View Latest Blog Entries
Close
Categories
Testing & Assessment Certification Standard & Regulation Aging Wires & Systems Maintenance & Sustainment Protection & Prevention Management Conference & Report Research Miscellaneous Arcing
Popular Tags
Visual Inspection High Voltage AS50881 MIL-HDBK MIL-HDBK-525 FAR Electromagnetic Interference (EMI) AS4373 Maintenance FAR 25.1707 Wire System Circuit Protection
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 Aluminum arc damage Arc Damage Modeling Tool Arc Fault (AF) Arc Fault Circuit Breaker (AFCB) Arc Resistance 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 B230 ASTM B355 ASTM B470 ASTM D150 ASTM D2671 ASTM D495 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 installation 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 EMI 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 Filter Line Cable 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-F-5372 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 Scrape Abrasion Secondary Harness Protection separation separation distance 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

Blog

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

Commonalities between EWIS and structured risk assessments for life extension programs

One of the criticisms of the EWIS risk assessment field is that it is an inexact science. Another is that no real value is achieved from performing an EWIS risk assessment. This article reviews these criticisms and shows how the EWIS risk assessment process follows accepted industry standards for aircraft assessment. The value of these […] Read more

What to look for with polyimide wire aging

Key to continued aircraft airworthiness is regular visual inspection of the wiring. However, depending on the particular wire insulation installed on the aircraft, the signs of degradation can vary significantly. This article will review what to look for when inspecting polyimide-based wires. The first thing is understanding the wire construction. A standard polyimide wire follows […] Read more

Here are some tips on conductor solderability with wire systems

An important property of a wire conductor is solderability (the ease of soldering the conductor) with wire systems. This property is greatly affected by the type of platting a wire has. Some conductor platting types such as Tin provide for an easy wetting of the conductor and soldering. Other platting types such as Nickel-platted conductors […] Read more

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

Subtopic: Applying Technology to your Fleet – Step #2 The next step after determining the operating conditions within the aircraft is to review the aircraft from the fleet level. This is if you are considering an aircraft wire life extension program. This fleet level assessment examines utilization; basically, it evaluates the fleet’s variability (age, service […] Read more

Results of intrusive inspection on aircraft wire systems

In the Basic concepts of Wire Degradation article, we reviewed the degradation of wire insulation from a laboratory perspective. This article discusses some the findings of the Federal Aviation Administration (FAA) Intrusive Inspection Project fact-finding committee with information on aircraft wire systems. One of the most thorough publicly available sources for understanding the aging of […] Read more

Basic concepts in understanding aircraft wire degradation

Aircraft wire degradation often means a reduction in a wire insulation’s ability to withstand physical, electrical, or chemical strain. Such reductions can lead to insulation breaches, which can result in system interruption. All modern wire insulations are long chains of molecules called polymers. Over time, due to various types of stress, there is wire degradation. […] Read more

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

Subtopic: Applying Technology to your Fleet – Step #1 For purposes of aircraft wire life extension, start with identifying what wires are on the aircraft (see Lectromec’s When should you consider adopting a wire life extension program? Part III article article). It is then necessary to perform a selective sampling of the aircraft. Obviously, the […] Read more