What was found
DURING COMPLIANCE OF AGUSTA TB 109-50B PT. 2, 25-HOUR MAIN ROTOR BLADE INSPECTION, A CRACK WAS FOUND STARTING FROM THE TRAILING EDGE EXTENDING CHORD-WISE FOR APPROXIMATELY 40 MM, 2070 MM FROM THE BLADE ROOT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING COMPLIANCE OF AGUSTA TB 109-50B PT. 2, 25-HOUR MAIN ROTOR BLADE INSPECTION, A CRACK WAS FOUND STARTING FROM THE TRAILING EDGE EXTENDING CHORD-WISE FOR APPROXIMATELY 40 MM, 2070 MM FROM THE BLADE ROOT.