N86, cancelled Dec 24, 2025
Service difficulty reports · 22
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 = 'N86' AND deregistration_id = 'N86-2025-12-24' 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 = 'N86' AND deregistration_id = 'N86-2025-12-24' 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 2022FA0000640Hose · rupturedLOSS OF THE # 3 HYDRAULIC SYSTEM IN FLIGHT. EMERGENCY DECLARED AND LANDING GEAR WAS MANUALLY DEPLOYED. UPON INSPECTION, THE NLG DOOR ACTUATOR HOSE WAS FOUND TO BE RUPTURED.SDR RU3A2021100100013None · none“FUSELAGE SKIN BUCKLED AFT OF NOSE LANDING FOLLOW UP DOOR” ON LOGBOOK PAGE 270398 DATED JULY 29, 2021 HOURS 14193.3 LANDINGS 5792
THE AIRCRAFT WAS FERRIED UP TO WICHITA ON AUGUST 19, 2021 HOURS 14,194.1 LANDINGS 5793 LOGBOOK PAGE 270402.
10/01/2021 DETERMINSDR RU3A2021030300004Warning Light · illuminatedFLAPS FAIL LIGHT ILLUMINATED ON APPROUCHSDR RU3A201912065069Switch · out of adjustNOSE GEAR DID NOT RETRACT ON TAKEOFF. NOSE DOOR OPEN LIGHT REMAINED ILLUMINATED. ACCOMPLISHED GEAR DISAGREE CHECKLIST. MA ADJUSTED LH LANDING GEAR DOOR (NOSE) OPEN SWITCH S1GK TO CORRECT THIS ISSUESDR RU3A201912062068Connector · looseNOSE GEAR DID NOT RETRACT. DOOR LIGHT REMAINED ON. COMPLETED GEAR DISAGREE CHECKLIST. FOUND LOOSE BACKSHELL AND CANNON PLUG CONNECTION GOING TO NOSE LANDING GEAR SELECTOR VALVE HARNESS. TIGHTENED BACKSHELL AND CANNON PLUG. NO FURTHER ISSUES.SDR RU3A2018092524045Sensor · failedINBOARD ANTI-SKID FAIL ANNUNCIATOR ON. LT WHEEL SPEED SENSOR WAS REPLACED. OPERATIONAL CHECK SATISFACTORY.SDR RU3A2018092523044Module · intermittentOUTBOARD ANTI-SKID LIGHT ILLUMINATED WHEN GEAR EXTENDED WOULD NOT RESET. FOUND ANTI-SKID CONTROL PANEL LT LIGHT MODULE INTERMITTENT. THE ISSUE WAS RESOLVED BY REPLACING THE ANTI-SKID CONTROL PANEL.SDR RU3A20180529022Accelerometer · faultyRIGHT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16000 FEET. REMOVED AND REPLACED ENGINE VIBRATION ACCELEROMETER.SDR RU3A20180523019Signal Cond Unit · malfunctionedRT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16,000 FEET. REMOVED AND REPLACED ENGINE VIBRATION SIGNAL CONDITIONER.SDR RU3A20180312013Crank Assy · crackedPASSENGER DOOR LATCH MECHANISM CRANK CRACKED.SDR RU3A2018031200001Crank Assy · crackedPASSENGER DOOR LATCH MECHANISM CRANK CRACKED.SDR RU3A20170810023Landing Gear · malfunctionedLEFT MAIN LANDING GEAR UNSAFE AFTER LOWERING GEAR. PULLED MANUAL RELEASE WITH NO CHANGE IAW CHECKLIST. RESET MANUAL RELEASE PER SERVICE CENTER MX DIRECTION. GEAR CAME DOWN 30 SECONDS LATER. EMERGENCY WAS DECLARED.SDR RU3A20160513009Shutoff Valve · malfunctionedBLEED AIR FAIL LIGHT ILLUMINATED WHEN BLEED AIR IN CLOSED POSITION. REPLACEMENT OF THE PNEUMATIC SOV SOLVED THE ISSUE. NO FURTHER ACTION REQUIRED.SDR RU3A20150618014Flap · lack of lubeFLAPS FAIL ON INITIAL TAKE OFF. FAILED AT 18^. AIRSPEED REACHED 240 KIAS WITH NO OVER SPEED WARNING. COMPLIED WITH OVER SPEED INSPECTION. LUBED FLAPS.SDR RU3A20131126014Unknown · malfunctionedAFTER TAKEOFF COULDN’T RAISE GEAR, THEN WOW INPUT LIGHT CAME ON. LIGHT WENT OUT AFTER 2 MIN. GEAR HANDLE REMAINED LOCKED DUE TO MOMENTARY WOW INPUT FAILURE, TROUBLESHOOTING CONTINUING.SDR RU3A20130509008Unknown · malfunctionedUPON COMPLETION OF A LOW APPROACH, GEAR HANDLE SELECTED UP FOR CLIMBOUT. AFTER MAINS RETRACTED, NOSE GEAR REMAINED EXTENDED AND RED LIGHT IN HANDLE CONTINUED FLASHING. INITIALLY NO OTHER INDICATIONS. AFTER HOLDING AND APPROXIMATELY 40 MINUTES AFTER INITIAL SDR RU3A20121211002Windshield · crackedRIGHT SIDE WINDSHIELD ANTI-ICE FAILURE IN CRUISE FLIGHT. PERFORMED WINDSHIELD ANTI-ICE FAILURE AS DIRECTED IN ABNORMAL PROCEDURE. CONTINUED ON ORIGINAL ROUTE TO PLANNED DESTINATION. APPROX 20 MIN LATER NOTICED CRACK OF OUTER PLY OF RIGHT SIDE WINDSHIELD. CSDR RU3A1117Hinge Fitting · crackedREMOVED RUDDER TO NDI ATTACH FITTINGS. DURING INSPECTION A CRACK IN UPPER FITTING WAS DETECTED. DURING STRIPPING OF PAINT, DISCOVERED PITTING AROUND BUSHING INSERT. CORROSION WAS DEEP INTO BRACKET AT EDGE OF BUSHING. THIS UPPER HINGE FITTING AND BUSHING SISDR RU3A1108Downlock Switch · faultyWHILE MANEUVERING FOR APPROACH, CREW LOWERED LANDING GEAR. BOTH MAIN GEAR INDICATIONS WERE "DOWN AND LOCKED". NOSE INDICATOR DID NOT ILLUMINATE. NOSE DOOR OPEN LIGHT REMAINED ILLUMINATED AND AIRCRAFT BUFFETED INDICATING NOSE DOORS WERE OPEN. THE LIGHT IN TSDR RU3A1021Warning Message · false activationON DESCENT THRU 160 BOTH THROTTLES WERE BROUGHT TO IDLE. NR 2 LOW OIL PRESSURE LIGHT CAME ON, AND LOW OIL PRESSURE TAPE INDICATED LOW. N1 LT 65 PERCENT, RT 34 PERCENT, POWER RE-APPLIED AND ENGINE RECOVERED. MX CHECKED ENGINE ON GROUND AND NO FAULT FOUND.SDR RU3A0923Windshield · crackedIN CRUISE FLIGHT, LEFT PILOT WINDSHIELD CRACKED THE ENTIRE VERTICAL LENGTH OF THE WINDOW. PRESSURIZATION WAS CHECKED AND ABNORMAL CHECKLIST FOR WINDSHIELD OUTER FACE PLY FAILURE WAS ACCOMPLISHED. ATC AND FICO WERE ADVISED AND TURN AROUND CONDUCTED. UNEVENTFSDR RU3A99001Cover · brokenANC - AIRPORT RAMP. AIRCRAFT OBSERVED TO BE LEAKING FUEL FROM THE LOWER TAIL SECTION WITHIN A FEW MINUTES FOLLOWING APU START. THE AIRCRAFT ENGINES WERE NOT STARTED. THE APU WAS SHUT DOWN WITHOUT FURTHER INCIDENT AND THE FLIGHT CANCELLED. INVESTIGATION REV
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