What was found
CRACKED SPLICE AND CLIP ANGLE ON LT WING INTERNAL FIXED LEADING EDGE STA XFS 194. SPLICE AND CLIP WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05 AND DWG9937517 REV J.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SPLICE AND CLIP ANGLE ON LT WING INTERNAL FIXED LEADING EDGE STA XFS 194. SPLICE AND CLIP WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05 AND DWG9937517 REV J.