What was found
INSPECTION FOUND A .625 INCH CRACK, RT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .625 INCH CRACK, RT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.