AC 20-128: Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor and Fan Blade Failures

United States. Department of Transportation. Federal Aviation Administration

doi:10.21949/1514163

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AC 20-128: Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor and Fan Blade Failures

1988-03-09
By United States. Department of Transportation. Federal Aviation Administration

[PDF-250.59 KB]

English

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Details:

Alternative Title:

Advisory Circulars from 1988
Corporate Creators:

United States. Department of Transportation. Federal Aviation Administration
Subject/TRT Terms:

[+]

Air Pilots Air Transportation Guidelines
Publication/ Report Number:

AC 20-128
DOI:

https://doi.org/10.21949/1514163
Resource Type:

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

This advisory circular (AC) sets forth a method of compliance with the requirements of §§ 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 (compressor and turbine) failure and engine fan blade failures. It is for guidance and to provide a method of compliance that has been found acceptable. As with all AC material, it is not mandatory and does not constitute a regulation.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

[+]

urn:sha256:38638c2238d4dc8cdc6b579b89b7e7887554525b02747853ca46446d80a8b6af
Download URL:

https://rosap.ntl.bts.gov/view/dot/70909/dot_70909_DS1.pdf
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AC 20-128: Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor and Fan Blade Failures

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