What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING TIP RIB UPPER FLANGE BY INBOARD AFT CORNER OF FUEL VENT OUTLET. THE CRACK WAS STOP DRILLED IAW SRM 51-30-2. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING TIP RIB UPPER FLANGE BY INBOARD AFT CORNER OF FUEL VENT OUTLET. THE CRACK WAS STOP DRILLED IAW SRM 51-30-2. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.