Apparently the bible for determining if a longeron (or other member) can be straightened or needs to be spliced is a Structural Repair Manual. What's the closest thing to a SRM for a '46 Tcraft?
Also - Are there any cases on a fuselage where metal can be heated, bent, then treated to regain it's strength (sorry, I don't know the terms, though I think 'temper' and 'anneal' fit in there somewhere) ?- Mike
Also - Are there any cases on a fuselage where metal can be heated, bent, then treated to regain it's strength (sorry, I don't know the terms, though I think 'temper' and 'anneal' fit in there somewhere) ?- Mike
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