What was found
CORROSION ON THE LEFT WING OUTBOARD FLAP INTERNAL CASE INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-57-44-400-001A AND PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IAW AMM 27-54-00-710-001-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON THE LEFT WING OUTBOARD FLAP INTERNAL CASE INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-57-44-400-001A AND PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IAW AMM 27-54-00-710-001-A.