG 201A.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03862Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 71, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03861Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 70, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03860Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 61, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03859Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 71, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03858Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 60, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03857Fitting · corrodedHEAVY CORROSION ON CLIP AT FRAME 69, BETWEEN STRG 56-57 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03824Profile · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE AT BULK CARGO COMP FLOOR STRUCTURE BETWEEN FRAME 63-64, Y-805, RT. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03823Profile · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE AT BULK CARGO COMP FLOOR STRUCTURE BETWEEN FRAME 64-67, Y-805, RT. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03819Longeron · corrodedCORROSION ON LONGITUDINAL PROFILE AT BULC CARGO COMPARTMENT FLOOR STRUCTURE BETWEEN FRAME 67-69, STRG 45-47 RT. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03817Angle · corrodedCORRODED COUPLING ANGLE AT FRAME 69, STRINGER 49-51 RHS. REPLACEMENT OF COUPLING ANGLE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03814Plate · corrodedCORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 38.1-38.2, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03813Plate · corrodedCORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 22-23, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03812Plate · corrodedCORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 21-22, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03811Plate · corrodedCORRODED SHEAR PLATES AT FWD CARGO COMPARTMENT BETWEEN FRAME 38.2-39, STRG 43-44 LT AND RT. REPLACEMENT OF SHEAR PLATES IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03810Plate · corrodedCORRODED SHEARPLATES AT FWD CARGO COMPARTMENT BETWEEN FRAME 36-37 AND FRAME 38.1-38.2 RT, STRG 43-44. REPLACEMENT OF SHEAR PLATES IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03809Wedge · corrodedFOUND CORROSION ON RT ELEVATOR TRAILING EDGE WEDGE, BETWEEN RIB ER12-ER28. REPAIR OF ELEVATOR TRAILING EDGE WEDGE IAW SRM 55-21-11/CONFIG 2/PG 1-3.Sep 17, 2007 · N804FD · Airbus A310324 · Elevator StructureSDR 07FDEA03808Web · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 23 LT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03807Web · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 36 RT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03806Web · damagedFOUND DAMAGED WEB PLATES BETWEEN FRAME 85-86, STRG 33 RT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03805Strut · corrodedCORRODED CROSS STRUTS FWD OF FRAME 86 RT, STRG 15. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03804Strut · corrodedCORRODED CROSS STRUTS FWD OF FRAME 84 LT, STRG 15. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03803Seat Track · corrodedHEAVY CORROSION ON SEAT TRACK BETWEEN FRAME 14-19, Y-450 RT. REPLACEMENT OF SEAT TRACK IAW SRM 51-72-10.Sep 17, 2007 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03790Frame · failedFOR REPLACEMENT OF STRINGER 50 LT AND RT FROM THE COUPLING FWD OF FRAME 55 (NON ROUTINE DR106) IT IS NECESSARY TO CUT FRAME 54.2 BETWEEN STRG 50-51, LT AND RT FRAME SPLICE REPAIR PERFORMED ON BOTH SIDES LT AND RT AS PER A300-600 FREIGHTER SRM 53-10-13/ FIG 203Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA03785Profile · corrodedCORRODED CORNER PROFILE (FITTING) BETWEEN FRAME 63-64 LT, CARGO COMPARTMENT FLOOR STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF CORNER PROFILE (FITTING) IAW SRM 51-72-10.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03784Fitting · corrodedCORRODED FITTING AT FRAME 63, STRG 44 LT OF CARGO COMPARTMENT FLOOR STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03782Floorbeam · corrodedCORROSION ON CROSSBEAM AT FRAME 63 LT, CARGO COMPARTMENT FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA03781Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM FRAME 60 LT, CARGO COMPARTMENT FLOOR STRUCTURE. SPLICE REPAIR AT CROSSBEAM PERFORMED IAW SRM 53-10-15/FIG 207.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA03780Beam · corrodedSEVERAL CORRODED AREAS ON SILLBEAM OF AFT CARGO COMPARTMENT CUT OUT. REPAIR PERFORMED BY REPLACEMENT BY INSTALLING AIRFRAME AND HARDWARE KIT: SR5317-99A00500 AND SR5317-99H01200 IAW SRM 53-17-18/FIG 207 / TB. 203. DEVIATIONS FROM SRM 53-17-18/FIG 207. INSTASep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA03779Stringer · corrodedCORROSION ON STRINGER 51, BETWEEN FRAME 36-37 LT, AFTER BLENDING IS THE REMAINING THICKNESS OUT OF LIMIT IAW SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03778Stringer · corrodedHEAVY CORROSION ON THE FLANGE OF STRINGER 51 RT, BETWEEN FRAME 45-46, REMAINING THICKNESS AFTER BLENDING IS OUT OF LIMIT. REPAIR PERFORMED BY CUTTING OUT DAMAGED PART AND INSTALLING A REPAIR ANGLE (4 MM THICK) IAW EA 6-5318-81086 AND RAS 034265/005/2004 ISSUESep 14, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03777Support · misrepairedOLD ANGLE REPAIR ON LONGERON (SUPPORT) BETWEEN FRAME 13B-16A, Y-953, FLOOR STRUCTURE, NOT CONFORM TO SRM 53-12-15 / FIG 207. REPAIR OF SUPPORT LONGERON PERFORMED IAW SRM 53-12-15/FIG 207.Sep 14, 2007 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03776Skin · misrepairedFOUND OLD REPAIR DOUBLER ON AFT PAX DOOR RT OUTER SKIN LOWER EDGE, NOT CONFORM TO SRM 52-10-00/FIG 204. REPAIR RENEWED AS PER SRM 52-10-00/FIG 204.Sep 14, 2007 · N804FD · Airbus A310324 · Cargo/Baggage DoorsSDR 07FDEA03774Skin · chafedCHAFING DAMAGE AT ONE POSITION AND CRACK WITH DEFORMATION AT ANOTHER LOCATION ON FIXED LEADING EDGE D-NOSE SKIN RT, BETWEEN TRACK 3 AND TRACK 4. REPAIR PERFORMED BY BLENDING OUT DAMAGES AT BOTH POSITIONS, REMOVING FASTENER OF HOLE IN AREA OF CRACK WITH ROTOTESep 14, 2007 · N815FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA03772Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM FRAME 63 LT, Y1110 AND Y1160 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA03768Rib · misalignedTHS TIPS ON LT AND RT SIDE WERE DAMAGED AND SENT TO AN OUTSIDE VENDOR FOR REPAIR, SO TIPS FROM N812FD WERE CANNIBALIZED FOR USE ON N815FD, BUT THE THS RIB FASTENER HOLES MISMATCH TO TIP HOLES. REPAIR PERFORMED BY REPLACEMENT OF RIB ON LT AND RT THS IAW EA 6-5Sep 14, 2007 · N815FD · Airbus A310324 · Horizontal Stabilizer, Spar/RibSDR 07FDEA03763Fitting · corrodedCORROSION ON THE WHOLE LOWER SURFACE OF THE LT PYLON PYRAMID, FWD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED AS PER SRM 54-51-81 BY BLENDING OUT CORROSION, REPROTECTION BY CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-92174 AND RAS 039464/014Sep 14, 2007 · N815FD · Airbus A310324 · Nacelle/Pylon, Attach FittingsSDR 07FDEA03761Angle · mismanufacturedLESS EDGE MARGIN (5-6 MM) AT ANGLE, STR 26 RT BETWEEN FRAME 65-66 AND FRAME 67-68 AND ON LT BETWEEN FRAME 70-71, STRG 26. IT'S IMPOSSIBLE TO INSTALL DAN5-6X FASTENERS DURING PTOF. REPAIR PERFORMED BY INSTALLING REPAIR ANGLE FABRICATED IN EFW-DRS (RE0074-201 Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03757Plate · crackedCRACKED SHEAR PLATE BETWEEN FRAME 32-33, STRG 44 RT. REPLACEMENT OF SHEARPLATE IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03755Fitting · gougedGOUGE AT AFT PYLON TO ENGINE FITTING, RT PYLON. REPAIR PERFORMED BY SMOOTH BLEND OUT TO ELIMINATE SHARP EDGES AND REPROTECTION AS PER SRM WITH CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-92173 AND RAS 039403/010/2005.Sep 14, 2007 · N815FD · Airbus A310324 · Nacelle/Pylon, Attach FittingsSDR 07FDEA03752Plate · corrodedHEAVY CORRODED AND CRACKED SHEAR PLATES BETWEEN FRAME 79-80, STRG 26 LT AND RT. REPLACEMENT OF SHEAR PLATES LT AND RT IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03748Plate · damagedDAMAGED SHEARPLATE (DENTED AND CRACKED) BETWEEN FRAME 38.1-38.2. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03745Frame · damagedNICK ON FRAME 61, STRG 15 LT AND THREE OPEN FASTENER HOLES. REPAIR PERFORMED BY BLEND OUT NICK AND CLOSING BLIND OPEN FASTENER HOLES IAW EA 6-5317-92170 AND RAS/DATLS/0002688/2005 ISSUE A.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA03738Panel · corrodedFOUND EXFOLIATION CORROSION ON FAIL/SAFE RING AT LOWER AFT CORNER OF FWD PAX DOOR RT, FRAME 15-16A. REPAIR PERFORMED BY REWORK, NDT INSPECTION AND FILLING THE REWORKED AREA WITH SEALANT IAW EA 6-5312-92165 AND RAS/AS/0181/2005 ISSUE A.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03732Strap · damagedDAMAGED SEALING STRAP AT FWD CARGO DOOR CUT OUT, FRAME 25A RT, OUT OF LIMIT IAW SRM 51-10-10. REPLACEMENT OF STRAP IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03730Angle · corrodedFOUND CORRODED ANGLE AT FRAME 101 REAR SIDE OF FIREWALL, STRG 5 RT. REPLACEMENT OF ANGLE IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03729Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM FRAME 61 AFT CARGO COMP FLOOR STRUCTURE, RT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA03728Skin · delaminatedFOUND DELAMINATION ON CORE FILLER AT TRAILING EDGE SKIN OF INBOARD FLAP RT. DELAMINATED CORE FILLER REPAIRED IAW SRM 57-53-12/FIG 209/SH 2/VERSION 3.Sep 14, 2007 · N815FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA03726Floor Support · corrodedFOUND CORROSION ON LONGITUDINAL PROFILE BETWEEN FRAME 63-64, Y-805 RT, AFT CARGO COMPARTMENT FLOOR STRUCTURE. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03725Fitting · corrodedHEAVY CORROSION ON CORNER FITTING FRAME 54.2 BETWEEN P41-45 LT. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous Structure
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