What was found
DURING C/W AD 80-11-04, IT WAS NOTICED THE WELD ON THE RIGHT FRONT OF THE V-FIN ATTACH FITTING WAS CRACKED. REMOVAL VERIFIED A 1 INCH CRACK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C/W AD 80-11-04, IT WAS NOTICED THE WELD ON THE RIGHT FRONT OF THE V-FIN ATTACH FITTING WAS CRACKED. REMOVAL VERIFIED A 1 INCH CRACK.