What was found
HFEC SURFACE INSPECTION FOUND CRACK APPROX 0.18" AS MARKED ON LHS BS903.5 LBL89 BELOW WL200 AT THE FRAME INNER CHORD TRANSITION RADIUS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC SURFACE INSPECTION FOUND CRACK APPROX 0.18" AS MARKED ON LHS BS903.5 LBL89 BELOW WL200 AT THE FRAME INNER CHORD TRANSITION RADIUS.