What was found
HFEC SURFACE INSPECTION FOUND A CRACK APPROXIMATELY 0.18 OF AN INCH ON BS 883.5 LBL 89 BELOW WL 200 ON THE FRAME INNER TRANSITION RADIUS. REPAIRED IAW 5311-01195-09C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC SURFACE INSPECTION FOUND A CRACK APPROXIMATELY 0.18 OF AN INCH ON BS 883.5 LBL 89 BELOW WL 200 ON THE FRAME INNER TRANSITION RADIUS. REPAIRED IAW 5311-01195-09C.