What was found
TWO SPOTS OF BLENDED CORROSION ON TOP SIDE OF L/H WING REQUIRES NDT AND POSSIBLE SUBMITTAL TO FALCON JET. AFTER BLENDING AND NDT THE TWO BLENDS WERE MAPPED AND SUBMITTED TO FALCONJET ENGINEERING FOR REVIEW. FALCONJET ENGINEERING DIVIDED THE SUBMITTAL INTO TWO PROJECTS. FOR THE BLEND ON THE L/H WING TRAILING EDGE UPPER SKIN BETWEEN RIB 14 AND RAIL 6, THICKNESS REMAINING AFTER BLENDING IS STRUCTURALLY ACCEPTABLE PER DFJ LETTER F2000 57-23-2-108 DATED 3/26/18. AT THE SECOND BLEND LOCATION ON THE L/H WING UPPER SURFACE RIB 7 AND CENTER SKIN AFT SEAM THE THICKNESS REMAINING AFTER BLENDING IS STRUCTURALLY ACCEPTABLE PER DFJ LETTER F2000 57-21-2-257 DATED 3/30-2018.