What was found
INSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE AT RT WING LEADING EDGE FLAP WELL LOWER STIFFENER, FS 150. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 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 IN FORWARD ANGLE AT RT WING LEADING EDGE FLAP WELL LOWER STIFFENER, FS 150. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.