What was found
INSPECTION FOUND A 2.75 AND 1 INCH CRACK IN RIB INSIDE RT WINGTIP, ACCESSED THROUGH PANEL NR 8811. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.75 AND 1 INCH CRACK IN RIB INSIDE RT WINGTIP, ACCESSED THROUGH PANEL NR 8811. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.