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2025 Vol.29, Issue 6 Preview Page

TECHNICAL PAPERS

31 December 2025. pp. 75-82
Abstract
References
1

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2

European Union Aviation Safety Agency(EASA), “CS-E Amendment 5 : Certification Specifications and Acceptable Means of Compliance for Engines CS-E.”

3

US Department of Defense, “MIL-HDBK -516C : Airworthiness Certification Criteria,” 2014.

4

US Department of Defense, ”MIL-HDBK -1783B : Engine Structural Integrity Program,” 2004.

5

Pratt&Whitney, “PW F100 Engine Celebrates 50 Years of Service and 30 Million Flight Hours,” Pratt&Whitney, Jul. 19, 2022, https://www.prattwhitney.com/en/newsroom/news/2022/07/19/pw-f100-engine-celebrates-50-years-of-service-and-30-million-flight-hours (accessed Sep. 12, 2025).

6

Alex, S., “GE Aviation Celebrates 50 Years’ Service - CF6 Engine,” GE Aerospace, Jul. 30, 2021, https://www.geaerospace.com/news/articles/product/ge-aviation-celebrates-50-years-service-cf6-engine (accessed Sep. 12, 2025).

7

National Transportation Safety Board, “United Airlines Flight 232 Mcdonnell Douglas DC-10-10 Sioux Gateway Airport Sioux City, Iowa,” NTSB/ AAR-90/06, 1990.

8

National Transportation Safety Board, “Uncontained Engine Failure and Subsequent Fire American Airlines Flight 383 Boeing 767-323, N345AN Chicago, Illinois,” NTSB/AAR-18/01, 2018.

9

National Transportation Safety Board, “Uncontained Engine Failure Delta Air Lines Flight 1288 Mcdonnell Douglas MD-88, N927DA Pensacola, Florida,” NTSB/AAR-98/01, 1998.

10

National Transportation Safety Board, “Safety Recommendation,” A-06-60 through–64, Aug. 28, 2006.

11

Federal Aviation Administration(FAA), “AIA Report on High Bypass Ratio Turbine Engine Uncontained Rotor Events and Small Fragment Threat Characterization,” Vol.1, 2010.

12

Federal Aviation Administration(FAA), “Advisory Circular 33.70-1 : Guidance Material for Aircraft Engine Life-Limited Parts Requirements,” 2014.

13

Federal Aviation Administration(FAA), Amdt. 33-22, 72 FR 50860, 2007.

14

Federal Aviation Administration(FAA), “Nondestructive Evaluation of Manufacturing-Induced Anomalies,” DOT/FAA/AR-10/32, 2011.

15

Davide, S., “DARPA’S OPEN MANUFACTURING TO FULLY UNRAVEL POTENTIAL OF METAL 3D PRINTING,” 3D Printing Industry, Aug. 11, 2014, https://3dprintingindustry.com/news/3d-printing-open-manufacturing-research-program-31142/ (accessed Sep. 12, 2025).

16

Federal Aviation Administration(FAA), “Guidelines to Minimize Manufacturing Induced Anomalies in Critical Rotating Parts – 2022 Revision,” DOT/ FAA/TC –23/8, 2023.

17

IAQG, “AS9100 QUALITY MANAGEMENT SYSTEMS-REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS,” http://iaqg.org/standard/9100-qms-requirements-for aviation-space-and-defense-organizations/ (accessed Sep. 12, 2025).

18

PRI, “NADCAP Committed to Absolute Quality,” PRI, http://www.p-r-i.org/nadcap (accessed Sep. 12, 2025).

19

ISO, “ISO/IEC 17025:2017, General requirements for the competence of testing and calibration laboratories,” ISO, 2017, http://www.iso.org/standard/ 66912.html (accessed Sep. 12, 2025).

Information
  • Publisher :The Korean Society of Propulsion Engineers
  • Publisher(Ko) :한국추진공학회
  • Journal Title :Journal of the Korean Society of Propulsion Engineers
  • Journal Title(Ko) :한국추진공학회지
  • Volume : 29
  • No :6
  • Pages :75-82
  • Received Date : 2025-07-07
  • Revised Date : 2025-09-12
  • Accepted Date : 2025-10-01