N6813J
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 = 'N6813J' 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 = 'N6813J' 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 HYIA20260818001Switch · faultyPILOT REPORTED THE LANDING GEAR EXTENDED BY ITSELF WITH GEAR HANDLE IN UP POSITION. MAINTENANCE INSPECTED LANDING GEAR SELECTOR SWITCH, NO DEFECTS FOUND. THE SWITCH WAS REPLACED AS A PRECAUTION, WITH NO FURTHER DEFECTS NOTED.SDR HYIA20221215001Circuit Breaker · failedPILOT REPORTED SMOKE OBSERVED FROM SIDE PANEL. MAINTENANCE INSPECTED ANTI-COLLISION CIRCUIT BREAKER SWITCH AND WIRING, FOUND SWITCH INOP AND WIRE INSULATION BURNT ON LOAD SIDE OF SWITCH. REPAIRED DAMAGED ANTI-COLLISION LIGHT SWITCH WIRE IAW 402C WDM CHAPTER 20SDR HYIA20190128001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB LOCATED AT LEFT WING STATION 106.79. THIS CRACK STARTS AT A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT TRUNION SUPPORT AND EXTENDS FORWARD APPROXIMATELY .900 IN. THIS RIB WILL SDR HYIA2017010500001Engine · shutdownPILOT REPORTED THE RIGHT ENGINE SHUTDOWN IN FLIGHT. OPENSDR HYIA20171117001Torque Tube · failedWHILE IN CRUISE, THE RT RUDDER PEDAL WENT TO THE FLOOR, FULL FORWARD. THE PILOT DID NOT HAVE ANY RUDDER AUTHORITY, BUT THE AIRCRAFT REMAINED IN STRAIGHT AND LEVEL FLIGHT. DIVERTED AND LANDED SAFELY WITH NO ISSUES. THE AIRCRAFT WAS UNABLE TO TAXI FROM THE RUSDR HYIA20170705001Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, TWO CRACKS WERE IDENTIFIED IN THE LT OUTBOARD NACELLE FITTING.SDR HYIA20170503001Cylinder · brokenPILOT REPORTED SHUDDERING AND VIBRATION FROM LEFT ENGINE. UPON INSPECTION MAINTENANCE FOUND THE CYLINDER ROTOCOIL BROKEN. CYLINDER WAS REPLACED, ADDITIONAL DETAILS TO BE CONVEYED UPON TEARDOWN ANALYSIS.SDR HYIA20140414025Drag 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 SDR HYIA20140414007Drag 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 & ASDR HYIA20140415065Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWSDR HYIA20140415052Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE SDR HYIA6813J1024Resistor · burnedCREW REPORTED, IN CRUISE, STRONG ELECTRIAL SMELL IN COCKPIT. CREW DIVERTED. MX INSPECTED ACFT, R & R OVERHEATED CABIN HEATER FAN HIGH - LOW RESISTOR. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.SDR 1356813112207Fitting · leakingPILOT NOTICED FUEL SMELL IN COCKPIT DURING HEATER START UP AND SHUT DOWN, WHEN BRINGING AIRCRAFT TO FLEET CENTER AT END OF NIGHT. MAINTENANCE FOUND PUMP OUTLET FITTING LEAKING. MAINTENANCE TIGHTENED FUEL PUMP OUTLET FITTING AND AS A PRECAUTIONARY MEASURE REMSDR 135N6813JLENGConnecting Rod · destroyedPILOT REPORTED RPM/POWER LOSS, SHUT ENGINE AS A PRECAUTIONARY MEASURE, RETURNED TO DEPARTURE AIRPORT.SDR 1350606N6813JCircuit Breaker · defectiveAVIONICS CIRCUIT BREAKER FAILED IN THE ON POSITION.SDR 13500527N6813Circuit Board · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.SDR HYI2003F00020Liner · damagedAFTER LANDING, ON ROLLOUT, AIRCRAFT STARTED VEERING TO THE LEFT. CREW WAS UNABLE TO STRAIGHTEN OR TURN RIGHT EVEN WITH DIFFERENTIAL POWER OR RT RUDDER. AIRCRAFT WAS SHUTDOWN ON RUNWAY. TOWED TO HANGER. MECHANIC UNABLE TO DUPLICATE CONDITION, REMOVED AND RESDR HYI2001F00002Master Switch · inoperativeCREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE ON PREFLIGHT. MAINTENANCE REMOVED AND REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. (PTRS-2001B5540)
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