Certification Analysis Using the Uncontained Engine Debris Damage Assessment Model (UEDDAM)

Details

• Creators:
  Phifer, Ellen
• Corporate Creators:
  SURVICE Engineering
• Corporate Contributors:
  Naval Air Warfare Center (U.S.). Aircraft Division ; United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Subject/TRT Terms:
  • Air engines
  • Aircraft
  • Engines
  • Hazards
  • Data models
  • Hazard mitigation
  • Failure
  • Certification
  • Analysis
  • Risk
  More +
• Publication/ Report Number:
  DOT/FAA/TC-21/24
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  March 2019 – February 2021
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration
• Abstract:
  This report documents how to use the Uncontained Engine Debris Damage Assessment Model (UEDDAM) to perform rotor burst hazard analyses in support of aircraft design and certification activities. Using a generic twin-engine aircraft as a case study, general guidance and recommended processes are provided on the use and function of UEDDAM in aircraft design optimization and hazard mitigation. Additional uses of UEDDAM within the overarching domain of aircraft safety, to include hole size calculations in support of decompression analyses, are also discussed.
• Format:
  PDF
• Funding:
  N68936-17-D-0028
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/57987/dot_57987_DS1.pdf
• File Type:
  [PDF - 14.11 MB]
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha256:5718a8d6a9c0bf3d622a098453e6f5b2dad79842589e2b09630996a84872bebb