What was found
CORROSION ON CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y=+12. REMOVED AND REPLACED CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y=+12 IAW SRM 51-40-08.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y=+12. REMOVED AND REPLACED CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y=+12 IAW SRM 51-40-08.