SAE AIR1537A
Current
The latest, up-to-date edition.
REPORT ON AIRCRAFT ENGINE CONTAINMENT
Hardcopy , PDF
English
01-08-1996
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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 |
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