N290CA
Service difficulty reports · 19
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 = 'N290CA' 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 = 'N290CA' 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 HYIA20261001001Beam · crackedDURING HIGH TIME ENGINE BEAM REPLACEMENT, UPON REMOVAL OF ENGINE BEAM A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD FACE OF THE RH INBOARD ENGINE BEAM. THIS CRACK IS EMANATING FROM A FASTENER LOCATION COMMON TO THE INBOARD VERTICAL CROSS OVER BEAM UPRIGHT (OESDR HYIA20250522002Rib · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT UPPER OUTBOARD RIB CAP COMMON TO THE CLOSEOUT RIB LOCATED AT RWS 106.79 (OEM: 5122115-12). THIS CRACK WAS IDENTIFIED IN THE RADIUS OF THE CAP TRAVELING FORWARD AND AFT, AND MEASURES APPRSDR HYIA20250522001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE RIGHT HAND OUTBOARD NACELLE FITTING P/N: 5292029-32. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TESDR HYIA20240718006Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE LEFT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20240221001Engine · failedON APPROACH PILOT NOTICED A SUDDEN "BANG" ACCOMPANIED BY SLIGHT POWER & RPM LOSS ON THE LEFT ENGINE. SMOKE AND OIL BEGAN COMING FROM LEFT ENGINE. OIL PRESSURE DROPPED AND PILOT SECURED THE ENGINE PER COMPANY PROCEDURES. INITIAL INSPECTION FOUND THE NUMBER 6 CYSDR HYIA20210924001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND OUTBOARD ENGINE BEAM (P/N: 5654109-8) IN THE AREA UNDERNEATH THE FORWARD ENGINE MOUNT DOUBLER. THIS CRACK TRAVELS LEFT TO RIGHT ACROSS THE TOP FACE OF THE BEAM AND PARTIALLY DOWN THE OUTBOARDSDR HYIA20181123001Windshield · failedDURING CLIMB OUT PIC TURNED ON WINDSHIELD HEAT. UPON REACHING CRUISE, BURNING SMELL AND SMOKE NOTICED FROM LOWER LEFT SIDE OF WINDSHILED. PIC TURNED OFF HEAT
AND SMELL/SMOKE DISAPPEARED AND STOPPED.THE WINDSHIELD WAS TESTED AND CONTINUITY FOUND BAD. THE WINDSSDR HYIA20180316002Control Cable · brokenPILOT REPORTED THE LEFT RUDDER DOES NOT MOVE, A SNAP WAS HEARD WHEN MAKING A LEFT TURN. MAINTENANCE INSPECTED AND FOUND THE FORWARD LEFT RUDDER CABLE BROKEN NEAR THE FORWARD PULLEY. LAST VISUAL INSPECTION OF AREA OCCURRED 134.8 HOURS PRIOR TO FAILURE. CABLE SDR HYIA20161026001Piston · damagedPILOT REPORTED ON CLIMB OUT, RIGHT ENGINE MANIFOLD PRESSURE DROPPED, COINCIDED WITH ROUGHNESS FOLLOWED SHORTLY AFTER BY ENGINE FAILURE. THE AIRCRAFT LANDED SAFELY WITH NO INJURIES. INSPECTION OF RT ENGINE REVEALED A PRE-IGNITION EVENT WITHIN THE NR 5 CYLINDESDR HYIA20160902118Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160902100Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION, EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160718002Transistor · failedPILOT REPORTED INSTRUMENT PANEL LIGHT DIMMER SWITCH FOR ENGINE INSTRUMENTS SMOKED, DIMMER DOES NOT WORK. MAINTENANCE TROUBLESHOT AND FOUND DIMMABLE PANEL TRANSISTOR AND HEAT SINK FAILED. REPLACED THE DIMMABLE PANEL TRANSISTOR AND HEAT SINK ASSEMBLY, AND REPLACSDR HYIA20160803033Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20141217001Caliper · defectiveRIGHT BRAKE PEDAL INEFFECTIVE. PEDAL GOES TO FLOOR & DOES NOT HOLD ACFT DURING RUN-UP. R & R THE RT BRAKE CALIPER & BRAKE PADS.SDR HYIA2014052303Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED AT INBD AFT FACE. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL NEW RT NACELLE INBD ENG BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTSDR HYIA20140523001Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT LWR U CHANNEL. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL RT NACELLE CROSSOVER BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTLISDR HYIA20130316001Spar · damagedDAMAGE WAS DISCOVERED ON THE FRONT UPPER SPAR CAP. OPENSDR HYIA20130308001Spar Cap · crackedDURING A SCHEDULED MX EVENT CRACKS FOUND ON THE REAR SPAR WEB CRACKS AT FLOOR SUPPORT LOCATIONS. THERE WERE ALSO 5 MISS DRILLS IN THE TOP OF THE REAR SPAR THAT WERE NOTED. AFTER REVIEWING ENGINEERING REPAIR OPTIONS, THE DECISION WAS MADE TO REPLACE REAR SPAR SDR HYIA20140414003Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A
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