What was found
CORROSION ON INTERNAL STRUCTURE LOWER SILL BETWEEN FRAME 16 TO FRAME 18 AT LEVEL S TR 23L AT LOWER FUSELAGE. REPLACED LOWER SILL LOCATED FRAME 16 TO FRAME 20 AT LEVEL STR 23L AT LOWER FUSELAGE IAW SRM 51-72-11 AND DWG D53110339.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON INTERNAL STRUCTURE LOWER SILL BETWEEN FRAME 16 TO FRAME 18 AT LEVEL S TR 23L AT LOWER FUSELAGE. REPLACED LOWER SILL LOCATED FRAME 16 TO FRAME 20 AT LEVEL STR 23L AT LOWER FUSELAGE IAW SRM 51-72-11 AND DWG D53110339.