KR> Your Thoughts on my Thoughts

2008-10-28 Thread GARY ROBISON
Smith" To: "KRnet" Sent: Tuesday, October 28, 2008 12:25 AM Subject: Re: KR> Your Thoughts on my Thoughts Ron Smith KR2SSXL Buckeye Arizona mercedesm...@yahoo.com http://ronsmith.myphotoalbum.com/albums.php Gary wrote: That covers the front spar, the rear one is goi

KR> Your Thoughts on my Thoughts

2008-10-27 Thread Ron Smith
Ron Smith KR2SSXL Buckeye Arizona mercedesm...@yahoo.com http://ronsmith.myphotoalbum.com/albums.php Gary wrote: That covers the front spar, the rear one is going to be a little more work. I will require a dihedral bend and one that sweeps it forward. My thought is to put the dihedral ben

KR> Your Thoughts on my Thoughts

2008-10-27 Thread Ron Smith
--- On Mon, 10/27/08, GARY ROBISON wrote: From: GARY ROBISON Subject: KR> Your Thoughts on my Thoughts To: "KR_NET" List-Post: krnet@list.krnet.org Date: Monday, October 27, 2008, 6:49 PM Hello all, I have had my plans for a few weeks now and I am chewing on some ideas th

KR> Your Thoughts on my Thoughts

2008-10-27 Thread Dave Arbogast, CISSP
Served many wooden ships in battle for a thousand years (about ?) - should be more than strong enough for you. -dave GARY ROBISON wrote: > > My thoughts are to do exactly that only not cut the caps into quarter inch > strips, but to steam > > and bend them with a jig holding the proper angle unt

KR> Your Thoughts on my Thoughts

2008-10-27 Thread Mark Langford
GARY ROBISON wrote: > I really like the idea Mike suggested on his comment page. > Mikes thought was to incorporate the dihedral bend for the spars "inside" > the fuselage. > Find it here: http://home.hiwaay.net/~langford/kopinion.html#bent Yep, Mike's a pretty smart guy. You'd be wise to follow

KR> Your Thoughts on my Thoughts

2008-10-27 Thread GARY ROBISON
Hello all, I have had my plans for a few weeks now and I am chewing on some ideas that need to be addressed before I get started with the 88. I really like the idea Mike suggested on his comment page. Mikes thought was to incorporate the dihedral bend for the spars "inside" the fuselage. Find