N997FD
Service difficulty reports · 158
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 = 'N997FD' 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 = 'N997FD' 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 FDEA201101180267Attach Fitting · corrodedUPPER CARGO AFT GALLEY DECK AND ATTACH FITTING CORRODED IN NUMEROUS AREAS LBL 63 TO RBL 63. FOUND OUT OF LIMITS. REMOVE DAMAGE IAW SRM 51-10-02. R & R UPPER CARGO AFT GALLEY DECK IAW SRM 51-40-02. R & R DECK PLATE AND ATTACH FITTINGS IAW SRM 51-40-02. CSDR FDEA201101130130Frame · gougedAFT CARGO COMPT FRAME GOUGED AT STA 1480, BETWEEN STR 24R AND 25R, UPPER CHORD SPLICE. REMOVED PRODUCTION SPLICE FROM FRAME BS 1480, S24R/25R, SRM 51-40-02. GOUGES FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, PG. 103. NEW SPLICE FABRICATED ON TRSDR FDEA201101060040Crease Beam · corrodedUPPER CARGO INNER CREASE BEAM RBL 63, FS 1600 TO 1620, CORRODED. REMOVED CORROSION PER SRM 51-20-02. FOUND TO BE OUT OF LIMITS PER SRM 53-60-13, FIG.101, DETAIL 8; BEFORE: .080", AFTER: .063", LOSS: .017". REMOVED AND REPLACED CREASEBEAM, PER SRM 51-40-02,SDR FDEA201101040007Gate · corrodedR-4 DOOR LWR GATE, LWR EDGE HAS PITTED CORROSION. REMOVED CORROSION FROM LWR GATE ASSY IAW SRM 51-10-02. CHECKED LIMITS ON REMAINING MATERIAL OF LWR GATE, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02. R & R LWR GATE ASSY IAW SRM 51-40-02. PERFORMED R-4 DOORSDR FDEA201012154691Floorbeam · corrodedFLOORBEAM UPPER CHORD AT STA 345 HAS SEVERAL CORROSIONS BETWEEN BL 0 TO LBL 45. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-57, FIG 101, DETAIL III. ORIG MATT .125 AFTER REWORK .087 EXCEEDS MAX OF 10 PERCENT, REMOVED DAMAGED UPPER SDR FDEA201012144669Seat Track · gougedMCD SEAT TRACK STA1080 - 1180 HAS GOUGES, WORN AREAS. LBL24.75 FABRICATED MCD SEAT TRACK, BS 1080-1180, LBL 24.75, FROM BAC 1520-792, BATCH 904663, IAW SRM 53-40-52, P 2, FIG 1. SEAT TRACK PLACED ON PANEL RACK. SEAT TRACK DAMAGE WAS DETERMINED TO BE OUT OF LSDR FDEA201012104632Fuel Cell · corrodedCTR FUEL TANK UPPER SURFACE HAS CORROSION UNDER STUB BEAM ATTACHMENTS AT STA940, RBL64. ACCOMPLISHED WING-CTR-UPPER SKIN PLANK CORROSION REPAIR, WS 18, RBL 65, IAW EA F-5710-146245, STEPS 1-10. REF FAA FORM 8100-9, DATED 03/11/2011. CAT. "A" MAJOR REPAIR.SDR FDEA201012104631Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER SURFACE BS700 RBL48 TO RBL58 HAS CORROSION. REMOVED CORROSION FROM BS 700, RBL 48-58, PER SRM 51-10-02. ORIGINAL MATERIAL; .125", MATERIAL LOSS; .046", W=2", L=7". FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101, DETAIL 2. CU
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