Lacking extensive background in composite structures inspection, Where can I access information on the tools and techniques used to properly identify voids in these types of blades.
I have seen inspectors in the U.S.Army use 'Tapping Tools' to inspect for debonding of honeycomb structures in OH-58's. Does the same rules apply for the structure of 'Deuce'Blades? I know anything is possible with time and money, and I have darn little of both, but I do love helicopters and would really appreciate some enlightenment on the subject. Thanks!!
I have seen inspectors in the U.S.Army use 'Tapping Tools' to inspect for debonding of honeycomb structures in OH-58's. Does the same rules apply for the structure of 'Deuce'Blades? I know anything is possible with time and money, and I have darn little of both, but I do love helicopters and would really appreciate some enlightenment on the subject. Thanks!!