Inspector_Tim
lvl.2
Flight distance : 35899 ft
United States
Offline
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This has probably been asked/mentioned before, and sorry if so. I'm guessing as the stress crack issue rears it's head more as a problem etc, wouldn't there be an add on type plate or similar to re-enforce such area? There may be forces concentrated on specific areas and stress cracks are occurring. Would seem opening and re-enforcing with CA or epoxy/carbon fibers, a shear plate external to shell or shell replacement are about it, correct?
Would there be an assumed loss of warranty if a user were to open shell and re-enforce/strengthen themselves in an informed decision to do so and not be out the use of the their product for 2 + months? |
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