As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HFEC INSPECTION FOUND 01 EA CRACK OF LEFT BS883.5 FRAME INNER CHORD TRANSITION RADIUS AT LBL 89 BELOW WL200,IT IS ABOUT 0.2 INCH LONG. CARRIED OUT THE REPAIR AT LH FRAME INNER CHORD OF BS 883.5 LBL89 BELOW WL200 AS PER SB 767-53A0209 REV. 2 JUNE 07, 203.