EIA-STD-RS-170EIA-STD-RS-343-ASTANAG 3350-1995MIL-C-39029-1988MIL-STD-1553-1978SAE AS 4113-1989ASD-TR-87-5028MIL-A-8591MIL-B-5087MIL-C-38999MIL-C-45662MIL-E-6051MIL-HDBK-235MIL-HDBK-1553MIL-STD-461MIL-STD-462MIL-STD-704MIL-STD-1498MIL-ST
适用范围
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 aircrafts 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.