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 FDEA200903020776Fitting · corrodedFOUND CORROSION ON CORNER FITTING C 58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Mar 2, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902250714Stringer · corrodedFOUND CORROSION ON STRINGER P 51, C 70-71. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902250713Stringer · corrodedFOUND CORROSION ON STRINGER P 55, C 72-73. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902250712Stringer · corrodedFOUND CORROSION ON STRINGER P 54, C 70-71. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902250711Stringer · corrodedFOUND CORROSION ON STRINGER P 45, C 71-72. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902250710Skin · corrodedFOUND CORROSION ON SKIN PANEL C 39-40, P 28-29 RT REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT INSPECTION IAW RAS 70517297/005/2008 ISS A.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200902250709Skin · corrodedFOUND SKIN CORROSION AND A MISPLACED HOLE AT C 38-38.1, P 29-30 RT. REPAIR PERFORMED BY CORROSION REMOVAL AND INSTALLING NEW AND OVERSIZED FASTENER IAW RAS/EFW/9000151/2008 ISS A, APPROVED BY EA 6-5310-120214.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200902250708Skin · damagedFOUND A FASTENER WITH TO SHORT EDGE DISTANCE IN FUSELAGE SKIN AT C 68, P 32-33 RT. DOUBLER REPAIR PERFORMED IAW RAS/EFW/9000149/2008 ISS A, APPROVED BY EA 6-5310-120183.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200902250707Skin · corrodedFOUND CORROSION ON SKIN , C57, P 13 LT BEHIND THE LIMIT. DOUBLER REPAIR PERFORMED IAW RAS/EFW/9000154/2008 ISS A, APPROVED BY EA 6-5330-120222.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200902250706Fitting · damagedFOUND ON MANHOLE INTEGRAL FITTING C 38 OLD TEMPORARY REPAIR (MANHOLE FITTING CHANGE) IAW RAS/DABRE/7006140/2006 ISS C. THE REPAIR WAS UPDATED IN A PERMANENT REPAIR BY SOME FASTENER CHANGES IAW RAS/DAHAM/4026700/2008 ISS B, APPROVED BY A 6-5310-120167.Feb 25, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200902250705Stiffener · crackedFOUND CRACK IN CENTER SPAR CUTOUT IN STIFFENER, C 44, IN HOLE NR 3 REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND PERFORMING NDT IAW RAS 70517477/009/2009 ISS A, APPROVED BY EA 6-5710-120225.Feb 25, 2009 · N750FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200902240697Floor Support · corrodedFOUND CORROSION ON SILL BEAM C 24A-26, P 42-43 RT. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND REWORK THE HOLES IAW RAS/EFW/9000155/2008, APPROVED BY EA 6-5310-120217.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902240696Floorbeam · corrodedFOUND TOP CAP BEAM HEAVY CORRODED ON C 60 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200902240695Beam · corrodedFOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT IN BEAM A537-10004-204. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS /EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200902240694Support · corrodedFOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT ON SKIN REINFORCEMENT A537-10007-206. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS /EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902240693Skin · corrodedFOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT ON SKIN PANEL A537-76533-000. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS/EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200902240691Floorbeam · corrodedFOUND CORROSION ON CROSS BEAM C 58 RT SLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 A.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200902240690Rib · dentedFOUND 2 DENTS ON LEADING EDGE RIB 12-13 OF CENTER FLAP LT PATCH REPAIR PERFORMED IAW SRM 57-50-00 FIG 208.Feb 24, 2009 · N750FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200902240689Fitting · corrodedFOUND CORNER FITTING C 63 LT CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902240688Stringer · corrodedFOUND CORROSION ON STRINGER P45,C 72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902240687Stringer Splice · corrodedFOUND STRINGER COUPLING ON C 72 , P45 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902240686Stringer Splice · corrodedFOUND STRINGER COUPLING ON C 65 , P44 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902240685Fitting · corrodedFOUND CORNER FITTING ON C 65 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 24, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902240684Attach Fitting · corrodedFOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018, APPROVED BY EA 6-5450-120174.Feb 24, 2009 · N750FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR FDEA200902240683Attach Fitting · corrodedFOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018.Feb 24, 2009 · N750FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR FDEA200902060474Failsafe · damagedFOUND TOOLMARK AT FAIL SAFE RING FRAME C 73A - 74, P26 RT REPAIR PERFORMED BY REWORK OF TOOLMARK IAW RAS/EFW/9000156/2008 ISSUE A, APPROVED BY EA 6-5310-120203.Feb 6, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200902050460Profile · corrodedFOUND CORROSION ON PROFILE C63-64, LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 5, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200902040446Beam · corrodedIN KRUEGER FLAP AREA, WING LE ON BEAM HEAVY CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 4, 2009 · N750FD · Airbus A300B4622R · Wing Main, Frame StructureSDR FDEA200902040445Support · corrodedFOUND IN KRUEGER FLAP AREA , ON WING LE A SUPPORT CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 4, 2009 · N750FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200902040444Fitting · crackedFOUND CRACK AT GANTRY 3 RT, C 49 REPAIR PERFORMED BY DOUBLER INSTALLATION IAW DRAWING R538-10581.Feb 4, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200902040443Fitting · crackedFOUND CRACK AT GANTRY 3 RT, C 49 REPAIR PERFORMED BY DOUBLER INSTALLATION IAW DRAWING R538-10581.Feb 4, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200902030430Stringer · corrodedFOUND CORROSION ON STRINGER P 53, C 57.1-57.2 OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW RAS/EFW/9000146/2008 ISS A, APPROVED BY EA 6-5310-120179.Feb 3, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200902030429Doubler · corrodedFOUND CORROSION AT INNER DOUBLER C 72-73, P 42 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 3, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200901300404Floorbeam · corrodedFOUND CORROSION SPOTS ON CROSSBEAM C 62 OUT OF SRM LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901300402Floorbeam · corrodedFOUND CROSSBEAM C 64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901300401Attach Fitting · corrodedFOUND IN AFT CARGO COMPARTMENT FITTING FOR ATTACHMENT OF LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200901300400Profile · corrodedFOUND IN AFT CARGO COMPARTMENT LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901300399Profile · corrodedFOUND IN AFT CARGO COMPARTMENT LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901300398Stringer Splice · corrodedFOUND CORRODED STRINGER COUPLING AT C 19, P 50 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 30, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200901290378Stringer · corrodedFOUND CORRODED STRINGER P 44 RT, C 33-34 SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200901290377Floorbeam · corrodedFOUND CORRODED CROSSBEAM C 69 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290376Floorbeam · corrodedFOUND CORRODED SHORT CROSSBEAM C 63 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290375Fitting · damagedFOUND DAMAGED LONGITUDINAL PROFILE C 66-67 , Y-805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200901290374Profile · damagedFOUND DAMAGED LONGITUDINAL PROFILE C 67, Y 90. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901290373Profile · corrodedFOUND DAMAGED LONGITUDINAL PROFILE C 66 , Y 805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901290372Floorbeam · corrodedFOUND CORRODED CROSSBEAM C 67 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290371Floorbeam · corrodedFOUND CORRODED CROSSBEAM C 67. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200901290370Profile · corrodedFOUND CORRODED LONGITUDINAL PROFILE C 67-69 RT AT BCD-CUT OUT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200901290369Fitting · corrodedFOUND CORRODED CORNER FITTING C 65 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200901290368Floorbeam · corrodedFOUND CORRODED CROSSBEAM AT C 63, Y 1100MM SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jan 29, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, Floor Beam
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