AC 35.37-1: Composite Propeller Blade Fatigue Substantiation

doi:10.21949/1514581

i

AC 35.37-1: Composite Propeller Blade Fatigue Substantiation

1993-05-11
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Alternative Title:

Advisory Circulars from 1993
Corporate Creators:

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

Air Pilots Air Transportation Guidelines
Publication/ Report Number:

AC 35.37-1
DOI:

https://doi.org/10.21949/1514581
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 an acceptable method, but not the only method, by which composite propeller blades can be fatigue evaluated for determination of safe vibratory loadings, as required by Federal Aviation Regulations (FAR) 35.37.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha-512:efcc58e5208c355b895ab5097626211d726947c7035b7ad47be1e786f5cee1418dcac47fa400b50ea3fa00a245e39212c1ef04934e8a05bc9d4b38f7ae74ed7f
Download URL:

https://rosap.ntl.bts.gov/view/dot/71326/dot_71326_DS1.pdf
File Type:

[PDF - 491.99 KB ]

File Language:

English

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Details

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