# Service difficulty reports: Cirrus Design SF50 A list on [Cirrus Design SF50](https://openairdocs.org/model/cirrus-design-sf50.md). Newest first. General aviation reporting is voluntary. - [SDR 2026FA0000432](https://openairdocs.org/sdr/2026FA0000432.md): Fadec · faulted · May 22, 2026 · N21SM · Cirrus SF50 · Engine Controls > PART 91 FLIGHT, NO PAX ONBOARD. FLIGHT LEVEL 27,000 PILOT RECEIVED A FADEC NO DISPATCH, AND THEN SUBSEQUENTLY FADEC FAIL. HAD RED X’S ON MULTIPLE ENGINE DATA READOUTS, BUT NO ENGINE PERFORMANCE CHANGE. PILOT WAS ENROUTE TO ADDISON, HE FOLLOWED ONBOARD CHE - [SDR 2025F00193](https://openairdocs.org/sdr/2025F00193.md): Fuel Control · failed · Aug 13, 2025 · N71NP · Cirrus SF50 · Fuel Control/Turbine Engines > RECEIVED A RED CAS MESSAGE "FADEC NO DISPATCH" AND "FUEL DEGRAD 58". FUEL CONTROL UNIT WAS REPLACED WITH NEW AND WILLIAMS IN. WISB-73-1045 WAS COMPLIED WITH TO REMEDY THIS ISSUE. - [SDR CTUR20250606016](https://openairdocs.org/sdr/CTUR20250606016.md): Unknown · odor · May 7, 2025 · N304CW · Cirrus SF50 · Air Distribution System > PILOT REPORTED STRONG ODOR COMING FROM THE VENTILATION SYSTEM DURING FLIGHT. ADDITIONALLY WHEN CABIN HEAT IS SET TO FULL, THE AIR OUTPUT IS NOT NOTICEABLY WARM. CIRRUS TECHNICAL SUPPORT RETRIEVED THE FLIGHT DATA FOR THE MAY 7TH FLIGHT. NO DEFECTS NOTED. MAINTE - [SDR 2025FA0000025](https://openairdocs.org/sdr/2025FA0000025.md): Shutoff Valve · unknown · Dec 8, 2024 · N90DP · Cirrus SF50 · Hydraulic System, Main > ON STATIC TAKEOFF FROM HDC ON 12-08-24, TAKEOFF POWER WAS SET WITH BRAKES HELP. CREW ALERT MESSAGE CAME UP INDICATING BLEED PRESSURE HIGH. PILOT REDUCED THROTTLE AND TURNED BLEED AIR SWITCH OFF. AN ADDITIONAL CREW ALERT MESSAGE CAME UP SHOWING BLEED TEMP HIGH - [SDR PCPR202411071](https://openairdocs.org/sdr/PCPR202411071.md): Brake Pads · disintegrated · Nov 6, 2024 · N222XT · Cirrus SF50 · Landing Gear Brake System > DURING CONDITIONING OF NEW BRAKE PADS THE LEFT BRAKE FAILED RESULTING IN LOSS OF BRAKING AND LOSS OF STEERING CONTROL. UPON EXAMINATION THE LEFT BRAKE OUTBOARD BRAKE PAD LINING WAS MISSING FROM THE BACKING PLATE. PIECES OF THE LINING WERE FOUND IN THE BRAKE A - [SDR 2024FA0000426](https://openairdocs.org/sdr/2024FA0000426.md): Pad · deteriorated · Jun 5, 2024 · N26SE · Cirrus SF50 · Landing Gear Brake System > BRAKE BAD MATERIAL DISINTEGRATING OFF BRAKE PAD - [SDR 2024FA0000425](https://openairdocs.org/sdr/2024FA0000425.md): Pad · deteriorated · Jun 5, 2024 · N24AH · Cirrus SF50 · Landing Gear Brake System > BRAKE PAD MATERIAL FOUND DISINTEGRATING. NO OVERHEATING NOTED OR SEEN. NO OVERHEAT CAS MESSAGE RECORDED. - [SDR 2024FA0000235](https://openairdocs.org/sdr/2024FA0000235.md): Spring · short · Mar 20, 2024 · N616TS · Cirrus SF50 · Aileron Control System > AILERON FAILED TO RETURN TO NEUTRAL POSITION DURING ROLL CENTERING SPRING FUNCTIONAL TEST IN ACCORDANCE WITH AMM CH 27-10. INVESTIGATION REVEALED THE FACTORY-INSTALLED CENTERING SPRING IS INCORRECT (TOO SHORT) PER THE IPC CH 27-10-02. THE AILERON CENTERING SPR - [SDR WI5R2023112100001](https://openairdocs.org/sdr/WI5R2023112100001.md): Compressor · damaged · Nov 21, 2023 · N585PK · Cirrus SF50 · Turbine Engine Compressor Section > DURING “ON-FUSELAGE” CHECK 3 SCHEDULED HOT-SECTION MAINTENANCE ON FJ33-5A ENGINE SERIAL NUMBER 233606, INSTALLED ON CIRRUS SF50-0005 (N585PK), OUR REPAIR STATION SPECIALIST DISCOVERED METAL DEBRIS IN THE DIFFUSER SECTION OF THE ENGINE. DUE TO THIS FINDING, TH - [SDR WI5R2023111700001](https://openairdocs.org/sdr/WI5R2023111700001.md): Compressor · damaged · Nov 14, 2023 · N19VJ · Cirrus SF50 · Turbine Engine Compressor Section > FJ33-5A ENGINE SERIAL NUMBER 361138, FROM AIRCRAFT SF50-0236 (N19VJ), WAS RETURNED TO THE REPAIR STATION FOR SCHEDULED CHECK 3 HOT-SECTION MAINTENANCE. TYPICALLY, CHECK 3 MAINTENANCE IS PERFORMED “ON-FUSELAGE”; HOWEVER, ENGINE 361138 WAS SELECTED FOR WILLIAMS - [SDR 2023FA0000535](https://openairdocs.org/sdr/2023FA0000535.md): Unknown · unknown · Sep 9, 2023 · N32NS · Cirrus SF50 · Landing Gear Retraction/Extension System > LANDING GEAR WOULD NOT EXTEND NORMALLY. EXTENDED GEAR USING ALTERNATE GEAR EXTENSION. - [SDR 2023F00264](https://openairdocs.org/sdr/2023F00264.md): Unknown · unknown · Aug 31, 2023 · N32NS · Cirrus SF50 · Flight Control System > AILERON TRIM NOT RESPONDING; A/C DIFFICULT TO CONTROL; PULL CB; STILL COULD ONLY GET LIMITED CONTROL - [SDR 2023FA0000367](https://openairdocs.org/sdr/2023FA0000367.md): Shutoff Valve · unknown · Jul 13, 2023 · N19VJ · Cirrus SF50 · Pneumatic System > DURING CLIMBOUT ECS BLEED OVERHEAT OBSERVED AND SMELL OF BURNING IN CABIN - [SDR 2023F00101](https://openairdocs.org/sdr/2023F00101.md): Sensor · inoperative · Mar 29, 2023 · N14VJ · Cirrus SF50 · Engine Oil System (Airframe Furnished) > OIL PRESSURE WARNING IN FLIGHT AND LOSS OF OIL PRESSURE INDICATIONS ON EIS DISPLAY - [SDR 2023F00047](https://openairdocs.org/sdr/2023F00047.md): Not Reported · not reported · Feb 7, 2023 · N14VJ · Cirrus SF50 · Aircraft Fuel Distribution System > BOTH FUEL VALVES FAILED. - [SDR 2023F00041](https://openairdocs.org/sdr/2023F00041.md): Not Entered · not entered · Feb 1, 2023 · N23VJ · Cirrus SF50 · Standard Practices/Structures > MULTIPLE CAS MESSAGE APPEARED SUDDENTLY WHILE CRUISING AT FL 310 EG: IPS ENGINE INLET OFF, STICK PUSHER FAIL, EMERGENCY BATT FAIL, PITCH MET ACTIVE, CABIN PRESSRE CTRL FAIL, IPS WING/STAB FAIL, SPD NO CONMPARE, STALL SPEED HIGH, FUEL VALVES BOTH FAIL, FADEC N - [SDR 2022F00492](https://openairdocs.org/sdr/2022F00492.md): Autopilot Sys · failed · Dec 12, 2022 · N30VJ · Cirrus SF50 · Auto Flight System > AUTOPILOT FAILED TO DISCONNECT A/P LIGHT WAS EXTINGUISHED. - [SDR 2022FA0000732](https://openairdocs.org/sdr/2022FA0000732.md): Autothrottle Sys · malfunctioned · Nov 25, 2022 · N15VJ · Cirrus SF50 · Auto Throttle System > PILOT STATED DURING CLIMB OUT, AUTO THROTTLE ENGAGED, PULLING POWER BACK TO IDLE AND PITCHED AIRCRAFT NOSE UP AND WAS UNABLE TO DISENGAGE. TRIED TO COMMAND AIRCRAFT, ONCE DETERMINED UNABLE, DEPLOYED CAPS (CIRRUS AIRFRAME PARACHUTE SYSTEM) - AIRCRAFT BEING INVE - [SDR 2022FA0000593](https://openairdocs.org/sdr/2022FA0000593.md): None · none · Oct 11, 2022 · N23VJ · Cirrus SF50 · Aircraft Fuel System > FUEL VAVLE BOTH FAIL - [SDR 2022F00330](https://openairdocs.org/sdr/2022F00330.md): Fuel Control · abnormal · Sep 8, 2022 · N102JL · Cirrus SF50 · Engine Fuel and Control > FADEC CTRL DEGRADED 58 (FUEL METERING VALVE) ENGINE POWER FLUCTUATES AT MCT ON LANDING, THRUST LEVER IDLE POWER REMAINED AT 26% - [SDR VJ3R202209070016](https://openairdocs.org/sdr/VJ3R202209070016.md): Housing · broken · Aug 22, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070015](https://openairdocs.org/sdr/VJ3R202209070015.md): Housing · broken · Aug 10, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070014](https://openairdocs.org/sdr/VJ3R202209070014.md): Housing · broken · Jul 27, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070013](https://openairdocs.org/sdr/VJ3R202209070013.md): Housing · broken · Jul 11, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070012](https://openairdocs.org/sdr/VJ3R202209070012.md): Housing · broken · Jun 30, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070011](https://openairdocs.org/sdr/VJ3R202209070011.md): Housing · broken · Jun 29, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070010](https://openairdocs.org/sdr/VJ3R202209070010.md): Housing · broken · Jun 28, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070009](https://openairdocs.org/sdr/VJ3R202209070009.md): Housing · broken · Jun 28, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070008](https://openairdocs.org/sdr/VJ3R202209070008.md): Housing · broken · Jun 27, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070007](https://openairdocs.org/sdr/VJ3R202209070007.md): Housing · broken · Jun 27, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070006](https://openairdocs.org/sdr/VJ3R202209070006.md): Housing · broken · Jun 10, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070005](https://openairdocs.org/sdr/VJ3R202209070005.md): Housing · broken · May 23, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070004](https://openairdocs.org/sdr/VJ3R202209070004.md): Housing · broken · May 23, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070003](https://openairdocs.org/sdr/VJ3R202209070003.md): Housing · broken · May 23, 2022 · Cirrus SF50 · Ignition System > THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED - [SDR VJ3R202209070001](https://openairdocs.org/sdr/VJ3R202209070001.md): Housing · broken · Apr 8, 2022 · Cirrus SF50 · Ignition System > RETARD BREAKER POINT LEAD WIRE ATTACHED TO DISTRIBUTOR HOUSING, HAS TERMINAL END BROKEN. WIRE IS TOO SHORT TO CRIMP NEW TERMINAL END ON. WIRE IS ATTACHED TO HOUSING WITH EPOXY LIKE COVERING AND NO ALLOWANCE IN THE MAINTENANCE MANUAL FOR SPLICING OR REPLACING - [SDR 2022F00062](https://openairdocs.org/sdr/2022F00062.md): None · none · Feb 17, 2022 · N26VJ · Cirrus SF50 · Fuselage Structure (General) > FADEC CRTL DEGRADED. FADEC NO DISPATCH. - [SDR 2021FA0000408](https://openairdocs.org/sdr/2021FA0000408.md): Transponder · defective · Dec 18, 2021 · N81DX · Cirrus SF50 · Pneumatic System > SLC IS REPORTING N1DX, AN R66 IN FLORIDA, AS WELL AS N81DX OUT OF SLC AS N1DX. IT IS NOT A ONE TIME OCCURRENCE. IT’S BEEN GOING ON FOR MONTHS. - [SDR 2021F00381](https://openairdocs.org/sdr/2021F00381.md): Pitot System · frozen · Dec 6, 2021 · N102J · Cirrus SF50 · Pitot/Static System > DISCREPANCY FROM PILOT MARK HARRIS; SFD IAS AND ALT MISCOMPARE ALERTS FOLLOWED BY FROZEN IAS AND ALTITUDE INDICATIONS. AT 6000, INSTRUMENTS RETURNED TO NORMAL. FINDINGS AND FIX ARE STILL IN WORKS AND WILL BE REPORT ONCE COMPLETED. CIRRUS AIR SAFETY TEAM - [SDR VSNA20211120001](https://openairdocs.org/sdr/VSNA20211120001.md): Duct · unsecure · Nov 1, 2021 · N803LU · Cirrus SF50 · Air Distribution System > ON DEPARTURE, RECEIVED ECS CONTROL OVERHEAT, ECS CONTROL FAIL, TCV FAIL, AND A BURNING ODOR. TROUBLESHOT THE BLEED AIR SYSTEM TO SEE THE CAUSE OF THE CAS MESSAGES. FOUND THE AIRE DUCT LOOSE ON THE RAM AIR PLENUM TO BASS HEAT EXCHANGER PLENUM IN THE TAIL CONE - [SDR 2021F00046](https://openairdocs.org/sdr/2021F00046.md): Fault Message · false activation · Mar 7, 2021 · N21VJ · Cirrus SF50 · Fuel Controlling System > DURING CRUISE FLIGHT WITH ENGINE IPS HEAT ON FOR APPROX. 30 MIN. IN IMC FLIGHT CONDITIONS THE CAS WARNING RED "FADEC NO DISPATCH" AND AMBER FADEC DEGRADE ILLUMINATED AND COULD NOT BE RESET AS INSTRUCTED IN THE PILOTS CHECK LIST. PILOT HAD FULL CONTROL AT ALL - [SDR VSNA202102230001](https://openairdocs.org/sdr/VSNA202102230001.md): B-Nut · leaking · Feb 8, 2021 · N15VJ · Cirrus SF50 · Hydraulic System, Main > AIRCRAFT AFTER TAKEOFF AND AFTER THE LANDING GEAR WAS RETRACTED THE RIGHT MAIN GEAR REMAINED DOWN AND LOCKED, THE LEFT MAIN AND NOSE GEAR RETRACTED NORMALLY. PILOT SELECTED THE LANDING GEAR DOWN AND THE TWO EXTENDED AND ALL THREE INDICATED DOWN AND LOCKED. P - [SDR ESMR2019092601](https://openairdocs.org/sdr/ESMR2019092601.md): Actuator · defective · Sep 20, 2019 · N204HS · Cirrus SF50 · Stabilizer Actuator > PILOT ABORTED TAKEOFF DUE TO ABNORMAL PITCH CONTROL PRESSURE NEEDED TO ROTATE / TAKEOFF. THE LT MAIN WHEEL / TIRE ASSEMBLY WAS LOCKED UP IN THE PROCESS OF STOPPING THE AIRCRAFT WITH THE BRAKES. THE ENSUING 2100 + FOOT SKID DESTROYED THE TIRE, AND SEVERELY DAMA - [SDR AMCR20181218005](https://openairdocs.org/sdr/AMCR20181218005.md): Start Button · stuck · Dec 17, 2018 · N679DV · Cirrus SF50 · Engine Starter > DURING ELECTRICAL POWER-UP IN THE HANGAR FOR A MAINTENANCE POSTFLIGHT INSPECTION, THE ENGINE IMMEDIATELY STARTED TO MOTOR. THE BATTERY SWITCHES WERE TURNED BACK OFF AND THE MOTORING STOPPED. WHILE EXAMINING THE START/STOP PUSHBUTTON SWITCH, THE SWITCH WAS FOUN - [SDR WI5R2018101200000](https://openairdocs.org/sdr/WI5R2018101200000.md): Blade · missing · Oct 12, 2018 · N52CV · Cirrus SF50 · Turbine Engine Compressor Section > AFTER A FIELD EVENT, THE REQUIRED VIBRATION TESTING INDICATED UNACCEPTABLE 1ELP LEVELS AROUND.8 IPS. FIELD TROUBLE SHOOTING DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE HAS CONFIRMED ONE MISSING 3RD STAGE IP BLADE. THE IP ROTOR - [SDR WI5R.20180606](https://openairdocs.org/sdr/WI5R.20180606.md): Rotor · fractured · Jun 5, 2018 · N9943H · Cirrus SF50 · Turbine Engine Compressor Section > THE ACFT WAS SQUAWKED FOR A BANG NOISE DURING FLIGHT. THE ENGINE WAS BORESCOPE INSPECTED AND FOUND TO HAVE A DAMAGED HPC ROTOR. DISASSEMBLY OF THE ENGINE REVEALED A MISSING THIRRD STAGE IP BLADE. HPC ROTOR WAS SECONDARY DAMAGE. - [SDR 2018FA0000103](https://openairdocs.org/sdr/2018FA0000103.md): Duct · melted · Mar 13, 2018 · N344PV · Cirrus SF50 · Pneumatic Distribution System > ECS BLEED HOT AND THEN OVERHEAT MESSAGE. ON REMOVING THE INTERIOR OF THE BAGGAGE COMPARTMENT, IT WAS DISCOVERED THAT THE RAM AIR PLENUM HAD MELTED. FURTHER REVIEW SHOWED THAT THE RAM AIR DUCT HAD COME OFF OF THE PLENUM ITSELF. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 aircraft_model_key = 'SF50' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cirrus-design-sf50/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.