What was found
INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN RT WING L/E PANEL 1222C. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 57-01, FIGURE 3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN RT WING L/E PANEL 1222C. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 57-01, FIGURE 3, AND 51-30-2.