What was found
(CAN) CRACK FOUND ON UPPER VERTICAL FIN LOWER SECTION OF LEADING EDGE BETWEEN TWO RIVETS, 2.6250 INCHES ABOVE STAMPED FITTING, 2.50 INCHES, LENGTH OF CRACK. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACK FOUND ON UPPER VERTICAL FIN LOWER SECTION OF LEADING EDGE BETWEEN TWO RIVETS, 2.6250 INCHES ABOVE STAMPED FITTING, 2.50 INCHES, LENGTH OF CRACK. (X)