Lycoming Aircraft Engines: List of Lycoming O-360 Variants, Lycoming O-320, Lycoming O-235, Lycoming IO-390, Lycoming O-360, Lycoming Gso-580

9781155634500: Lycoming Aircraft Engines: List of Lycoming O-360 Variants, Lycoming O-320, Lycoming O-235, Lycoming IO-390, Lycoming O-360, Lycoming Gso-580

Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. Pages: 30. Chapters: List of Lycoming O-360 variants, Lycoming O-320, Lycoming O-235, Lycoming IO-390, Lycoming IO-720, Lycoming GSO-580, Lycoming TIO-541, Lycoming XR-7755, Lycoming O-145, Lycoming O-540, Lycoming O-290, Lycoming O-340, Lycoming IO-580, Lycoming IO-233, Lycoming O-480, Lycoming ALF 502, Lycoming T55, Lycoming R-680, Lycoming O-233, Lycoming O-435, Honeywell LF 507, Lycoming T53. Excerpt: This is a list of the variants of the Lycoming O-360 aircraft engine. There are 167 different models within the O-360 family of engines, with 12 different prefixes. O-360-A1A180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. The base model. A four cylinder, horizontally opposed, air cooled, direct drive engine which includes provisions for supplying oil through the propeller shaft for installation of a single-acting controllable pitch propeller. First certified 20 July 1955.O-360-A1AD180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except it is equipped with a Bendix D4LN-2021 dual magneto instead of two single magnetos.O-360-A1C180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except with a rear mounted Bendix carburetor and 200 series magnetos.O-360-A1D180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except with Bendix 200 series magnetos.O-360-A1F180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except with Bendix 1200 impulse coupling, high altitude magnetos.O-360-A1F6180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1F except with counter-weighted crankshaft. The Cessna 177B Cardinal uses a Lyco...

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