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USAF ILA Handbook - ACC Practice Center - Defense Acquisition ...

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B. Relationship between Reliability, Availability<br />

and Maintainability, and Supportability<br />

(RAMS)<br />

B.1 Sustainment quality is driven by performance in RAMS. The PM should establish RAMS<br />

objectives early in the acquisition cycle (certain logistics RAMS criteria should be inserted as<br />

Key Performance Parameters (KPPs) in order to deliver sound weapons systems from a<br />

sustainment perspective) and address them as a design parameter throughout the acquisition<br />

process. The PM develops RAMS system support requirements based on the Initial Capabilities<br />

Document (ICD) or Capability Development Document (CDD) and TOC considerations and<br />

states them in quantifiable, operational terms measurable during Test and Evaluation (T&E).<br />

RAMS system requirements impact total life-cycle cost and all sustainment elements. These<br />

performance requirements are derived from and support the user’s system readiness objectives<br />

and are validated through the RAMS rationale process identified in AFI 10-602, Determining<br />

Mission Capability and Supportability Requirements.<br />

B.2 Application of RAMS and producibility activities during design, development, and<br />

sustainment is guided by a concise understanding of the concept of operations, mission profiles<br />

(functional and environmental), and desired capabilities. It is important to understand rationale<br />

behind RAMS and producibility activities and performance priorities. In turn, this rationale<br />

paves the way for decisions about necessary trade studies among system performance,<br />

availability, and system cost, with impact on the cost effectiveness of system operation,<br />

maintenance, and logistics support. The PM should use Modeling and Simulation (M&S) to<br />

demonstrate RAMS requirements, wherever appropriate to increase confidence in meeting<br />

RAMS requirements, reduce design risk, and possibly reduce overall program, including test,<br />

costs.<br />

B.3 The components of system Availability are a function of Reliability, Maintainability and<br />

Supportability (RMS) and Producibility. There are a number of useful references for these terms<br />

to include, the OSD guide Designing and Assessing Supportability in DoD Weapon Systems: A<br />

Guide to Increased Reliability and Reduced Logistics Footprint; AFI 63-107, Integrated Product<br />

Support Planning and Assessment; AFI 10-602, Determining Mission Capability and<br />

Supportability Requirements; and, DoD 3235.1-H, Department of <strong>Defense</strong> Test and Evaluation<br />

of System Reliability Availability and Maintainability -- A Primer. However, for the purposes of<br />

this handbook, the following definitions and information in Table B-1 are provided to illustrate<br />

the inter-relationship between these components and sustainment for consideration in conducting<br />

<strong>ILA</strong>s.<br />

• Reliability: The ability of a system to perform as designed in an operational<br />

environment over time without failure. Reliability requirements address mission<br />

reliability and logistics reliability. The former addresses the probability of carrying<br />

out a mission without a mission-critical failure. The latter is the probability of a<br />

Version 1: Jan 2006 25<br />

Air Force Independent Logistics Assessment <strong>Handbook</strong>

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