What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT FUSELAGE SKIN CORRODED ALONG LONGERON 20L BETWEEN FS 1197 AND FS 1208. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT FUSELAGE SKIN CORRODED ALONG LONGERON 20L BETWEEN FS 1197 AND FS 1208. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-2.