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Old February 13th 18, 11:51 AM posted to rec.aviation.soaring
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Default Worried about a leading edge crack in the fiberglass winglaminate of my PW-5

ANY damage to the wing forward of the mainspar MUST be inspected before further flight, repaired as necessary, and a logbook entry made.

I'm trying to imagine how one would inspect this to make sure there is no internal structural damage. X-ray?