What was found
FOUND CORROSION TO THE FRAME AT FS 605. CORROSION WAS BLENDED FROM THE VERTICAL WEB RESULTING 3” X 2” X 0.007” DEEP MATERIAL REMOVAL. CORROSION WAS ALSO NOTED BETWEEN THE SKIN & LOWER FLANGE. REPAIRED IAW EA 253-02457.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION TO THE FRAME AT FS 605. CORROSION WAS BLENDED FROM THE VERTICAL WEB RESULTING 3” X 2” X 0.007” DEEP MATERIAL REMOVAL. CORROSION WAS ALSO NOTED BETWEEN THE SKIN & LOWER FLANGE. REPAIRED IAW EA 253-02457.