Test run the engine with the prop pitch set to 8 degrees from the 10 degrees it wa set to earlier. The static RPM went from 2600 at 10 degrees to 2830 at 8 degrees. This will be satisfactory for test flight and optimized for takeoff and climb. All temperatures and oil pressure was normal. The fuel pressure was 5 psi at 2000 RPM and 3 psi at 2800 RPM.
Prop pitch will remain at 8 degrees for the first flights.
