Brief Description: PArt 3 - Drilling Platenuts and mounting avionics
Drilled holes through the carbon fiber panel and aluminum frame. Drilled and installed platenuts on all holes. Drilled center avionics stack and mounted plate nuts on the carbon fiber flange. Installed temporary panel screws. These are pan head #8 standard issue. May decide to go flush mount but will determine that after the avionics are installed and the panel is painted.
