N742FD

Service difficulty reports · 203

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 = 'N742FD' 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 08FDEA02703Skin · damagedAFTER REMOVAL OF OLD DOUBLER REPAIR IAW DR 276 FOUND STRINGER 2.9 DAMAGED AT LT INNER FLAP. REPAIR PERFORMED IAW RAS/FOK/150/2008 ISS C, APPROVED BY EA 6-5752-123003.Jul 4, 2008 · N742FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02702Skin · damagedFOUND OLD DOUBLER REPAIR ON LT INNER FLAP LOWER SKIN BETWEEN RIB 1C-4 NOT PERFORMED IAW RAS/FOK/140/2002 (DOUBLER THICKNESS). REPAIR RENEWED IAW RAS/FOK/150/2008 ISS C, APPROVED BY EA 6-5752-123003.Jul 4, 2008 · N742FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02701Fitting · damagedFOUND DAMAGE AT HOLE H CENTER TANK FITTING C 47 RT REPAIR PERFORMED BY REAM UP UNTIL DAMAGE REMOVAL, NDT FOR CRACK FREE AND SPOTFACING IAW RAS 70510800/026/2008 ISS A, APPROVED BY 6-5710-120111.Jul 4, 2008 · N742FD · Airbus A300B4622R · Wing, Attach FittingsSDR 08FDEA02700Frame · damagedFOUND MISDRILLED HOLE AT C 75A, P26 LT. REPAIR PERFORMED BY INSTALLING A BUSH IAW RAS/EFW/9000050/2008 ISS B, APPROVED BY EA 6-5318-120121.Jul 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA02699Stringer · corrodedFOUND CORROSION AT STRINGER P 52 LT, C 54.3-55. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FLAP PEENING IAW RAS/EFW/9000056/2008 ISS A, APPROVED BY EA 6-5316-123004.Jul 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02698Stringer · corrodedFOUND CORROSION AT STRINGER P 53 LT, C 54.3-55. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FLAP PEENING IAW RAS/EFW/9000055/2008 ISS A, APPROVED BY EA 6-5316-123004.Jul 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02697Stringer · corrodedFOUND CORROSION AT STRINGER P 56 LT, C 55-58. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FLAP PEENING IAW RAS/EFW/9000048/2008 ISS A, APPROVED BY EA 6-5316-120115.Jul 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02696Spar · crackedFOUND CRACK ON PYLON NR 2 LOWER SPAR UPPER SURFACE, RIB 10A. REPAIR PERFORMED IAW DRAWING R546-10344 AND RAS/70507447/004/2008 ISS A, APPROVED BY EA 6-5450-120039.Jul 4, 2008 · N742FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA02695Skin Panel · corrodedFOUND CORROSION ON LT WING TOP SKIN, REAR SPAR AREA RIB 25-29 REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CRACK FREE IAW RAS/BAE/1007272/2008 ISS A, APPROVED BY EA 6-5720-120108.Jul 4, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02694Strap · unknownFOUND OLD REPAIR ON RT AFT PYLON BOX NOT PERFORMED IAW DRAWING R546-10314. REPAIR RENEWED IAW DRAWING R546-10314 AND RAS 034632/010/2004 ISS A, APPROVED BY EA 6-5451-120101.Jul 4, 2008 · N742FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA02693Skin Panel · corrodedFOUND CORROSION ON SKIN PANEL AT EMERGENCY EXIT C56A-57A, P15 LT REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000045/2008 IIS.B, APPROVED BY EA 6-5316-120052.Jul 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02562Support · corrodedFOUND CORROSION ON SUPPORT C11-19 Y-1456 AND Y1959 SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207.Jun 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02561Floorbeam · chafedFOUND CORROSION ON FLANGE C12A-13A, Y - 730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02560Support · corrodedFOUND CORROSION ON SUPPORT C11-14, Y 730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02559Support · corrodedFOUND CORROSION ON SUPPORT C11-14, Y-730 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02383Channel · damagedFOUND A DOUBLE HOLE IN LT WING TIP END RIB CHANNEL. REPAIR PERFORMED BY OVERSIZING, PLUGGED THE HOLE AND FASTENER INSTALLATION AT ORIGINAL LOCATION IAW RAS /BAE/1007232/2008 ISS A, APPROVED BY EA 6-5730-120058.Jun 23, 2008 · N742FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA02352Strut · corrodedFOUND CORROSION SPOTS AT AFT FACE OF LT CROSS STRUT C85 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-00.Jun 20, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02322Spar · crackedFOUND CRACKED FASTENER HOLE IN CENTER SPAR WEB C 44. REPAIR PERFORMED BY CUT OUT THE DOUBLER, ROTOTEST FOR CRACK FREE CONDITION AND REAM UP UNTIL CRACK REMOVAL IAW RAS 70507029/021/2008 ISS A, APPROVED BY EA 6-5710-120043.Jun 19, 2008 · N742FD · Airbus A300B4622R · Wing SparSDR 08FDEA02321Skin · chafedFOUND 2 CHAFING MARKS AT LT OUTER FLAP TOP SKIN, RIB 3A-4 AND 14A-15A REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION AND INSTALLING NEW CHAFING PLATES IAW RAS/FOK/131/2008 ISS A, APPROVED BY EA 6-5754-120125.Jun 19, 2008 · N742FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02320Sill · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL BEAM REPAIR PERFORMED BY CUT OUT OF DAMAGED SILL BEAM AND REPAIR IAW SRM 53-17-18 PB 201, APPROVED BY RAS/DAHAM/4024836/2008 ISS A AND EA 6-5317-120050.Jun 19, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02172Profile · corrodedFOUND CORROSION ON LONGITUDINAL PROFILE C 63-64, Y140. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02175Coupling · damagedFOUND A GAP BETWEEN COUPLING AND FRAME 65 RT, P21 REPAIR PERFORMED BY REMOVING THE COUPLING AND REPLACE IAW SRM 51-72-10.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02174Stiffener · chafedFOUND CHAFING MARK AT VERTICAL MEMBER Y-1456, Z-1870 REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION IAW RAS 70510754/009/2008 ISS A, APPROVED BY EA 6-5315-120112.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02173Stringer · corrodedFOUND CORROSION AT STRINGER P55, C 64-65. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02171Floorbeam · corrodedFOUND CORROSION ON CROSS BEAM PROFILE C 67RHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02170Web · corrodedFOUND CORROSION ON WEB C 64, P56-56`. REPAIR PERFROMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 6, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02142Skin · damagedFOUND SCRATCHES AND NICKS ON FUSELAGE SKIN C 79-80, BELOW P 26 LHS. REPAIR PERFORMED BY REWORK OF DAMAGED AREA IAW SRM 51-73-10, NDT FOR CRACK FREE, APPROVED BY RAS/DAHAM/4024994/2008 ISS A AND EA 6-5318-120119.Jun 4, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02131Skin · damagedFOUND 2 NICKS ON TOP SKIN C 46-47, TRACK 4-5 RT REPAIR PEFORMED BY SMOOTH BLEND OUT, SPOTFACING AND NDT FOR CRACK FREE CONDITION IAW RAS 70507169/004/2008, APPROVED BY EA 6-5710-120053.Jun 3, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02130Diaphragm · damagedFOUND TOOLING MARKS ON DIAPHRAGM C47-54, TRACK 5 LT-5 RT. REPAIR PERFORMED BY BLEND OUT THE TOOLING MARKS, NDT FOR CRACK FREE. INSTALLING A DOUBLER AT C53-54, BEAM 1-2 RT IAW RAS 70510882/020/2008, APPROVED BY EA 6-5315-120114.Jun 3, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02121Web · corrodedFOUND CORRODED WEB AT PAX DOOR 4 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 3, 2008 · N742FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA02119Skin · dentedFOUND OLD DENT ON FUSELAGE C 73-74, P 45-46 LT OUT OF LIMIT IAW SRM 53-10-12. DOUBLER REPAIR PERFORMED SRM 53-10-12 FIG 225.Jun 3, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02118Skin · damagedFOUND OLD BUSHING REPAIR ON FUSELAGE SKIN C 83, P 5 LT WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REMOVING OF BUSHING, CHECK THE HOLE AND INSTALL BUSH IAW SRM 53-10-12 FIG 221.Jun 3, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02117Floorbeam · corrodedFOUND CORROSION SPOTS ON CROSS BEAM C 72, C 46-46`. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 3, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02116Failsafe · corrodedFOUND CORROSION ON LT FWD PAX DOOR FAIL/SAFE RING IN TWO AREAS (C 14 AND C16 LOWER CORNER). REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10, NDT FOR CRACK FREE CONDITION AND INSTALLING 1ST OVERSIZED FASTENER IAW RAS 70507043/009/2008 ISS A, APPROJun 3, 2008 · N742FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA02115Floorbeam · corrodedFOUND CORROSION ON UPPER FLANGE C 27 RT BETWEEN OUTER STRUT AND CORNER FITTING. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jun 3, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02114Fitting · damagedFOUND TOOLING MARKS ON PICK UP FITTING GANTRY 5 LT, C 47 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 3, 2008 · N742FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA02042Floorbeam · corrodedFOUND CORROSION ON OLD TOP CAP BEAM C 32 LT, TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 FIG 207.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02041Floorbeam · corrodedFOUND CORROSION ON TOP CAP BEAM C 35 RT BETWEEN OUTER STRUT AND CORNER FITTING TOP CAP BEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02049Profile · corrodedFOUND CORROSION ON LONGITUDINAL PROFILE C 67-69,P 45 RT, BCD CUT OUT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02048Beam · corrodedFOUND CORROSION ON BEAM 10 C 67-69,P 45 RT, BCD CUT OUT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02047Structure · corrodedFOUND CORROSION ON BULK CARGO DOOR CUT OUT C 67-69, P 44-48 RT ON SEALING SECTION REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02046Door Frame · corrodedFOUND CORROSION ON BULK CARGO DOOR CUT OUT C 67 -69, P 44-48 RT ON SECTION BEAM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02045Floorbeam · corrodedFOUND ON CROSS BEAM C 63 LT HEAVY CORROSION, CROSS BEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02044Floorbeam · corrodedFOUND OLD TOP CAP BEAM REPAIR WITH NEW CORROSION TOP CAP REPAIR RENEWED IAW SRM 53-10-15 FIG 207.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02043Frame · chafedFOUND CHAFING MARKS ON FRAME C 22 RT, P 14-15 OUT OF LIMIT. FRAME REPAIR PERFORMED IAW SRM 53-10-13 FIG 202.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA02040Web · crackedFOUND CRACKS ON INTERNAL WEB BETWEEN BEAM 3 AND 4 LT/RT. REPAIR PERFORMED BY CRACK STOP HOLE AND DOUBLER INSTALLATION IAW RAS 70507081/004/2008, APPROVED BY EA 6-5315-120051.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02039Web · crackedFOUND CRACKS ON INTERNAL WEB BETWEEN BEAM 1 AND 2 LT/RT. REPAIR PERFORMED BY CRACK STOP HOLE AND DOUBLER INSTALLATION IAW RAS 70507081/004/2008, APPROVED BY EA 6-5315-120051May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02038Structure · corrodedFOUND CORROSION ON PAX DOOR 4 LT BOTTOM SEALING SECTION REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 30, 2008 · N742FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA02037None · noneFOUND OLD DOUBLER REPAIR ON FUSELAGE C 73, P45-46 RT DOUBLER REPAIR RENEWED IAW SRM 53-10-12 FIG 228.May 30, 2008 · N742FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02036Stringer · corrodedFOUND CORROSION ON STRINGER P50, C39-41. CORROSION REWORKED AND NDT FPR CRACK FREE CONDITION PERFORMED IAW RAS 70507182/009/2008, APPROVED BY EA 6-5315-120102.May 30, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
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