What was found
FOUND CORROSION ON LEFT FLAP LEADING EDGE STIFFENER/ DOUBLER. MAINTENANCE FITTED AND INSTALLED NEW STIFFENER/DOUBLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION ON LEFT FLAP LEADING EDGE STIFFENER/ DOUBLER. MAINTENANCE FITTED AND INSTALLED NEW STIFFENER/DOUBLER.