What was found
INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7.