Brendan, I'll toss out something to think about. I don't know the answer so perhaps someone will chime in with more information. I don't know the impact of where the hinge point for the belly brake is located; behind or forward of the aft spar. N133RM is a KR-2S and the hinge point is 6-8" forward of the aft spar. On my last KR2, I installed the hinge directly under the aft spar. It seems that the nose pitch adjustment is more pronounced on 133RM though it also extends further down. There are more variables than just the hinge location but I wonder what the physics difference is in location. ? John Bouyea N133RM KR-2S – imported, fixed & flying www.bouyea.net/cur_proj/N133RM OR81/ Hillsboro, OR
-----Original Message----- So my thoughts on a belly board and why some people are getting different results. I am going to use engineering logic to say that the angle the belly board deploys to would dramatically affect how the airplane pitches under deployment. Brendan palmer Marysville oh N422AB
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