What was found
CORROSION ON THE HORIZONTAL FLANGE OF THE SUPPORT TEE IN BETWEEN THE UPPER VERTICAL LEG AND THE ATTACH WEB. THE CORROSION WAS REMOVED BY BLENDING AND LEAVING A MINIMUM THICKNESS OF 0.080€? FROM 0.092€? PARENT PER EA 767-53-016376.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON THE HORIZONTAL FLANGE OF THE SUPPORT TEE IN BETWEEN THE UPPER VERTICAL LEG AND THE ATTACH WEB. THE CORROSION WAS REMOVED BY BLENDING AND LEAVING A MINIMUM THICKNESS OF 0.080€? FROM 0.092€? PARENT PER EA 767-53-016376.