Often on the net the question is asked "can the KR qualify as light sport"?  Another option might be "self-launching motor glider".

Here are the requirements.

(  The FAA policy staff has confirmed to EAA that the previously referenced advisory circular, AC 21.17-2, remains valid guidance despite it not being referenced in the order. They are considering adding the reference back in the next revision.

AC 21.17-2 defines a self-launching glider as:

a) The number of occupants does not exceed two
b) Maximum weight does not exceed 850 kg (1874 pounds), and
c) The maximum weight to wing span squared (w/b2) does not exceed 3.0 kg/m2 (0.62 lb./ft.2) )

Does anyone know, is maximum weight the maximum T.O. weight with pilot / passenger or the empty weight of the aircraft?    If "empty weight" then a KR1 with a 25' wingspan would be 625 pounds, an easy mark to hit.  If "maximum T.O. weight then a 500 pound KR1 with 28' span, a 200 pound pilot, and 14 gallon of fuel would be legal.  Huummmmmmm..................

Isn't the medical requirement for "self-launching motor glider" just a drivers license?

Larry Flesner

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