Jump to content

Notice: Effective July 1, 2024, Vertical Forums will be officially shut down. As a result, all forum activity will be permanently removed. We understand that this news may come as a disappointment, but we would like to thank everyone for being a part of our community for so many years.

If you are interested in taking over this Forum, please contact us prior to July 1.

BHT 222U Rotor Blade Tap Test for Voids??


hmesser
 Share

Recommended Posts

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!!

Link to comment
Share on other sites

Now this screams "FLY BY NIGHT" operation.

I wonder though, should all of this information not already be available to you in the maintenance manuals???

 

The comment about the heavy maintenance not possible on a regular basis scares me. If I have sent you a resume in the past looking for work, could you please tear it up, I''m having second thoughts....

Link to comment
Share on other sites

Join the conversation

You can post now and register later. If you have an account, sign in now to post with your account.

Guest
Reply to this topic...

×   Pasted as rich text.   Paste as plain text instead

  Only 75 emoji are allowed.

×   Your link has been automatically embedded.   Display as a link instead

×   Your previous content has been restored.   Clear editor

×   You cannot paste images directly. Upload or insert images from URL.

Loading...
 Share

×
×
  • Create New...