Enhancing Damage Tolerance Analysis with Method-Specific Probability of Detection Data
References
- Aeronautical Sciences. (2017). Airframe structural fatigue.
https://aeronauticausa.com/wp-content/uploads/2023/10/AAS-2017-P12004-Airframe-Structural-Fatigue.pdf - Berens, A. P. (2000). Probability of detection (POD) analysis for the advanced retirement for cause (RFC) / engine structural integrity program nondestructive evaluation system development (AFRL-ML-WP-TR-2001-4010). Air Force Research Laboratory.
- European Union Aviation Safety Agency. (n.d.). Acceptable means of compliance for CS-25.571 (AMC 25.571).
- European Union Aviation Safety Agency. (n.d.). Certification memorandum: Installation of antennas on large aeroplanes (CS-25).
- European Union Aviation Safety Agency. (n.d.). CS-25 amendment 19—Change information.
- European Union Aviation Safety Agency. (2023). Easy access rules for large aeroplanes (CS-25).
https://www.easa.europa.eu/en/document-library/easy-access-rules/online-publications/easy-access-rules-large-aeroplanes-cs-25 - Federal Aviation Administration. (1978). Amendment 25–45 to 14 CFR Part 25—Airworthiness standards: Transport category airplanes.
- Federal Aviation Administration. (1995). Transport airplane and engine issue area general structures harmonization working group task 5: Damage tolerance.
-
Federal Aviation Administration. (2015). Advisory Circular 91-82A: Fatigue Management Programs for In-Service Issues.
https://www.faa.gov/documentLibrary/media/Advisory_Circular/AC_91-82A_with_Change_1.pdf Federal Aviation Administration 2015 Advisory Circular 91-82A: Fatigue Management Programs for In-Service Issueshttps://www.faa.gov/documentLibrary/media/Advisory_Circular/AC_91-82A_with_Change_1.pdf - Federal Aviation Administration. (2023). Damage tolerance and fatigue evaluation of structure (14 CFR §25.571).
https://drs.faa.gov/browse/excelExternalWindow/CFR_20230118_0025_C_25-571_00000.0001 - Miedlar, P. C., Berens, A. P., Gunderson, A., & Gallagher, J. P. (2002). Damage tolerant design handbook: Guidelines for the analysis and design of damage tolerant aircraft structures (AFRLVA-WP-TR-2003-3002). University of Dayton Research Institute.
- Nondestructive Testing Information Analysis Center. (2000). Nondestructive evaluation (NDE) capabilities data book (3rd ed.). NTIAC.
- The Boeing Company. (n.d.). Design for durability and damage tolerance (D6-24958). Boeing Commercial Airplanes.
- Treloar, A. E. (1939). Elements of statistical reasoning. Williams & Wilkins.
DOI: https://doi.org/10.2478/fas-2025-0004 | Journal eISSN: 2300-7591
Language: English
Submitted on: Apr 3, 2026
Accepted on: May 4, 2026
Published on: Jun 4, 2026
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
Related subjects:
© 2026 Scott A. Fohrman, Narendra Kumar Gadwal, Mark E. Barkey, Marcus Perry, Easir Arafat Papon, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution 4.0 License.