Williams FJ44: Difference between revisions - Wikipedia


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The '''Williams FJ44''' is a family of small, two-spool, [[turbofan]] engines produced by [[Williams International]]/[[Rolls-Royce Holdings|Rolls-Royce]] for the light [[light business jet]] market. Until the recent boom in the [[very light jet]] market, the FJ44 was one of the smallest turbofans available for civilian applications. Although basically a Williams design, Rolls-Royce was brought into the project, at an early stage, to design, develop and manufacture an air-cooled high-pressure (HP) turbine for the engine. The FJ44 first flew on July 12, 1988 on the [[Scaled Composites Triumph|Scaled Composites/Beechcraft Triumph]] aircraft.

The [[Williams FJ33]] is a smaller engine based on the basic FJ44 design.