What was found
LEFT WING, LEADING EDGE INTERNAL STRUCTURE, STIFFENER CRACKED INSIDE FLAP KRUEGER BAY. INSTALLED NEW STIFFENER AT LT WING, LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21,
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING, LEADING EDGE INTERNAL STRUCTURE, STIFFENER CRACKED INSIDE FLAP KRUEGER BAY. INSTALLED NEW STIFFENER AT LT WING, LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21,