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

Overlooked but critical: Impact of storage on aircraft EWIS components

Management

Aircraft maintenance engineers do not pay much attention to the impact of storage on electrical components. This article discusses several aspects of storage in the general category of the electrical wire interconnection system (EWIS), or aircraft EWIS components. We will examine the stowage of connectors, waveguides, harnesses, as well as capping and stowage of terminal wires in Severe Weather and Moisture Prone (SWAMP) areas.

Conductor Stowage Background

Stowage of conductors is dependent on the aircraft’s operational requirements. There are four categories that determine the aircraft’s components’ state:

  1. Operational – The conductors are ready for flight status.
  2. Non-operational – The conductors are not ready for flight status (they will require major maintenance either scheduled or unscheduled).
  3. Long term – The system’s components are available for use during specific mission configurations, but are not regularly used on a daily basis for longer than a month.
  4. Short term – The system’s components are removed for maintenance for less than a month.

These categories are combined to make statuses such as “operational-long term” and “non-operational-short term” to describe the state of the aircraft and its components. Each of these statuses has its own set of instructions for stowing and cleaning the connectors. (See Lectromec’s EWIS SLEP: Five Days in the Desert article for more information on the boneyard).

Connector Stowage

For operational-long term and operational-short term aircraft connectors, military standard metal covers are preferred and should be used over plastic covers. However, if the standard metal covers are not available, then the end of the connector can be wrapped in pressure sensitive tape for electrical connectors and secured with lacing tape. Before sealing the connector, it should be cleaned.

Aircraft EWIS Components
The More Electric Aircraft design concept will require additional attention to EWIS certification. Find out more on how to address your EWIS risk assessment needs.

As for the non-operational-long or short term aircraft, the requirements are the same as those for the operational-short term aircraft.

SWAMP Areas

Wires and connectors located in SWAMP areas are required to have extra layers of protection. During the cleaning the connector prior to starting the procedure, a Corrosion Prevention Compound (CPC) must be applied to the conductor. Failure to apply a CPC prior to connector stowage and re-application at required intervals will result in corrosion damage to the connector. Note that this is for storage applications and should not be used for in-service conditions (see Lectromec’s Corrosion Prevention Compounds (CPCs) and EWIS).

When in SWAMP areas, wrap the connector end with stretch seal tape then apply a heat-shrink end cap on top of it. In order to prevent moisture accumulation in the conductor during stowage, secure the connector vertically using a clamp or tying and lacing tape.

WAVEGUIDES

Waveguides are important yet incredibly fragile devices. Waveguides must be kept extremely clean and dry—even the slightest amount of moisture or smallest speck of dirt can reduce their effectiveness in transmitting proper wave forms. Since they are so fragile, only pressure sensitive tape should be used on the waveguides.

After ensuring that it is clean and dry, simply tape over the end with the tape overlapping to ensure all openings are covered. Depending on the temperature and vibration application of the waveguide, different lacing and tying tape should be considered to secure the device.

CAP and Stow

There are three ways to stow and cap terminals and wires based on the environmental applicability and the temperature of the area.

  1. Heat-shrinkable end caps – Environmental applications up to 150°C
  2. Stub splices M81824/13 – Same as above
  3. Pre-insulated end caps that be crimped – Non-environmental applications up to 105°C

After the ends are secure, coil the wire into a loose coil and secure it.

Conclusion

It is incredibly crucial to pay attention to detail when dealing with a high risk area like a SWAMP area or high risk devices like wave guides. Failing to do so may reduce the effectiveness of the wire system and may require more maintenance. Thus, it is important to store and care for wires properly so that they are not exposed to additional degradation. Following these steps will ensure longevity of the aircraft and make it safer for use.

Emma Schwoerer

Emma Schwoerer

Emma is a full time engineering student at The George Washington University. She works at Lectromec as a junior engineer on a variety of projects including wire testing, aged platform assessment, and arc damage modeling.