What was found
CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 883.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX. 0.5" IN LENGTH AS MARKED. FRAME INNER CHORD REPAIR CARRIED OUT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 883.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX. 0.5" IN LENGTH AS MARKED. FRAME INNER CHORD REPAIR CARRIED OUT.