N999FD
Service difficulty reports · 109
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 = 'N999FD' 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.
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 = 'N999FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201101180272Skin · damagedPREVIOUS BLEND OUT AT STA 1377.5 2.3" ABOVE STR 25L ON FUSELAGE SKIN. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET. II. REPAIRED IAW SRM 53-00-01. REPAIR NR 16, THIS IS CAT "B" REPAIR FROM TIME OF REPAIR 16,000 F/C WITH REPEAT INSPECTIONS AT EVERY 6,00SDR FDEA201101150178Stringer · corrodedSTRINGER 22-R INSIDE FWD CARGO COMPARTMENT BS 740-760 HAS CORROSION. REMOVED CORROSION ON S-22R STA 740-760 IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.0 D=.020. ORIGINAL MATERIAL .071 AFTER REWORK .051. NO ALLOWABLE DAMAGE FOR SF STRINGERS. REPAIRED STRINGER SDR FDEA201101130137Seat Track · gougedMAIN CABIN, STA 418-440, RBL 25, WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE FROM SEAT TRACK STA 418-440 RBL 25 AND FOUND TO OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201101130134Seat Track · gougedMAIN CABIN, STA 418-440, RBL 45,WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE ON SEAT TRACK STA 418-440 RBL 45 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201101130132Floorbeam · corrodedMAIN CABIN,STA 377, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION ON PREVIOUSLY INSTALLED FLOORBEAM REPAIR AT STA 377, RBL 11 IAW SRM 53-0051, REPAIR 3 FOUND TO BE OUT OF LIMITS ARIG MAT 0.125 AFTER REWORK 0.101. REMOVED FLOOSDR FDEA201101110105Floorbeam · corrodedFLOORBEAM, STA 1661, BL 0, WL 208 CORRODED MAIN CABIN. REMOVED CORROSION ON FLOORBEAM, STA 1661, BL 0 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. ORIG MATERIAL .125 MATERIAL LOSS .035. R & R STA 1661 FLOORBEAM IAW SRM 51-40-02. CATEGORSDR FDEA201101070073Skin · corrodedNR 3 SLAT LOWER SURFACE AT SEAM BETWEEN SLAT AND AERODYNAMIC SEAL HAS CORROSION. REMOVED CORROSION ON NR 3 SLAT LOWER SURFACE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L-139" X 1" X D=.063 ORIG MATERIAL .063 AFTER REWSDR FDEA201101070074Angle · corrodedNR 10 SLAT COVE ANGLE CORRODED. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. ORIG MATERIAL .063 AFTER REWORK .000 MATERIAL LOSS .063 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L= 131" X W=2" X D=.063. R & R COVE ANGLE IAW SRM 51-40-02. SDR FDEA201101070072Channel · corrodedNLG WHEELWELL FWD BOTTOM "L" CHANNEL AT STA 263 JUST BELOW NLG DOOR UNSAFE LIGHT IS CORRODED. COMPLIED WITH EA F-5310-146250. MAJOR REPAIR.
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