What was found
RIGHT WING OTBD FLAP, LOWER FWD INBD STRESS PANEL HAD A SPOT OF CORROSION THAT WAS BLENDED OUT OF LIMITS ON NR-0570. REPAIRED PANEL IAW VACUUM CUT METHOD IAW SRM 57-53-01 & 51-70-01 & REA 47177REA03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING OTBD FLAP, LOWER FWD INBD STRESS PANEL HAD A SPOT OF CORROSION THAT WAS BLENDED OUT OF LIMITS ON NR-0570. REPAIRED PANEL IAW VACUUM CUT METHOD IAW SRM 57-53-01 & 51-70-01 & REA 47177REA03.