What was found
CRACK IN LEADING EDGE RUDDER SKIN RT SIDE JUST BELOW TOP HINGE. REMOVED THE RUDDER UPPER LEADING EDGE SKIN AND INSTALLED NEW . ALL WORK WAS DONE IAW SRM 51-40-03 AND 51-40-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN LEADING EDGE RUDDER SKIN RT SIDE JUST BELOW TOP HINGE. REMOVED THE RUDDER UPPER LEADING EDGE SKIN AND INSTALLED NEW . ALL WORK WAS DONE IAW SRM 51-40-03 AND 51-40-06.