N750FD

Service difficulty reports · 260

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 = 'N750FD' 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.

SDR FDEA200901290367Attach Fitting · crackedFOUND ATTACHMENT FITTING FOR CROSSBEAM C 61 RT CRACKED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200901290366Floorbeam · corrodedFOUND CORRODED CROSSBEAM C 61 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290365Stringer · corrodedFOUND CORRODED STRINGER P44 , C65 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200901290364Floorbeam · corrodedFOUND CORRODED CROSS BEAM C 66. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290363Frame · damagedFOUND ON C 73 NO GAP BETWEEN FRAME AND STRINGER REPAIR PROFILE IN AREA OF FLUSH SKIN REPAIR. REPAIR PERFORMED BY CUT THE FRAME AT C 73 BETWEEN P56LH-56RH AND REPAIR IAW SRM 53-10-13 FIG 203 AND REPLACE THE STRINGER COUPLING IAW DRAWING R539-70631.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200901290362Fitting · corrodedFOUND CORRODED CORNER FITTING AT C 32 LT IN FORWARD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAT SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901290361Flange · damagedFOUND OVERSIZED HOLES AT UPPER FLANGE C 32 LT, C 38.1 AND C 30 RT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901290360Flange · damagedFOUND OVERSIZES HOLES AT UPPER FLANGE C 34 LT/RT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901190237Doubler · corrodedFOUND CORROSION ON TCAS DOUBLER C20-21 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 19, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200901190236Crossbeam · damagedTO LESS EDGE DISTANCE IN CROSS BEAM COUPLING AT C 64 RT REPAIR PERFORMED BY REPLACEMENT OF 2 ANGLES IAW SRM 51-72-10.Jan 19, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Structure
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