What was found
CORROSION FOUND ON THE RIGHT WING TRAILING EDGE INTERCONNECTING STRUT, INBOARD FLAP. REPLACED THE STRUT IAW AMM 27-51-44-400-001-A, AND PERFORMED OPERATIONAL TEST OF THE FLAPS SYSTEM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION FOUND ON THE RIGHT WING TRAILING EDGE INTERCONNECTING STRUT, INBOARD FLAP. REPLACED THE STRUT IAW AMM 27-51-44-400-001-A, AND PERFORMED OPERATIONAL TEST OF THE FLAPS SYSTEM.