MIL-STD-1796A(USAF)
5.2.7 Tests and demonstrations.
The contractor shall perform component development tests on any new technology or high risk items. The contractor shall conduct development testing to characterize environmental and durability performance of the basic design.
5.2.8 Life management.
The contractor shall establish the adequacy of the required maintenance support concept for each avionics subsystem to maintain system integrity, or propose alternative support concepts with justification. Requirements and preliminary design for maintenance and diagnostics shall be completed, to include expected BIT coverage, false alarm rate, and recording/reporting methods.
5.3 Phase III: Design and manufacturing development (complete by CDR).
Phase III consists of all the tasks that occur between PDR and CDR, including detailed design, manufacturing methods development, final trade studies, analyses, and prototype testing.
5.3.1 Planning and coordination.
The contractor shall document any changes (from earlier phases) to system, subsystem and component integrity requirements in the AIMP and flow them down to subsystems and subcontractors.
5.3.2 Design criteria.
The contractor shall document any changes (from earlier phases) to integrity design criteria and flow the changes down to subsystems and subcontractors. These changes are often the result of tests such as data measured in flight on a prototype vehicle.
5.3.3 Characterizing the environment.
The contractor shall document any changes (from earlier phases) to system level environmental data and subsystem level environmental criteria and flow the changes down to subsystems and subcontractors. These changes are often the result of tests such as data measured in flight on a prototype vehicle.
5.3.4 Characterizing materials and components.
The contractor shall identify materials, parts and devices used in the design that are subject to parts obsolescence and define the method to be used to provide and maintain these parts over the life of the system. The contractor shall identify any usage of lead-free solder and lead-free electronics and shall address associated risks and mitigations.
The contractor shall implement processes that mitigate risks to Parts Integrity and shall identify known and projected risks.
5.3.5 Identification and tracking of critical items and critical functions.
The contractor shall update assessments of the level of criticality of each avionics item. The contractor shall identify and document the performance of any avionics flight or safety critical
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