What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON AFT FUSELAGE LOWER SKIN FROM FS 802 TO FS 996, BETWEEN LONGERON 26 RIGHT TO 26 LEFT. REPLACE LOWER SKIN FROM FS 802 TO FS 996 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON AFT FUSELAGE LOWER SKIN FROM FS 802 TO FS 996, BETWEEN LONGERON 26 RIGHT TO 26 LEFT. REPLACE LOWER SKIN FROM FS 802 TO FS 996 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.