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Four-cylinder, horizontally opposed, 340.4 cubic inches (5.58 litres), 170 hp (127 kW) at 2700, dry weight 250 lb (113 kg), Marvel-Schebler MA-4-5 carburetor, Scintilla S4LN-20 and S4LN-21 magneto. Minimum fuel grade 91/96 avgas. Identical to the A1A but with no provision for a hydraulic propeller control. Certified on 16 November 1956. [2]
Engine model with increased maximum continuous rating and the generator pad omitted, approved for helicopter installations. It produces 250 hp (186 kW) at 3000 rpm, with a compression ratio of 7.3:1, a dry weight of 405 lb (184 kg) and fitted with a Marvel MA-4-5 carburetor. Type certified on March 30, 1951. [1] O-435-2 Military engine model. [4]
In 1950 Standard introduced the Hygrade System, simplified carburetor kits for tune-ups and light overhauls. [3] Standard Motor Products had its Initial public offering in 1960 [3] and was listed on the New York Stock Exchange (NYSE) in 1977. [4] [5] [6] In 1963 it entered the wholesale parts market with a new subsidiary, Marathon Parts. [3]
250 hp (186 kW) at 2600 rpm, dry weight 484 lb (220 kg), supercharged model. Certified 2 February 1955. [4] O-470-4 225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), previously designated 0-470-13B. It is identical to the Model 0-470-13A except for the Bendix-Stromberg Model PS-5CD carburetor in place of the PS-5C.
The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2. [4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3 ⁄ 16 inch (4.8 mm), developing 210 hp (160 kW). [5] [6]
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