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EMBRAER Perspective on the Challenges for the Introduction of Scheduled SHM (S-SHM) applications into Commercial Aviation Maintenance Programs

机译:EMBRAER展望将预定的SHM(S-SHM)应用程序引入商业航空维护计划所面临的挑战

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This paper presents an overview of the challenges an original equipment manufacturer (OEM) such EMBRAER may face to introduce scheduled structural health monitoring (S-SHM) applications in the maintenance programs of its commercial aviation aircraft models. S-SHM solutions have the potential to reduce aircraft operators direct maintenance costs and fleet downtime while keeping aircraft airworthiness at a minimum maintenance downtime and costs. As part of new approach in terms of scheduled maintenance practices, the replacement or complementation of traditional structural inspections tasks by new maintenance procedures taking credit of SHM technologies must be done in ways that meet the expectations and requirements of Regulatory Authorities, OEMs and airlines maintenance and engineering departments related to topics such as: safety, continued airworthiness, cost/benefits ratio, S-SHM systems' built-in redundancies and reliability to support higher fleet availability, as well as necessary mechanics qualification. Besides the efforts for validation, verification, qualification and certification of such systems to deliver the expected effectiveness levels to verify structural integrity and withstanding the operational conditions to which it will be exposed, an OEM intended to offer their customers with the benefits of S-SHM solutions will be required initially to revise its policy and procedures handbooks (PPH) to adopt the new S-SHM Air Transport Association's Maintenance Steering Group 3 (MSG-3) Methodology guidelines. This will alter in different ways the current Maintenance Review Board processes conducted by each OEM to develop and revise the minimum scheduled maintenance program for a given commercial aircraft type certificate. The contents of the Maintenance Review Board Reports (MRB) will need to be revised in order to clearly indicate the scope and frequencies of each approved S-SHM task, and how they will replace, complement and/or be an alternative means of compliance of the more traditional maintenance tasks types such as general and detailed visual inspections (GVI and DET, respectively). Additionally, the Airplane Maintenance Manuals (AMM) will need to be revised to include specific S-SHM procedures on how to perform the intended inspection, how to proceed when degradation is detected in the monitored structures and how to repair such systems in case of failures.
机译:本文概述了诸如EMBRAER的原始设备制造商(OEM)在其商用航空飞机模型的维护计划中引入计划的结构健康监测(S-SHM)应用程序时可能面临的挑战。 S-SHM解决方案有可能减少飞机运营商的直接维护成本和机队停机时间,同时将飞机适航性保持在最小的停机时间和成本下。作为按计划进行维护的新方法的一部分,必须采用符合SHM技术的新维护程序替换或补充传统的结构检查任务,并且必须满足监管机构,OEM和航空公司维护和维护部门的期望和要求。工程部门涉及的主题包括:安全性,持续适航性,成本/收益比,S-SHM系统的内置冗余和可靠性以支持更高的机队可用性以及必要的机械师资格。除了努力进行此类系统的验证,验证,鉴定和认证,以提供预期的有效性水平以验证结构完整性并承受其所面临的操作条件外,OEM还将为客户提供S-SHM的好处最初将需要解决方案来修订其政策和程序手册(PPH),以采用新的S-SHM航空运输协会的维护指导小组3(MSG-3)方法学指南。这将以不同的方式改变由每个OEM进行的当前维修审查委员会流程,以开发和修改给定商用飞机型号合格证的最低定期维修计划。维护审查委员会报告(MRB)的内容将需要修改,以清楚地表明每个已批准的S-SHM任务的范围和频率,以及它们将如何替代,补充和/或成为替代性的遵守方式。比较传统的维护任务类型,例如常规和详细的外观检查(分别为GVI和DET)。此外,飞机维修手册(AMM)将需要修订,以包括有关如何执行预期检查,在受监视结构中检测到退化时如何进行以及在发生故障时如何维修此类系统的特定S-SHM程序。 。

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