Continental LTSIO-360-RB
Service difficulty reports · 30
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 = 'LTSIO360RB' 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 = 'LTSIO360RB' 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 2016FA0000554Bolt · not reported
DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, INDEX NUMBER 90) DAMAGED CHANNEL-TUNEL-RIGHT, PN95599-003 (SECTION II, FUSELAGE GROUP, FIGURE NR 12, INSDR AU510002135Pump · contaminatedRT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002136Pump · contaminatedRT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AU510002141Pump · contaminatedRT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.SDR AUS20040254Servo · contaminated(AUS) RT ENGINE FCU REGULATOR AIR SECTION CONTAMINATED WITH OIL.SDR 2002FA0001225Magneto · inoperativeWHILE TRAINING, A/C SIMULATED ZERO THRUST SINGLE ENGINE APPROACH. WHEN POWER WAS REAPPLIED, ENGINE WAS FOUND DEAD AND WOULD NOT RESPOND TO ANY INPUTS FOUND IN EMERGENCY PROCEDURES CHECKLIST. A SINGLE ENGINE LANDING WAS MADE WITHOUT INCIDENT. FOUND BOTH MAGNSDR 2002F00934Flange · failedTHE ATTACHMENT FLANGE OF THE INDUCTION MANIFOLD (NR2 CYLINDER) FAILED CAUSING ROUGH RUNNING OF THE ENGINE.SDR AUS20020509Washer · unlocked(AUS) RT ENGINE SCAVENGE PUMP COVER BOLT TAB WASHERS WERE NOT LOCKED. THE BOLTS WERE TIGHT. AREA HAD NOT BEEN DISTURBED SINCE FACTORY ASSEMBLY.SDR 20010425CW003Piston · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN FLIGHT AND ON THE GROUND CONTROLLER REPLACED.SDR 20010411CW012Servo · inoperativeCOULD NOT ADJUST OVERLY RIGHT MIXTURE. SENT FOR FACTORY SERVICE. INSTALLED ON AIRCRAFT STILL COULD NOT ADJUST. SENT BACK TO FACTORY FOR REPAIRS. NOTE THESE UNITS ARE INSTALLED ON NEW AIRCRAFT, THIS IS 3RD SET OF SERVOS ON THIS AIRCRAFT.SDR 20001102SH002Controller · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20001102SH003Servo · inoperativeUNABLE TO ADJUST MIXTURE AND IDLE WILL NOT STAY SET. (X)SDR 20001019SH017Servo · malfunctionedIN-FLIGHT, WHEN MIXTURE WAS LEANED TO CRUISE SETTING AT ABOUT 9 GALLON/HOUR, THE MIXTURE WENT UP TO 3 GALLONS PER HOUR. SERVO REMOVED AND A NEW ONE INSTALLED IAW PIPER MANUAL. (X)SDR 20001017SH009Controller · maladjustmentTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20001017SH020Servo · failedENGINE DIED AT IDLE, UNABLE TO ADJUST MIXTURE. (X)SDR 20001017SH019Controller · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20001019SH021Controller · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20000913SH030Servo · inoperativeUNABLE TO ADJUST FUEL FLOW AND IDLE MIXTURE. NEW SERVO. (X)SDR 20000913SH031Servo · malfunctionedFUEL FLOW RIGHT ENGINE DROP 3 GALLONS PER HOUR. IN-FLIGHT, CHT AND TIT TEMP WENT HIGHER THAN THE OTHER ENGINE. ENGINE STARTED TO RUN ROUGH. ENGINE WAS SHUT DOWN IN-FLIGHT AND A SAFE LANDING ON ONE ENGINE WAS MADE. INSPECTION OF ENGINE FOUND THE RIGHT FUEL SDR 20000912SH025Pump · failedWITH TOP END FUEL PRESSURE SET IAW SPEC, AT IDLE, THE PUMP PRESSURE DROPS TO LOW. LESS THAN 25 PSI TO OPERATE FUEL SERVO AT IDLE. (X)SDR 20000911SH033Servo · faultyENGINE RUNNING RICH AND BLOWING BLACK SMOKE. UNABLE TO ADJUST MIXTURE. REMOVED AND SENT BACK TO TCM. (X)SDR 20000925SH032Servo · failedTHROTTLE HARD TO MOVE IN FLIGHT, SERVO REMOVED AND A NEW ONE INSTALLED. OVER FOUR POUNDS TO MOVE CONTROL. (X)SDR 20000925SH033Tube · crackedNR 2 INTAKE TUBE ON RIGHT ENGINE CRACKED AT THE FLANGE WHERE IT MOUNTS TO THE CYLINDER . INTAKE TUBE WAS REPLACED AND TCM HAS BEEN INFORMED. (X)SDR 20000925SH034Tube · crackedNR 6 INTAKE TUBE ON RIGHT ENGINE CRACKED AT THE FLANGE WHERE IT MOUNTS TO THE CYLINDER. INTAKE TUBE WAS REPLACED AND TCM HAS BEEN INFORMED. (X)SDR 20000925SH039Tube · crackedTHE PILOT REPORTED THE RIGHT ENGINE RUNNING ROUGH AND VIBRATION. THE ENGINE WAS SHUT DOWN AND A SAFE LANDING WAS MADE. AIRCRAFT WAS TAKEN TO MAINTENANCE AND INSPECTION WAS DONE ON THE ENGINE, NR 4 INTAKE TUBE WAS FOUND CRACKED AT THE FLANGE OF TUBE WHERE IT SDR 20000925SH040Servo · failedWHEN BOOST PUMP IS TURNED ON, FUEL FLOW DROPS, ENGINE RUNS ON THE LEAN SIDE. REPLACED SERVO. (X)SDR 20000925SH036Servo · failedSTIFF THROTTLE ARM, OVER 4 POUNDS TO MOVE CONTROL. (X)SDR 20000919SH020Pump · inoperativeIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)SDR 20000919SH022Pump · inoperativeIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)SDR 20000912SH026Pump · failedIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. PRESSURE WAS ALSO ERRATIC. (X)
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