FLYBOYJ said:
I could tell you on the Corsair you're looking at up to .125. The Zero looked about .032 - .040. The Mustang about .075.
If rebuilt, I could tell you that the Zero would have to use close to the original thickness of sheet metal. After the restoration the FAA has to do their thing and before an airworthiness certificate is issued. The restorer will have to prove to an FAA inspector that what was used on the retoration was close if not the same material on the original structure.
Well, that is not always true. On the Corsair for instance, virtually all flying planes have the wing fabric replaced with aluminum sheeting, and usually tail surface fabric too for that matter. The historic fabric is impossible to get - it was very expenensive and was soaked in a fireproofing liquid that it turned out was a significant health hazard for the crews working with it. Aluminum is much cheaper and much easier to maintain. The main purpose of the fabric covering was to reduce vulnerablity to enemy fire - civilian Corsairs don't expect to be taking any hits so....
On the Zero, they'd be wanting assurances it was safe to fly - thicker sheetmetal would not necessarily make it unsafe to fly as long as it was balanced properly, it might even make the plane safer. The main reason to do it would be to future reduce maintance requirements.
=S=
Lunatic