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  2. Continental O-200 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-200

    The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.

  3. Superior Air Parts - Wikipedia

    en.wikipedia.org/wiki/Superior_Air_Parts

    Thielert already had a business relationship with Superior, as it had been engaged in the production of Superior's after-market engine cylinders. [ 3 ] In 2008, Superior Air Parts' parent company Thielert declared bankruptcy , Superior itself filed for Chapter 11 bankruptcy on 31 December 2008 and laid off many of its staff.

  4. Rolls-Royce/Continental O-200-A - Wikipedia

    en.wikipedia.org/.../Continental_O-200-A&redirect=no

    Retrieved from "https://en.wikipedia.org/w/index.php?title=Rolls-Royce/Continental_O-200-A&oldid=540102732"

  5. Franklin O-200 - Wikipedia

    en.wikipedia.org/wiki/Franklin_O-200

    The Franklin O-200 (company designation 4AC-199) was an American air-cooled aircraft engine of the early 1940s. The engine was of four-cylinder, horizontally-opposed layout and displaced 200 cu in (3 L). The power output ranged between 65 hp (48 kW) and 100 hp (75 kW) depending on variant. The O-200-5 (4ACG-199) featured a geared propeller drive.

  6. Lycoming IO-390 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_IO-390

    The IO-390 was developed from the similar IO-360 engine, by using cylinders from the IO-580 [citation needed] to increase the O-360's cylinder bore. (Although the IO-390 cylinder assembly [ 4 ] is not the same part number as the IO-580, [ 5 ] the cylinder barrels of both have a 5.318 bore and 4.375 stroke dimension.)

  7. List of Lycoming O-360 variants - Wikipedia

    en.wikipedia.org/wiki/List_of_Lycoming_O-360...

    200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1A but uses a fixed-pitch propeller. [4] AIO-360-A2B 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1A but has one impulse coupling magneto and provision for a fixed-pitch propeller.

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    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!

  9. Lycoming Engines - Wikipedia

    en.wikipedia.org/wiki/Lycoming_Engines

    Lycoming Engines is a major American manufacturer of aircraft engines.With a factory in Williamsport, Pennsylvania, Lycoming produces a line of horizontally opposed, air-cooled, four, six and eight-cylinder engines including the only FAA-certified aerobatic and helicopter piston engines on the market.