1: The F-00043 was temporarily install onto the upper forward fuselage skin. 2: Match drill #27 was made to hole into the F-1202D-L 3: The area to be romeved from the F-1202D-L was marked. 4: The material was removed. 5: A nutplate was removed from the F-1202D-L. 6: Two nutplates were attached to the aft side of the F-1202D-L 7: Match drill #40 was made using the nutplate holes as guide. 8: The nutplate and holes drilled in the previous step were dimpled. 9: the nutplates were riveted to the forward side oif the F-1202D-L
