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THE 360 SERIES IS A FAMILY OF AIR COOLED, NATURALLY ASPIRATED, HORIZONTALLY OPPOSED, 6-CYLINDER, GASOLINE, FUEL INJECTED, SPARK IGNITION, FOUR-STROKE, DIRECT DRIVE, RIGHT (CW) ROTATING, AIRCRAFT ENGINE WITH MANUAL ENGINE CONTROLS FOR FIXED WING AIRCRAFT. CERTIFIED FUELS: 100/100LL . AvGas minimum & alternative fuels. DISPLACEMENT:
aircraft operating instructions established by the airframe manufacturer. Continental Motors engine operating instructions are developed using factory controlled parameters that are not necessarily the same as those specifications required to satisfy a specific aircraft I engine installation. Because of this difference the
Engines of models described herein conforming with this data sheet (which is a part of Type Certificate No. 286) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulation...
This data sheet which is part of Type Certificate No. A37CE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
You can find the TCDS for an aircraft on our website. You can also contact your nearest Flight Standards District Office , Aircraft Certification Office, or Manufacturing Inspection District Office.
Air Speeds. Flight Envelope. Approved Operations Capability Wing Span: 10,81m Length: 8,30m Height: 2,25m. Engine 1: Lycoming O-360-A1A Engine 2: Lycoming O-360-A1AD Engine 3: Lycoming O-360-A1D Engine 4: Lycoming O-360-A2A Engine 1 - 4: US E-286 Maximum speed 2700rpm Maximum continuous speed 2700rpm n = +3,8.
Note: The engine dry mass is based on the basic engine specification which includes: engine loom with brackets, electrical engine starter, oil-coolant heat exchanger, integrated oil tank, exhaust systems with turbochargers and wastegates, oil pumps and water pumps.
