What was found
FOD IMPACT DAMAGE TO FUSELAGE SKIN PANEL (P/N 85320300). THIS REPAIR COVERS TWO DAMAGE AREAS LOCATED AT X=291.4. THE FIRST DAMAGE IS A SKIN PUNCTURE 2 INCHES FORWARD OF FUSELAGE STATION X=291.4 IMMEDIATELY UNDER STRINGER S-18S. THE SECOND DAMAGE LOCATION IS TWO DENTS AND PENETRATIONS 2.0 INCHES FORWARD OF FUSELAGE STATION X=291.4 BETWEEN STRINGERS S-19S AND S20S. PERFORMED (NDT) HFEC INSPECTION IAW DASH 8 NDT MANUAL PSM 1-82-7A PART 6 51-00-01, NO CRACKS NOTED. PERFORMED BOND TEST WITH NO DISBOND NOTED. REPAIRED AFFECTED AREAS IAW STS ENGINEERING SOLUTIONS ENGINEERING AUTHORIZATION 5-2010-211