What was found
LH WING, WING TO FUSE ATTACHMENT ANGLE IS CRACKED AT FS 449.85. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE LH WING TO FUSELAGE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH WING, WING TO FUSE ATTACHMENT ANGLE IS CRACKED AT FS 449.85. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE LH WING TO FUSELAGE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.