MIL-STD-1796A(USAF)
5.5.2 Design criteria.
No major or specific tasks are identified for this element during this phase.
5.5.3 Characterizing the environment.
No major or specific tasks are identified for this element during this phase.
5.5.4 Characterizing materials and components.
A parts obsolescence program shall be established aimed at identifying parts obsolescence issues as soon as practicable in the program life cycle and identify cost-effective mitigation for each identified part. The program shall establish suitable replacements for obsolete and no- longer-available components needed to maintain the system. Mitigations for lead-free electronics shall be implemented. The contractor and/or parts procuring agency shall define and implement a plan to require all replacement parts to meet the same level of Parts Integrity as the original parts.
5.5.5 Identification and tracking of critical items and critical functions.
Tracking of flight and safety critical items, and the flight and safety critical functions definition and analysis that justifies their status as being flight or safety critical shall be maintained.
5.5.6 Analysis.
No major or specific tasks are identified for this element during this phase.
5.5.7 Tests and demonstrations.
No major or specific tasks are identified for this element during this phase.
5.5.8 Life management.
Any life-limited items shall be tracked. Tracking data is needed to determine when additional spares must be procured, maintenance must be scheduled, etc. The contractor, in conjunction with the operational unit, shall implement a deficiency tracking system to track and respond to deficiencies identified by users of the system. The contractor shall define repair procedures that will maintain the integrity of repaired items. A "bad actor" program to identify and track troublesome fielded items shall be implemented.
6 NOTES
(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.)
6.1 Intended use.
The intended use of AVIP is to identify the design tasks needed to achieve high reliability, long life, safe operation and supportability of aviation electronics in operational environments.
6.2 Acquisition requirements.
Acquisition documents should specify the following:
a. Title, number, and date of this standard.
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