What was found
LEFT VERTICAL STIFFENER CHORD, NLG WW, STA 287 HAS 3" CRACK, INDICATION LOCATED 10.75" FROM THE NOSE WW TOP PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STIFFENER CHORD, NLG WW, STA 287 HAS 3" CRACK, INDICATION LOCATED 10.75" FROM THE NOSE WW TOP PANEL.