What was found
INSPECTION FOUND A .25 INCH CRACK IN RT WING TIP UPPER SURFACE, JUST FORWARD OF PANEL 6641. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RT WING TIP UPPER SURFACE, JUST FORWARD OF PANEL 6641. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.