What was found
CRACK AROUND THE FASTENER AT NO.3 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN. INSTALLED REPAIR IAW SRM 57-42-01-2R-8. STEP 4L. AND 21-157-02763-WIP1. INSTALLED ACCESS PANELS AND FLEX SKIN IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK AROUND THE FASTENER AT NO.3 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN. INSTALLED REPAIR IAW SRM 57-42-01-2R-8. STEP 4L. AND 21-157-02763-WIP1. INSTALLED ACCESS PANELS AND FLEX SKIN IAW SRM 51-40-02.