This document establishes techniques for validating that an Aircraft Station interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
The purpose of this document is to provide methods for validating that an aircraft's store electrical interface complies with the aircraft station interface (ASI) requirements of MIL-STD-1760C. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760.
The purpose of this document is to provide methods for validating that an aircraft's store electrical interface complies with the aircraft station interface (ASI) requirements of MIL-STD-1760C. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760.
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