Validation Methods for MIL-STD-1760B Aircraft Station Interfaces
Also Known As: SAE AS47641A, SAE AS 47641
The SAE AS 47641A:2017 standard provides methods and techniques for validating the compliance of an Aircraft Station Interface (ASI) with the interface requirements outlined in MIL-STD-1760B Notice 3. This standard is specifically applicable for the validation of aircraft that are designed according to MIL-STD-1760B Notice 3. For aircraft designed to MIL-STD-1760A Notice 2, the validation standard AS4764 Issued 1995-04 is used.
The purpose of this standard is to ensure that the ASI meets the requirements specified in MIL-STD-1760B Notice 3, which establishes the interface standards for aircraft systems. The validation methods described in this standard enable organizations to verify that the ASI conforms to the interface requirements and operates correctly.
| Descriptors | Test equipment and instrumentation; Test procedures; Performance tests; Lightning protection; Defense industry; Electromagnetic compatibility; High voltage systems; Identification numbers; Aircraft |
| ICS Codes | 33.100 - Electromagnetic compatibility (EMC) 49 - Aircraft and space vehicle engineering 91.120.40 - Lightning protection |
| Language(s) | English |
| File Size | 3.6 MB |
