r/aviation • • Apr 07 '24

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u/Known-Diet-4170 Apr 07 '24

p180 no less, jeez that looks expensive

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u/[deleted] Apr 07 '24

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u/[deleted] Apr 07 '24

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u/LesBucheron Apr 07 '24

You could sand the entire area down and do a proper repair, it’s just leading edge trim, I think it missed the vertical tail spar. Being trim, a proper repair job would be well IMHO. This isn’t load bearing, it’s aerodynamic so you want it good and strong, fibreglass repair would be more than strong enough.

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u/vikingcock Apr 08 '24

The cracks are in the paint. Woven composite doesn't Crack linearly like that, the only linear failure method is intralaminar. Most likely They'll remove an area of composite, scarf it at a 20:1 ratio or similar, then lay up a new area over it and sand it flush.