The aircraft electrical system includes a 28 VDC starter/generator, 28VDC battery, and an external power receptacle. Is this statement true or false?

The statement regarding the aircraft electrical system being composed of a 28 VDC starter/generator, a 28 VDC battery, and an external power receptacle is indeed considered true. In the T-6B aircraft, the electrical system is designed around a 28-volt direct current architecture, which integrates these components to provide a reliable power source for various systems.

The starter/generator functions by both starting the engine and generating electrical power during operation, while the battery serves to provide power on the ground and during start-up. The inclusion of an external power receptacle allows for ground support and battery maintenance, enhancing the versatility and operational capability of the electrical system.

As such, the correct answer to the question should acknowledge that the statement is true concerning the components of the electrical system.