What was found
INSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.