Английская Википедия:Continental IO-346

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Шаблон:Short description

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.[1]

Design and development

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 269¾ lb or 297 lb including the generator and starter. The ignition system consists of dual magnetos, one Scintilla S4RN-201 and one S4RN-205 or, alternatively, two Slick Electro 449 magnetos.[1][2]

Variants

IO-346-A
Base model, certified 27 July 1962[2]
IO-346-B
Identical to IO-346-A except it incorporates provisions for a hydraulic propeller control. Certified 23 June 1964.[2]

Applications

Файл:BeechcraftA23MusketeerC-FSJL.jpg
1965 model Beechcraft A23 Musketeer equipped with the IO-346 engine

Specifications (IO-346)

Reference: Engines for Homebuilt Aircraft & Ultralights[1] Шаблон:Pistonspecs

See also

References

Шаблон:Reflist


Шаблон:Continental aeroengines

  1. 1,0 1,1 1,2 1,3 1,4 1,5 1,6 1,7 Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 63. TAB Books, 1983. Шаблон:ISBN
  2. 2,0 2,1 2,2 2,3 Шаблон:Cite web