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The Wheeler–Schebler Carburetor Company was one of the Indianapolis's most important auto parts manufacturers and the last automobile parts factories in Indianapolis, Indiana to survive from the first decades of the 20th century. The Wheeler–Schebler Carburetor Company Building was the company's original building at the Barth Avenue site. [3]
It produces 260 hp (194 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 468 lb (212 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on May 12, 1961. [3] TVO-435-B1A (military designation O-435-25A)
The Marvel Oil Company (also known as Marvel Carburetor Company; Marvel-Schebler Carburetors since 1928) was founded by Burt Pierce in 1923. [2] Before World War I, the company produced carburetors for automobiles and aircraft. Some of these encountered problems with clogged jets, prompting Pierce to formulate a blend of chemicals and petroleum ...
The Continental O-470 engine is a family of carbureted and fuel-injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed especially for use in light aircraft by Continental Motors. Engines designated "IO" are fuel-injected. [1] [2]
Walbro and Tillotson carburetors for small engines. Weber carburetor, Italian, now made in Spain, owned by Magneti Marelli. Wheeler–Schebler Carburetor Company. Zama Group, primarily an OEM provider. Zenith Carburetor Company, American subsidiary of Société du carburateur Zénith. Zenith Carburettor Company (British), used on Austin cars.
The 130 hp (97 kW) O-240 was a new engine design derived from the six-cylinder Continental O-360 and introduced in 1971. It is generally similar in overall dimensions to the Continental O-200, but with a higher 8.5:1 compression ratio, designed to run on 100/130 avgas.
In May 1963 a new injection system designed by Rochester was installed that produced nearly the same output as the Marvel-Schebler system. Performance of the most recent development engine was compared with a 4X1 140 hp (104.4 kW) engine on 5 November 1963; the injected engine produced approximately 14 hp (10.4 kW) more.
180 hp (134 kW) at 2900 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1D but with dynafocal mounts and a different series Marvel carburetor. [1] [2] HO-360-B1A 180 hp (134 kW) at 2900 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as C2D but with a different cam shaft. [1] [2] HO-360-B1B