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SF 27 / 27M

SF 27 / 27M


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Developed in 1964 from the earlier Zugvogel and SF-26, the Sf-27A was a Standard Class design intended to compete with Schleicherメs Ka-6E. It has typical Scheibe steel-tube structure (with a fiberglass nose section), all-flying tail, Schempp-Hirth type dive brakes and semi- reclining seating. The wing ribs are spaced only 4 inches apart and heavy plywood skins cover 85 % of the surface in order to help maintain the laminar profile. The SF-27M was a self-launching version of the SF-27A. The 2-cycle, 4-cylinder Hirth engine and propeller are mounted on a retractable pylon behind the cockpit. ATC

construction

wingspan: 15 m
lenght: 7,05 m
weight of empty craft: 205 kg
max. take off weight: 320 kg

flying characteristic

cruising speed: 85 km/h
stall speed: 60 km/h
never exceeded speed: 200 km/h
gliding ratio: 34 at 85 km/h
published under GNU or Creative Commons Attribution-ShareAlike License 2-3.0.

09/06/2011
Můj \"Fanouš\" má MTOW 330 kg

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