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The FAA is adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Model 402C and 414A airplanes. This AD requires repetitively inspecting the engine mount beams for cracks and contacting Cessna for FAA-approved corrective action if cracks are found. This AD also requires sending an inspection report to the FAA and to Cessna. This AD was prompted by reports of cracks found across the engine mount beams. The FAA received reports of cracks found on the engine mount beams of certain Cessna Aircraft Company (Cessna) Model 402C airplanes. The cracks found run across the beam and extend beyond the doubler located under the aft engine mount and aft of the forward engine mount. Investigation revealed that the cause of the cracks is fatigue. The engine beam mounts of the Cessna Model 402C airplanes are the same type design as that of the Cessna Model 414A airplanes. This condition, if not detected and corrected, could result in failure of an engine mount beam and could lead to engine separation with consequent loss of power and loss of control. The FAA is issuing this AD to correct the unsafe condition on these products. gov by searching for and locating Docket No. FAA-2015-0839, or you may see ADDRESSES at the same Web site for other ways to access this service information. DATES: This AD is effective April 24, 2015.
机译:美国联邦航空局(FAA)对某些塞斯纳飞机公司(Cessna)的402C和414A型飞机采用了新的适航性指令(AD)。该广告要求反复检查发动机悬臂梁是否存在裂纹,如果发现裂纹,请联系塞斯纳以获得FAA批准的纠正措施。本指令还要求向FAA和Cessna发送检查报告。该AD的报告是在发动机支架横梁上发现了裂纹的报道。美国联邦航空局收到了某些塞斯纳飞机公司(Cessna)402C型飞机的发动机支架横梁上发现裂纹的报告。发现的裂纹横穿横梁,并延伸到位于发动机后部支架下方和发动机前部支架后部的加倍器。调查显示,裂纹的原因是疲劳。塞斯纳402C型飞机的发动机横梁安装座与塞斯纳414A型飞机相同。如果没有检测到并纠正这种情况,可能会导致发动机安装梁出现故障,并可能导致发动机分离,从而导致功率损失和控制失控。美国联邦航空局(FAA)签发了该指令以纠正这些产品上的不安全状况。在gov上搜索并找到编号为FAA-2015-0839的文件,或者您可能会在同一网站上看到“地址”,以了解其他访问此服务信息的方式。日期:本广告于2015年4月24日生效。

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    《Light Plane Maintenance》 |2015年第8期|3-3|共1页
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  • 入库时间 2022-08-18 01:57:28

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