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

United States. Department of Transportation. Federal Aviation Administration

doi:10.21949/1514164

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ROSA P serves as an archival repository of USDOT-published products including scientific findings, journal articles, guidelines, recommendations, or other information authored or co-authored by USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to ensure public access to scientific information.

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

1997-03-25
By United States. Department of Transportation. Federal Aviation Administration

[PDF-1.67 MB]

English

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Details:

Alternative Title:

Advisory Circulars from 1997
Corporate Creators:

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

[+]

Air Pilots Air Transportation Guidelines
Publication/ Report Number:

AC 20-128A
DOI:

https://doi.org/10.21949/1514164
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 §§ 23.901(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.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

[+]

urn:sha-512:27d27435e18dc902072eded5b2dc86345551e1b8984d5c7cfee6d139a61569e8e4ffb9a8d9b32254b781b21633e26ee3831691c28d67fe6fc457fe15700bc773
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https://rosap.ntl.bts.gov/view/dot/70910/dot_70910_DS1.pdf
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AC 20-128A: Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor Failure

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