What was found
CORROSION AROUND BOLTS IN WEB BS 1013, LBL 44, WL 208 ON UNDERSIDE. ORIGINAL THICKNESS .040. REPLACED WEB. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AROUND BOLTS IN WEB BS 1013, LBL 44, WL 208 ON UNDERSIDE. ORIGINAL THICKNESS .040. REPLACED WEB. (M)