What was found
(AUS) MAIN ROTOR BLADE LEADING EDGE UPPER SURFACES PEELING AWAY. FURTHER INSPECTION FOUND INTERGRANULAR CORROSION ON THE LOWER SURFACE. EDDY CURRENT INSPECTION CONFIRMED INTERNAL CORROSION. PART TC: 2,209.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) MAIN ROTOR BLADE LEADING EDGE UPPER SURFACES PEELING AWAY. FURTHER INSPECTION FOUND INTERGRANULAR CORROSION ON THE LOWER SURFACE. EDDY CURRENT INSPECTION CONFIRMED INTERNAL CORROSION. PART TC: 2,209.