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<strong>Development</strong> <strong>of</strong> <strong>an</strong><br />

<strong>Improved</strong> <strong>Fire</strong> <strong>Test</strong><br />

<strong>Method</strong> <strong>an</strong>d <strong>Criteria</strong> <strong>for</strong><br />

Aircraft Electrical<br />

Wiring<br />

Presented to:<br />

The International Aircraft Material<br />

<strong>Fire</strong> <strong>Test</strong>ing Working Group<br />

By: John Reinhardt, Project M<strong>an</strong>ager, PMP<br />

Date: March 4-5, 2008<br />

Federal Aviation<br />

Administration


Outline<br />

• Project Initiating Process<br />

� Project Charter<br />

� Preliminary Scope Statement<br />

• Pl<strong>an</strong>ning Process<br />

� Develop Project Mgt Pl<strong>an</strong><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 />

2 <strong>of</strong> 27


Initiating Process<br />

PROJECT CHARTER<br />

• Date <strong>of</strong> Request: 24 October 2007<br />

• Sponsor: Jeff Gardlin, FAA Tr<strong>an</strong>sport Airpl<strong>an</strong>e Directorate<br />

• Program M<strong>an</strong>ager: Gus Sarkos, FAA <strong>Fire</strong> Safety<br />

• Project M<strong>an</strong>ager: John Reinhardt, PMP, FAA <strong>Fire</strong> Safety<br />

• FAA Business Needs (FAA Flight Pl<strong>an</strong> FY 2008):<br />

� Achieve the lowest possible commercial air carrier<br />

fatal accident rate:<br />

- Currently (2007): 8.8828 fatalities per 100 million<br />

persons onboard<br />

- FY 2012: 7.65 fatalities per 100 million persons<br />

onboard<br />

- FY 2025: 4.44 fatalities per 100 million persons<br />

onboard<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 />

3 <strong>of</strong> 27


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


Initiating Process<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 />

5 <strong>of</strong> 27


Initiating Process<br />

PROJECT CHARTER (CONT.)<br />

• Objectives:<br />

�Develop a fire test method <strong>for</strong> aircraft electrical<br />

wiring that could adequately discriminate<br />

between poorly per<strong>for</strong>ming wire insulation<br />

materials <strong>an</strong>d fire worthy ones when exposed to<br />

a realistic fire scenario.<br />

• Requirements:<br />

� Submit a final report documenting the<br />

developmental project <strong>an</strong>d the new test method.<br />

• Due Date (milestone):<br />

� 30 June 2009: Draft Final Report<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 />

6 <strong>of</strong> 27


Initiating Process<br />

PRELIMINARY SCOPE STATEMENT<br />

• This project will focus on the flammability<br />

characteristics <strong>of</strong> aircraft wiring insulation only.<br />

• It will consider the Radi<strong>an</strong>t Heat P<strong>an</strong>el test<br />

apparatus as a c<strong>an</strong>didate replacement.<br />

• Excluded: wire arcing, design issues,<br />

installation issues, mainten<strong>an</strong>ce issues, FAA<br />

policies, etc.<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 />

7 <strong>of</strong> 27


Outline<br />

• Project Initiating Process<br />

� Project Charter<br />

� Preliminary Scope Statement<br />

• Pl<strong>an</strong>ning Process<br />

� Develop Project Mgt Pl<strong>an</strong><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 />

8 <strong>of</strong> 27


Pl<strong>an</strong>ning Process<br />

- PROJECT MANAGEMENT PLAN<br />

• Scope<br />

• Time<br />

• Cost<br />

• Quality<br />

• Hum<strong>an</strong> Resource<br />

• Communications<br />

• Risk<br />

• Procurement<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 />

9 <strong>of</strong> 27


Pl<strong>an</strong>ning Process<br />

- SCOPE<br />

• Pl<strong>an</strong>ning<br />

• Definition<br />

• Create Work Breakdown Structure (see next slide)<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 />

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Pl<strong>an</strong>ning Process: Scope<br />

Work Breakdown<br />

Structure<br />

1.1 Review Historical In<strong>for</strong>mation<br />

1.2 Meet with Stakeholders<br />

1.3 Define <strong>Fire</strong> Threat<br />

1.4 <strong>Test</strong> <strong>Method</strong>s Selection<br />

1.5 Material Selection<br />

1. NEW FLAMMABILITY<br />

TEST FOR AIRCRAFT<br />

WIRING<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 />

1.6 Material <strong>Test</strong>ing<br />

1.7 Evaluate <strong>Test</strong> <strong>Method</strong>s<br />

1.8 Select/Modify Selected <strong>Test</strong> <strong>Method</strong><br />

1.9 Verify <strong>Test</strong> <strong>Method</strong><br />

1.10 Publish <strong>Test</strong> <strong>Method</strong><br />

Federal Aviation<br />

Administration<br />

11 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.1 Reviewed Historical In<strong>for</strong>mation<br />

• Title 14 Code <strong>of</strong> Federal Regulations Part 25.1713:<br />

“<strong>Fire</strong> Protection: EWIS”<br />

• Title 14 Code <strong>of</strong> Federal Regulations Part 25,<br />

Appendix F Part I(a)(3) – “Electrical System<br />

Components”<br />

• Title 14 Code <strong>of</strong> Federal Regulations Part 25,<br />

Appendix F Part I(b)(7) – “Sixty Degree <strong>Test</strong>”<br />

• Report DOT/FAA/AR-TN04/32 – “An Evaluation <strong>of</strong><br />

the Flammability <strong>of</strong> Aircraft Wiring,” Cahill, 2004<br />

• Report DOT/FAA/AR-04/21 – “MIL-W-22759 Vertical<br />

Flammability <strong>Test</strong> Versu the 60 Degree Flammability<br />

<strong>Test</strong>,” Gomez, 2004<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 />

12 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.1 Reviewed Historical In<strong>for</strong>mation<br />

• Report DOT/FAA/AR–00/42, ‘‘Aircraft Materials<br />

<strong>Fire</strong> <strong>Test</strong> H<strong>an</strong>dbook.’’ 2000<br />

• Report DOT/FAA/CT-89/21 – “Flammability,<br />

Smoke, <strong>an</strong>d Dry Arc Tracking <strong>Test</strong>s <strong>of</strong> Aircraft<br />

Electrical Wire Insulations” Cahill, 1989<br />

• SAE Aerospace St<strong>an</strong>dard AS4373, “<strong>Test</strong> <strong>Method</strong>s<br />

<strong>for</strong> Insulated Electric Wire.” 2007<br />

• IEC 60332-1, “<strong>Test</strong>s on Electric Cables Under <strong>Fire</strong><br />

Conditions – Part 1: <strong>Test</strong> on a Single Vertical<br />

Insulated Wire <strong>an</strong>d Cable.”<br />

• IEC 60332-3-10, “<strong>Test</strong>s on Electric Cables Under<br />

<strong>Fire</strong> Conditions – Part 3-10: <strong>Test</strong> <strong>for</strong> Vertical Flame<br />

Spread <strong>of</strong> Vertically-Mounted Bunched Wires or<br />

Cables – Apparatus<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 />

International Electrotechnical Commission<br />

Federal Aviation<br />

Administration<br />

13 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.1 Reviewed Historical In<strong>for</strong>mation<br />

• “Assessing the <strong>Fire</strong> Per<strong>for</strong>m<strong>an</strong>ce <strong>of</strong> Electric Cables (FIPEC)” by P. V<strong>an</strong> Hees,<br />

<strong>an</strong>d J. Axelsson, SP Sweden, S.J. Grayson <strong>an</strong>d A.M. Green, Interscience<br />

Communications UK, H Breulet, ISSeP Belgium <strong>an</strong>d U Vercellotti, CESI Italy<br />

• Report Number UCRL-93936, “Procedure <strong>for</strong> R<strong>an</strong>king <strong>Fire</strong> Per<strong>for</strong>m<strong>an</strong>ce <strong>of</strong><br />

Electrical Cables” by Hasegawa, Staggs <strong>an</strong>d Fern<strong>an</strong>dez-Pello, 1986<br />

• Federal <strong>Test</strong> <strong>Method</strong> St<strong>an</strong>dard No. 228, “Cable <strong>an</strong>d Wire, Insulated; <strong>Method</strong> <strong>of</strong><br />

<strong>Test</strong>ing,“1951<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 />

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Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.2 Meet with Stakeholders<br />

• FAA Sponsor<br />

• FAA Program M<strong>an</strong>ager<br />

• FAA <strong>Fire</strong> Safety Researchers<br />

• International Aircraft Materials <strong>Fire</strong> <strong>Test</strong><br />

Working Group<br />

• OEMs<br />

• Other<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 />

15 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.3 Define <strong>Fire</strong> Threat<br />

• Report DOT/FAA/AR-99/44 – “<strong>Development</strong><br />

<strong>of</strong> <strong>Improved</strong> Flammability <strong>Criteria</strong> <strong>for</strong> Aircraft<br />

Thermal Acoustic Insulation,” September 2000<br />

• And, Report DOT/FAA/AR-08/XX –<br />

“<strong>Development</strong> <strong>of</strong> <strong>Improved</strong> Flammability<br />

<strong>Criteria</strong> <strong>for</strong> Aircraft Ducting,” 1 st Qtr 2008<br />

• <strong>Fire</strong> Threat: 101.6 by 101.6 by 228.6-mm<br />

Ureth<strong>an</strong>e Foam Block (Density: 16.02 kg/m 3 )<br />

• Environment:<br />

� Sea Level<br />

� Narrow-body attic<br />

� Insulation bl<strong>an</strong>kets in attic<br />

� Insulated duct in attic<br />

� Quasi-Std Ambient Temperature<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 />

16 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.4 <strong>Test</strong> <strong>Method</strong>s Selection<br />

MEASUREMENT<br />

<strong>Fire</strong> Propagation<br />

Burn Area<br />

After Flame Time<br />

Drip Flame Time<br />

Total Heat Release<br />

Heat Release Rate<br />

Onset Temperature<br />

Combustion Temperature<br />

% Char<br />

60-Degree Bunsen<br />

Burner <strong>Test</strong><br />

Intermediate-<br />

Scale<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 />

MATERIAL TEST METHOD<br />

Microscale Combustion<br />

Calorimeter<br />

Federal Aviation<br />

Administration<br />

Radi<strong>an</strong>t Heat<br />

P<strong>an</strong>el<br />

17 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope: WBS 1.5 Material Selection<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 />

18 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.6 Material <strong>Test</strong>ing<br />

• <strong>Test</strong>s to be conducted:<br />

• 60-Degree Bunsen Burner <strong>Test</strong><br />

• Micro-scale Combustion Calorimeter<br />

• Intermediate-scale <strong>Fire</strong> <strong>Test</strong><br />

• Radi<strong>an</strong>t Heat P<strong>an</strong>el <strong>Test</strong> (Aircraft Ducting<br />

Version)<br />

• Other (as needed)<br />

• Results will help r<strong>an</strong>k materials based on their<br />

flammability characteristics.<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 />

19 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.7 Evaluate <strong>Test</strong> <strong>Method</strong>s<br />

MEASUREMENT<br />

<strong>Fire</strong> Propagation<br />

Burn Area<br />

After Flame Time<br />

Drip Flame Time<br />

Total Heat Release<br />

Heat Release Rate<br />

Onset Temperature<br />

Combustion Temperature<br />

% Char<br />

Current small-scale test measures:<br />

- <strong>Fire</strong> Propagation (Burn Length)<br />

- After flame time<br />

- Drip flame time<br />

60-Degree Bunsen<br />

Burner <strong>Test</strong><br />

Intermediate-<br />

Scale<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 />

MATERIAL TEST METHOD<br />

Microscale Combustion<br />

Calorimeter<br />

Federal Aviation<br />

Administration<br />

Radi<strong>an</strong>t Heat<br />

P<strong>an</strong>el<br />

Radi<strong>an</strong>t heat p<strong>an</strong>el test measures:<br />

- <strong>Fire</strong> Propagation<br />

- After Flame Time<br />

20 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.8 Select/Modify Selected <strong>Test</strong> <strong>Method</strong><br />

• The Radi<strong>an</strong>t Heat P<strong>an</strong>el (RHP) test machine is the<br />

plat<strong>for</strong>m currently used to test the flammability <strong>of</strong><br />

aircraft thermo acoustic insulation materials <strong>an</strong>d<br />

possibly, in the future, aircraft ducting.<br />

• The RHP test machine will be evaluated to<br />

determine if it could be used as a testing plat<strong>for</strong>m <strong>for</strong><br />

aircraft electrical wire bundles.<br />

• If the RHP plat<strong>for</strong>m doesn’t work out, <strong>an</strong>other<br />

plat<strong>for</strong>m will be identified, evaluated, <strong>an</strong>d selected.<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 />

21 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.9 Verify <strong>Test</strong> <strong>Method</strong> (Scope<br />

Verification)<br />

• The results <strong>of</strong> the data obtained from the developed<br />

fire test method will be compared against the results<br />

obtained during the intermediate-scale fire test. Of<br />

interest, will be in<strong>for</strong>mation about fire propagation <strong>an</strong>d<br />

burning time.<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 />

22 <strong>of</strong> 27


Pl<strong>an</strong>ning Process: Scope<br />

WBS 1.10 Publish <strong>Test</strong> <strong>Method</strong><br />

• Major Milestone<br />

• Draft Final Report must be submitted by 30<br />

June 2009<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 />

23 <strong>of</strong> 27


Pl<strong>an</strong>ning Process<br />

- TIME<br />

-COST<br />

• Project Activity Definition<br />

• Project Activity Sequencing<br />

• Project Activity Resource Estimate<br />

• Project Activity Duration Estimate<br />

• Schedule<br />

- G<strong>an</strong>tt Chart<br />

• Estimating & Budgeting (TBD)<br />

- QUALITY<br />

-<br />

• Material Inspection & Conditioning<br />

• Systems/instrumentation calibrations<br />

• Measurements Accuracy<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 />

24 <strong>of</strong> 27


Pl<strong>an</strong>ning Process<br />

-HUMAN RESOURCE<br />

• Input from IAMFTWG task group members will be<br />

requested<br />

• Work will be conducted by FAA <strong>Fire</strong> Safety Team<br />

& SRA technical staff<br />

• Responsibility Assignment Matrix will be provided<br />

- COMMUNICATIONS<br />

• In<strong>for</strong>mal Oral Presentations: FAA internal<br />

• Formal Oral Presentations: IAMFTWG<br />

• In<strong>for</strong>mal Written (E-mails): FAA & IAMFTWG<br />

• Final Formal Written Report<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 />

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Pl<strong>an</strong>ning<br />

RISK PLAN<br />

• FAA Safety Office<br />

• OSHA<br />

• Risk Mitigation/Response Pl<strong>an</strong><br />

• Etc.<br />

-PROCUREMENT PLAN<br />

• Create list <strong>of</strong> required materials, equipment,<br />

<strong>an</strong>d other resources<br />

• Request sellers response<br />

• Select vendors<br />

• Purchase require resources<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 />

26 <strong>of</strong> 27


Final Words<br />

Questions?<br />

Anyone interested in joining<br />

this task group?<br />

Contact:<br />

John Reinhardt<br />

609-485-5034<br />

john.reinhardt@faa.gov<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 />

27 <strong>of</strong> 27

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