Abstract
Electrical power system generates, regulates and distributes electrical power throughout the A/C. Aircraft electrical system includes power generation and power distribution system. Distribution of aircraft has contactors, which are located in the plates outside of the power distribution system, to provide control of the system. It is the main system energizing all the equipment on the aircraft. Verification of the system on the laboratory is a critical testing activity to achieve a safe system design. Functional checks, performance and compatibility with the related standards are needed to be tested before aircraft ground and flight tests.
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