What was found
MAIN ROTOR BLADE T/E COMPOSITE WEDGE DEBONDED BETWEEN STA 126.00 AND STA 148.00 AND T/E EXTRUSION CORRODED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN ROTOR BLADE T/E COMPOSITE WEDGE DEBONDED BETWEEN STA 126.00 AND STA 148.00 AND T/E EXTRUSION CORRODED.