Scheibe SF 40: Difference between revisions
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[[Category:German civil utility aircraft |
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[[Category:Scheibe aircraft|Scheibe]] |
[[Category:Scheibe aircraft|Scheibe]] |
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Revision as of 09:36, 23 October 2017
| SF 40 Allround | |
|---|---|
| Role | Ultralight monoplane |
| National origin | Germany |
| Manufacturer | Scheibe Aircraft |
| First flight | 1995 |
The Scheibe SF 40 is a German two-seat ultralight aircraft designed and built by Scheibe Aircraft.
Design
The SF 40 is a two-seat low-wing ultralight monoplane with a fixed tricycle landing gear.[1] It has a fabric-covered steel-tube fuselage with fabric-covered glass-fibre wings.[1] The first SF 40 powered by a Sauer four-stroke engine flew in 1995 but after five were built it was replaced in 1997 by an improved variant, the SF 40C.[1] The SF 40C is powered by a Rotax 912 engine with a two-bladed propellor, a shorter wing span than the original with increased fuel capacity.[1] The SF 40C was awarded a type certificate in May 1998.[1]
Variants
Specifications (SF 40C)
Data from [1]
General characteristics
- Crew: 2
Performance
References
- Notes
- Bibliography
- Paul Jackson, ed. (1999). Jane's All the World's Aircraft 1999-2000. Jane's Information Group Limited. ISBN 0-7106-1898-0.
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