What was found
CRACK FOUND ON VERTICAL STABILIZER SKIN STA ZFS=18 LT SIDE FWD SECTION. INSTALLED REPAIR ON THE SKIN IAW SRM 55-01 FIG.2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON VERTICAL STABILIZER SKIN STA ZFS=18 LT SIDE FWD SECTION. INSTALLED REPAIR ON THE SKIN IAW SRM 55-01 FIG.2.