(iS) Fuel System Testing: The fuel supply hose was removed from the RH fuel manifold on the engine. With a container marked on one gallon the fuel pump 1 and fuel pump 2. First fuel pump 1 was checked with and had no debris, the fuel come out clean, the same with fuel pump 2. The fuel line was reconnected. Fuel pump 1 switch, fuel pump 2 switch was run for 30 seconds and the pressure was: Fuel pump 1 switch: 43.6 Fuel pump 2 switch: 43.4 And both: 43.6 Turned off the master switch and there were no leaks.
Propeller and spinner installation: The spinner was removed. The prop blade pitch was set, Prop bolt torque and prop tracking was checked, The spinner was reinstalled. The pitot tube tracking was 1/32".
The master switch was turned on. The ignition lane A and B was "OFF". One wing pin was inlatch a red warning light comes on and the starter circuit was disables.
