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 07FDEA04398Spar · damagedSHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH IAW EA 6-5720-82852 AND RAS /BAE/1000689/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Wing SparSDR 07FDEA04397Floorbeam · damagedFOUND OLD MISDRILLED HOLE AT CROSSBEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04396Stringer · damagedFOUND MISDRILLED HOLES AT STRINGER 41 LT, C33-34 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04395Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04394Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04393Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04392Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04391Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04390Stringer · corrodedFOUND CORRODED STRINGER SEGMENT P 57 AT C 72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04389Floorbeam · corrodedFOUND CROSSBEAM C 63 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04388Flange · corrodedFOUND CORRODED FLANGE AT C61-62, P 56 RT-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04387Stringer · corrodedFOUND CORRODED STRINGER P 21 LT, BETWEEN 55/58-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04386Panel · crackedFOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 07FDEA04370Plate · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR. 33 LT REPLACEMENT OF WEB PLATE IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04369Plate · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR 39 LT AND RT. REPLACEMENT OF WEB PLATES LT AND RT IAW SRM 51-72-10Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04368Fitting · corrodedCORROSION ON UPPER RUN OUT FITTING BETWEEN FRAME 16A-17, STRG 44 RT, AFTER REWORK NO REMAINING THICKNESS WAS EXISTED. REPLACEMENT OF UPPER RUN OUT FITTING IAW. REPAIR DRW R536-10440 ISSUE C.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04367Skin · chafedFOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB 27 OTHER ASNA0081A FASTENERS ARE INSTALLED ACC TO DRW A578-44242/SHEET 16, IAW AI-STATEMENT 942-03Sep 28, 2007 · N806FD · Airbus A310324 · Leading Edge DevicesSDR 07FDEA04365Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NEW SKIN INSERT IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04364Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04363Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04362Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 1 AND SLAT TRACK 2, LEADING EDGE SKIN, RT WING. NOSE SKIN REPAIR RENEWED, NEW REPAIR SKIN IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04360Skin · chafedFOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04359Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04358Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous StructureSDR 07FDEA04357Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous StructureSDR 07FDEA04356Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 6, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 6 LT IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous StructureSDR 07FDEA04355Skin Panel · misinstalledFOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN FRAME 11-12, STGR 25-26 LT IAW RAS 031880/026/2004 ISSUE A THIS REPAIR WAS ONLY AUTHORIZED FOR ONE FERRY FLIGHT TO DRESDEN BECAUSE OF SOME DEVIATIONS AGAINST SRM 53-12-12/FIG 202. REPAIR PERFORMED BY Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04354Skin · corrodedOLD DOUBLER REPAIR AT RT WING-LET TO STATIC DISCHARGER NO. V, FINAL REPAIR IS NECESSARY. AFTER REMOVAL OF DOUBLER FOUND ADDITIONAL CORROSION AND A MISDRILLED HOLE ON THE SKIN OF INBOARD PANEL OF RT FENCE. REPAIR PERFORMED BY SKIN CUTOUT AND INSTALLING FABRICSep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04353Skin · failedEXISTING EXTERNAL REPAIR DOUBLER ON NOSE SKIN OF OUTBOARD RT FLAP, RIB 10.5 (PANAM EA X3157J518). PERMANENT REPAIR WAS CARRIED OUT ON 25-APR-1994 BY REPLACING THE INSTALLED DOUBLER WITH A 1,8MM THICK ONE AND THE EXISTING FASTENERS WITH BLIND RIVETS CR35Sep 28, 2007 · N806FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04350Skin · corrodedCORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 16A, AFT UPPER CORNER. REPAIR PERFORMED BY BLENDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A.Sep 27, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04349Skin · corrodedCORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 14, FWD UPPER CORNER. REPAIR PERFORMED BY BLENDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A.Sep 27, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04348Skin · corrodedCORROSION ON FAIL/SAFE RING PAX DOOR NR 1 FUSELAGE SKIN PANEL AT FRAME 14, STGR 25 RT, AROUND THREE FASTENERS. REPAIR PERFORMED BY BLENDING CORROSION, HFEC INSPECTION IN THE AREA, ROTOTEST OF HOLES FOR NIL CRACK FINDINGS WITH OVERSIZING HOLES FOR TRANSITION FSep 27, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04346Skin Panel · wornELONGATED HYDRAULIC FITTING HOLE NR 1 ON RT WING LOWER SKIN, PYLON SUPPORT BRACKET, RIB 8. REPAIR OF HOLE NR 1 PERFORMED BY OVERSIZING AND BUSHING IAW EA 6-5720-82851 AND RAS/BAE/1000639/2005 ISSUE A.Sep 27, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04345Skin · delaminatedFOUND DELAMINATIONS ON RUDDER SIDE PANEL IN AREA OF HINGE ATTACHMENTS AT ALL GFRP-FITTINGS LT AND RT: BR1, BR2, BR4 LOWER, BR4 CENTER, BR4 UPPER, BR5, BR6 AND BR7. DELAMINATION REPAIR OF GFRP FITTING CONNECTION AT ALL HINGE FITTINGS PERFORMED IAW SRM 55-41-12Sep 27, 2007 · N806FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04344Skin · failedFOUND OLD DOUBLER REPAIR ON LOWER PANEL, CENTER BOX OF INBOARD FLAP RT, RIB 9-11, NOT IAW SRM 57-52-12/FIG 205, DOUBLER EDGES, LENGTH OF DOUBLER SHEET NOT ALLOWED. REPAIR RENEWED AS PER SRM 57-52-12/FIG 205, RIB 9. REPAIRED AS PER SRM 51-40-51/FIG 202, ALL ISep 27, 2007 · N806FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04343Skin · failedFOUND OLD REPAIR ON CLOSING RIB 21, INNER FLAP RT FINAL REPAIR ON FLAP BY REPLACEMENT OF END RIB 21 IAW SB A310-57-2055/PARA 2 F.Sep 27, 2007 · N806FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04229Fitting · corrodedFOUND CORROSION SPOT ON LT FWD PAX DOOR FITTING AT XP715 BETWEEN BEAMS 3 AND 5. REPAIR PERFORMED BY CUTTING-OUT THE FITTING WEB IN ORDER TO REMOVE CORROSION AND PERFORMING HFEC INSPECTION OF THE REWORKED AREA, INSTALLING REPAIR DOUBLER WITH MONEL RIVETS IAW ESep 24, 2007 · N803FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA04228Web · damagedDAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04227Web · damagedDAMAGED WEB PLATE BETWEEN FRAME 85-86, STR 33 RT. REPLACEMENT OF WEB IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04226Web · damagedFOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 33 RT. REPLACEMENT OF WEB IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04225Support Fitting · corrodedFOUND CORROSION ON THS SUPPORT FITTING, STA 93, RIB3 LT. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Horizontal Stabilizer StructureSDR 07FDEA04220Stringer · corrodedCORROSION ON STRINGER 43 LT AT FRAME 38. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04217Skin · delaminatedFOUND EXISTING REPAIRS ON THE STOP-SURFACES ON SPOILER NR 4 RT, MONEL RIVETS NSA5414-32 AND WASHERS WERE USED INSTEAD OF NSA1919-M FASTENERS ON TOP SKIN RIB 01 AND 19, DELAMINATION ON TOP SKIN AT STOP-FITTING AREAS. REPAIR PERFORMED BY FABRICATE BOND AN ANGLESep 24, 2007 · N803FD · Airbus A310324 · SpoilersSDR 07FDEA04216Skin · delaminatedFOUND EXISTING REPAIRS ON THE STOP-SURFACES ON SPOILER NR 4 LT, MONEL RIVETS NSA5414-32 AND WASHERS WERE USED INSTEAD OF NSA1919-M FASTENERS ON TOP SKIN RIB 01 AND 19, DELAMINATION ON TOP SKIN AT STOP-FITTING AREAS. REPAIR PERFORMED BY FABRICATE BOND AN ANGLESep 24, 2007 · N803FD · Airbus A310324 · SpoilersSDR 07FDEA04215Skin · damagedENLARGED HOLES IN FUSELAGE SKIN AT BEAM 10 BETWEEN FRAME 68-69 AND AT FRAME 67 BETWEEN STRINGER 43-44 RT, BULK CARGO DOOR CUT OUT. REPLACEMENT OF BEAM 10 IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04211Frame · crackedCRACKED VERTICAL FRAME SEGMENT 3.1 ON RT EMERGENCY EXIT DOOR BETWEEN FRAME 42A-43A, BETWEEN BEAM 5 AND 6. REPLACEMENT ON FRAME SEGMENT IAW SRM 51-72-10.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04210Stringer · corrodedHEAVY CORROSION ON STRG 27 RT, BETWEEN FRAME 74-75 AND FRAME 75-75A. PARTIAL REPLACEMENT OF STRINGER 27 RT, C74-76 WITH THREE COUPLINGS BETWEEN FRAME 73A-74, FRAME 74-75 AND FRAME 75A-76 IAW EA 6-5318-82912 AND RAS/DAHAM/4019688/2005 ISSUE A.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04208Beam · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-60. AREA IS UNDER FRAME 59A. REPAIR PERFORMED BY CUT OUT SILL BEAM WEB AND INSTALLING REPAIR ANGLE AND FILLER IAW EA 6-5317-82915 AND RAS/DAHAM/4019686/2005 ISSUE A.Sep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04205Skin Panel · misrepairedEXISTING INTERNAL SKIN FLUSH DOUBLER REPAIR BETWEEN FRAME 83-84, STRG 38 RT- 40 RT, NOT CONFORM TO SRM 53-10-12/FIG 227. DOUBLER THICKNESS OF ONLY 1,8MM. INSTALLED FLUSH REPAIR IS ACCEPTABLE AS PERMANENT REPAIR, REPLACEMENT OF RIVETS LN9198-4000 ON EACH SIDSep 24, 2007 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04200Skin · damagedFOUND DAMAGED AREA ON RUDDER, TRAILING EDGE, LOWER SIDE. REPAIR PERFORMED BY LAMINATING THE EDGE IAW SRM 55-41-12/FIG 208A WITH GLASFABRIC.Sep 24, 2007 · N803FD · Airbus A310324 · Rudder, Plate/Skin
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