What was found
CORROSION ON CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y= +12 SEVERAL SPOTS. REMOVED AND REPLACED CENTER FUSELAGE III RH SEAR PANEL AT FR 87-FR 88 AND Y +12 IAW SRM 51-40-02, 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 SEVERAL SPOTS. REMOVED AND REPLACED CENTER FUSELAGE III RH SEAR PANEL AT FR 87-FR 88 AND Y +12 IAW SRM 51-40-02, 51-40-08.