ADS-68-IS, AERONAUTICAL DESIGN STANDARD INTERFACE STANDARD AIRCRAFT ELECTRICAL POWER CHARACTERISTICS

ADS-68-IS, AERONAUTICAL DESIGN STANDARD INTERFACE STANDARD AIRCRAFT ELECTRICAL POWER CHARACTERISTICS. The primary purpose of this standard is to provide the requisite information to promote compatibility between aircraft electrical power, external electrical power, and the airborne equipment that uses that power, with MIL-STD-704 serving as the governing document. Accordingly, the content of past versions of MIL-STD-704 is presented here to enable comparisons of the detailed requirements. To ensure that an individual piece of equipment will work satisfactorily in multiple types of aircraft, a worstcase set of electrical interface criteria should be developed from the applicable versions of MIL-STD-704 and subsequently imposed as an interface requirement for that equipment to ensure compatibility with the various types of aircraft being addressed.