Tue Feb 23, 2010 8:34 pm
gregv wrote:excellent thread, thanks for taking the time to post pics and descriptions of what's going on!
Out of curiosity, what kind of inspection process would the fuselage be subjected to in a case like this? If there was no history of previous damage would it strictly be a series of visual inspections, or are there other ndt processes involved, such as some sort of magnafluxing? Are sample areas de-rivited to check for corrosion between the stringer/longerons and skin? Is there any kind of check for trueness, like using a laser setup or a jig of sorts, or does a inspection for wrinkles in the skin do that job?
Again, just curious, not trying to suggest that something needs to be done that hasn't etc., I'm just interested in how you judge how far you need to go to make sure everything is as it should be.
cheers
greg v.
Tue Feb 23, 2010 9:36 pm
Wed Feb 24, 2010 2:04 pm
Wed Feb 24, 2010 3:39 pm
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Thu Jun 10, 2010 6:44 pm
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Mon Jul 19, 2010 9:25 pm
Obergrafeter wrote:I know its' neccessary corrosion protection, but did Grumman (or Eastern) bother with it originally?
Mon Jul 19, 2010 9:30 pm
Tue Jul 20, 2010 12:07 am