The goal of this paper is to review the statistical methods used in the aerospace industries to evaluate NDE reliability. The techniques presented are consistent with the damage tolerant design and structural maintenance philosophies of the aerospace industry. The first part of this paper establishes the evaluation criteria and discusses the history of NDE reliability evaluations. The second part describes the state-of-the-art analysis methods through examples from the retirement for cause (RFC) inspection system evaluation. The last part of the paper discusses some techniques used to rate operator performance and deal with false calls
The need to quantify and validate nondestructive inspection (NDI) performance capabilities has becom...
PDFTech ReportLTR-FA4H2-9402FuselagesStochastic processesCrackingFatigue (Mechanics)AirframesUnited ...
On-line NDE practices typically emerge through a sequence of steps starting with the selection of a ...
Changes in aircraft design concepts in recent years from “Safe-Life / Fail-Safe” to “Damage-Toleranc...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
The evaluation of the RFC/NDE System has produced capability characteristics in the format of â vs. ...
Current nondestructive evaluation techniques generally do not produce identical indications when app...
This paper presents results of Monte Carlo simulation of the Retirement-for-Cause (RFC) engine maint...
The damage tolerance approach to structural safety is based on the predicted growth of the “largest”...
Nondestructive evaluation (NDE) is widely used in the aerospace industry during scheduled maintenanc...
A key ingredient in the establishment of safe life times for critical components is the means of rel...
Nondestructive Inspection (NDI) plays a key role in assessing the condition of materials, components...
The RFC/NDE System comprises automated eddy current and ultrasonic inspection stations developed by ...
Starting with the damage tolerance design of structures in aerospace applications [1] it became obvi...
The methods developed to predict the reliability of aircraft structures depend upon inspection effec...
The need to quantify and validate nondestructive inspection (NDI) performance capabilities has becom...
PDFTech ReportLTR-FA4H2-9402FuselagesStochastic processesCrackingFatigue (Mechanics)AirframesUnited ...
On-line NDE practices typically emerge through a sequence of steps starting with the selection of a ...
Changes in aircraft design concepts in recent years from “Safe-Life / Fail-Safe” to “Damage-Toleranc...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
The evaluation of the RFC/NDE System has produced capability characteristics in the format of â vs. ...
Current nondestructive evaluation techniques generally do not produce identical indications when app...
This paper presents results of Monte Carlo simulation of the Retirement-for-Cause (RFC) engine maint...
The damage tolerance approach to structural safety is based on the predicted growth of the “largest”...
Nondestructive evaluation (NDE) is widely used in the aerospace industry during scheduled maintenanc...
A key ingredient in the establishment of safe life times for critical components is the means of rel...
Nondestructive Inspection (NDI) plays a key role in assessing the condition of materials, components...
The RFC/NDE System comprises automated eddy current and ultrasonic inspection stations developed by ...
Starting with the damage tolerance design of structures in aerospace applications [1] it became obvi...
The methods developed to predict the reliability of aircraft structures depend upon inspection effec...
The need to quantify and validate nondestructive inspection (NDI) performance capabilities has becom...
PDFTech ReportLTR-FA4H2-9402FuselagesStochastic processesCrackingFatigue (Mechanics)AirframesUnited ...
On-line NDE practices typically emerge through a sequence of steps starting with the selection of a ...