EIA 933 : 2015
Current
The latest, up-to-date edition.
REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN
Hardcopy , PDF
English
01-01-2015
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
|
| IEEE 1332-2012 | IEEE Standard Reliability Program for the Development and Production of Electronic Products |
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| SAE ARP6379 | Processes for Application-Specific Qualification of Electrical, Electronic, and Electromechanical Parts and Sub-Assemblies for Use in Aerospace, Defense, and High Performance Systems |
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| SAE AS5553B | Counterfeit Electrical, Electronic, and Electromechanical (EEE) Parts; Avoidance, Detection, Mitigation, and Disposition |
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| SAE ARP4754A | 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 |
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| MIL-HDBK-338 Revision B:1998 | ELECTRONIC RELIABILITY DESIGN HANDBOOK |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING 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 ARP5890A | 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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