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This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 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-1760 Notice 3. 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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Published:
07/12/2012
File Size:
1 file , 3.1 MB