EIA 933 : 2015
Current
The latest, up-to-date edition.
REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN
Hardcopy , PDF
English
01-01-2015
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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 ARP 6379 : 2016 | PROCESSES FOR APPLICATION-SPECIFIC QUALIFICATION OF ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL PARTS AND SUB-ASSEMBLIES FOR USE IN AEROSPACE, DEFENSE, AND HIGH PERFORMANCE SYSTEMS |
| EIA STD 4899 : 2017-05 | REQUIREMENTS FOR AN ELECTRONIC COMPONENTS MANAGEMENT PLAN |
| SAE AS 5553B : 2016 | COUNTERFEIT ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL (EEE) PARTS; AVOIDANCE, DETECTION, MITIGATION, AND DISPOSITION |
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| 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 |
| IEC 62396-5:2014 | Process management for avionics - Atmospheric radiation effects - Part 5: Assessment of thermal neutron fluxes and single event effects in avionics systems |
| 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 |
| SAE ARP 5890 : 2011 | GUIDELINES FOR PREPARING RELIABILITY ASSESSMENT PLANS FOR ELECTRONIC ENGINE CONTROLS |
| 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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