# Service difficulty reports: Continental TSIO-360-CB A list on [Continental TSIO-360-CB](https://openairdocs.org/engine/continental-tsio-360-cb.md). Newest first. General aviation reporting is voluntary. - [SDR 2015FA0000439](https://openairdocs.org/sdr/2015FA0000439.md): Engine · failed · Feb 3, 2015 · Cessna T337G · Engine (Reciprocating) > AFTER TAKEOFF, IN CRUISE FLIGHT AT 7,000' ASL, FRONT ENGINE OIL PRESSURE DROPPED TO LOWER RED-LINE LIMIT, OIL TEMPERATURE WAS NORMAL APPROXIMATELY 150F AND ENGINE RUNNING SMOOTHLY. WITHIN 10 SECONDS, ENGINE WENT FROM SMOOTH RUNNING CONDITION TO A LOSS OF 300- - [SDR YYE2008F00000](https://openairdocs.org/sdr/YYE2008F00000.md): Pump · failed · Dec 1, 2008 · N5CS · Cessna T337G · Hydraulic Pump (Electric/Engine), Main > THE PRIMARY ELECTRIC/ HYD LANDING GEAR PUMP FAILED. THE ATTEMPT TO LWR THE GEAR WITH THE MANUAL GEAR LEVER ALSO FAILED, RESULTING IN A GEAR UP LANDING. THE PRIMARY PUMP FAILURE MAY HAVE CAUSED THE MANUAL PUMP FAILURE. (K) - [SDR JNE2008F00000](https://openairdocs.org/sdr/JNE2008F00000.md): Starter · failed · Aug 21, 2008 · N1ZJ · Cessna T337G · Engine Starter > INSTALLED TWO FACTORY ENGINES. AFTER SEVERAL TEST RUNS, THE FRONT STARTER SOLENOID FAILED ON. REPLACED THE SOLENOID WITH AN NEW MFG SOLENOID. ON A TEST FLIGHT ELECTRICAL FAILURE OCCURRED. IT HAPPENED BECAUSE OF AN OVERLOAD OF THE BATTERY AND ELECTRICALSYST - [SDR 2005FA0000812](https://openairdocs.org/sdr/2005FA0000812.md): Landing Gear · vibrates · Jun 7, 2005 · N1169G · Amtr LANCAIRES · Nose/Tail Landing Gear > SEVERE NOSE GEAR SHIMMY DURING LANDING. NOSE GEAR STRUT SERVICED WITH MIL-H-5606, REQUIRED 30-WT FORK OIL. NEXT FLT A SEVERE SHIMMY AGAIN. INSP REVEALED ENG MOUNT BROKEN 6 PLACES AS A RESULT. ENG MOUNT & NOSE GEAR STRUT REPLACED, ON NEXT FLT, A SEVERE NOSE - [SDR CA041108007](https://openairdocs.org/sdr/CA041108007.md): Cable · frayed · Nov 5, 2004 · Cessna T337G · Autopilot Main Servo > (CAN) AT INSPECTION THE AUTOPILOT ROLL SERVO BRIDLE CABLE WAS FOUND TO BE FRAYED WHERE IT RUNS OVER IT'S PULLEYS. - [SDR CA040930002](https://openairdocs.org/sdr/CA040930002.md): Skin · cracked · Sep 29, 2004 · Cessna T337G · Wing, Plate/Skin > (CAN) DURING INSPECTION, CRACKS WERE DISCOVERED AT THE IB END OF THE LT AND RT UPPER OB WING SKINS WHERE THEY UNDERLAP THE FUEL TANK BAY COVERS. THE CRACKS ARE LOCATED IN THE RADIUS OF CUTOUT AREAS IN THE SKINS WHERE THE STINGERS JOIN AT WING STATION 150.0. T - [SDR 2004FA0000397](https://openairdocs.org/sdr/2004FA0000397.md): Impulse Coupling · broken · May 1, 2004 · N8AH · Cessna T337G · Magneto/Distributor > PILOT REPORTED REAR ENGINE WAS HARD TO START. AFTER TROUBLESHOOTING, THE LT MAGNETO WAS REMOVED. UPON INSPECTION THE IMPULSE COUPLING WOULD NOT ROTATE IN THE CORRECT DIRECTION. THE MECH WAS NOT SURE IF WRONG IMPULSE COUPLING OR SPRING TURN BACKWARD. DUE TO - [SDR CA040122002](https://openairdocs.org/sdr/CA040122002.md): Control Cable · frayed · Jan 21, 2004 · Cessna T337G · Trailing Edge Flap Control System > (CAN) DURING INSPECTION IT WAS DICOVERED THAT THESE CABLES (2EA. 1 LT AND 1 RT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE. - [SDR CA040122003](https://openairdocs.org/sdr/CA040122003.md): Control Cable · frayed · Jan 21, 2004 · Cessna T337G · Trailing Edge Flap Control System > (CAN) DURING INSPECTION IT WAS DISCOVERED THAT THESE CABLES (2EA. 1 LEFT AND 1 RIGHT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE. - [SDR CA031119004](https://openairdocs.org/sdr/CA031119004.md): Coupling · separated · Oct 30, 2003 · Cessna T337G · Exhaust Turbocharger > (CAN) COUPLING SEPARATED FROM TURBOCHARGER COMPRESSOR HOUSING CAUSING INDUCTION LEAK AND RESULTING POWER LOSS. - [SDR 2003FA0000433](https://openairdocs.org/sdr/2003FA0000433.md): Turbocharger · misinstalled · Mar 31, 2003 · Cessna P337H · Exhaust Turbocharger > TURBOCHARGER UNABLE TO BOOST MANIFOLD PRESSURE. REMOVED TURBOCHARGER AND FOUND EXCESSIVE CLEARANCE BETWEEN T-WHEEL AND HOT SECTION HOUSING. INCORRECT PARTS ASSEMBLED INTO A COMPLETE UNIT. INSPECT PRODUCT PRIOR TO RELEASING TO SERVICE. - [SDR CA991229039](https://openairdocs.org/sdr/CA991229039.md): Propeller · corroded · Dec 10, 1999 · Reims FT337GP · Propeller Assembly > (CAN) PROPELLER SEIZED DUE CORROSION. - [SDR 2000ZZZX364](https://openairdocs.org/sdr/2000ZZZX364.md): Crankshaft · cracked · Jul 1, 1999 · N2QJ · Cessna T337G · Reciprocating Engine Power Section > FOUND CRANKSHAFT FLANGE CRACKED (APPROXIMATELY 2.5 INCHES) ON BACK SIDE. ENGINE IS A FACTORY REBUILT WITH 48 HOURS AND NO RECORDED DAMAGE HISTORY. ENGINE INSTALLED IN REAR POSTION. - [SDR CA980811015](https://openairdocs.org/sdr/CA980811015.md): Cylinder · separated · Jul 31, 1998 · Cessna P337H · Reciprocating Engine Cylinder Section > (CAN) DURING FLIGHT, THE PILOT HEARD A LOUD NOISE, COMING FROM THE REAR ENGINE, FOLLOWED BY A DROP IN MANIFOLD PRESSURE AND ON LANDING A REDUCTION IN OIL PRESSURE. THE ENGINE SHUTDOWN ON THE RUNWAY. INSPECTION FOUND THE NR 4 CYLINDER SPLIT AT THE BARREL. - [SDR 96ZZZX700](https://openairdocs.org/sdr/96ZZZX700.md): Valve Guide · excess wear · Jan 30, 1996 · N777NB · Cessna T337G · Reciprocating Engine Cylinder Section > FREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS - [SDR 96ZZZX701](https://openairdocs.org/sdr/96ZZZX701.md): Valve · excess wear · Jan 30, 1996 · N777NB · Cessna T337G · Reciprocating Engine Cylinder Section > FREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS - [SDR 95ZZZX6536](https://openairdocs.org/sdr/95ZZZX6536.md): Crankshaft · cracked · Nov 14, 1995 · N6LH · Reciprocating Engine Power Section > ENGINE WAS WINDMILLING DURING A GEAR-UP LANDING (10-11-95) AT ROCKY MOUNTAIN AIRCARE. REPAIRED BELLY AND HAD PROP OVERHAULED AT H & H. REINSTALLED PROPELLER WITH A DIAL INDICATOR RUN-OUT CHK ONLY, WAS RETURNED TO SERVICE AS AIRWORTHY. DURING THE INSPECTION, ## 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 engine_model_key = 'TSIO360CB' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/continental-tsio-360-cb/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.