What was found
INSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.