What was found
RIGHT WING LEADING EDGE CAVITY, FRONT VERTICAL ANGLE STIFFENER AT L/E STA 652 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING LEADING EDGE CAVITY, FRONT VERTICAL ANGLE STIFFENER AT L/E STA 652 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.