Continental TSIO-360-MB
Service difficulty reports · 17
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 = 'TSIO360MB' 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 = 'TSIO360MB' 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 2016FA0000363B-Nut · brokenFUEL LINE FROM PRIMER SOLENOID TO THROTTLE BODY,BROKE IN HALF UNDER B-NUT, CAUSING THE ENGINE TO LOSE FUEL SUPPLY TO THROTTLE BODY.SDR CA140730017Tube · worn(CAN) DURING A TRIM SERVO REPLACEMENT. THE TRIM TUBE ASSEMBLY WAS RUBBING ON A RIVET LOCATED ON THE ELT SHELF IN THE TAIL OF THE AIRCRAFT. THE TUBE HAS A WALL OF 0.035" OF THICKNESS. TUBE WAS WORN TO A WALL THICKNESS OF APPROX 0.10" THICK. TRIM TUBE WAS REPLACSDR FK8R20130311001Cylinder · crackedDURING ANNUAL INSPECTION, AN OIL LEAK WAS FOUND AT THE BOTTOM OF THE NR 2 CYLINDER AFTER WASHING THE ENGINE AND RUNNING IT AGAIN IT WAS NOTICED THAT THE OIL WAS LEAKING FROM THE CYLINDER IN THE AREA WHERE THE BARREL ATTACHES TO THE HEAD. THE CYLINDER HAD BEENSDR CSE001Magneto · misrepairedENGINE WILL NOT RUN ON LEFT MAGNETO. INSPECTION IN THE WORKSHOP REVEALED THAT THE WOODRUFF DRIVE KEY BETWEEN THE DRIVE SHAFT AND DRIVE COUPLING WAS MISSING.SDR AUS20030601Cylinder · failed(AUS) ENGINE NR 1 CYLINDER BARREL FAILED IN AREA APPROXIMATELY TWO FINS FROM TOP OF BARREL. CYLINDER HEAD AND ATTACHED SECTION OF BARREL SEPARATED. SEVERE DAMAGE TO ENGINE.SDR 20001109SH025Vernatherm · bentRETAINING NUT ROLL PIN TO SECURE THE NUT. THE SHAFT ON WHICH THE NUT IS INSTALLED WAS BENT JUST BEHIND THE NUT. SUBMITTER HAS SEEN SEVERAL NOW WITH THIS CONDITION AND THEY ARE ALL FROM FACTORY REMAINS OR NEW ENGINES FROM RECENT YEARS. THIS ONE REBUILT 2-8-9SDR 20000331SH010Plate · mismanufacturedWHEN LT AND RT MAGNETOS WERE BEING INSTALLED ON ENGINE AFTER INTERNAL INSPECTION OF MAGNETOS, NOTED MAGNETO HOLD-DOWN PLATES FROM ENGINE STUD TO MAGNETO MOUNTING FLANGE ONLY ENGAGED FLANGE BY APPROXIMATELY .0625 INCH IF MOUNTED EVEN, OR ONLY ONE CORNER OF PLATSDR 20000331SH011Plate · mismanufacturedWHEN LT AND RT MAGNETOS WERE BEING INSTALLED ON ENGINE AFTER INTERNAL INSPECTION OF MAGS, NOTED MAGNETO HOLD-DOWN PLATES FROM ENGINE STUD TO MAGNETO MOUNTING FLANGE ONLY ENGAGED FLANGE BY APROXIMATELY .0625 INCH IF MOUNTED EVEN, OR ONLY ONE CORNER OF PLATE IS SDR CA990927036Bolt · failed(CAN) THROUGH-BOLT P/N 630693-1060 BROKE THROUGH BEFORE REACHING SPECIFIED TORQUE. UPON INSPECTION, IT WAS NOTED THAT A CRACK HAD DEVELOPED PREVIOUSLY AND ONLY ABOUT 50 PERCENT OF BOLT STILL HOLDING. PART REMOVED FROM SERVICE.SDR 98ZZZX2459Induction Tube · crackedNOTICED FUEL STAINS AROUND CYLINDER NR 3. REMOVED AND INSPECTED, INDUCTION TUBE WAS CRACKED AROUND FLANGE.SDR 98ZZZX1856Intake Tube · crackedINTAKE TUBE CRACKED AT FLANGE. SUBMITTER STATED RESEARCH OF AIRCRAFT RECORDS DETERMINED THIS WAS THE THIRD INDUCTION TUBE IN THIS LOCATION THAT HAD CRACKED IN 1,100 HOURS. PART MISALIGNED WITH INDUCTION PLENUM.SDR 97ZZZX3088Impulse Cam · crackedHEARD LOUD POP WHEN INSTALLING IMPULSE ASSEMBLY WHEN 15 POUNDS/FOOT OF TORQUE WAS REACHED. REMOVED AND FOUND INNER HUB OF IMPULSE CRACKED IN THREE PLACES.SDR 97ZZZX806Hose · bindDURING C/W SB M81-21, IT WAS NOTED TURBO OIL LINE WAS SHORT AND IN A BIND. SUBMITTER SUGGESTS ADDING 45 DEGREE FITTING ON HOSES TO RELIEVE PROBLEM.SDR AU960232Cylinder · separated(AUS) NO4 CYLINDER HEAD SEPARATED FROM CYLINDER BARREL IN AREA OF SCREWTHREADS - PRE-EXISTING CRACK IN SCREW THREAD AREASDR 95ZZZX5234Guide Seal · defectiveAFTER COMPLAINCE WITH TELEDYNE CONTINENTAL SB CSB-95-4 REGARDING IMPROPERLY INSTALLED INTAKE VALVE GUIDE SEALS, FOUND 2 OF 6 DEFECTIVE SEALS ON ENGINE NOTED. TWO FWD CYLINDERS NR 5 AND NR 6 HAD BROKEN SEALS. REMOVED AND REPLACED ALL INTAKE VALVE GUIDE SEALS SDR 95ZZZX4593Gasket · screws looseAFTER TALKING TO ANOTHER MECHANIC WHO HAD SIMILAR PROBLEM (LOOSE ROCKER COVER SCREWS), CHECKED SUBJECT AIRCRAFT AND FOUND LIKE CONDITION. DUE TO SILICONE GASKETS BEING INSTALLED, FOUND SCREWS WOULD LOOSEN OVER TIME. RE-INSTALLED SCREWS USING LOCKTITE TO PREVSDR 95ZZZX657Distributor · teeth failedENGINE DEVELOPED VIBRATION ON TAKEOFF. AFTER LANDING AND MAG CHECK, LT MAGNETO DEAD. DISASSEMBLY FOUND DISTRIBUTOR GEAR WITH EIGHT TEETH MISSING. FOUND ALL TEETH IN MAGNETO HOUSING. MAGNETO DISTRIBUTOR GEAR DATED 9-13-91 O/H BY MIDSTATES AIRCRAFT ENGINE, T
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