What was found
INSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF LT WING LEADING EDGE PANEL BETWEEN SLATS NR 3 AND NR 4. REPAIRED IAW SRM 51-20-01 AND 51-70-17.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF LT WING LEADING EDGE PANEL BETWEEN SLATS NR 3 AND NR 4. REPAIRED IAW SRM 51-20-01 AND 51-70-17.