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By: Michael Traskos

Guidelines for aircraft wiring: Magnet wire

Magnet wire is a conductor (copper or aluminum) with a thin insulation used in motors or transformers that is used in aircraft wiring. The wire is wound around a core to generate a magnetic field when an electrical voltage is applied – hence the name magnet wire. A key characteristic of a magnet wire is […] Read more

Guidelines for aircraft wiring: Which tests?

Aircraft wiring details are rarely found in common wire specifications. In fact, there is not a consistent set of specification tests for aerospace wiring. One wire type requires testing of the wicking properties, whereas the other does not. As an engineer, this can be unnerving at times, because it prevents a simple comparison between the […] Read more

When should you consider adopting an aircraft wire life extension program? Part VII

Through this series of articles, we have gone over all of the components that are necessary to perform a full risk assessment to maximize wire life extension. In this article, we will examine what a comprehensive risk assessment entails. Read more

Aircraft wire failure and incident investigation, Part II

A couple of weeks back, we wrote the Wire Failure and Incident Investigation article that reviewed some of the characteristics of wire failure and the means to detect them in a post aviation incident investigation. That article focused mostly on the conductor failure mechanisms. The three failure mechanisms that will be covered in this article […] Read more

Aircraft wire degradation and new research on red plague

We have addressed the red plague concept behind the aircraft wire degradation process in the For wire systems, there is no perfect conductor, not even a silver plated one article. However, since this issue has been spurring a new level of interest every five years, we are updating you on the new developments. To briefly […] Read more

A response to the TWA800 accident involving wire damage: SFAR-88

The SFAR88 requirements and related regulations (66 Fed. Reg. (May 7, 2001)) was the immediate FAA response to the TWA800 accident investigation involving wire damage. The investigation, conducted by the NTSB, indicated that the probable cause was a wire failure that resulted in additional energy being transferred to the fuel quantity indicating system (FQIS). This […] Read more

Understanding wire failure risk levels for aircraft EWIS

To determine the risk level for each EWIS component, one needs to look at the combination of failure probability and failure severity. This article will review the different levels for of failure probability and failure severity. Read more

Aircraft wire failure and incident investigation, Part I

The hazard of aircraft wire failure and electrical arcing will exist for as long as there is a need to deliver electrical power through wires. While electrical arcing is a common occurrence, the factors that impact an arcing event are often not well understood. This article reviews each step involved in electrical arcing, from what […] Read more

Aircraft EWIS failure and the process of electrical arcing

The hazard of aircraft EWIS failure and electrical arcing will exist for as long as there is a need to deliver electrical power through wires. While electrical arcing is a common occurrence, the factors that impact an arcing event are often not well understood. This article reviews each step involved in electrical arcing, from what […] Read more

When should you consider adopting an aircraft wire insulation assessment program? Part VI

SubTopic: Determining the Severity of Failure for wire life extension. A wire insulation assessment is a significant step forward in understanding the condition of the wire system and the topic of aircraft wire life extension for aerospace. However, to achieve a full system risk assessment, the assessment of probability of failure must be combined with […] Read more