N745FD

Service difficulty reports · 216

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 = 'N745FD' 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 08FDEA01017Skin Panel · damagedFOUND AN OLD FLUSH REPAIR AT C35, P34-35RH, WHICH IS NOT COMPATIBLE WITH P TO F CONVERSION REPAIR RENEWED (EXTERNAL DOUBLER INSTALLED) IAW. SRM 53-10-12 FIG.225 AND 53-10-14 FIG.201A, APPROVED BY RAS/EFW/9000022/2008 AND EA 6-5314-117137Mar 18, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01015Fitting · corrodedFOUND ON PYLON NR 1 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTING IAW SB 54-6017, APPROVED BY EA 6-5451-114936.Mar 18, 2008 · N745FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA01014Fitting · corrodedFOUND ON PYLON NR 2 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTING IAW SB 54-6017, APPROVED BY EA 6-5451-114936.Mar 18, 2008 · N745FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA01013Doubler · corrodedFOUND CORROSION AT VENTURI OUTLET DOUBLER C72-73, P41-44LT, REPAIR PERFORMED BY REPLACEMENT OF DOUBLER IAW SRM 51-72-10.Mar 18, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA00932Floorbeam · corrodedFOUND TOP CAP BEAM C 35 LT CORRODED. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Mar 14, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA00930Flange · damagedFOUND DAMAGED BEARING SUPPORT FLANGE AT C 68-69, P34 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Mar 14, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA00929Floorbeam · damagedFOUND A DOUBLE HOLE AT CROSSBEAM C 62, Y-405. SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG 207.Mar 14, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA00869Web · crackedFOUND CRACKS ON WEBS BETWEEN TRACK 1-2 LT. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS 70503745/2008 ISS A, APPROVED BY EA 6-5315-115282.Mar 11, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA00868Web · crackedFOUND CRACKS ON WEBS BETWEEN TRACK 3-4 LT/RT, 3-4 LT: 16MM 3-4RH:15MM. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS 70503745/2008 ISS A, APPROVED BY EA 6-5315-115282.Mar 11, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA00677Rib · chafedFOUND CHAFING MARKS ON RT SLAT NR 2 LEADING EDGE, RIB 5-15. REPAIR PERFORMED BY BLEND OUT IAW RAS/FOK/026/2008 ISS A, APPROVED BY EA 6-5743-115268.Mar 3, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA00676Rib · chafedFOUND CHAFING MARKS ON LT WING LEADING EDGE STRUCTURE, SLAT JACK NR 1 INNER RIB HOLE EDGE. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1006441/2008 ISS A, APPROVED BY EA 6-5741-114935.Mar 3, 2008 · N745FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 08FDEA00675Skin · chafedFOUND SEVERAL SCRATCHES ON LT SLAT NR 2 UPPER SKIN TRACK RIB 5 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/025/2008 ISS A, APPROVED BY EA 6-5743-114932.Mar 3, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA00674Diaphragm · dentedFOUND DENTS AND NICKS IN DIAPHRAGMS, C47-48, TRACK 2 LT TO 2 RT REPAIR PERFORMED BY REWORK OF NICK AND NDT FOR CRACK FREE CONDITION IAW RAS/70503778/2008 ISS A, APPROVED BY EA 6-5315-115283.Mar 3, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA00607Skin · corrodedCORROSION ON LT WING BOTTOM SKIN UPPER SURFACE AT RIB 5 AFT OF REAR SPAR. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CRACK FREE CONDITION, FLAP PEENING IAW RAS/BAE/1006416/2008 ISS A, APPROVED BY EA 6-5720-114931.Feb 26, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA00606Skin · chafedCHAFING MARKS FOUND ON LT OUTER WING BOTTOM SKIN REINFORCING PLATE AT RIB 7. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS AND NDT FOR CRACK FREE IAW RAS/BAE/1006409/2008 ISS A, APPROVED BY EA 6-5720-114930.Feb 26, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA00605Doubler · corrodedFOUND KRUEGER FLAP DOUBLER AT C 38, 28-33 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 26, 2008 · N745FD · Airbus A300B4622R · Leading Edge Devices
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