AC 33-5: Turbine Engine Rotor Blade Containment/Durability

doi:10.21949/1514579

i

AC 33-5: Turbine Engine Rotor Blade Containment/Durability

1990-06-18
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Alternative Title:

Advisory Circulars from 1990
Corporate Creators:

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

Air Pilots Air Transportation Guidelines
Publication/ Report Number:

AC 33-5
DOI:

https://doi.org/10.21949/1514579
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) provides guidance and acceptable methods, but not the only methods, that may be used by an applicant in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha-512:7ad9ab48662c0ffb45de6287389cb3594e5eef026c6238f80940f61ab356d25889ab2ffd1e1326a8454da63d3da02c21e488a7054945a6a3d91e0202b546f93f
Download URL:

https://rosap.ntl.bts.gov/view/dot/71324/dot_71324_DS1.pdf
File Type:

[PDF - 372.58 KB ]

File Language:

English

ON THIS PAGE

Details

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.