MIL-STD-1796A(USAF)
TABLE I. Summary of AVIP requirements - Continued.
5.1 Phase 1 Design information Proposal and contract |
5.2 Phase 2 Prelim planning & design Complete by PDR |
5.3 Phase 3 Design & manufacturing development Complete by CDR |
5.4 Phase 4 Verification & production Complete by delivery |
5.5 Phase 5 Force management/ operational |
|
Analysis |
Analytical basis and approach to analyses established |
FMECA on critical avionics items conducted Thermal, vibration, shock, etc, effects on equipment analyzed |
Analysis of each item (e.g., circuit board) for response to environment completed Design analyzed for compliance to Rel, Maint & Diagnostics requirements Avionics impacts on FMECA analyzed |
Rel, Maint & diagnostics analyses updated Durability analyses updated to reflect final design and results of test |
|
Tests and demonstrations |
Environmental verification (qual) requirements established |
Component development tests conducted for new or high risk items Development tests to characterize basic design conducted |
Environmental and Durability development test and analysis complete Risk Reduction tests complete Environmental and acceptance tests defined |
Environmental and durability verifications complete SIL tests related to integrity (e.g., FMET) complete Acceptance test performed/valida ted Diagnostic tests validated |
|
Life management |
Maintainability and Diagnostics requirements established Strategy to address component obsolescence & component performance improvements proposed |
Support concept defined Maintenance & Diagnostics requirements refined |
Anti-tamper protection methods impact on integrity defined |
Adequacy of source of repair and level of repair established Go/NoGo criteria for fielded system established and validated Integrity issues addressed in TO's Special maintenance for Anti-tamper defined |
Life limited items tracked Deficiency tracking system implemented Repair processes controlled Bad actor program implemented |
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