What was found
INSPECTION FOUND A 1 INCH CRACK LOCATED IN THE RADIUS OF THE HUB ADJACENT TO THE PART NUMBER/SERIAL NUMBER. THIS PART WAS EDDY CURRENT TESTED IAW DUNLOP 32-40-02(4), REV. 41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK LOCATED IN THE RADIUS OF THE HUB ADJACENT TO THE PART NUMBER/SERIAL NUMBER. THIS PART WAS EDDY CURRENT TESTED IAW DUNLOP 32-40-02(4), REV. 41.