Validation Methods for MIL-STD-1760 Aircraft Station Interfaces
Also Known As: SAE AS4764A, SAE AS 4764
SAE AS 4764A:2017 is a standard that outlines the validation methods for aircraft station interfaces in compliance with MIL-STD-1760. It provides techniques and guidelines for verifying that an aircraft station meets the interface requirements specified in MIL-STD-1760.
The standard aims to ensure that the interface between aircraft and various equipment, such as weapons and stores, adheres to the specifications and standards laid out in MIL-STD-1760. It establishes a framework for testing and validating the functionality and compatibility of the aircraft station interfaces.
By following the procedures outlined in SAE AS 4764A:2017, aerospace engineers and technicians can verify that an aircraft station's interface meets the necessary requirements, focusing on aspects such as electrical, mechanical, and data communication compatibility. The standard helps to ensure that the integration of aircraft systems and equipment is done correctly and in accordance with industry standards.
| Descriptors | Lightning protection; Defense industry; Electromagnetic compatibility; High voltage systems; Identification numbers; Aircraft; Failure analysis; Humidity; Electric power; Test equipment and instrumentation |
| ICS Codes | 33.100 - Electromagnetic compatibility (EMC) 49 - Aircraft and space vehicle engineering 91.120.40 - Lightning protection |
| Language(s) | English |
| File Size | 16.0 MB |
