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 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

The process for identifying an EWIS problem on an aircraft often follows these steps:

  • At some point during aircraft operation a system malfunctions and the pilot reports the malfunction.
  • Maintenance starts by replacing the system component. Depending on schedule and criticality, the maintenance action is scheduled. Often, the first action to be taken is the replacement of the Line-Replaceable Unit (LRU).
  • With the LRU replaced, a system check is done and the aircraft is released.
  • The LRU is sent for inspection/repair.
  • The LRU is inspected and marked as “No Fault Found” (NFF).
  • The “defective” device is returned to inventory.
  • The EWIS is examined and the original problem is detected.

There is a reason for this type of maintenance: it is easier to replace a LRU than to track down an intermittent EWIS problem. From a financial perspective, this cycle requires a large inventory of LRUs to support this type of maintenance action.

EWIS failure trends

Lectromec recently performed a review of the FAA’s SDR database to determine how close the actual EWIS failure numbers were to those that were reported. One of the problems often found when searching for reported EWIS failures is that the failures are often hidden within the failure reporting of other systems. This example was reported as a flap control system problem:

“FLAP UP LIMIT SWITCH HAS SEVERAL REPORTED OCCURRENCES INVOLVING ARCING AND SMOKE GENERATING BEHIND THE MASTER CAUTION PANEL. THE SWITCH WAS SAID TO BE ARCING AND SPARKING WHICH LED TO A BURNED SWITCH CREATING SEVERAL WIRES TO BE BURNED AND SINGED TOGETHER.” (Reference SDR Control number: 2014FA0000419)

Although this was an EWIS problem, it was not marked in the proper category. For those that are looking to glean information from their maintenance database, it is likely that this key information is being missed. Those looking for a process for pulling data from a maintenance database, Task #2 in the USAF’s EWIS SLEP handbook, MIL-HDBK-525, provides an effective and efficient way of tackling this. The same process can be applied to commercial maintenance systems. Ideally, the maintainers are trained to place each component into the right code. However, if you review the scenario described above, there can be flexibility in this process.

The review of the 2014 SDR data, found that maintainers are doing an excellent job in filing EWIS problems. A manual review of over 800 records found that roughly 8% of EWIS problems are attributed to the wrong system (e.g. flight control system versus flight control system wiring). The most common reason for this misattribution appears to be that the system was identified to have suffered a functional problem when the actual source of the problem was a physical one that was related to wiring issues.

Overall EWIS reliability

A review of the last four years of EWIS failure data reported through FAA’s SDR database shows some promising trends. Five component types were examined during this research: wires, wire harnesses, splices, cables, and connectors. Four out of the five of the categories (wires, wire harnesses, cables, and connectors) examined from the SDR database showed a decline in failure count. Note that these are raw results and have not been individually examined.

The most dramatic decline over the four-year period has been with cables. From 2011, which saw 211 ‘cable’ service difficulties to only 144 in 2014, it is a 46% drop. Taking all five of the categories together, 2014 has seen a 30% decline in reported EWIS problems. This is truly encouraging from an aircraft reliability standpoint.

EWIS failure trends

As a check to see if this decline in the number of EWIS failure incidents was due to a general decline in total system incidents reported to the SDR or a trend particularly associated with wires, several weeks were examined in 2011 and 2014. The evaluation found that, on average, there were 15% more incidents reported through the FAA SDR system from 2011 to 2014. This makes it even more impressive given that the number of reported wire incidents have declined.

Analysis

Potential reasons for this overall decline:

  • The implementation of the FAA’s EZAP (Enhanced Zonal Awareness Procedure) caused a spike of EWIS related reports, where inspections found latent EWIS failures. The latest results for 2014 may be what should be expected annually.
  • It has been seven years since the FAA released the new EWIS regulations and seventeen years since the last major incident attributed to EWIS. Perhaps maintainers are becoming complacent with examining/reporting EWIS problems.

If the results are to be believed, the industry is going the right way in design, manufacturing, and maintaining its EWIS.

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. In September 2014, Michael was appointed as an FAA DER with a delegated authority covering EWIS certification.