N740CA
Service difficulty reports · 20
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 = 'N740CA' 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 = 'N740CA' 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 HYIA20220316001Propeller · crackedPILOT REPORTED THE LEFT PROPELLER CONTROL WAS UNRESPONSIVE AT CLIMB OUT AND PERFORMED AN AIR RETURN. COMPANY MAINTENANCE INSPECTED THE LEFT PROPELLER AND FOUND CRACKS IN THE PROPELLER HUB AT ALL 3 BLADE SOCKET LOCATIONS. AT BLADE 1 LOCATION THE CRACK IS APPRSDR HYIA20210311002Wire · chafedTHE PILOT REPORTED A BURNING SMELL AFTER THE AUTOPILOT CB POPPED DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND CHAFFED WIRING AT THE PTT SWITCH. THE WIRES WERE REPAIRED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20181218002Cable Assy · failedPILOT REPORTED RIGHT ENGINE THROTTLE STUCK AT 35 INCHES MAP. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. INSPECTION FOUND THE RIGHT THROTTLE CABLE PROPERLY ATTACHED AT BOTH ENDS, AND THE CABLE FAILED INTERNALLY. THE CABLE SDR HYIA20180906001Door Frame · corrodedWHILE CONDUCTING OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT FS 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOVASDR HYIA20180827002Fitting · corrodedDURING MAINTENANCE, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE RIGHT NACELLE OUTBOARD FITTING, AROUND THE FASTENER HOLES OF THE TOP FORWARD FACE OF THE FITTING, JUST FORWARD OF THE FIREWALL. THE DEPTH OF THIS CORROSION IS .019 IN. THE FITTING WAS REPLACESDR HYIA20180827001Crossbeam · chafedDURING MAINTENANCE, CHAFING DAMAGE WAS FOUND ON THE RIGHT NACELLE CROSSOVER BEAM.SDR HYIA09092017001Rotor Coil · damagedCREW REPORTED ENGINE ROUGHNESS IN FLIGHT AT POWER REDUCTION FOR CRUISE AND MIXTURE FULL RICH. THE ACFT LANDED SAFELY AT ITS INTENDED DESTINATION WITH NO ISSUE. INSPECTION DISCOVERED LOW DIFFERENTIAL COMPRESSION CHECK RESULT AT CYLINDER NR 4 OF THE LT ENGINESDR HYIA20170826001Cylinder · damagedCREW REPORTED A STRONG VIBRATION FROM RT ENGINE AS MIXTURE WAS REDUCED BELOW 100 PPH. THE CREW ENRICHED THE MIXTURE AND ELECTED TO DIVERT TO KHYA AS A PRECAUTION. INSPECTION DISCOVERED LOW DIFFERENTIAL COMPRESSION, 0 PSI/80PSI, AT CYLINDER POSITION NUMBER 1SDR HYIA20170718001Indicator · faultyPILOT REPORTED SMELL OF SMOKE IN COCKPIT UPON ACTIVATION OF WEATHER RADAR. MAINTENANCE INSPECTED AND DETERMINED TO BE DUE TO FAULTY INDICATOR. SYSTEM WAS PLACED ON MEL.SDR HYIA20160825096Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160825095Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION, EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160825094Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160706001Clamp · loosePILOT REPORTED LT PROP LEVER DOES NOT CONTROL RPM, LT PROP WILL NOT FEATHER. MAINTENANCE INSPECTED AND FOUND THE LT PROPELLER GOVERNOR CONTROL CABLE BRACKET ATTACH CLAMPS TO BE LOOSE. MAINTENANCE ADJUSTED AND SECURED LT PROP GOVERNOR CABLE BRACKET IAW AMM CHSDR HYIA20151019001Rod · severedPILOT REPORTED ON APPROACH, WHEN FLAPS DEPLOYED TO 30 DEGREES THE ACFT ROLLED AGGRESSIVELY TO THE RIGHT. INSPECTED & FOUND THE RT FLAP OTBD FLAP ROD SEVERED. R & R THE FLAP ROD, OPERATIONALLY CHECKED GOOD.SDR HYIA20151002001Governor · defectivePILOT REPORTED RT PROPELLER OVERSPEED INDICATION ON CLIMB OUT, THEN DIFFICULTY CONTROLLING THE PROPELLER AT A STEADY RPM AFTER THAT POINT. R & R THE RT ENG PROPELLER GOVERNOR, OPERATIONAL & LEAK CHECKED GOOD WITH NO FURTHER DEFECTS AT THAT TIME.SDR HYIA20150624003Panel · openPILOT REPORTED WING LOCKER LT SIDE OPENED IN FLIGHT. INSPECTED LATCH OF LT WING LOCKER WITH NO DEFECTS FOUND. REMOVED LATCH COVER, INSPECTED ALL PINS & RODS, INSPECTED HINGES, INSPECTED SAFETY LATCH WITH NO DEFECTS FOUND.SDR HYIA20150515001Latch · unsecureLT WING LOCKER OPENED IN FLIGHT. INSPECTED & SECURED THE LT WING LOCKER LATCH. OPERATIONALLY CHECKED GOOD.SDR HYIA20150428001Caliper · failedTHE LT BRAKE STUCK & THE RT BRAKE FAILURE DURING TAXI. VISUALLY CHECKED THE RT BRAKE, SERVICED MASTER CYLINDER & BLED BRAKE SYS. REPLACED LT BRAKE CALIPER & SERVICED BRAKE SYS. BOTH SIDES OPERATIONALLY CHECKED GOOD.SDR HYIA20150312001Indicator · failedPILOT REPORTED A FAINT SMELL AFTER WEATHER RADAR STOPPED WORKING INFLIGHT. THE CB DID NOT POP. R & R WEATHER RADAR INDICATOR & TRANSCEIVER ANTENNA WITH NO FURTHER SMELLS NOTED.SDR HYIA20140414042Drag 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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