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SAE AS47642

Validation Methods for MIL-STD-1760C Aircraft Station Interfaces

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Organization: SAE
Publication Date: 1 June 2017
Status: active
Page Count: 182
scope:

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.

Purpose

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.

 

Document History

SAE AS47642
June 1, 2017
Validation Methods for MIL-STD-1760C Aircraft Station Interfaces
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...
March 1, 2007
Validation Methods for MIL-STD-1760C Aircraft Station Interfaces
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...
March 1, 2007
Validation Methods for MIL-STD-1760C Aircraft Station Interfaces
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...
June 1, 2004
Validation Methods for MIL-STD-1760C Aircraft Station Interfaces
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...

References

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