As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ANGLE IN LINE WITH STRINGER 10R BETWEEN FS625.30 AND 640.00 HAS APPROX 1.5" CRACK STARTING FROM AFT EDGE GOING FORWARD ON FUSELAGE SKIN FLAT SIDE AND APPROX. CENTERLINE OF FLAT. (FILED CLOSED) REMOVED AND REPLACED ANGLE IN LINE WITH STRINGER 10R BETWEEN FS625.30 AND 640.00 TO SRM 51-42-21. COMPLETED TACK ARD 51-900-1003-SKY AND M-337