What was found
DURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING CRACKED IN THE VERTICAL STAB. THE CRACK WAS FOUND USING EDDY CURRENT INSPECTION METHODS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING CRACKED IN THE VERTICAL STAB. THE CRACK WAS FOUND USING EDDY CURRENT INSPECTION METHODS.