N651DL
Service difficulty reports · 307
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 = 'N651DL' 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 = 'N651DL' 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 DL757951968Te Wedge · delaminatedDURING SHOP INSPECTION, 757 SLAT PANEL WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR DL757950506Skin · puncturedRT SIDE OF FUSELAGE SKIN HAS A 3 INCH DIAMETER HOLE PUNCTURED AT FS STA 465 AT STR 20RT. REPAIRED PER SRM 53-00-01 FIG 205 PAGE 212-215 AND ERA 301133-14 FOR FASTENER SUBSTITUTION DAMAGE OCCURED AND REPAIRED DURING HMV, VISIT.SDR DL757950443Wedge · delaminatedDURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT T/E WEDGE WAS FOUND TO BE DELAMINATED. REPAIRED BY PLACING WEDGE PER SRM 57-43-02.SDR DL757950412Floor Beam · corrodedAT HMV, CORROSION ON TOP FLANGE OF FLOORBEAM FS 324 RBL 50. CLEANED CORROSION AND REPAIRED PER SRM 53-10-08.SDR DL757950411Floorbeam · corrodedAT HMV, FLOORBEAM FS 324 WAS CORRODED AT RBL 0. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-08 PAGE 201.SDR DL757950404Hi-Lock · failed3 FASTENERS LOOSE, 1 FASTENER HAS SHEARED HEAD IN NR 2 PYLON STRUCTURE STA 107.7 AT WL 139.909 (REF DWG 311N3110 SH 1 B-9).SDR DL757950410Skin · crackedDURING HMV, #3 AFT FLAP LOWER SURFACE CRACKED AT CENTER OF FLAP. REPAIRED PER SRM 57-70-17.
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