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Worried about a leading edge crack in the fiberglass wing laminate ofmy PW-5
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February 13th 18, 12:39 PM posted to rec.aviation.soaring
Eric Munk
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Worried about a leading edge crack in the fiberglass wing laminate of my PW-5
At 11:51 13 February 2018,
wrote:
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?
That part of the wing does not have internal structure to speak of. Damage
to D-nose sandwich structure is easily detectable by an experienced LAME.
Eric Munk
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