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FAA AC 20-128:1997

FAA AC 20-128:1997 Design Considerations For Minimizing Hazards Caused By Uncontained Turbine Engine And Auxiliary Power Unit Rotor Failure Provides a method of compliance with the requirements of section 23.901(f), 23.903(b)(1), 25.901(d) and 25.903(d)(1) of the Federal Aviation Regulations (FAR) pertaining to design precautions taken to

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Table of Contents

1PURPOSE
2CANCELLATION
3APPLICABILITY
4RELATEDDOCUMENTS
5BACKGROUND
6DEFINITIONS
7DESIGNCONSIDERATIONS
8ACCEPTEDDESIGNPRECAUTIONS
9ENGINEANDAPUFAILUREMODEL
10SAFETYANALYSIS
APPENDIX1AC-20-128AUSER'SMANUAL-RISKANALYSIS
METHODOLOGYforUNCONTAINEDENGINE/APUFAILURE

Abstract

Provides a method of compliance with the requirements of section 23.901(f), 23.903(b)(1), 25.901(d) and 25.903(d)(1) of the Federal Aviation Regulations (FAR) pertaining to design precautions taken to minimize the hazards to an airplane in the event of uncontained engine or auxiliary power unit (APU) rotor failures.

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