What was found
PROPELLER WAS SUBMITTED FOR C/W AD 97-18-02, SB 217. BOTH BLADES WERE FOUND CRACKED IN THE RETENTION RADIUS USING EDDY CURRENT INSPECTION EQUIPMENT. CRACKS ARE ESTIMATED AT 50 PERCENT OF CIRCUMFERENCE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PROPELLER WAS SUBMITTED FOR C/W AD 97-18-02, SB 217. BOTH BLADES WERE FOUND CRACKED IN THE RETENTION RADIUS USING EDDY CURRENT INSPECTION EQUIPMENT. CRACKS ARE ESTIMATED AT 50 PERCENT OF CIRCUMFERENCE.