Ron, You answered your own question. Greater stress on the WAF's. A safer solution would be to build a one piece laminated spar with the bend inside of the fuselage. There are a couple of builders doing this.
-----Original Message----- From: Ron Butterfield [mailto:rbutterfi...@mebtel.net] What would be the problems with moving the wing attach point in to the fuselage, then having straight wings all the way out? The only things I can see as problems are greater stress on the wing attach fittings _______________________________________ to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net please see other KRnet info at http://www.krnet.org/info.html Mark Jones (N886MJ) Wales, WI So close to flying I am growing feathers.
