N390DA
Service difficulty reports · 107
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 = 'N390DA' 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 = 'N390DA' 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 DL738040464Spar · damagedRT IB MAIN FLAP FRONT SPAR LOWER CHORD FOUND TO BE DAMAGED. DAMAGE WAS LOCATED BETWEEN 26 INCHES AND 34 INCHES FROM THE IB END OF SPAR. DAMAGE WAS REMOVED AND REPAIR INSTRUCTION ISSUED IAW ERA 090294-14.SDR DL738040485Spar · damagedREPAIR OF RIGHT INBOARD MAIN FLAP FRONT SPAR LOWER CHORD.SDR DL738021137Indicator · faultyFLAPS COMMANDED TO 5 DEG, STOPPED SHORT OD FLAPS 1. NEEDLES SPLIT PRIOR TO LANDING, NEEDLES MATCHED AT/SHORT OF FLAPS 1 DEG. REPLACED INDICATOR, OPERATED FLAPS SEVERAL TIMES. OPS OK. BITE OF FSEU, NO FAULTS FOUND, NO CURRENT FAULTS.SDR DL738020429Fseu · malfunctionedTRAILING EDGE FLAPS EXTENDED AT 240 KTS TO FIVE DEGREES, FLAPS STOPPED AT MID POSITION BETWEEN UP AND 1. T/S-READ FSEU BITE, NO FAULTS. REPLACED FSEU PER M/M, NO FAULTS. INSPECTED FLAPS AND FLAPS OPERATE NORMALLY. OK FOR SERVICE.SDR DL738020388Sensor · inoperativeAFTER SELECTING FLAP SETTING 2 DEGREES AT AIRSPEED 210 KNOTS THE FLAPS SPLIT ASYMMETRICALLY. THE RIGHT TRAILING EDGE FLAP WAS AT 1.75 DEGREES AND THE LEFT TRAILING EDGE FLAP INDICATED 1.3 DEGREES. PROCEDURE FOLLOWED IAW QR HANDBOOK. LANDING ACCOMPLISHED NOSDR DL738011736Eec · malfunctionedENGINE CONTROL LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED EEC BITE. LT AND RT EEC FAULT 73-31671. PROBE HEAT FAULT. T/S PER FIM, CKD OK. RAN ENGINE TO TAKEOFF PWR. NO FAULTS, NO LIGHTS. OK FOR SERVICE. NOTE: PROBLEM INVOLVED BOTH ENGINES. CRESDR DL738010627Charger · inoperativeINTERIOR EMERGENCY LIGHTS INOPERATIVE AT ROW 16ABC. REPLACED CHARGER AND BATTERY COMBINATION.
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