Damage-Tolerance and Fatigue Evaluation of Structure

doi:10.21949/1403457

i

Damage-Tolerance and Fatigue Evaluation of Structure

1997-02-18
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Corporate Creators:

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

Airframes Airplanes Compliance Damage-tolerance Failure Fatigue (Mechanics) Fatigue Evaluation Requirements Safe-Life Scatter Factors Structure Transport Aircraft
DOI:

https://doi.org/10.21949/1403457
Resource Type:

Organization Info
Geographical Coverage:

United States
Corporate Publisher:

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

This advisory circular (AC) sets forth an acceptable means of compliance with the provisions of Part 25 of the Federal Aviation Regulations (FAR) dealing with the damage-tolerance and fatigue evaluation requirements of transport category aircraft structure. It also provides rational guidelines for the evaluation of scatter factors for the determination of life for parts categorized as Safe-Life.
Format:

PDF
Collection(s):

US Transportation Collection
Main Document Checksum:

urn:sha-512:2cc778d1a2b77b75f2c5555edc57de443126e4423881a3129bf639b5e92f8492afcc0a84b9261392d00e380c072e0bc129079476462b92b4b351abcadbc74c96
Download URL:

https://rosap.ntl.bts.gov/view/dot/12882/dot_12882_DS1.pdf
File Type:

[PDF - 900.29 KB ]

File Language:

English

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Details

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