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Application of Hysol carbon doublers for reinforcement.
Visual confirmation of the installed carbon doubler.
Cutting a 1/4" plywood piece for the wing brace.
Drilling an 8mm hole for snug fit onto the spar.
Indicates the front inlet has been installed.
Application of Hysol end caps on pushrods.
Cleaning pushrods and end caps with alcohol.
Locating and cutting slits for ventral fin installation.
Drilling holes in the fuselage for fin screws.
Trimming the cockpit floor for proper canopy fit.
Center of Gravity located 4.25" behind the wing leading edge.
Taileron throws set at 0.75" left and 0.75" right.
Elevator throws set at 1.25" up and 1.25" down.
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General