The second door was a factory option for a while.
most/all were subsequently converted to two doors.
so, it was part of the type design which in theory should eliminate or at least simplify the need for a field approval.
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Have you removed the fabric from the rudder yet?
Not overly complicated to repair the rudder. Can be done on a flat bench. The trailing edge lower section is suseptible to corrosion as are the other "catch water" points....
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Yes I understand. Overlap is supposed to be minimum 1" but I hear ya.
There is a big difference in the stability however. When there is structure under the joint, the joint is subject to shear only.
You may have seen the demo, or maybe done the test yourself... glue joints...
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In the whole scheme of things... of all the time involved in a recover/restoration, and given the huge downside of a seem letting go on a finished aircraft, I simply can't imagine not taking the relatively short time to stitch the joint.
Then relax with the piece of mind you've enabled....
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