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KFM 107

The KFM 107 is a two-cylinder, two-stroke, single ignition, horizontally opposed aircraft engine designed for ultralight aircraft and motor gliders.

Development
The KFM 107 is a conventional twin-cylinder engine that is very compact and light weight at only in its 107s version. The engine features single capacitor discharge ignition, a single Tillotson butterfly-type carburetor, integral fuel pump, tuned exhaust system and reed valve induction. It was offered with 2:1 belt drive reduction system. Starting is electric starter or recoil starter. Most versions of the 107 produce at 6300 rpm for five minutes for take-off and at 6080 rpm continuous. ==Variants==
Variants
;107s: "Standard" version, direct drive, recoil start, , weight ==Applications==
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