N751FD

Service difficulty reports · 308

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 = 'N751FD' 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 FDEA200906252298Window Frame · corrodedFOUND CORRODED ATTACHMENT HOLES IN LT AND RT WINDSHIELD FRAMES. REPAIR PERFORMED BY OVERSIZING SOME HOLES, NDT FOR CRACK FREE CONDITION AND BUSHING INSTALLATION IAW RAS 70520006/039/2009 ISS.A, APPROVED BY EA 6-5310-131202Jun 25, 2009 · N751FD · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA200906152107Skin · corrodedFOUND CORROSION ON SKIN C 39-40, P 27 -28 LT. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS 70519745/010/2009 ISSA., APPOVED BY EA 6-5310-129195.Jun 15, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906091998Beam · corrodedFOUND CORROSION ON BEAM FOR KRUEGER FLAP STRUCTURE RHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.Jun 9, 2009 · N751FD · Airbus A300B4622R · Wing Main, Frame StructureSDR FDEA200906091997Skin · dentedFOUND DENT AND SCRATCHES AT P16RH, C 94-95 REPAIR PERFORMED BY BLEND OUT THE SCRATCHES IAW RAS/EFW/9000189/2009 ISS.A , APPROVED BY EA 6-5310-129189.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906091996Structure · chafedFOUND CHAFING MARKS ON CROSS SHEET OF RT EMERGENCY EXIT AT P 15, C 57A-57.1 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000177/2009 ISS.A , APPROVED BY EA 6-5310-120192.Jun 9, 2009 · N751FD · Airbus A300B4622R · Emergency ExitsSDR FDEA200906091995Skin · damagedFOUND NONRECORDED SKIN REPAIR ON C 38.1-39, P 43-47 LT. OLD REPAIR REMOVED AND THE SKIN PANEL PARTIALLY REPLACED IAW. DWG R539-06915, ISS. B, APPROVED BY RAS/EFW/9000180/2009 AND EA 6-5310-129199.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906091994Stringer · corrodedFOUND CORROSION ON STRINGER P 50, C 57.3-58. SPLICE REPAIR PERFORMED IAW. RAS/EFW/9000190/2009 ISS. A, APPROVED BY EA 6-5310-129188.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906091993Skin · dentedFOUND DENT IN THE FUSELAGE SKIN BUTT JOINT P 39RH, C 18-20. REPAIR PERFORMED BY REPLACING A SECTION OF BUTT STRAP AND INSTALLING A DOUBLER IAW DWG R537-06916 AND RAS/DAHAM/402759/2009 ISS. A, APPROVED BY EA 6-5330- 129193.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906091992Frame · corrodedFOUND CORROSION ON REAR SLANTING FRAME AT C53, P 41-42. REPAIR PERFORMED BY REWORK OF CORROSION AND NDT FOR CORROSION FREE CONDITION IAW. RAS 70521674/009/2009 ISS. A, APPROVED BY EA 6-5310-120193.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200906091991Skin · corrodedFOUND CORROSION ON FUSLAGE SKIN AROUND DME ANTENNA 2. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING A DOUBLER IAW. RAS/EFW/9000192/2009 ISS. A, APPROVED BY EA 6-5330-129162.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906091990Attach Fitting · corrodedFOUND CORROSION ON ATTACH FITTING FOR KRUEGER FLAP STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 9, 2009 · N751FD · Airbus A300B4622R · Wing, Control Surface Attach FittingsSDR FDEA200906091988Window Frame · corrodedFOUND CORROSION ON RT SLIDING WINDOW FRAME AT STATIC DISCHARGERS REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CORROSION FREE CONDITION IAW RAS 70521635/005/2009 ISS.A, APPROVED BY EA 6-5310-131221.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906091987Beam · corrodedFOUND CORROSION ON LT LOWER EDGE BEAM C 88-90, P28LT REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CORROSION FREE CONDITION IAW RAS/EFW/9000204/2009 ISS.A , APPROVED BY EA 6-5310-131209.Jun 9, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906041922Frame · gougedFOUND A GOUGE IN OUTER FLANGE OF FRAME 47 NEAR P26 LT. REPAIR PERFORMED BY REWORK OUTER FLANGE AT RUN OUT TO ELIMINATE THE GOUGE AND NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000182/2009 ISS. A, APPROVED BY EA 6-5310-131203.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200906041923Doubler · corrodedFOUND CORROSION ON CORNER DOUBLER ON PAX DOOR FRAME SHELL C75A-76, P 26-27 LT. REPAIR PERFORMED BY REWORK ON THE CORROSION, NDT FOR CRACK FREE AND CORROSION FREE CONDITION IAW RAS/EFW/9000184/2009 ISS. A, APPROVED BY EA 6-5310-131204.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906041920Beam · corrodedFOUND CORROSION IN LONGITUDINAL BEAM BETWEEN C 73A-75A, P 26RH REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000184/2009 ISS.A , APPROVED BY EA 6-5310-131205.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906041919Failsafe · damagedFOUND TOOLING MARKS ON LT AFT PAX DOOR FAIL SAFE RING AT C 73A, P26 REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, PERFORM NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000185/2009 ISS A, APPROVED BY EA 6-5310-129192.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906041917Doubler · crackedFOUND CRACK IN REINFORCEMENT DOUBLER ON LOWER SIDE OF DIAPHRAGM BETWEEN GANTRY4-5 AT C 49. REPAIR PERFORMED BY CUT-OUT OF DIAPHRAGM REINFORCING AND INSTALLING A SPLICE WITH FILLER IAW RAS 70520358/012/2009 ISS.A , APPROVED BY EA 6-5310-129200.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906041916Skin · corrodedFOUND CORROSION ON FUSELAGE SKIN C 67, P44-45 RH REPAIR PERFORMED BY BLEND OUT THE CORROSION , PERFORM NDT FOR CORROSION AND CRACK FREE CONDITION IAW RAS/EFW/9000199/2009 ISS. A, APPROVED BY EA 6-5330-129164.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906041915Beam · corrodedFOUND DEEP CORROSION SPOT AT A HOLE IN AFT CARGO DOOR SILL BEAM C 62A-63 REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING A BUSHING IN THE HOLE IAW RAS/EFW/9000205/23009 ISS.A , APPPROVED BY EA 6-5310-129177Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906021888Fitting · crackedFOUND CRACK IN ATTACHMENT FITTING BETWEEN SILL STRUCTURE AND CROSS BEAM C59RH. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200906021896Stringer · corrodedFOUND CORROSION ON STRINGER P 48, C 61-64 LT STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14 FIG 201.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906021891Doubler · damagedFOUND IN THE AREA OF KRUEGER FLAP, THE DOUBLER ON SKIN C38--38.1, P 30-34 WITH FOUR REWORKED AREAS NOT PERFORMED IAW SRM 51-74-10. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906021890Floorbeam · damagedFOUND NON RECORDED TOP CAP BEAM REPAIR AT C 27, LT. SPLICE REPAIR RENEWED IAW SRM 53-10-15 FIG.207.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200906021889Floor Support · corrodedFOUND CORROSION ON BEAM 10 , C 67-69, P 45-47 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200906021887Floorbeam · corrodedFOUND CROSS BEAM C 62 IN BAD CONDITION (CORROSION SPOTS, OLD REWORKS) REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200906021886Floorbeam · corrodedFOUND CORROSION SPOTS ON CROSS BEAM C 63 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200906021885Floorbeam · damagedFOUND WRONG MATERIAL NEEDED FOR CROSS BEAM AT C 66 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200906021884Stringer · corrodedFOUND CORROSION ON STRINGER P 51RH, C 63-64 STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906021883Stringer · corrodedFOUND CORROSION ON STRINGER P 48, C 69-71 STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906021882Stringer · corrodedFOUND CORROSION ON STRINGER P 51, C 71-72 STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906021881Stringer · corrodedFOUND CORROSION ON STRINGER P 56, C 69-74 STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG.201Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906021880Skin · dentedFOUND DEEP DENT ON KRUGER FLAP NOSE SKIN REPAIR PEFORMED BY REPLACEMENT OF PART IAW. SRM 57-45-12.Jun 2, 2009 · N751FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA200906021879Skin · damagedFOUND AN OLD REWORK IN SKIN , C73, P 55 RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 225.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906021878Seat Track · crackedFOUND CRACK AT TRACK 5 RT, C51A DOUBLER REPAIR PERFORMED IAW DRAWING R538-10583.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906021877Frame Splice · chafedFOUND CHAFING MARK IN FRAME SPLICE C 18 LT. REPAIR PEFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200906021876Fitting · damagedFOUND TOOLING MARK ON CONNECTING FITTING C 91 LT. REPAIR PEFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200906021874Fitting · corrodedFOUND CORROSION ON CORNER FITTING C58RH. REPAIR PEFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200906021870Fitting · corrodedFOUND CORROSION ON CORNER FITTING C 63 LT IN AFT CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200906021869Floorbeam · corrodedFOUND CORROSION ON SHORT CROSS BEAM C 63 RT IN AFT CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 2, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200905281833Floorbeam · damagedFOUND NON RECORDED CROSSBEAM REPAIR C 57RH, AD-Y-805. SPLICE REPAIR RENEWED IAW SRM 53-10-15 FIG 208.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200905281832Skin · damagedFOUND AN EXISTING BLEND OUT AREA AT C57, P 26RT REPAIR PERFORMED BY POLISHING TO SMOOTH FINISH AND NDT FOR CRACK FREE CONDTION IAW. RAS/EFW/9000179/2009 ISS. A, APPROVED BY EA 6-5310-129143May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200905281831Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 56LT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200905281830Frame · damagedFOUND EXISTING BLEND OUT AREA ON C 56A, P 13RH. REPAIR PERFORMED BY POLISHING TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000176/2009 ISS.A , APPROVED BY EA 6-5310-129161.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200905281829Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 58 LT AND RT SPLICE REPAIRS PERFORMED IAW SRM 53-10-15 FIG 207.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200905281828Stringer · damagedFOUND TOOLING MARKS ON STRINGER P 14RH, C 57-57.1. REPAIR PERFORMED BY BLEND OUT AND NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000178/2009 ISS A, APPROVED BY EA 6-5310-129163.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200905281827Floorbeam · corrodedFOUND CORROSION ON SHORT CROSSBEAM C 67 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.May 28, 2009 · N751FD · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905281826Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 67 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 28, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200905281825Stringer · corrodedFOUND CORROSION ON STRINGER P 44 LT, C 37. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.May 28, 2009 · N751FD · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA200905281824Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT C 12A-17, Y1959 SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207.May 28, 2009 · N751FD · Airbus A300F4605R · Fuselage Miscellaneous Structure
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