Date: November 07, 2008 at 05:40:11 From: pat, [wet-lst.uni-duisburg.de] Subject: Re: static load test ailerons
This could be the solution but it is not so easy, because then we would need an additional angle on the top of the aileron and an additionel hole, angle etc. on the top of the wing. Have you tried this setup, yet? pat