What was found
LEFT WING LEADING EDGE VERTICAL ANGLE AT THE OUTBOARD CORNER OF THE INBOARD SLAT AT STA XS 250.089 IS CRACKED AT THE LWR END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-3-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE VERTICAL ANGLE AT THE OUTBOARD CORNER OF THE INBOARD SLAT AT STA XS 250.089 IS CRACKED AT THE LWR END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-3-0.