View Latest Blog Entries
Close
Categories
Testing & Assessment Certification Standard & Regulation Aging Wires & Systems Maintenance & Sustainment Management Conference & Report Protection & Prevention Research Miscellaneous Arcing
Popular Tags
Visual Inspection High Voltage AS50881 MIL-HDBK MIL-HDBK-525 FAR AS4373 Maintenance Electromagnetic Interference (EMI) FAR 25.1707 Wire System Arcing Damage
All Tags in Alphabetical Order
2021 25.1701 25.1703 abrasion AC 33.4-3 AC 43 Accelerated Aging accessibility ADMT Aging Systems AIR6808 AIR7502 Aircraft Power System aircraft safety Aircraft Service Life Extension Program (SLEP) altitude arc damage Arc Damage Modeling Tool Arc Fault (AF) Arc Fault Circuit Breaker (AFCB) Arc Track Resistance Arcing Arcing Damage AS22759 AS22759/87 AS23053 AS29606 AS4373 AS4373 Method 704 AS50881 AS5692 AS6019 AS6324 AS81824 AS83519 AS85049 AS85485 AS85485 Wire Standard ASTM B355 ASTM B470 ASTM D150 ASTM D2671 ASTM D8355 ASTM D876 ASTM F2639 ASTM F2696 ASTM F2799 ASTM F3230 ASTM F3309 ATSRAC Attenuation Automated Wire Testing System (AWTS) Automotive Avionics backshell batteries bend radius Bent Pin Analysis Best of Lectromec Best Practice bonding Cable Cable Bend cable testing Carbon Nanotube (CNT) Certification cfr 25.1717 Chafing Chemical Testing Circuit Breaker circuit design Circuit Protection cleaning clearance Coaxial cable cold bend collision comparative analysis Compliance Component Selection Condition Based Maintenance Conductor Conductor Testing conductors conduit Connector Connector rating connector selection connector testing connectors contacts Corona Corrosion Corrosion Preventing Compound (CPC) corrosion prevention Cracking creepage D-sub data analysis data cables degradat Degradation Delamination Derating design safety development diagnostic Dielectric breakdown dielectric constant Dimensional Life disinfectant Distributed Power System DO-160 dry arc dynamic cut through E-CFR electric aircraft Electrical Aircraft Electrical Component Electrical Power Electrical Testing Electrified Vehicles Electromagnetic Interference (EMI) Electromagnetic Vulnerability (EMV) Electrostatic Discharge EMC EMF EN2235 EN3197 EN3475 EN6059 End of Service Life End of Year Energy Storage engines Environmental Environmental Cycling environmental stress ethernet eVTOL EWIS certification EWIS Component EWIS Design EWIS Failure EWIS sustainment EWIS Thermal Management EZAP FAA FAA AC 25.27 FAA AC 25.981-1C FAA Meeting failure conditions Failure Database Failure Modes and Effects Analysis (FMEA) FAQs FAR FAR 25.1703 FAR 25.1707 FAR 25.1709 Fault fault tree Fixturing Flammability fleet reliability Flex Testing fluid exposure Fluid Immersion Forced Hydrolysis fuel system fuel tank ignition Functional Hazard Assessment functional testing Fundamental Articles Fuse Future Tech galvanic corrosion Glycol Gold Gold plating Green Taxiing Grounding hand sanitizer handbook Harness Design harness protection hazard Hazard Analysis health monitoring heat shrink heat shrink tubing high current high Frequency high speed data cable High Voltage High Voltage Degradation HIRF History Hot Stamping Humidity Variation HV connector HV system ICAs IEC 60851 IEC60172 IEEE immersion insertion loss Inspection installation installation safety Instructions for Continued Airworthiness insulating material insulating tape Insulation insulation breakdown insulation resistance insulation testing interchangeability IPC-D-620 ISO 17025 Certified Lab ISO 9000 J1673 Kapton Laser Marking life limit life limited parts Life prediction life projection Lightning lightning protection liquid nitrogen lithium battery lunar Magnet wire maintainability Maintenance Maintenance costs Mandrel mean free path measurement mechanical stress Mechanical Testing MECSIP MIL-C-38999 MIL-C-85485 MIL-DTL-17 MIL-DTL-23053E MIL-DTL-3885G MIL-DTL-38999 MIL-E-25499 MIL-HDBK MIL-HDBK-1646 MIL-HDBK-217 MIL-HDBK-454 MIL-HDBK-516 MIL-HDBK-522 MIL-HDBK-525 MIL-HDBK-683 MIL-STD-1353 MIL-STD-1560 MIL-STD-1798 MIL-STD-464 MIL-T-7928 MIL-T-7928/5 MIL-T-81490 MIL-W-22759/87 MIL-W-5088 MIL–STD–5088 Military 5088 modeling moon MS3320 NASA NEMA27500 Nickel nickel plating No Fault Found OEM off gassing Outgassing Over current Overheating of Wire Harness Parallel Arcing part selection Partial Discharge partial discharge at altitude Performance physical hazard assessment Physical Testing polyamide polyimdie Polyimide-PTFE Power over Ethernet power system Power systems predictive maintenance Presentation Preventative Maintenance Program Probability of Failure Product Quality PTFE pull through Radiation Red Plague Corrosion Reduction of Hazardous Substances (RoHS) regulations relays Reliability Research Resistance Revision C Rewiring Project Risk Assessment S&T Meeting SAE SAE Committee Sanitizing Fluids Secondary Harness Protection separation Separation Requirements Series Arcing Service Life Extension Severe Wind and Moisture-Prone (SWAMP) Severity of Failure shelf life Shield Shielding Shrinkage signal signal cable Silver silver plated wire silver-plating skin depth skin effect Small aircraft smoke Solid State Circuit Breaker Space Certified Wires Splice standards Storage stored energy superconductor supportability Sustainment System Voltage Temperature Rating Temperature Variation Test methods Test Pricing Testing testing standard Thermal Circuit Breaker Thermal Endurance Thermal Index Thermal Runaway Thermal Shock Thermal Testing tin Tin plated conductors tin plating tin solder tin whiskering tin whiskers top 5 Transient Troubleshooting TWA800 UAVs UL94 USAF validation verification video Visual Inspection voltage voltage differential Voltage Tolerance volume resistivity vw-1 wet arc white paper whitelisting Winding wire Wire Ampacity Wire Bend Wire Certification Wire Comparison wire damage wire failure wire performance wire properties Wire System wire testing Wire Verification wiring components work unit code

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

Aging Wires & Systems

This is the second in a series of articles addressing the concepts associated with an Electrical Wire Interconnection System (EWIS) analysis of aging aircraft. In other words, when to consider an aircraft wire life extension program. The last article addressed the reasons to consider implementing EWIS assessment as part of a wire life extension program. This article reviews the fundamental concepts behind risk and risk assessment and how it is applied to an EWIS investigation.

If you are interested in wire life extension, you may want to read the The Big Three Wire System Degradation Assessment Options article.

What is Risk?

Let’s start with what should be the first question, “What is risk?” Risk is often a misapplied term. When applied to an engineering process or assessment of a system, risk can be simplified to being a combination of failure probability and failure severity.

wire life extension
Risk is easy to understand. Understanding how to put it all together takes data and analysis.

Probability of Failure

The probability of failure is a numeric quantity that is typically based on field data or laboratory analysis that determines the degradation of the wire (more on this in future articles). The probability of failure then paired with the qualitative assessment on the failure severity. The acceptable level for combined probability and severity is dependent upon the actual use. A low value system may have a high probability of failure and may not need to be resolved, whereas a high-value/mission-critical system must have a much lower threshold. It is the analysis of these two factors that is central to an EWIS assessment for an aging aircraft.

Suppose only the probability of failure were examined for the wiring on the aircraft. What would this accomplish? There would certainly be benefits from this:

  • The worst harnesses would be identified for replacement.
  • Good harnesses would be identified thus reducing the overall cost of harness replacement
  • Projections could be made as to future failure probabilities

While these are all good metrics to be used to assist in making determinations for the life extension program, there are weaknesses of only examining the probability of failure. Some of these shortcomings include:

  • The impact of failure is not identified: Harnesses which contain mission critical system wires may not be identified (the acceptable probability of failure on these is much lower).
  • Harnesses that carry a large number of power wires may cause more damage in an arcing event. The nearby systems are also likely to be damaged are not identified.
  • Collocation of systems is not identified.

In some cases, it may be tempting to focus on a single aspect of the risk assessment, namely, the probability of failure. If all of the poor quality harnesses are replaced, then will not the aircraft be in like-new condition? True, but there are disadvantages to this:

  • It may be cost prohibitive to replace so may harnesses.
  • The down time is too long.
  • Maintenance efforts cannot be directed to monitor the most critical systems

Severity of Failure

As identified earlier, determining the severity of failure is important to the overall EWIS risk assessment process. In particular, it seeks to determine where failures can have the greatest impact on the aircraft airworthiness. In determining the severity failure, it is necessary to both consider the functional impacts to the aircraft (which systems are affected by a failure) and the physical impacts (what may be damaged may be caused from a wire failure).

Alone, the severity of failure does provide valuable insights into the aircraft:

  • System collocation
  • Identifying areas for directed maintenance
  • Identifying areas for routine visual inspections

While these are beneficial, it should be clear why this needs to be paired with the assessment of the wire condition. These two factors when combined provide a clear, cohesive picture of the current aircraft EWIS health, directed to focus on what matters most: a fully functional airworthy aircraft that can be maintained in a cost effective manner.

The next article in this series will focus on probability of failure assessments and how they are applied to aging aircraft.

Michael Traskos

Michael Traskos

President, Lectromec

Michael has been involved in wire degradation and failure assessments for more than a decade. He has worked on dozens of projects assessing the reliability and qualification of EWIS components.