What was found
DURING ROUTINE INSPECTION, FOUND M/R BLADE HAS EXCESSIVE LEADING EDGE CORROSION. POSSIBLE IMPROPER HEAT TREAT BY MATERIAL OR ALLOY FORMULATION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, FOUND M/R BLADE HAS EXCESSIVE LEADING EDGE CORROSION. POSSIBLE IMPROPER HEAT TREAT BY MATERIAL OR ALLOY FORMULATION.