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I learned to fly in a J-3 and I have owned various steel tube airplanes
over the years... I have helped to jig, drill, and ream the fuselage tabs and mount biplane wings... I doubt that there is any wear allowed by Piper at that lower spar attach tab... The hole in the fuselage tab should be a close tolerance fit for the bolt... I always considered the wing tip shake test to require no relative movement of the wing in relation to the strut/fuselage - other than the usual springing/bouncing of the entire airframe with a vigorous shake... With any slop in the strut flutter becomes an issue... I urge that you folks get an experienced steel tube airframe mechanic to make the repair soon... denny |
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