Brief Description: Worked on Wiring the Left Side of the Panel
Worked on Wiring the Left Side of the Panel.
Installed a "Keep Alive" terminal using the 1A power provided by the plug J7 Pin13. This power is needed to provide continuous power to the GRT EFIS clocks and will provide trickle charge power to the TCW IBBS.
Installed and wired Engine Switches to the Left Side Panel. One switch will control which Engine Power Fused Panels in the rear of the aircraft will be providing critical electrical power to the engine. This power is for the ECU, Main Fuel Pump, Propeller Control and Electronic Ignition/Fuel Injection. Each panel is capable of providing the power and together form a redundant engine electric power system. The other switch that was installed interrupts power to the ECU and the Ignition, two of the ciritical powers that would run continuously without this switch to remove power. It is a means of killing the engine.