N732FD

Service difficulty reports · 157

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 = 'N732FD' 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 07FDEA02712Frame · dentedSCRATCHED AND DENTED OUTER FLANGE OF C74, P26 RT AND LT. REPAIR PERFORMED BY REWORK SCRATCH AREA AND NOT DRESSING BACK THE DENT IAW RAS/DAHAM/4022387/2007 ISSUE "A" AND EA 6-5318-106496.Aug 2, 2007 · N732FD · Airbus A300B4605R · Fuselage Main, FrameSDR 07FDEA02711Attach Fitting · crackedCRACKED ATTACHMENT FITTING WHICH CONNECTS THE CROSSBEAM AND THE FRAME SEGMENT C60 RHS WITH THE SILLBEAM P/N ATTACH FITTING C60: A539-73610-200-51, ATTACH FITTING C60: A539-73610-200-00 AND ECKBESCHLAG: DR012131-200. REPAIR PERFORMED BY CUT THE TORSION BOX AREAug 2, 2007 · N732FD · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 07FDEA02693Web · crackedSEVERAL CRACKS FOUND ON WEBS, TRACK 1-2 AND 3-4 LT/RT AT C47. WEB P/N, A538-32100 AND A538-32103 REPAIR PERFORMED BY DRILLING CRACK STOP HOLES AND INSTALLING REPAIR DOUBLERS IAW RAS 052969/004/2007 ISSUE "A" AND E 6-5315-106499.Aug 1, 2007 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 07FDEA02614Skin · crackedCRACKS AT DIFFERENT HOLES AT CIRCUMFERENTIAL JOINT AT C13, AREA P9 AND BEAM 2, BOTH LT AND RT SIDE. REPAIR PERFORMED BY OVERSIZING HOLES IAW RAS 053024/026/2007 AND EA 6-5312-106506.Jul 26, 2007 · N732FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 07FDEA02599Skin Panel · corrodedCORROSION ON SKIN PANEL AROUND DME 2 ANTENNA, BETWEEN FRAME 30 -31, P54 LT/P54 RT. REPAIR PERFORMED BY CORROSION REMOVAL AND INSTALLING AN EXTERNAL DOUBLER BASED ON SRM 53-10-12 / FIG 225, COVERED BY EA 6-5314-106493.Jul 24, 2007 · N732FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 07FDEA02548Beam · corrodedCORROSION ON BEAM BULK CARGO DOOR CUT OUT REPAIR PERFORMED BY REPLACING THE PART IAW SRM 51-72-10.Jul 20, 2007 · N732FD · Airbus A300B4605R · Fuselage Main, StructureSDR 07FDEA02536Skin · corrodedCORROSION SPOTS ON FUSELAGE SKIN PANEL AT C39, P55 LT (P/N SPLICE A538-12119-200, SKIN PANEL A538-10775-200). REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING OVERSIZE FASTENER IAW EA 6-5315-106500 AND RAS 053011/010/2007 ISS A.Jul 20, 2007 · N732FD · Airbus A300B4605R · Fuselage Main, Plate/Skin
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