Application of Probability of Crack Detection to Aircraft Systems Reliability.

Brewer, John C.; Jeong, David Y.; John A. Volpe National Transportation Systems Center (U.S.)

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Application of Probability of Crack Detection to Aircraft Systems Reliability.

1993-08-31
By Brewer, John C. ; Jeong, David Y.

[PDF-924.97 KB]

English

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Details:

Creators:

Brewer, John C. ; Jeong, David Y.

Brewer, John C. ; Jeong, David Y. Less -
Corporate Creators:

John A. Volpe National Transportation Systems Center (U.S.)
Subject/TRT Terms:

[+]

Airframes Cracking Fatigue (Mechanics) Fuselages Stochastic Processes
Publication/ Report Number:

LTR-FA4H2-9402
Resource Type:

Tech Report
Corporate Publisher:

United States. Federal Aviation Administration
NTL Classification:

NTL-AVIATION-Aviation Safety/Airworthiness
Abstract:

This report describes three tasks related to probability of crack detection (POD) and aircraft systems reliablity. All three consider previous work in which crack growth simulations and crack detection data in the Service Difficulty Report (SDR) database were used to estimate the in-service POD. The first task compared the POD estimates with estimates obtained from other sources. The second task assessed the self-consistency of the estimate POD and the crack growth simulation. The third task integrated the POD estimates with crack growth data and residual strength models to assess the cumulative probability that damage will be detected as a function of loss in residual strength.
Format:

PDF
Collection(s):

Volpe Center
Main Document Checksum:

[+]

urn:sha256:d01ffb5981629ee9f02b75ff5135435ed39d065641ce184eaf8f476097ff11c9
Download URL:

https://rosap.ntl.bts.gov/view/dot/9571/dot_9571_DS1.pdf
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Application of Probability of Crack Detection to Aircraft Systems Reliability.

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