What was found
DURING AD 2005-04-09A VISUAL INSP COMPLIANCE, FOUND APPROX .2500 INCH ONE LEG BY .7500 INCH SECOND LEG CRACK IN THE DESIGNATED INSP AREA OF THE TARGET TAIL ROTOR BLADE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AD 2005-04-09A VISUAL INSP COMPLIANCE, FOUND APPROX .2500 INCH ONE LEG BY .7500 INCH SECOND LEG CRACK IN THE DESIGNATED INSP AREA OF THE TARGET TAIL ROTOR BLADE.