Provides a means to display the voltages at each of the following locations:
ESS 1 BUS
ESS 2 BUS
NON ESS BUS
Flight Control System Inverter
Describe the alternating current system and identify its power sources.
There are two static inverters (Solid-state) which each take an input of 28 v DC and produce 400 Hz, 115 Volt and 26 v alternating current. The avionics inverter works with the avionics and flight control system yaw axis. The FCS inverter works only with the flight control system. The inverters are controlled by circuit breakers on the overhead console.