View Single Post
  #15  
Old February 13th 18, 12:39 PM posted to rec.aviation.soaring
Eric Munk
external usenet poster
 
Posts: 179
Default 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.