Reviewed page 42D-02 and all steps were not applicable except for steps 3 and 14. NA steps disassembed avionics of an installed avionics system - not there yet so doesn't apply. Removed F-1240 forward top skin and snap bushings from F-1202K-L & -R instrument stack supports. (page 42D-02, steps 3 and 14). Page 42D-02 is complete.
Drilled out rivets and removed F-1202K-L & -R instrument stack supports and F-1202J-L & -R instrument stack angles. Final drilled holes #27 in center of panel base and drilled holes for nutplates. Dimpled and installed nutplates. (page 42D-03, steps 1, 2, and 4 through 7. Step 3 is NA). Page 42D-03 is complete
Clecoed F-00011 SkyView template to panel base and match drilled two holes. Final drilled holes to #19. (page 42D-04, steps 1 through 4). Page 42D-04 is complete.
