Easy to meet that constraint, the stall speed is the one you need to be concerned about. And it has to be "clean", no lift devices required. You can have them, but they cannot be used to test the stall speed.
Gross weight will probably be the thing you most have to keep in check to be able to meet that requirement. On Thursday, March 26, 2015 1:47 PM, Sid Wood via KRnet <krnet at list.krnet.org> wrote: ============= My hangar partner converted his Pulsar XP for LSA operation. Of course the Pulsar XP does meet all the LSA requirements except for the non-LSA cruise speed of 150 Kts. He tested the cruise speed for 120 Kts operation and noted the engine RPM. He placarded that engine RPM on the instrument panel. He then wrote the Washington FSDO that he was converting to LSA operation. He called the FSDO and they said his letter was on file and not to expect a reply. He made no modification to the aircraft other than the cruise RPM placard and a log book entry. He has been operating his Pulsar XP as an LSA for four years now. (And pays little attention to the LSA RPM placard.) Sid Wood Tri-gear KR-2 N6242 Mechanicsville, MD, USA -------------------------------------------------------------------- HAS ANY BODY SUCCESSFULLY CONVERTED THEIR KR 1 TO AN LSA? AND WHAT WERE THE REQUIREMENTS TO DO THIS. Marty Greg Martin _______________________________________________ Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search. To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org please see other KRnet info at http://www.krnet.org/info.html see http://list.krnet.org/mailman/listinfo/krnet_list.krnet.org to change options
