Amateur built aircraft are not type certified. These requirements do not
apply.

On Mon, Jul 9, 2018 at 8:26 AM, Kayak via KRnet <krnet@list.krnet.org>
wrote:

> I looked into this and a motor glider must have certain specs to qualify.
>
> IIRC, wing span to gross weight.  However, the sonex page states that
> tyhis may not apply to experimental category, and certainly a 27ft
> wingspan on a KR1 would fly more like a glider. Especially if equipped
> with a full feathering prop for example.
>
> Here it is:
>
> https://www.sonexaircraft.com/aircraft-certification/
>
>
> Definition of Motorglider or Powered Sailplane
>
> Sonex Aircraft, LLC accepts the formal definition of Powered
> Sailplanes for Type Certificated Aircraft from both the United States
> and the European Aviation Authorities. While it is not formally
> defined that an Aircraft Registered in the Experimental Category must
> meet these same criteria, any aircraft which does meet the criteria is
> an indisputable "Motorglider" or "Powered Sailplane." The language in
> both the U.S. and the European documents are nearly identical and the
> portion of the documents which apply to this definition as follows:
>
>
>
> United States Department of Transportation, Federal Aviation Administration
> Advisory Circular AC 21-17a, dated 10 February 1993
>
> 7. ACCEPTABLE CRITERIA.
>   b. Additional Criteria for Powered Gliders.
>     (1) Powered fixed wing gliders may be type certificated under
> Section 21.17(b) if:
>       (i) The number of occupants does not exceed two;
>       (ii) Maximum weight does not exceed 850 kg (1874 pounds); and
>       (iii) The maximum weight to wing span squared (w/b2) does not
> exceed 3.0 kg/M2 (0.62 lb./ft.2).
> NOTE: These criteria originated from JAR-22.
>
> Joint Aviation Authorities
> JAR-22 Amendment 7, dated 1 September 2003
>
> JAR 22.1 Applicability
> (a) This JAR-22 prescribes minimum airworthiness standards for the
> issue of type certificates, and changes to those certificates, for
> sailplanes and powered sailplanes in the utility U and aerobatic A
> categories:
>   (1)  Sailplanes the maximum weight of which does not exceed 750 kg:
>   (2)  Single engine (spark- or compression-ignition) powered
> sailplanes the design value W/b2 (weight to span2) of which is not
> greater than 3(W[kg], b[m]) and the maximum weight of which does not
> exceed 850 kg: and
>   (3)  Sailplanes and powered sailplanes the number of occupants of
> which does not exceed two.
>
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