What was found
INSPECTION TYPE:C COCKPIT BS 360 STR 10AL FRAME INNER CHORD FOUND CRACKS FROM 1EA FASTENERS HOLE AS MARKED, CRACK LENGTH .125 INCH. COCKPIT BS 360 STR 10-15L FRAME INNER CHORD REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C COCKPIT BS 360 STR 10AL FRAME INNER CHORD FOUND CRACKS FROM 1EA FASTENERS HOLE AS MARKED, CRACK LENGTH .125 INCH. COCKPIT BS 360 STR 10-15L FRAME INNER CHORD REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.