What was found
CORROSION ON CENTER FUSELAGE III LH SILL PLATE LOCATED AT FR 88 AND Y= +41. REMOVED AND REPLACED CENTER FUSELAGE III LH SILL PLATE LOCATED AT FR 88 AND Y= -41 IAW 51-41-01, 51-42-01, AND 51-43-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON CENTER FUSELAGE III LH SILL PLATE LOCATED AT FR 88 AND Y= +41. REMOVED AND REPLACED CENTER FUSELAGE III LH SILL PLATE LOCATED AT FR 88 AND Y= -41 IAW 51-41-01, 51-42-01, AND 51-43-03.