Williams FJ33-5A
Service difficulty reports · 19
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'FJ335A' 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 engine_model_key = 'FJ335A' 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 2026FA0000432Fadec · faultedPART 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 CHESDR 2025F00193Fuel Control · failedRECEIVED 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 PCPR202411071Brake Pads · disintegratedDURING 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 ASDR WI5R2023112100001Compressor · damagedDURING “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, THSDR WI5R2023111700001Compressor · damagedFJ33-5A 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 WILLIAMSSDR 2023FA0000535Unknown · unknownLANDING GEAR WOULD NOT EXTEND NORMALLY. EXTENDED GEAR USING ALTERNATE GEAR EXTENSION.SDR 2023F00264Unknown · unknownAILERON TRIM NOT RESPONDING; A/C DIFFICULT TO CONTROL; PULL CB; STILL COULD ONLY GET LIMITED CONTROLSDR 2023FA0000367Shutoff Valve · unknownDURING CLIMBOUT ECS BLEED OVERHEAT OBSERVED AND SMELL OF BURNING IN CABINSDR 2023F00101Sensor · inoperativeOIL PRESSURE WARNING IN FLIGHT AND LOSS OF OIL PRESSURE INDICATIONS ON EIS DISPLAYSDR 2023F00047Not Reported · not reportedBOTH FUEL VALVES FAILED.SDR 2023F00041Not Entered · not enteredMULTIPLE 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 NSDR 2022FA0000732Autothrottle Sys · malfunctionedPILOT 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 INVESDR 2022FA0000593None · noneFUEL VAVLE BOTH FAILSDR 2022F00330Fuel Control · abnormalFADEC CTRL DEGRADED 58 (FUEL METERING VALVE) ENGINE POWER FLUCTUATES AT MCT ON LANDING, THRUST LEVER IDLE POWER REMAINED AT 26%SDR 2022F00062None · noneFADEC CRTL DEGRADED. FADEC NO DISPATCH.SDR 2021F00046Fault Message · false activationDURING 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 ESMR2019092601Actuator · defectivePILOT 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 DAMASDR WI5R2018101200000Blade · missingAFTER 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.20180606Rotor · fracturedTHE 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.
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