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.

SDR 07FDEA04198Skin Panel · corrodedTWO CORROSION SPOTS OUT OF SRM LIMITS ON INTERNAL SKIN BETWEEN FRAME 19-20, STRG 51-52 LHS. REPAIR PERFORMED BY CORROSION REMOVAL, FLAP PEENING, NDT INSPECTION FOR CRACK FREE CONDITION AND INSTALLATION OF ENLARGED FILLER AND FINGER STRAP IAW EA 6-5313-82909 ASep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04197Angle · corrodedHEAVY CORROSION ON CONNECTING ANGLE FRAME 64, STRG 36 RT. REPLACEMENT OF ANGLE IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04194Frame · corrodedHEAVY CORROSION ON CROSS STRUT FRAME 87 LT, AFT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04193Skin Panel · corrodedTHREE CORROSION SPOTS ON INNER SKIN PANEL BETWEEN FRAME 18-19 AND BETWEEN STRG 49-51 LHS. REPAIR PERFORMED BY LOCAL CUT OUT AF SKIN PANEL BETWEEN STRG 49-50 AND SMOOTH REWORK OF REMAINING CORRODED AREAS, HFEC-, ROTOTEST INSPECTION AND INSTALLING EXTERNAL SKINSep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04192Frame · corrodedHEAVY CORROSION ON FRAME 37 BETWEEN STRG 54 LT AND 53 RT. FRAME SPLICE REPAIR PERFORMED IAW SRM 53-10-13/FIG 203.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04191Stringer · corrodedHEAVY CORROSION ON STRINGER 44 LHS, BETWEEN FRAME 20-23. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04187Fitting · damagedAREAS OF IMPACT DAMAGE FOUND ON THE AFT FACE OF THE OUTBOARD LUG ON THE RT WING PYLON MOUNTING (ATTACH FITTING), RIB 8-9. REPAIR PERFORMED BY BLENDING DAMAGE TO REMOVE ALL SHARP EDGES, HFEC INSPECTION AND INSTALLING NEW SELF-LUBRICATING BEARING IAW EA 6-5720-Sep 21, 2007 · N803FD · Airbus A310324 · Wing, Attach FittingsSDR 07FDEA04186Panel · crackedTWO CRACKS AT LEADING EDGE ACCESS PANEL NR 2 OF RUDDER INNER SKIN, HONEYCOMP CORE AND OUTER SKIN CRACKED AT ACCESS HOLE EDGES, MAX CRACK LENGTH = 75MM. REPAIR PERFORMED BY WET-LAY-UP REPAIR AS PER TD/K4/S1/19611/2005/A, APPROVED BY EA 6-5542-82890 AND RAS/DAHSep 21, 2007 · N803FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04185Support Fitting · crackedCRACKED SUPPORT FITTING BETWEEN FRAME 16A-17, STRG 44 RHS. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04184Crossbeam · corrodedCORROSION ON CROSS STRUT AT FRAME 84, STRG 15 RT FRONT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04183Crossbeam · corrodedFOUND CORROSION ON CROSS STRUT AT FRAME 87, STRG 15 RT AFT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04182Crossbeam · corrodedCORROSION ON CROSS STRUT AT FRAME 86, STRG 15 RT FRONT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04181Failsafe · damagedFOUND MISDRILLED FASTENER HOLES AT FRAME-FAIL-SAFE-RING, FUSELAGE SKIN BETWEEN FRAME 73-76, STRG 26-27 RHS. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION HL13VF8 (DAN8-8) FASTENERS IAW EA 6-5318-82891 AND RAS/DAHAM/4019615/2005 ISSUE A.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04180Fitting · corrodedCORROSION ON FITTING AT FWD PAX DOOR LT. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA04179Fitting · corrodedCORROSION ON FITTING AT FWD PAX DOOR LT. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA04177Flange · corrodedCORROSION ON OUTER FLANGE AT FRAME 91, BETWEEN STRG 45 LT-AD. REPLACEMENT OF OUTER FLANGE BETWEEN STRG 37 RT-37 LT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04176Web · damagedDAMAGED WEB PLATE AT STRG 36 RT, BETWEEN FRAME 86-87. REPLACEMENT OF WEB IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04175Stringer · corrodedCORROSION ON STRINGER 52 LT, BETWEEN FRAME 35-38.1. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04174Stringer · corrodedCORROSION ON STRINGER 51 LT, BETWEEN FRAME 37-38.1. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04173Plate · corrodedHEAVY CORROSION ON SHEAR PLATE BETWEEN FRAME 79-80, STRG 26 RT. REPLACEMENT OF CONN SEGMENT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04172Frame · corrodedHEAVY CORROSION ON CONNECTING SEGMENT FRAME 70, STRG 44 RT. REPLACEMENT OF CONN SEGMENT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04171Skin Panel · chafedCHAFING MARK FOUND ON LOWER INNER SKIN BETWEEN FRAME 46-47 AND STRG 44-45. REPAIR PERFORMED BY SMOOTHLY REWORK, DVI-HFEC-ROTOTEST INSPECTION AND INSTALLATION OF R1 OVERSIZED FASTENERS IF NECESSARY IAW EA 6-5315-82917 AND RAS 038213/011/2005 ISSUE A.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04170Web · failedIN AUGUST 1198: SEVERAL SPOTS OF CORROSION HAD BEEN FOUND ON VERTICAL WEB (SEGMENT) OF PRESSURE BULKHEAD AT FRAME 39, Y=0. REPAIRS HAD BEEN PARTIALLY PERFORMED IN ACCORDANCE WITH TD 582.0939/98 ISSUE A IN JULY 2005: NEW CORROSION FINDINGS HAVE BEEN REPORTED,Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04164Frame · corrodedHEAVY CORROSION ON FRAME SEGMENT AT EMERGENCY EXIT DOOT RT, BETWEEN BEAM 4-5. REPLACEMENT OF FRAME SEGMENT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04163Beam · corrodedHEAVY CORROSION ON BEAM NR 5 AT EMERGENCY EXIT DOOR RT, ZONE 844. REPLACEMENT OF BEAM NR 5 IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04160Skin Panel · damagedDAMAGES ON SKIN PANEL AT FRAME 33 BETWEEN STRG 38-39 RT. REPAIR PERFORMED BY REWORK DAMAGES TO A SMOOTH CONTOUR. MINIMUM THICKNESS FOLLOWING REWORK IS 1.37MM, NDT INSPECTION FOR CRACK FREE CONDITION AND ENLARGE THE INNER STRAP TO ACT AS A REPAIR DOUBLER IAW Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04157Plate · corrodedCORRODED SHEAR PLATE BETWEEN FRAME 36-37 LT, STRG 44. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04156Plate · corrodedCORRODED SHEAR PLATE BETWEEN FRAME 36-37 LT, STRG 44. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04155Plate · corrodedCORRODED SHEAR PLATES AT FOLLOWING AREAS: BETWEEN FRAME 32-33 RT, 33-34 RT, 32- 33 LT AND 33-34 LT. REPLACEMENT OF SHEAR PLATES IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04154Skin Panel · failedEXISTING FLUSH REPAIR ON SKIN BETWEEN FRAME 2-3 AD, CAUSED BY A FLIGHT TEST INSTALLATION CONFORM TO DRW A536-11822, GOT IN CONFLICTS WITH PTOF CONVERSION. REPAIR MODIFIED WITH A THIRD FASTENER ROW THROUGH ALL LAYERS CONFORM TO REPAIR DRW A536-11822 IAW. EA Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04153Strut · corrodedCORROSION ON U-STRUT AT UPPER EDGE OF AFT PAX DOOR LT, BETWEEN FRAME 73A-75A. REPLACEMENT OF STRUT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA04152Skin · chafedFOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK 7-8 OF RT WING. NOSE SKIN REPAIR PERFORMED IAW SRM 57-41-12/FIG 203, 204.Sep 21, 2007 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04151Coupling · damagedDAMAGED COUPLING AT STRG 4 LT BETWEEN FRAME 87-88. REPLACEMENT OF COUPLING IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04144Frame · corrodedCORROSION ON WEB AND INNER FLANGE OF FRAME 75A RT, AFT PAX DOOR BETWEEN STRG 26-27 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION AND FLAP PEENING IAW EA 6- 5318-82893 AND RAS/DAHAM/4019630/2005 ISSUE A.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04143Web · corrodedHEAVY CORROSION ON TWO SHEAR WEBS AT STRINGER 26 LT AND RT, BETWEEN FRAME 75A-76. REPLACEMENT OF BOTH SHEAR WEBS LT AND RT IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04142Stringer Splice · corrodedHEAVY CORROSION ON STRINGER SPLICE 32 RT, BETWEEN FRAME 64-65. REPLACEMENT OF STRINGER SPLICE IAW SRM 51-72-10.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04141Stringer · corrodedCORRODED STRINGER 54 RT BETWEEN FRAME 37-38. PARTIAL STRINGER INSTALLATION WITH TWO STRINGER SPLICE REPAIRS BETWEEN FRAME 36-37 AND 37-38 PERFORMED IAW SRM 53-10-14/FIG 201.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04140Skin Panel · corrodedCORROSION ON INTERNAL SKIN BETWEEN FRAME 37-38, STRG 53 RT - 54 LT. REPAIR PERFORMED BY BLEND OUT, HFEC/ROTOTEST INSPECTION AND FLAP PEENING IAW EA 6-5314-82916 AND RAS/DATLS/0002629/2005 ISSUE A.Sep 21, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04132Stringer · corrodedCORROSION ON STRINGER 53 LT BETWEEN FRAME 70-71 AND STRINGER 56 LT BELOW FRAME 70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04131Stringer · corrodedCORROSION ON STRINGER 51 RT BETWEEN FRAME 76-77. STRINGER REPAIR PERFORMED IAW FREIGHTER A300-600 SRM 53-10-14/FIG 206, APPROVED BY EA 6-5318-82875 AND RAS/DAHAM/4019558/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04126Stringer · misrepairedDURING CHANGING OLD DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 29-32 LT FOUND LESS EGDE MARGING IN STRINGER 32 LT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04124Skin Panel · failedOLD DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 29-32 LT IS NOT CONFORM TO SRM 53-10-12/FIG 225/SH 2, DOUBLER THICKNESS IS 1,6MM INSTEAD OF 1,8MM. REPAIR PERFORMED BY INSTALLING NEW SKIN DOUBLER IAW SRM 53-10-12/FIG 228/SH 2.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04121Frame · corrodedCORROSION ON MILLED FRAME 63A BETWEEN STRG 32-35 AND STRG 39-41 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION FOR NIL FINDINGS AND FLAP PEENING IAW EA 6-5317-82874 AND RAS/DAHAM/4019554/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04120Frame · corrodedHEAVY CORROSION ON MILLED FRAME 59A BETWEEN STRG 40-42 RT. REPAIR PERFORMED BY CUT OUT DAMAGED PORTION AND PARTIAL REPLACEMENT OF FRAME IAW DRW R539-70138 ISSUE F, APPROVED BY EA 6-5317-82873 AND RAS/DAHAM/4019557/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04118Attach Fitting · gougedDEEP GOUGE ON LT MIDDLE VERTICAL STABILIZER TO FUSELAGE ATTACH FITTING, OUTBOARD SIDE AFT AREA. REPAIR PERFORMED BY SMOOTH BLEND OUT AND NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5319-82881 AND RAS/DAHAM/4019574/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Vertical Stabilizer, Attach FittingsSDR 07FDEA04117Sill · corrodedCORROSION ON THE UPPER FLANGE AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-59A RT, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT AND FLAP PEENING IAW EA 6-5317-82872 AND RAS/DATLS/0002588/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04115Rib · corrodedFOUND CORRODED RIB 54 ON RUDDER. REPLACEMENT OF RIB 54 IAW SRM 55-41-19.Sep 20, 2007 · N803FD · Airbus A310324 · Rudder, Spar/RibSDR 07FDEA04113Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM FRAME 63 LT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04112Frame · corrodedOLD REPAIRS WITH NEW CORROSION AT FRAME 40 BETWEEN 51-52 LT, 54-55 LT, 54-55 RT AND 50-51 RT. REPAIR PERFORMED BY REMOVE EXISTING REPAIR ANGLES AND INSTALLING NEW FABRICATED ANGLES IAW EA 6-5315-82860 AND RAS 037936/008/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04111Skin Panel · failedFOUND OLD SMALL FLUSH DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 41-42 LHS, NOT CONFORM TO SRM. REPAIR PERFORMED BY INSTALLING NEW EXTERNAL DOUBLER IAW SRM 53-10-12/FIG 227.Sep 20, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/Skin
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