What was found
HFEC SURFACE INSPECTION FOUND CRACK APPROXIMATELY 0.15 AS MARKED ON RT BS 859.5 RBL 89 BELOW WL 200 AT THE FRAME INNER CHORD TRANSITION RADIUS. REPAIRED AND ACCOMPLISHED AS PER W/C:5311-01195 09B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC SURFACE INSPECTION FOUND CRACK APPROXIMATELY 0.15 AS MARKED ON RT BS 859.5 RBL 89 BELOW WL 200 AT THE FRAME INNER CHORD TRANSITION RADIUS. REPAIRED AND ACCOMPLISHED AS PER W/C:5311-01195 09B.