Ad
related to: continental fuel injection system maintenance cost
Search results
Results from the WOW.Com Content Network
The fuel-injected IO-240-A and -B were introduced in 1993. The A and B versions differ only in the type of fuel injector used. [1] [4] The IOF-240 is similar to the IO-240-B except that it employs an Aerosance FADEC system to control the ignition and fuel injection systems. [1]
The Continental IO-520 is a six-cylinder, horizontally opposed aircraft engine produced by Teledyne Continental Motors. First run in 1963 as a development of the IO-346 , it has been produced in versions incorporating fuel injection ( IO-520 ), turbo-charging ( TSIO-520 ), and gearing ( GTSIO-520 ).
Same as the IO-360-HB except for the modified spider induction system and the use of a TCM 639289A95 fuel injector. The crankshaft has one 6th and one 4½ order damper. [4] IO-360-G 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector.
The Continental IO-346 engine is a fuel-injected four-cylinder aircraft engine that was developed especially for the Beechcraft Musketeer Custom III by Continental Motors. It was produced for that aircraft between 1965 and 1969.
The Continental IO-550 engine is a large family of 9 liter fuel injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in light aircraft by Teledyne Continental Motors. The first IO-550 was delivered in 1983 and the type remains in production.
By the 1960s turbocharging and fuel injection arrived in general aviation and the company's IO-520 series came to dominate the market. [citation needed] In 1965, Ryan Aeronautical acquired a 50% stake in Continental Motors. [10] In 1969, Teledyne Incorporated acquired Continental Motors, which became Teledyne Continental Motors (TCM). [11]
The Continental IO-370 engine is a family of fuel injected four-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in light aircraft by Continental Aerospace Technologies. There is no carbureted version of this engine, which would have been designation O-370, therefore the base model is the IO-370.
Same as the A1A but with a Simmonds Type 530 fuel injector and without a tuned induction system. [2] [4] IO-360-B1B 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the B1A but with a Bendix RSA-5AD1 injector. Fuel pressure limit at inlet to diaphragm pump. [2] [4] IO-360-B1C
Ad
related to: continental fuel injection system maintenance cost