Airbus A310-324

Service difficulty reports · 1,439

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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 = '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.

SDR 07FDEA03724Beam · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-59A. SILL BEAM REPAIR PERFORMED BY CUT OUT AND INSTALLING A FILLER IAW SRM 53-17-18/FIG 202, APPROVED BY EA 6-5317-92153 AND RAS/DATLS/0002685/2005 ISSUE A.Sep 14, 2007 · N815FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA03678Profile · chafedFOUND AN OLD REPAIR (CUT OUT) FLANGE WITH CHAFING MARKS AT FRAME 16 LT, OUT OF LIMIT. REPLACEMENT OF FLANGE IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA03687Fitting · crackedCRACKED CORNER FITTING AT AFT CARGO DOOR CUT OUT (SILLBEAM) BETWEEN FRAME 63-63A. REPLACEMENT OF CORNER FITTING IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03644Angle · mismanufacturedLESS EDGE MARGIN (5-6 MM) AT ANGLES STRG 26 RT AT FRAME 69 AND STRG 26 LT FRAME 63 AND 65. IT'S IMPOSSIBLE TO INSTALL DAN5-6X OR DAN5-8 FASTENER DURING PTOF. REPAIR PERFORMED BY INSTALLING REPAIR ANGLES FABRICATED IN EFW-DRS (RE0074-201/RE0074-200) IAW SRM 5Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03642Fitting · crackedCRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG. 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03641Fitting · crackedCRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03634Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 50 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03633Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 49 LT . REPLACEMENT OF BRACKET IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03632Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 46 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03702Longeron · corrodedHEAVY CORROSION ON EXTRUSION (LONGERON) Y-953 RT, BETWEEN FRAME 12A-14, OUT OF LIMIT IAW SRM 53-10-00/TB 102. EXTRUSION REPAIR PERFORMED BY INSTALLING REINFORCING PROFILES IAW SRM 53-12-15/FIG 207.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03699Skin · corrodedCORROSION PITS ON TOP REAR SKIN OF THS LT. REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101, PIT AREAS BETWEEN 200 AND 1500 MMXMM) REWORK ARESep 13, 2007 · N815FD · Airbus A310324 · Horizontal Stabilizer, Plate/SkinSDR 07FDEA03698Skin · corrodedCORROSION PITS ON TOP FWD SKIN OF THS LT REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101(PIT AREAS BETWEEN 200 AND 1500 MMXMM) REWORK AREAS DSep 13, 2007 · N815FD · Airbus A310324 · Horizontal Stabilizer, Plate/SkinSDR 07FDEA03695Longeron · corrodedHEAVY CORROSION ON LONGERON Y730, BETWEEN FRAME 11-14, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONGERON (SUPPORT) IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03694Longeron · corrodedHEAVY CORROSION ON LONGERON Y1959 LT, BETWEEN FRAME 12A-19, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONGERON (SUPPORT) IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03693Web · damagedBOTH CROSS SHEETS AT FRAME 69 IN BULK CARGO COMPARTMENT DENTED AND CRACKED. REPLACEMENT OF BOTH CROSS SHEETS LT AND RT IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03691Crossbeam · corrodedCORRODED AND OLD REPAIRED CROSSBEAM AT FRAME 58 IN BULK CARGO COMPARTMENT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA03689Longeron · corrodedHEAVY CORROSION ON LONGERON Y-1959 RT, BETWEEN FRAME 12A -19, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONGERON IAW SRM 51-72-10.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03683Skin Panel · chafedCHAFING MARKS ON RT WING LEADING EDGE D-NOSE SKIN BETWEEN TRACK 5 AND 6 AND AREA AROUND JACK 3, OUT OF SRM LIMITS. PARTIAL SKIN REPLACMENT BETWEEN TRACK 5 AND 6 AND AROUND JACK 3 IAW SRM 57-41-12/FIG 203, 204 SRM REQUIRES MATERIAL DTD5070 TO ACCOMPLISH REPAIRSep 13, 2007 · N815FD · Airbus A310324 · Leading Edge DevicesSDR 07FDEA03680Skin Panel · misrepairedFOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN FRAME 34-35, STRG 42-44 RT, NOT CONFORM TO REPAIR DRW R537-06202 ISSUE B AND RAS/DABRE/1540.1/96 ISSUE A. REPAIR REMOVED, SKIN CUT AND NEW DOUBLER INSTALLED IAW EA 6-5314-92180A AND RAS/DABRE/7005554/Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03676Skin Panel · corrodedCORROSION PITS ON TOP SKIN PANEL BETWEEN FRAME 80-95, STRG 6 RT TO 6 LT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW EA 6-5319-92157 AND RAS/DAHAM/4019752/2005 ISSUE A.Sep 13, 2007 · N815FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03674Hinge Fitting · corrodedCORROSION ON AFT LUG OF HINGE FITTING NR 5 AND CHAFING MARKS INSIDE ATTACH, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF HINGE FITTING NR 5 IAW AMM 55-36-46 AND BLEND OUT SCRATCHES WITH FLAP PEENING INSIDE HINGE FITTING ATTACH IAW SRM 51-29-00.Sep 13, 2007 · N815FD · Airbus A310324 · Rudder StructureSDR 07FDEA03663Fitting · damagedFOUND MISDRILLED HOLE IN CORNER FITTING ADJACENT AND LESS MARGIN TO ROLLER TRACK HOLE, FRAME 60, CARGO FLOOR STRUCTURE, Y1460 LT. REPAIR PERFORMED BY CREATING AN OBLONG HOLE AND INSTALLING FASTENER WITH STRENGTHENING PLATE IAW 6-5317-95859 AND RAS/DAHAM/40202Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03662Door Frame · damagedTOOLING IMPACTS FOUND ON DOOR FRAME 14 UNDER DOOR STOP 8 LH, PAX DOOR 1. REPAIR PERFORMED BY SMOOTH BLEND OUT, DVI INSPECTING OF FASTENER HOLES AND HFEC INSPECTION OF BLENDED AREAS FOR CRACK FREE CONDITION IAW EA 6-5312-95486 AND RAS 041687/013/2005 ISSUE A.Sep 13, 2007 · N812FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA03659Frame · dentedTOOL IMPACT CAUSES DENT IN FRAME 71, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213 / FIG 203.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA03658Frame · dentedTOOL IMPACT CAUSES DENT IN FRAME 70, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213/FIG 203.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA03656Frame · corrodedHEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND REPAIR ANGLES IAW EA 6-5319-92229 AND RAS/DAHAM/4020157/2005 ISSUE B.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA03653Floor Support · corrodedHEAVY CORROSION ON FLOOR SUPPORT BETWEEN FRAME 14-17, STRINGER 26, Y-1959 RT. REPAIR PERFORMED BY REINFORCING WITH ANGLE IAW SRM 53-12-15/FIG 207.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03651Fitting · damagedMISDRILLED HOLE IN CORNER FITTING FRAME 54.1 RT DUE TO FAILED INSTALLED ROLLERTRACK ON CARGO FLOOR STRUCTURE. REPLACEMENT OF CORNERFITTING IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03650Angle · failedLESS MARGIN AT ONE HOLE AT FRAME 59, STRG 26 LT. NEW SUPPORT CAN'T BE INSTALLED BETWEEN FRAME 59 AND SEAT TRACK AS PER DRW, R539H0112. REPAIR PERFORMED BY INSTALLING REINFORCING PLATE WHICH IS FIXED WITH HI-LOK'S DAN5-5 IAW, SRM 51-72-10 AND EFW DD-0467024Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03648Skin · corrodedHEAVY CORROSION UNDER ANTI-CHAFING PLATE ON SKIN PANEL BETWEEN FRAME 92-94, STRG 9-13 LT AND RT, OUT OF LIMIT. REPLACEMENT OF BOTH SKIN-PANELS (FABRICATED BY EFW-DRS) IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03647Stringer · damagedSEVERAL MISDRILLED HOLES ON STRINGER 33 RT BETWEEN FRAME 69-70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 / SEC "C-C".Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03645Skin · dentedDENT IN BOTTOM SKIN OF LT ELEVATOR TRAILING EDGE (30X30X1,5). REPAIR PERFORMED IAW SRM 55-21-11/CONFIG 1/PARA 5D/FIG 204.Sep 13, 2007 · N812FD · Airbus A310324 · Elevator, Plate/SkinSDR 07FDEA03637Plate · crackedCRACKED SHEAR PLATES BETWEEN FRAME 79-80/82, STRG 26 LT AND RT. REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10.Sep 13, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03631Skin Panel · chafedCHAFING MARKS FOUND AROUND MANHOLE 9 APERTURE ON THE UPPER SURFACE OF THE BOTTOM WING SKIN PANEL NR 2 BETWEEN RIB 14-15, BOTH WINGS. REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT INSPECTION FOR CRACK FREE AND FILLING BLEND LEVEL RESIN IAW EA 6-5720-92205 AND RAS/Sep 13, 2007 · N812FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA03616Skin · corrodedFOUND SKIN BULGE (CORROSION) ON LEADING EDGE OF RT WING INBOARD FLAP, NEAR TO TRACK 1. REPLACEMENT OF L/E SKIN AT FLAP IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA03615Tube · crackedDAMAGED (CRACKED) TUBE ASSY BETWEEN FRAME 24-25, STRG 52 RT. REPLACEMENT OF TUBE ASSY IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03628Stringer · corrodedCORROSION ON STRINGER 53, 54 AND 55 LHS BETWEEN FRAME 70-71. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03627Web · damagedFOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 36 LT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18/PG 76/ ITEM 40.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03626Web · damagedFOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18 / PG 76 / ITEM 10.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03625Web · damagedFOUND DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 33 LT AND RT. REPLACEMENT OF WEB PLATES IAW SRM 51-72-10 AND SRM 53-19-18/PG 53.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03624Fitting · corrodedCORROSION ON FITTING AT FRAME 63, STR 41-45 LT, OUT OF LIMIT. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA03623Longeron · misrepairedFOUND SPLICE REPAIR ON EXTRUSION BETWEEN FRAME 12A-14, Y-953 RT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPLICE REPAIR ON EXTRUSION RENEWED IAW SRM 53-12-15/FIG 207.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03622Longeron · misrepairedFOUND TWO SPLICE REPAIRS ON EXTRUSION BETWEEN FRAME 15A-17, Y1959 LT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPLICE REPAIRS ON EXTRUSION RENEWED IAW SRM 53-12-15/FIG 207.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03621Plate · damagedSCRATCHED AND DENTED CORNER PLATE AT BEAM 5 FWD CARGO DOOR AT FRAME 25A. REPLACEMENT OF CORNER PLATE IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324 · Cargo/Baggage DoorsSDR 07FDEA03620Beam · damagedSCRATCHED AND DENTED BEAM 5 FWD CARGO DOOR BETWEEN FRAME 20B-21. REPLACEMENT OF BEAM IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324 · Cargo/Baggage DoorsSDR 07FDEA03619Floorbeam · damagedFOUND MISDRILLED HOLES AT CROSSBEAM FRAME 54.1 AND 54.2, Y-805. CROSSBEAM SPLICE REPAIR ON BOTH CROSSBEAMS PERFORMED IAW SRM 53-10-15/FIG 207.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA03618Skin Panel · corrodedCORROSION SPOT BELOW STRG 57 ON LONGITUDINAL LAP JOINT AT INNER SKIN SURFACE IS OUT OF LIMIT, FRAME 65-66, STRG 57 AD. BLEND OUT REPAIR APPROVED EA 6-5317-92204 AND RAS/DAHAM/4020031/2005 ISSUE A.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03617Skin Panel · failedOLD REPAIR DOUBLER ON FUSELAGE SKIN BULK CARGO DOOR CUTOUT AT FRAME 69, STRG 43-45. DOUBLER MATERIAL NOT CONFORM TO RAS/DAHAM/12953/2000 ISSUE B AND SOGERMA CARD 6007 (B24279). DOUBLER REPLACED IAW RAS/DAHAM/12953/2000 ISSUE B AND SOGERMA DR B24279 NR 6007.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA03614Stringer · corrodedHEAVY CORROSION ON STRINGER 53 LT BETWEEN FRAME 55/58-59, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03612Floorbeam · misrepairedOLD REPAIR AT CROSSBEAM FRAME 63 BETWEEN Y500 AND Y1160 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE, NOT CONFORM TO SRM 53-10-15 / 207. SPLICE REPAIR RENEWED IAW SRM 53-10-15/FIG 207.Sep 12, 2007 · N812FD · Airbus A310324 · Fuselage Main, Floor Beam
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