
MIL-HDBK-525 Base Document:2013
NA
Status of Standard is Unknown

Electrical Wiring Interconnect System (EWIS) Integrity Program
English
07-25-2013
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. CORE PROCESS TASKS
5. MANAGEMENT METHODS
6. FAILURE MODES AND LESSONS LEARNED
7. DETAILED REQUIREMENTS DEVELOPMENT
8. NOTES
APPENDIX A: ELECTRICAL WIRING INTERCONNECTION
SYSTEMS (EWIS) MINIMAL INITIAL TRAINING
PROGRAM CONTENT
APPENDIX B: EWIS TASK ONE - EWIS DOCUMENTATION
APPENDIX C: EWIS TASK TWO - DATA ANALYSIS
APPENDIX D: EWIS TASK THREE - PHYSICAL AIRCRAFT
INSPECTION
APPENDIX E: EWIS TASK FOUR - COMPONENT ASSESSMENT
APPENDIX F: EWIS TASK FIVE - RISK ASSESSMENT
APPENDIX G: EWIS TASK SIX - ACTION PLAN
APPENDIX H: EWIS TASK SEVEN - ITERATIVE EWIS
ASSESSMENT
Specifies weapons systems program offices a systematic process to assess an aircraft Electrical Wiring Interconnect System (EWIS) for overall condition, service life extension, and continued airworthiness.
DocumentType |
Standard
|
Pages |
113
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
NA
|
This handbook provides weapons systems program offices a systematic process that includes a series of core tasks used to assess an aircraft Electrical Wiring Interconnect System (EWIS) for overall condition, service life extension, and continued airworthiness. It aligns with the Mechanical Equipment and Subsystems Integrity Program (MECSIP) (see MIL-STD-1798) and makes extensive use of lessons learned from EWIS-related military, industry, and Federal Aviation Administration (FAA) Advisory Circulars (ACs) concerned with maintaining aircraft airworthiness. It contains a framework to achieve and maintain the physical and functional integrity of the EWIS. This process should be tailored to meet specific platform, program office, system and/or subsystem requirements or constraints.
The process and core tasks identified should also be tailored relative to platform status: whether in design, newly fielded, or based on years in sustainment. A program’s use of this process should provide the information necessary to initiate the appropriate trades relative to the cost of modification or integrity initiatives versus required performance, maintenance and mission impact, total operating cost, and aircraft availability. This handbook is for guidance only and cannot be cited as a requirement.
MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
FAA AC 25-16 : 0 | ELECTRICAL FAULT AND FIRE PREVENTION AND PROTECTION |
MIL R 5757 : K | RELAYS, ELECTROMAGNETIC, GENERAL SPECIFICATION FOR |
MIL-DTL-81381 Revision C:2005 | WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
FAA AC 25-26 : 2007 | DEVELOPMENT OF STANDARD WIRING PRACTICES DOCUMENTATION |
NEMA WC 27500 : 2015 | STANDARD FOR AEROSPACE AND INDUSTRIAL ELECTRICAL CABLE |
SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
FAA AC 120-102 : 2012 | INCORPORATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTO AN OPERATOR'S MAINTENANCE PROGRAM |
MIL-STD-882 Revision E:2012 | System Safety |
MIL-DTL-3950 Revision K:2016 | Switches, Toggle, Environmentally Sealed, General Specification for |
MIL DTL 17 : J | CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR |
MIL-HDBK-522 Revision A:2016 | GUIDELINES FOR INSPECTION OF AIRCRAFT ELECTRICAL WIRING INTERCONNECT SYSTEMS |
FAA AC 25-27 : 2010 | DEVELOPMENT OF TRANSPORT CATEGORY AIRPLANE ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS USING AN ENHANCED ZONAL ANALYSIS PROCEDURE |
MIL STD 1678 : NOTICE 1 | FIBER OPTICS TEST METHODS AND INSTRUMENTATION |
FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
FAA AC 43.13-1 : 0 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR |
MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
SAE ARP 4404 : 2013 | AIRCRAFT ELECTRICAL INSTALLATIONS |
FAA AC 120-97 : 2012 | INCORPORATION OF FUEL TANK SYSTEM INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTO OPERATOR MAINTENANCE OR INSPECTION PROGRAMS |
MIL L 87177 : A | LUBRICANT, CORROSION PREVENTIVE COMPOUND, WATER DISPLACING, SYNTHETIC |
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