N809TA
Service difficulty reports · 18
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 = 'N809TA' 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 = 'N809TA' 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 2021F00104Overheat Sensor · dirtyIN FLIGHT, CREW HAD WHEEL WELL OVERHEAT LIGHT AS WELL AS MASTER FIRE WARNING LIGHTS ILLUMINATE. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS EXTENDED. UPON LANDING, MAINTENANCE INSPECTION DETERMINED OVERHEAT SENSING LOOP CONNECTION WAS DIRTY, CLEANED AND PERFORMESDR FY4Y202009118008Skin · corrodedCORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 475 TO WS 525.SDR FY4Y202008013Battery · failedEMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.SDR FY4Y202008012Battery · inoperativeEMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.SDR FY4Y2020009118007Skin · corrodedCORROSION WAS FOUND AT AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 315 TO WS 475.SDR FY4Y202009118006Skin · corrodedCORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT INBOARD TO WS 195.SDR FY4Y202009118005Spar · corrodedCORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 135.SDR FY4Y202009108002Frame · corrodedCORROSION WAS FOUND AT AFT CARGO FWD BULKHEAD LOWER CHORD AT BS 727 BETWEEN S-25L AND 25R.SDR FY4Y202009118011Lug · corrodedCORROSION WAS FOUND AT FWD & AFT SURFACE OF RT SIDE HORIZONTAL STABILIZER REAR SPAR UPPER LUG.SDR FY4Y202009118010Spar · corrodedCORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 442.3.SDR FY4Y202009118009Spar · corrodedCORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 416.8.SDR FY4Y202009118004Spar · corrodedCORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 422.SDR FY4Y202009118003Spar · corrodedCORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 307.SDR FY4Y202009108001Keelbeam · corrodedCORROSION WAS FOUND AT KEEL BEAM LOWER CHORD AT AFT CARGO BS 727 S-27L (LENGTH: 3" WIDTH: 1"). REFER TO NRC CA1174-02-010.SDR JRAA2017081100446Skin · corrodedDURING A C1 CHECK, FOUND THE LEFT WING UPPER SURFACE WAS CORRODED ON REAR SPAR BETWEEN WS 150 - 205. CORROSION WAS BLENDED OUT BEYOND SRM LIMIT. REPAIRED IAW DOCUMENT ROO3 REV 01.SDR JRAA2017081100445Skin · corrodedDURING INSPECTION IAW CARD 53-30-00-101, FOUND FUSELAGE SKIN AT BS 1016 BETWEEN STRINGERS 24R - 25R WAS CORRODED. A REPAIR WAS CARRIED OUT IAW DOCUMENT 2016R002.SDR 2017FA0000444Skin · corrodedDURING A C1 CHECK, IAW TASK CARD 53-30-00-101, FOUND A CRACK ON FUSELAGE SKIN AT BS 937, STRINGER 24L. REPAIRED IAW REPAIR PLAN DOCUMENT 2016R001.SDR 2017FA0000443Stringer Fitting · corrodedDURING A C1 CHECK, DURING INSPECTION IAW TASK CARD53-88-80-101, FOUND BS 1016 STRINGER 17R FITTING CORRODED. THE STRINGER FITTING WAS REPLACED IAW ENGINEERING AUTHORIZATION B737-53-00-8.
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