MIL-STD-1796 Revision A:2011
Current
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AVIONICS INTEGRITY PROGRAM (AVIP)
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
Categorizes the design tasks needed to achieve high reliability, long life, safe operation and supportability of aviation electronics in operational environments.
| Committee |
FSC 15GP
|
| DevelopmentNote |
Supersedes MIL HDBK 87244. (11/2011) A NOTICE 1 - Notice of Validation. (10/2016)
|
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-HDBK-338 Revision B:1998 | ELECTRONIC RELIABILITY DESIGN HANDBOOK |
| GEIA HB 0005-1 : 2006 | PROGRAM MANAGEMENT/SYSTEMS ENGINEERING GUIDELINES FOR MANAGING THE TRANSITION TO LEAD-FREE ELECTRONICS |
| GEIA STD 0005-1 : 2012 | PERFORMANCE STANDARD FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER |
| MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
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