REPORT ON AIRCRAFT ENGINE CONTAINMENT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-08-1996

Publisher

SAE International

INTRODUCTION AND BACKGROUND
1. SCOPE
2. SUMMARY
3. CONCLUSIONS, OBSERVATIONS, AND RECOMMENDATIONS
4. DEFINITIONS
5. ANALYSIS OF DATA
6. SERVICE DATA
7. POTENTIAL FOR IMPROVEMENT
APPENDIX A
APPENDIX B - SUMMARY OF NON-CONTAINED ROTOR FAILURES
FOR COMMERCIAL AIRCRAFT JANUARY 1962 -
DECEMBER 1975

The study shall be directed to commercial aircraft service and include engine experience in both fixed wing aircraft and helicopters covering the time period from 1962 to the present.

DocumentType	Standard
Pages	46
PublisherName	SAE International
Status	Current

FAA AC 20-128 : 0	DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
FAA AC 33.14-1 : 0	DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS
FAA AC 33.70-2 : 2009	DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS