• Shopping Cart
    There are no items in your cart

MIL-HDBK-525 Base Document:2013

NA

NA

Status of Standard is Unknown

Electrical Wiring Interconnect System (EWIS) Integrity Program

Available format(s)

PDF

Language(s)

English

Published date

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

US$20.00
Excluding Tax where applicable

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.