What was found
DURING C-INSPECTION, FOUND THE FUSELAGE FRAME AT FS 945 CORRODED FROM LONGERON 24 LEFT TO LONGERON 30. REPLACED ANGLE IAW DC9 51-10-3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-INSPECTION, FOUND THE FUSELAGE FRAME AT FS 945 CORRODED FROM LONGERON 24 LEFT TO LONGERON 30. REPLACED ANGLE IAW DC9 51-10-3 AND 51-30-2.