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Deja Vu with Overlooked Safety-Critical Item Verification

机译:Deja Vu具有忽视的安全关键项项目验证

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Fifteen years ago, Contractor A performed a Failure Mode, Effects, and Criticality (FMECA) on an unnamed defense satellite system and identified several System Safety Criticality 1 and 2 single point failure modes (SPFMs). One of the ground rules of this FMECA was to accept all SPFMs with a probability of occurrence that is less than 0.001, i.e. one in one-thousand. After the program was into its fifth year, a Government auditor asked the contractor how was the reliability of each SPFM verified. The contractor could not answer that question because no Critical Item Control Plan had been included in the Quality Assurance section of the Statement of Work (SOW). Now fast forward to the present time. Contractor B performed a FMECA on an unnamed defense satellite system and identified several System Safety Criticality 1 and 2 structural failure modes. One of the ground rules of this FMECA was to accept all structural failure modes that meet the design-to safety margin requirements. However, when a Government auditor reviewed the contractor’s Hazard Tracking System, none of the hazard reports included evidence that the durability of safety-critical structural items had been verified. These two examples of overlooked safety-critical item verification occurred fifteen years apart, but they have the same root cause – a lack of understanding of the essential interactions between FMECA and Hazard Analysis. This paper compares three different FMECA standards to determine how their results would differ if applied in the same high-criticality mission US defense system acquisition program. In this study, the selection of applicable FMECA activities is based on the typical tailoring of the SMC-S-013, Section 5.2.2 (ref. 1). SMC-S-013 is one of the standards on the Space and Missile Systems Center (SMC) Mandatory Documents List for SMC Acquisitions, which is required on every SMC satellite acquisition contract. The second FMECA standard included in this study is the AIAA Standard S-102.2.4-2015, Capability-based Product Failure Modes, Effects, and Criticality Analysis (FMECA) Requirements (ref. 2). S-102.2.4-2015 is a commercial standard that defines a structured process for tailoring the contractor’s FMECA process so the overall effort is commensurate with the safety-criticality of the system. Finally, the third FMECA standard included in this study is MIL-STD-1543B, Task 204 and Task 208 (ref. 3), which was used in SMC Acquisitions from 1988 until the Acquisition Reform era started in 1998.
机译:十五年前,承包商A在未命名的防御卫星系统上执行了故障模式,效果和临界性(FMECA),并确定了几种系统安全临界模式1和2单点故障模式(SPFMS)。该FMECA的一个基本规则是接受所有SPFM,其出现概率小于0.001,即一千个。该计划进入第五年后,政府审核员要求承包商如何验证每个SPFM的可靠性。承包商无法回答该问题,因为没有关键的项目控制计划已被列入工作表的质量保证部分(播种)。现在快进到现在的时间。承包商B在未命名的防御卫星系统上执行了FMECA,并确定了几种系统安全临界方法1和2结构故障模式。此FMECA的一个基本规则是接受所有结构故障模式,满足设计 - 安全保证金要求。但是,当政府审核员审查承包商的危险跟踪系统时,危险报告都没有证据表明安全关键结构项目的耐用性已经过核实。这两个忽视的安全关键项目验证的例子分开了十五年,但它们具有相同的根本原因 - 缺乏对FMECA和危险分析之间基本相互作用的理解。本文比较了三种不同的FMECA标准,以确定当应用在同一高分辨率任务美国国防系统采集计划中的结果如何不同。在本研究中,选择适用的FMECA活动是基于SMC-S-013的典型剪裁,第5.2.2节(参考文献1)。 SMC-S-013是SMC收购的空间和导弹系统中心(SMC)强制性文件列表中的标准之一,这是每个SMC卫星收购合同所必需的。本研究中包含的第二个FMECA标准是AIAA标准S-102.2.4-2015,基于能力的产品故障模式,效果和临界分析(FMECA)要求(参考文献2)。 S-102.2.4-2015是一种商业标准,其定义了用于定制承包商的FMECA过程的结构化过程,因此整体努力与系统的安全关键性相称。最后,本研究中包含的第三个FMECA标准是MIL-STD-1543B,任务204和任务208(参考文献3),该任务204和任务208(参考文献3)是在1988年的SMC采集中使用,直到收购改革时代于1998年开始。

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