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Development of an Improved Fire Test Method and Criteria for ...

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Initiating Process<br />

PROJECT CHARTER (CONT.)<br />

• Project Justification:<br />

� The FAA initiated ef<strong>for</strong>ts to improve the<br />

fireworthiness <strong>of</strong> hidden areas in the<br />

aircraft (T/A Insulation, ducting <strong>an</strong>d wires)<br />

� Report DOT/FAA/AR-TN04/32, “An<br />

Evaluation <strong>of</strong> the Flammability <strong>of</strong> Aircraft<br />

Wiring,” (Cahill) concluded that the current<br />

FAA 60 degree test is not adequate <strong>for</strong><br />

qualification <strong>of</strong> wire bundles.<br />

� The Sixty Degree <strong>Test</strong>, Title 14 Code <strong>of</strong><br />

Federal Regulations Part 25, Appendix F<br />

Part I (b)(7)) <strong>an</strong>d Chapter 4 in the Aircraft<br />

Material <strong>Fire</strong> <strong>Test</strong> H<strong>an</strong>dbook, must be<br />

replaced.<br />

<strong>Development</strong> <strong>of</strong> <strong>an</strong> <strong>Improved</strong> <strong>Fire</strong> <strong>Test</strong> <strong>Method</strong> <strong>an</strong>d <strong>Criteria</strong> <strong>for</strong><br />

Aircraft Electrical Wiring<br />

Federal Aviation<br />

Administration<br />

4 <strong>of</strong> 27

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