An Aircraft electrical system market is a crucial and vital part of any aircraft. Between a light, piston-powered, single-engine general aviation aircraft and a contemporary, multi-engine commercial jet aircraft, there are significant differences in electrical system capacity and complexity. Nevertheless, the electrical systems for aircraft at both extremes of complexity contain a lot of the same fundamental parts. There are parts that can produce electricity in any aircraft electrical system market size. Generators or alternators are employed, depending on the aircraft, to generate electricity. These are typically engine-driven but can also be APU, hydraulic, or Ram Air Turbine-powered (RAT). The output of a generator is typically 115–120V/400HZ AC, 28V DC, or 14V DC. It is possible to use generator power straight away or to change the voltage or type of current by passing it through transformers, rectifiers, or inverters. The output of the generator will typically be sent to one or more distribution buses. Individual components are powered from the bus with circuit protection provided by wiring-integrated circuit breakers or fuses. The airplane battery is additionally charged using the generator output (s). In order to power diverse aircraft components, more complex electrical systems typically use multiple voltage systems that include AC and DC buses. Typically, the DC buses are powered by one or more Transformer Rectifier Units (TRUs), which convert primary AC power generation to DC voltage. An APU typically provides secondary AC generation for use both on the ground while the engines are off and in the air in the case of component failure. To offer redundancy in the event of multiple failures, tertiary generation in the form of a hydraulic motor or a RAT may also be integrated into the system. A particular arrangement is designed to power these buses in practically all failure scenarios, and essential AC and DC components are wired to specific buses. A static