SAE ARP 5890 : 2011
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GUIDELINES FOR PREPARING RELIABILITY ASSESSMENT PLANS FOR ELECTRONIC ENGINE CONTROLS
29-11-2018
01-01-2011
1. SCOPE
2. REFERENCES
3. RELIABILITY ASSESSMENT PLAN FOR ELECTRONIC
ENGINE CONTROLS
4. NOTES
APPENDIX A - SIMILARITY ANALYSIS EXAMPLES
APPENDIX B - DURABILITY ANALYSIS
APPENDIX C - OTHER SOURCES OF INFORMATION
Specifies guidelines for a Reliability Assessment Plan (herein also called the Plan), in which Electronic Engine Control manufacturers document their controlled, repeatable processes for assessing reliability of their products.
| Committee |
E-36
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| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy |
| IEC TS 62239-2:2017 | Process management for avionics - Management plan - Part 2: Preparation and maintenance of an electronic COTS assembly management plan |
| 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 |
| EN 62308 : 2006 | EQUIPMENT RELIABILITY - RELIABILITY ASSESSMENT METHODS |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| BS EN 62308:2006 | Equipment reliability. Reliability assessment methods |
| EIA STD 4899 : 2017-05 | REQUIREMENTS FOR AN ELECTRONIC COMPONENTS MANAGEMENT PLAN |
| EIA 933 : 2015 | REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN |
| PD IEC/TS 62239-2:2017 | Process management for avionics. Management plan Preparation and maintenance of an electronic COTS assembly management plan |
| 04/30101075 DC : DRAFT JUN 2004 | |
| I.S. EN 62308:2006 | EQUIPMENT RELIABILITY - RELIABILITY ASSESSMENT METHODS |
| IEC 62308:2006 | Equipment reliability - Reliability assessment methods |
| IEC TS 62239-2:2017 | Process management for avionics - Management plan - Part 2: Preparation and maintenance of an electronic COTS assembly management plan |
| 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 |
| GEIA HB 0005-2 : 2007 | TECHNICAL GUIDELINES FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER AND FINISHES |
| MIL-HDBK-87244 Base Document:1995 | AVIONICS/ELECTRONICS INTEGRITY |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| IEEE 1413 : 2010 | FRAMEWORK FOR RELIABILITY PREDICTION OF HARDWARE |
| IEC TS 62239-1:2015 | Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan |
| SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| VITA 51.1 : 2008 (R2013) | RELIABILITY PREDICTION MIL-HDBK-217 SUBSIDIARY SPECIFICATION |
| GEIA STD 0005-2 : 2012 | MITIGATING THE EFFECTS OF TIN WHISKERS IN AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS |
| SAE ARP 6338 : 2015 | PROCESS FOR ASSESSMENT AND MITIGATION OF EARLY WEAROUT OF LIFE-LIMITED MICROCIRCUITS |
| MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
| IEC 61709:2017 | Electric components - Reliability - Reference conditions for failure rates and stress models for conversion |
| GEIA STD 0005-1 : 2012 | PERFORMANCE STANDARD FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER |
| UTEC 80 811 : 2011 | RELIABILITY METHODOLOGY FOR ELECTRONIC SYSTEMS - FIDES GUIDE 2009 ISSUE A |
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