REPORT ON AIRCRAFT ENGINE CONTAINMENT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

08-01-1991

Publisher

SAE International

1 INTRODUCTION AND BACKGROUND
1.1 Purpose, scope, committee representation
1.2 Committee membership and activity
1.3 Aerospace information report (AIR 1537) summary
2 DEFINITIONS
2.1 Definition of non-containment
2.2 Definition of aircraft damage
3 SUMMARY OF RESULTS
4 CONCLUSIONS, OBSERVATIONS AND RECOMMENDATIONS
5 DATA SUMMARIES
5.1 Data organization
5.2 Commercial transport engine data - tables and figures
5.3 General aviation engine data - tables and figures
5.4 Rotorcraft engine data - tables and figures
6 POTENTIAL FOR IMPROVEMENTS
6.1 Aircraft damage data - flight safety record
6.2 Engine design
6.3 Aircraft design
6.4 Other considerations

DocumentType	Standard
Pages	111
PublisherName	SAE International
Status	Current
Supersedes	SAE AIR 4003 : 1987

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