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Engine Titanium Consortium - Center for Nondestructive Evaluation ...

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Task 2:<br />

Task 2.2<br />

Subtask 2.2.2:<br />

Inservice Inspection<br />

Inspection Development<br />

Transitions to Airline<br />

Maintenance<br />

High Speed Bolthole Eddy<br />

Current Scanning<br />

Team Members:<br />

HW: Tim Duffy, Jim Ohm, Waled Hassan<br />

ISU: Lisa Brasche<br />

GE: Tony Mellors, Shridhar Nath, Jon<br />

Bartos<br />

PW: Kevin Smith, Dave Bryson, Rob<br />

Stephan<br />

Students: None<br />

Program initiation date: June 15, 1999<br />

Objectives:<br />

To develop common fixtures to reduce inspection variables and arrive at a standardized inspection<br />

technique.<br />

To measure the process capability.<br />

To utilize this in<strong>for</strong>mation to develop an industry best practice document.<br />

Approach:<br />

<strong>Evaluation</strong> of Existing Processes: Ef<strong>for</strong>ts will concentrate on process improvements <strong>for</strong> and<br />

standardization of high speed bolt hole scanning. A detailed evaluation of existing OEM inspection<br />

processes and needs will be conducted. Current equipment and tooling will be analyzed to provide<br />

a baseline of existing inspection processes and their limitations. The data will be analyzed <strong>for</strong><br />

potential process improvements and identification of common tooling approaches. A survey of<br />

available commercial tooling will be included as part of the assessment and included in the baseline<br />

as possible.<br />

Development of Common Tooling: The ef<strong>for</strong>ts will then be focused on the detailed design and<br />

fabrication of common tooling with an emphasis placed on variability reduction and defect<br />

detectability improvements. An inspection demonstration will be conducted on a sample set of<br />

hardware from each of the industrial members <strong>for</strong> validation of process development. A<br />

comparison to the baseline data will be made. Working with task 3.1.3 an evaluation of the process<br />

POD will be conducted on existing bolt hole reliability specimens.<br />

Development of Common Process: A common inspection technique and best practices document<br />

will be developed. Currently AS4787, Eddy Current Inspection of Circular Holes in Nonferrous<br />

Metallic Aircraft <strong>Engine</strong> Hardware, serves as a standard <strong>for</strong> hole inspection. This document will be<br />

revised to reflect the results of the ETC ef<strong>for</strong>t. Recommendations <strong>for</strong> equipment improvements will<br />

be supplied to vendors and implications <strong>for</strong> further study will be provided to the FAA.<br />

Quarterly Report – January 1, 2002 –March 31, 2002<br />

print date/time: 6/6/2002 - 8:39 AM – Page 71

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