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Validation Effectiveness of Develop Maintainability Allocation on Aircraft Mechanical Components

机译:在飞机机械部件上开发可维护性分配的验证效力

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Maintainability Allocation is a process to identify the allowable maximum task time for each individual component. Consequently, this provides clear pictures to the designers to design and identify potential design improvement within allowable maintenance allocation time limits. During the design process elements such as missteps or misapplications most commonly occur. Here, the authors propose having the maximum target for each individual maintainability component. The main objective of this paper is to present the validation process of developed Maintainability Allocation to potentially eliminate previous problems. The process of validation begins with analysed all the data collected from Service Difficulty Reports (SDR) for selected aircraft. This is to understand the problems from existing aircraft before a new design is proposed through the process of Maintainability Allocation prediction. The validation processes have discovered the importance of utilising historical information such as feedback information. The second area is looking at the element of quantifying the data collected from aircraft feedback information which contains various types of information that could be used for future improvement. Validation process shows that feedback information has helped to identify the critical and sensitive components that need more attention for further improvement. The study shows that the aircraft maintenance related feedback information systems analyses were very useful for deciding maintainability effectiveness; these include planning, organising maintenance and design improvement. There is no doubt that feedback information has the ability to contribute an important role in design activities. The results also show that maintainability is an important measure that can be used as a guideline for managing efforts made for the improvement of aircraft components.
机译:可维护性分配是一个识别每个单个组件的允许最大任务时间的过程。因此,这为设计人员提供了清晰的图片来设计和识别允许维护分配时限内的潜在设计改进。在设计过程中,诸如MISSteps或最常见的误用。在这里,作者提出了每个个体可维护性组分的最大目标。本文的主要目的是介绍开发可维护性分配的验证过程,以潜在地消除以前的问题。验证过程开始于分析了从服务难度报告(SDR)所收集的所有数据进行选定的飞机。这是通过可维护性分配预测的过程提出新设计之前了解现有飞机的问题。验证过程已发现利用诸如反馈信息的历史信息的重要性。第二个区域正在寻找量化从飞机反馈信息中收集的数据的元素,该信息包含可用于将来改进的各种类型的信息。验证过程显示反馈信息有助于识别需要更多关注以进一步改进的关键和敏感组件。该研究表明,飞机维护相关反馈信息系统分析对于决定可维护性有效性非常有用;这些包括规划,组织维护和设计改进。毫无疑问,反馈信息有能力在设计活动中贡献重要作用。结果还表明,可维护性是一种重要的措施,可作为管理为改进飞机组件的努力的指导。

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