A Case Study Using Failure Mode Effect Testing to Support the MIL-HDBK-516C Airworthiness Certification-Reference-Cited by-同舟云学术

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A Case Study Using Failure Mode Effect Testing to Support the MIL-HDBK-516C Airworthiness Certification

Published:2024-01-22 Issue: Volume: Page:1-6
ISSN:
Container-title:2024 Annual Reliability and Maintainability Symposium (RAMS)
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Author:

Yu Yangyang¹,Schmidt Blair¹,Swope Vanessa¹

Affiliation:

1. General Atomics Aeronautical Systems, Inc.,Poway,California,USA,92064

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10457287/10457579/10457697.pdf?arnumber=10457697

Reference7 articles.

1. MIL-HDBK-516C: Department of Defense Handbook Airworthiness Certification Criteria;Department of Defense,2014

2. AC-17 –01: Airworthiness Circular Verification Expectations for Select Section 15 Criteria;Department of the Air Force,2017

3. A Perspective on the State of Research on Fault Injection Techniques;Yu;Research Report, University of Virginia,2001

4. Concise Encyclopedia of System Safety

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