Abstract: An electrical plug is provided for supplying electricity comprising a plug with two sections, a body section and a detachable faceplate section. The faceplate is compact and is fabricated using a hard flexible plastic which enables the faceplate to act as a cover to the plug and enhances the resistance of the plug to the wear and tear of its field uses. The faceplate can be secured onto the body of the plug without any stress cracking using screws despite the compact thickness of the faceplate.

Abstract: A method, system and assembly for transferring electrical power adapted to provide power to a grounded aircraft is provided. The assembly comprises a first and second insulated electrical conductor and a plug body, attached to ends of these conductors. A first contact and a second contact is provided within the plug body, having electrically conductive connections with the first and second conductors. A non conductive support bar disposed at least partially within the plug body separating at least portions of the first contact and the first conductor from the second contact and the second conductor.

Abstract: A method, system and assembly for transferring electrical power adapted to provide power to a grounded aircraft is provided. The assembly comprises a first and second insulated electrical conductor and a plug body, attached to ends of these conductors. A first contact and a second contact is provided within the plug body, having electrically conductive connections with the first and second conductors. A non conductive support bar disposed at least partially within the plug body separating at least portions of the first contact and the first conductor from the second contact and the second conductor.