USAF ILA Handbook - ACC Practice Center - Defense Acquisition ...
USAF ILA Handbook - ACC Practice Center - Defense Acquisition ...
USAF ILA Handbook - ACC Practice Center - Defense Acquisition ...
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D-11. Systems Engineering (continued)<br />
Evaluation Criteria<br />
2. Failure Reporting, Analysis and Corrective Action System (FRACAS)<br />
Milestone<br />
B C FRP<br />
• A FRACAS is established and failures are analyzed and trended for product X U<br />
support visibility.<br />
• A FRACAS is performed on engineering development models, pre-production X U<br />
units and production units.<br />
3. System Reviews<br />
• System requirements, including supportability, are flowed to subcontractors. X U<br />
• The preliminary design review, including supportability, has been conducted. X<br />
• The critical design review, including supportability, has been conducted. X<br />
• The production readiness review has been performed to include an assessment of X<br />
system supportability requirements.<br />
4. Manufacturing Planning<br />
• A manufacturing plan has been developed and includes: X U U<br />
o A defect/variation prevention program.<br />
o Manufacturing processes that have defined yield levels and have been<br />
validated.<br />
o Environmental stress screening to precipitate latent, intermittent or<br />
incipient defects or flaws introduced during the manufacturing process.<br />
5. Quality Assurance<br />
• A Deficiency Reporting (DR) Program is established per TO 00-35D-54, <strong>USAF</strong> X U U<br />
Deficiency Reporting and Investigating System, to identify the root cause and<br />
take corrective action to resolve deficiencies identified during DT&E, OT&E<br />
and sustainment.<br />
• Ensure acceptance inspection requirements are identified for items to be<br />
X U<br />
accepted at source.<br />
6. Parts and Materials Selection<br />
• Guidance and/or requirements should be documented in a parts and materials X U U<br />
design guide before the start of design, addressing parts selection, derating and<br />
testability factors. Adherence to the guidelines should be verified at design<br />
reviews.<br />
• Identification of COTS/NDI reliability is required. X U U<br />
• Parts and materials selected are qualified to the worst-case DRMP and detail X<br />
design environments. Uprating or upscreening of parts is not a best practice and<br />
should not be performed.<br />
• Parts derating is required for all electronic/electrical components. Electrical<br />
parameters of parts are characterized to requirements derived from the DRMP to<br />
ensure that all selected parts are reliable for the proposed application.<br />
X<br />
Version 1: Jan 2006 75<br />
Air Force Independent Logistics Assessment <strong>Handbook</strong>