EIA 933 : 2015
Current
The latest, up-to-date edition.
REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN
Hardcopy , PDF
English
01-01-2015
FOREWORD
1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. PLAN ADMINISTRATION
5. PLAN TERMS, DEFINITIONS, ABBREVIATIONS,
INITIALS, AND ACRONYMS
6. NOTES
APPENDIX A - COTS ASSEMBLY INTEGRATION REPORT
APPENDIX B - MITIGATION METHODS
APPENDIX C - COMPLIANCE MATRIX
Pertains to the development of Plans for integrating and managing COTS assemblies in electronic equipment and Systems for the commercial, military, and space markets; as well as other ADHP markets that wish to use this document.
Committee |
APMC
|
DocumentType |
Standard
|
Pages |
16
|
PublisherName |
Government Electronics & Information Technology Association
|
Status |
Current
|
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SAE AS 5553B : 2016 | COUNTERFEIT ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL (EEE) PARTS; AVOIDANCE, DETECTION, MITIGATION, AND DISPOSITION |
SAE AS 6174 : 2014 | COUNTERFEIT MATERIEL - ASSURING ACQUISITION OF AUTHENTIC AND CONFORMING MATERIEL |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
VITA 51.2 : 2016 | PHYSICS OF FAILURE RELIABILITY PREDICTIONS |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
IEC TR 62240-1:2013 | Process management for avionics - Electronic components capability in operation - Part 1: Temperature uprating |
SAE AS 9100D : 2016 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS |
IEC TS 62239-1:2015 | Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan |
MIL-HDBK-338 Revision B:1998 | ELECTRONIC RELIABILITY DESIGN HANDBOOK |
SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
IEC 62396-4:2013 | Process management for avionics - Atmospheric radiation effects - Part 4: Design of high voltage aircraft electronics managing potential single event effects |
MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
MIL-STD-882 Revision E:2012 | System Safety |
GEIA STD 0016 : 2012 | PREPARING A DMSMS MANAGEMENT PLAN |
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IEC 62396-3:2013 | Process management for avionics - Atmospheric radiation effects - Part 3: System design optimization to accommodate the single event effects (SEE) of atmospheric radiation |
GEIA STD 0010 : 2008 | BEST PRACTICES FOR SYSTEM SAFETY PROGRAM DEVELOPMENT AND EXECUTION |
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GEIA STD 0005-1 : 2012 | PERFORMANCE STANDARD FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER |
EIA STD 4899 : 2017-05 | REQUIREMENTS FOR AN ELECTRONIC COMPONENTS MANAGEMENT PLAN |
MIL-STD-3018 Base Document:2007 | Parts Management (S/S by MIL-STD-11991) |
GEIA STD 0008 : 2011 | DERATING OF ELECTRONIC COMPONENTS |
IEC 62396-1:2016 | Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment |
AS/NZS ISO 9001:2016 | Quality management systems - Requirements |
GEIA EIA649B:2011 | CONFIGURATION MANAGEMENT STANDARD |
GEIA STD 0003 : 2006 | LONG TERM STORAGE OF ELECTRONIC DEVICES |
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