Assessing conditions of aircraft wiring

Data processing: measuring – calibrating – or testing – Measurement system in a specific environment – Mechanical measurement system

Reexamination Certificate

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Reexamination Certificate

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07925453

ABSTRACT:
A method of assessing potential conditions affecting aircraft electrical wiring systems. Electrical wiring system components potentially affected by a potential failure condition of the aircraft are identified. Probabilistic and/or statistical methods are used to determine exposure of one or more wire segments of the identified component(s) to hazard and whether the exposure meets a predetermined safety threshold. Effects of potential failure modes of the identified segment(s) on a system safety assessment for the electrical wiring systems are evaluated. This method can be used to facilitate compliance with aircraft safety regulations.

REFERENCES:
patent: 7536284 (2009-05-01), Linzey et al.
W. G. Linzey, Development of an Electrical Wire Interconnect System Risk Assessment Tool, Sep. 2006, p. 1-34.
Enhanced Airworthiness Program for Airplane Systems/Fuel Tank Safety (EAPAS/FTS); Federal Register/vol. 72, No. 216, Dated Thursday, Nov. 8, 2007; pp. 63364-63414.
Proposed Rules; Federal Register/vol. 70, No. 193, Dated Oct. 6, 2005; pp. 58548-58552.
Notice of Proposed Amendment (NPA) No. 2007-01; European Aviation Safety Agency (EASA); pp. 1-148.
Hasson, Jeff et al. “Boeing's Safety Assessment Processes For Commercial Airplane Designs”, AIAA/IEEE Digital Avionics Systems Conference—Proceedings 1997 IEEE, vol. 1, 1997, pp. 4.4-1-4.4-4, XP002540691.
Mazzuchi, Thomas A. et al. “A Paired Comparison Experiment for Gathering Expert Judgment For An Aircraft Wiring Risk Assessment”, Reliability Engineering and System Safety, Elsevier Applied Science, GB, vol. 93, No. 5, Mar. 16, 2007, pp. 722-731, XP022424831.

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