What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FUSELAGE EXTERIOR SKIN FROM FS 588 SPLICE TO FS 669 SPLICE AT LONGERON 26 LEFT TO 26 RIGHT. REPLACED SKIN 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 FUSELAGE EXTERIOR SKIN FROM FS 588 SPLICE TO FS 669 SPLICE AT LONGERON 26 LEFT TO 26 RIGHT. REPLACED SKIN IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.