N741FD
Service difficulty reports · 198
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N741FD' AND registry_match = 'registration' 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 n_number = 'N741FD' AND registry_match = 'registration' 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 08FDEA01073Doubler · damagedFOUND OLD REPAIR ON PRESSURE BULKHEAD C 39, P55 WITH NEW DEFECTS (CHAFING MARKS AND POSSIBLE CRACK IDENTIFICATION IN HOLE). REPAIR PERFORMED BY OVERSIZING THE HOLE, CUT THE STRINGER P55 AND INSTALLING A SPECIAL REPAIR COUPLING IAW DRAWING R538-10691, APPROVSDR 08FDEA01072Skin · corrodedFOUND CORROSION AROUND STATIC DISCHARGER OUTBOARD, WING TIP RT. REPAIR PERFORMED BY BLEND OUT OF CORRODED AREA AND INSTALLING A REPAIR PATCH IAW RAS/FOK/319/2007 ISS A, APPROVED EA 6-5730-114859.SDR 08FDEA01071Frame · dentedFOUND DENT AT C74, P26-27 LT/RT REPAIR PERFORMED BY REWORK OF FRAME OUTER FLANGE AT P26 LT/RT, NDT FOR CRACK FREE IAW RAS/EFW/9000010/2008 ISS A, APPROVED BY EA 6-5318-114865SDR 08FDEA01019Skin Panel · misrepairedOLD REPAIR C 36-37, P 13-14 RT IS NOT PERFORMED IAW RAS/DABRE/7002005/2002. DOUBLER REPAIR RENEWED IAW RAS/DABRE/7009016/20008 ISS B AND DRAWING R5370627, APPROVED BY EA 6-5314-115238.SDR 08FDEA01018Crossbeam · corrodedFOUND CORROSION AT CROSS BEAM C 63 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.SDR 08FDEA00928Skin · misrepairedEXISTING REPAIR ON LT SLAT NR 2, LEADING EDGE AREA INBOARD END, WITH MIS-DRESSED HOLES FOUND. REPAIR PERFORMED BY INSTALLING A DOUBLER IAW RAS /FOK/320/2008 ISS A, APPROVED BY EA 6-5743-114857.SDR 08FDEA00927Flap Track · crackedCRACKS FOUND IN HOLE 15 FLAP TRACK BEAM 2 LT. REPAIR PERFORMED BY INSTALLING SB 57-6006 (OVERSIZING AND COLD WORKING OF HOLES), APPROVED BY EO 6-5750-7-3000 PT 1.SDR 08FDEA00926Flange · chafedFOUND CHAFING MARKS ON C 50, P50LH ON AFT FLANGE. REPAIR PERFORMED BY REPLACEMENT OF FLANGE IAW SRM 53-15-87.SDR 08FDEA00813Panel · damagedFOUND DOUBLE HOLES IN TORSION BOX SHEET C 59-60, P 44-46 RT. REPAIR PERFORMED BY CUT OUT THE TORSION BOX AND INSTALLING A SPLICE IAW. SRM 53-17-18 FIG.206.SDR 08FDEA00812Panel · damagedFOUND TORSION BOX PANEL C 63-64, P44-46RH DAMAGED. REPAIR PERFORMED BY SPLICE PLATE REPAIR IAW SRM 53-17-18, FIG 206.SDR 08FDEA00811Skin · dentedDENT WITH CRACK FOUND AT AFT CARGO DOOR SKIN PLATE REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING A DOUBLER IAW/RAS/DAHAM/4024234/2008 ISS A, APPROVED BY EA 6-5230-115241.SDR 08FDEA00695Sill · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL BEAM C63-63A. REPAIR PERFORMED BY REMOVAL OF CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/900011/2008 ISS A, APPROVED BY EA 6-5317-114871.SDR 08FDEA00694Rib · wornFOUND WEAR IN RT MLG RIB 5 LUGS, FORWARD RIB 5 REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALLING OVERSIZE BUSH IAW DRAWING R572-49221.SDR 08FDEA00693Gusset · corrodedCORROSION FOUND ON GUSSET LT FWD PAX DOOR CUT OUT LOWER AFT CORNER. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00657Skin · chafedPREVIOUS REPAIR IN AREA OF STATIC PORTS FOUND. REPAIR PERFORMED BY REWORK TO MINIMUM SKIN THICKNESS OF 1.04MM IAW RAS/DABRE/7009009/2008 ISS B, APPROVED BY EA 6-5314-115247.SDR 08FDEA00612Failsafe · corrodedCORROSION FOUND ON LT FWD DOOR FAIL/SAFE RING, LOWER AFT CORNER. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION IAW. RAS 70503237/006/2008 ISS A, APPROVED BY EA 6-5312-114886.SDR 08FDEA00609Skin · corrodedCORROSION FOUND ON RT WING BOTTOM SKIN IN RIB 8 AND STRINGER 18 AREA. REPAIR PERFORMED BY BLEND OUT OF CORROSION, NDT FOR CRACK FREE AND OVERSIZING OF FASTENER IAW RAS/BAE/1006317/2008 ISS A, APPROVE DBY EA 6-5720-114868.SDR 08FDEA00608Skin · corrodedCORROSION FOUND ON RT WING BOTTOM SKIN RIB 1-2 AND REAR SPAR AND AFT OF REAR SPAR. REPAIR PERFORMED BY REWORK OF CORROSION AND OVERSIZING THE HOLES IAW RAS/BAE/1006320/2008 ISS A, APPROVED BY EA 6-5720-114867.SDR 08FDEA00561Skin Panel · dentedFOUND DENT ON SKIN C 15A-16, P 33 LT. REPAIR PERFORMED BY DRESS OUT THE DENT AND NDT FOR CRACK FREE CONDITION IAW RAS 70502446/009/2008 ISS A, APPROVED BY EA 6-5312-114873.SDR 08FDEA00508Beam · damagedFOUND AT AFT PAX DOOR LT UNDER BEAM 8 FRAME SEGMENT DAMAGED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00407Plate · misrepairedFOUND 2 SHEAR PLATES AT C 79-80, P 26 LT/RT NOT CONFORM TO SRM 53-18-18 FIG 4. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00406Plate · chafedSCRUB MARKS AT RT EMERGENCY EXIT COVER PLATE. REPAIR PERFORMED BY REWORK OF DAMAGE, NDT FOR CRACK FREE CONDITION, FLAP PEENING IAW RAS/EFW/9000009/2007 ISS A, APPROVED BY EA 6-5316-114863.SDR 08FDEA00405Floorbeam · corrodedCORROSION AT TOP CAP BEAM C30 RT, C35 RT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.SDR 08FDEA00404Stringer · chafedFOUND DEEP SCRATCH AT STRINGER 38 LT, C58-59. SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.SDR 08FDEA00403Stringer · corrodedFOUND CORROSION AT STRINGER 53 RT, C28-29. SPLICE REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201.SDR 08FDEA00402Stringer · corrodedCORROSION AT STRINGER 51 LT, C57.2-57.3 SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.SDR 08FDEA00401Floorbeam · corrodedCORROSION AT TOP CAP BEAM, C57, Y-450. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.SDR 08FDEA00400Floorbeam · corrodedCORROSION AT TOP CAP BEAM, C63, Y1470 REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.SDR 08FDEA00399Stringer · corrodedCORROSION ON STRINGER P 54 LT, C 61-64 REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.SDR 08FDEA00398Floorbeam · corrodedCORROSION ON TOP CAP BEAM C 57.2, Y 480 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.SDR 08FDEA00397Attach Fitting · corrodedCORROSION ON ATTACH FITTING TO TOP CAP BEAM, C 61 REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10.SDR 08FDEA00396Floorbeam · corrodedCORROSION ON TOP CAP BEAM C61 REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10.SDR 08FDEA00395Fitting · corrodedCORROSION ON CORNER FITTING C 35 LT REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10.SDR 08FDEA00394Floorbeam · corrodedCORROSION FOUND ON TOP CAP BEAM C 62 LT, Y450. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 208.SDR 08FDEA00392Stringer Clip · corrodedSTRINGER COUPLING C 65, P52 LT CORRODED. REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10.SDR 08FDEA00391Stringer Splice · corrodedSTRINGER COUPLING C 19, P46 AND 48 LT CORRODED REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10.SDR 08FDEA00384Floor Support · corrodedCORROSION ON FLOOR SUPPORT C 11-17, Y-1456 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00383Floor Support · corrodedCORROSION FOUND ON FLOOR STRUCTURE C 11-14, Y730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00382Floor Support · corrodedCORROSION FOUND ON FLOOR STRUCTURE C 11-14, Y-730, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA00381Web · crackedFOUND CRACKS AT C 47 IN WEBS BETWEEN TRACK 3-4 LT/RT. CRACK LENGTH TRACK 3-4 LT: 6 MM, TRACK 3-4 RH: 13MM. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/AS/003/2008 ISS A, APPROVED BY EA 6-5315-114876.SDR 08FDEA00380Web · crackedFOUND CRACKS AT C 47 IN WEBS BETWEEN TRACK 1-2 LT/RT. CRACK LENGTH TRACK 1-2 LH: 10MM, TRACK 1-2 RT: 13MM REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/AS/003/2008 ISS A, APPROVED BY EA 6-5315-114876.SDR 08FDEA00372Skin · crackedCRACKED HOLES FOUND DURING ACCOMPLISHMENT OF EO6-5750-7-5000 AT RIB 7, INNER FLAP LT AND DAMAGED NOSE SKIN JOINT STRIP. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AT HOLE ON RIB 7 AND REMOVAL OF CRACK AT NOSE SKIN JOINT STRIP IAW RAS/FOK/015/2008 ISSUE ASDR 08FDEA00364Skin · crackedDENT AND CRACK FINDING ON RT CENTER FLAP TRAILING EDGE LOWER SKIN. REPAIR PERFORMED BY INSTALLING A EXTERNAL PATCH IAW RAS/FOK/011/2008, APPROVED BY EA 6-5753-114875.SDR 08FDEA00349Fitting · corrodedFOUND CORRODED CORNER FITTINGS AT C27 LT AND RT, CARGO FLOOR STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF CORNER FITTINGS IAW SRM 51-72-10.SDR 08FDEA00319Fitting · damagedCENTER WING-TOOL MARK AND DAMAGED FASTENERS AT C 47 RT AFT FACE AT P26 REPAIR PERFORMED BY REWORK OF TOOL MARKS, HFEC INSPECTION FOR CRACK FREE AND REMOVAL OF AFFECTED FASTENERS WITH HL112VF8 IAW, RAS 057234/008/2007 ISS A , APPROVED BY EA 6-5710-114864.SDR 08FDEA00308Diaphragm · scratchedFOUND SCRATCHES ON BOTTOM SKIN OF DIAPHRAGM AT TRACK 4-5 LT, C48. REPAIR PERFORMED BY REWORK THE SCRATCHES IAW RAS 057541/004/2008 ISS A AND EA 5-5315-114877.SDR 08FDEA00307Diaphragm · dentedFOUND DENTS IN PRESSURE DIAPHRAGM AT TRACK 3-5,C48-54 LT AND TRACK 4-5, C51-53 RT REPAIR PERFORMED BY NDT-INSPECTION FOR CRACK FREE CONDITION AND LET THE DENTS AS IT IS IAW RAS 057541/004/2008 ISS A AND EA 6-5315-114877.SDR 08FDEA00306Rib · damagedFOUND ON RT INNER FLAP LOWER SKIN RIB 18-19 AN OLD DOUBLER REPAIR WITHOUT ANY DOCUMENTATION DOUBLER REPAIR RENEWED IAW RAS/FOK/006 2008 ISS A, APPROVED BY EA 6-5752-114854.
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