What was found
STIFFENER CORRODED ON RIGHT I/B FLAP FORWARD SPAR INBOARD END. REMOVED & REPLACED STIFFENER IAW B767 SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STIFFENER CORRODED ON RIGHT I/B FLAP FORWARD SPAR INBOARD END. REMOVED & REPLACED STIFFENER IAW B767 SRM 51-40-02.