What was found
INSPECTION TYPE:C+SI, ON REMOVAL OF CENTER SECTION REAR SPAR UPPER CHORD SEVERAL STIFFENERS FOUND DAMAGED AND CORRODED. REPLACED STIFFENERS IAW 51-30-02 AND DWG 65C21531.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C+SI, ON REMOVAL OF CENTER SECTION REAR SPAR UPPER CHORD SEVERAL STIFFENERS FOUND DAMAGED AND CORRODED. REPLACED STIFFENERS IAW 51-30-02 AND DWG 65C21531.