The pictures gathered here show the end stage of the panel design development. It was driven by two primary factors: 1) Requirements of a minimal Corvair engine driven aircraft, 2) Engine control and instrumentation layout similar to C150/152 which I did my primary flight training in and will no doubt fly in from time to time. Development of this panel has gone through multiple iterations and the final version shown here as design drawing is based on analysis of circuit requirements for running the Corvair engine's critical electrical systems (ignition and power generation) and the non-critical electrical systems (lighting and avionics). I decided for traditional panel over software driven multi-display systems, though power and space is provided for COTS devices to run foreflight. I have spent at least 36 hours on the design and accumulation of tools and materials which converge on the panel itself. All electrical is being installed to standards defined in AC 43.13-B