What was found
FOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09.