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

doi:10.21949/1514163

i

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

File Language:

English

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Alternative Title:

Advisory Circulars from 1988
Corporate Creators:

United States. Department of Transportation. Federal Aviation Administration
Corporate Publisher:

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

AC 20-128
DOI:

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

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Description:

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
Download URL:

https://rosap.ntl.bts.gov/view/dot/70909/dot_70909_DS1.pdf
File Type:

[PDF - 250.59 KB]
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha-512:84e54b756723e3430b1329c04d02f2a06869e162fa744be951ad7d23d866e2d4edd8c26bbafeba4bef81811048e57421997155723f7011e0e8f0be29f3011feb

File Language:

English

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