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#6
May 23rd 06, 09:31 PM
posted to rec.aviation.homebuilt
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Airframe finishing and tooling
nondem wrote:
The plane design I'm building uses 2x2x.125" 6061-T6 for the fuselage frame. I did notice that older versions of the same plans specified 6063-T351. I checked the specs on both and as I remember the 6061 is a stronger alloy. There is almost no aluminum sheet used in this design either...Just angles/square and round tubing for the most part. That sounds a lot like one of the late Graham Lee's UL designs. Close? Richard 
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