As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CA 1464/119 CORROSION AT RH SIDE FUSELAGE AT STA 1115-1128, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1115-1128, S-20R. REMOVED 0.004" MATERIAL AND REMAINING 0.067" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND 53-00-01 ALLOWABLE DAMAGE 1 (R130).