Search results
Results from the WOW.Com Content Network
The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces 175 hp (130 kW) whereas the ungeared O-300 produces 145 hp (108 kW). [1] The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines.
Continental O-300; Continental O-470; Continental IO-520; Continental O-526; R. Continental R-670; T. Continental T51; Continental CD-230; Continental Tiara series
The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010. [1] [2] The engine is available in both naturally aspirated, fuel injected IO-360 models and turbocharged TSIO-360 ...
In 1905, Continental Motors was born with the introduction of a four-cylinder, four stroke cycle L-head engine operated by a single camshaft. In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [1] A Continental engine in a 1948 Divco delivery ...
There is no carbureted version of the engine, which would have been designated O-346 and therefore the base model is the IO-346. [1] [2] The IO-346 was designed to run on 91-98 avgas. The engine has a dry weight of 269.75–297 lb (122–135 kg) including the generator and starter.
Continental's 747 services from Chicago and Denver to Los Angeles and Honolulu set the standard for service in the western U.S. [7] [11] On June 1, 1972, Continental's widebody DC-10 service began. Six had insisted that Continental place a large order for DC-10s with manufacturer McDonnell Douglas .
Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!
Same as the IO-360-A1B6 but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1C 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1C but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1D