大风和沙尘天气特检的执行

每年春季大风和沙尘天气都会把特检工卡重新撸一遍,主要在于各航司解读。在2019年编写了SOP并获得各航司邮件批复后,这个疑问少了很多,但还是有相关疑问。整合疑问和波音的答复,有以下要点。

1,到底什么情况下需要执行特检 4-4417619877

The subject AMM conditional inspection is subjective. It is the operator’s responsibility to determine if the inspection is necessary when or after the aircraft has been exposed to the subject conditions.

2, 做什么样检查深度 3-3277500197

Boeing recommends that operators use their past experience to guide them in deciding whether or not an inspection is necessary, and the level of the inspections that are necessary. Boeings Extreme Dust/Sand Conditional Inspection criteria is a guide for operators to use when there are reports of sand intrusion and or extreme dust deposits on airplanes due to a wind storm. When operators are using Boeings Extreme Dust/Sand Conditional Inspection procedure and the careful documentation of the outcome can be used to further establish a baseline of Hainan Airlines own inspection.

3,停放的飞机需不需要做 3-4335252938

The dirt environments are areas with extreme dust or sand condition. Please note, that datum AMM Section 05-51-27/201 is written for cases where it was confirmed that the airplane was exposed directly to sand/dust during sand or dust storms. In general we recommend that operators use their past experience to guide them in deciding whether or not an inspection is necessary, and the level of the inspections that are necessary. If the environmental event is sufficient to create the possibility that static ports, pitot tubes, or other locations listed in the conditional extreme dust/sand inspection procedure to be reported to have deposits of fine-grained calcareous silt or clay material, then Boeing recommends performing the conditional inspections. Please note, that subject procedure is also applicable to parked airplanes, which were affected by the sand storm. Intervals provided in the SUBTASK 05-51-27-200-004 are flight hours.

4,钢索发现扬尘后的检查 4-4338594668

Boeing Service Request System We recommend cleaning and relubricating the cables, pulleys and any operating mechanisms affected. HNA may wish to inspect the control cables after approximately 3 months and 6 months to ensure no further damage has occurred to the control cables. Exposure to dust and/or sand will cause contaminants to accumulate on the control cable grease. If not cleaned, this can lead to shortened cable life as wells as higher control forces and sluggish operation of the associated flight control system.

5,经历沙尘后的建议 3-3277500197

Because dust and sand are inert particles, they will not cause harm to exterior fuselage/wing structure/airplane skin. Boeing recommends removing the dust/sand as soon as possible so that it does not get ingested into the engines, the air distribution system, or other internal areas of the aircraft. Dust/sand that blows through the area may also contain contaminants that can lead to premature corrosion of certain areas if those contaminants are not removed promptly.

VSV作动筒安装衬套磨损

自有案例。

运行中常在更换VSV作动器的时候,发现衬套磨损的情况,有几个件是常磨的,特对功用和材料做一解释。

实际上,VSV作动筒和曲柄组件的衬套材料为两种,一种是Inconel718(含铌、钼的沉淀硬化型镍铬铁合金),一种是填充了石墨的聚酰亚胺,其中有石墨的衬套为EIPC的280/290,是专门用于磨损,可以保护270(link),作动筒杆端和曲柄组件孔,这种衬套发料也较多;其它衬套是镍铬铁合金,这种材料具有高的抗拉强度、疲劳强度、抗蠕变强度和断裂强度,尽管强度高,但在VSV作动筒作动时,这些衬套多少会受到往复冲击力,使得其防旋转表面和周向贴合面都会有少许的磨损,类似下图实物所示;这类磨损标准可以在在发动机手册中获取到,并不在AMM中体现。但建议直接更换,否则还得安排持续监控和更换。所以非必要时不要考虑参考发动机手册保留使用。

主轮螺栓断裂工程措施回顾(2021)

因2021年以来1-3月,每个月发生了一起主轮螺栓断裂的事件,进行工程措施回顾。

从案例分析看,与此前结论一致,钢刹车主轮毂安装螺栓出现断裂的根本原因是含碳量高的不锈钢材质抗蠕变能力不足导致的。现有工程措施中通过角力矩磅紧和定期报废螺杆的方式来进行预防,同时通过磁粉检测方式来识别早期的表面裂纹,针对今年以来的螺栓断裂情况,提出了几项措施。包括:发生两起的修理厂质量审核、包修协议的复核、出现断裂螺栓整套报废等提升建议。

前厕所漏水工程调查2021

回顾从2020年4月新措施实施以来,机队的表现看,典型问题有两个:

1,溢水管堵塞问题,上一轮工卡修改后标准不明确,导致堵塞管路不能被发现。通过修改工卡,明确溢水检查的方式来提升。

2,冲水活门本体渗漏问题,除2020年以前发现的无法完全关闭,新增从供水活门排气口渗漏的问题。该问题厂家已经识别,并在重新设计中,但当前目标是要到2022年才有可能得到新构型的引入,对于这种突发失效,与冲水、液体流动、活门阀体的复位有关,无有效手段提前识别和捕获。从现有机队部件失效看最低的失效时间为6469FH,建议考虑对前厕所现有装机件做一轮返厂升级,更换厂家已识别的漏水隐患部件。待2022年新设计出来后,再执行整体改装。

因详细可靠性调查类,机队数据涉及公司商密,请使用公司主管以上人员邮箱,向HNATJSTD@HNAIR.COM索取。

Untitled

标题襟翼系统由于感应到不对称而旁通
编号737NG-FTD-27-17002
章节27
适用性737NG
日期2021年3月
机队影响ALL
是否关闭
背景机队中常发后缘襟翼旁通故障,是由于左右襟翼位置不一致导致。
并产生相关的代码27-52259 or 27-52260, and occasionally 27-52261。
改进状态波音做了很多调查研究,对实际改善不强。
临时措施对于襟翼不对称旁通事件,波音建议首先通过FIM进行排故,
如未能确定故障,可考虑同时更换后缘襟翼传感器和指示器。
另外波音建议根据 737-SL-24-207检查并清洁插头
最终方案波音修订了FIM 27-51Task 813/820,
以便在襟翼不对称关闭事件后提供更好的故障排除建议。
波音公司启动了737NG-SRP-27-0300,
以修改襟翼位置指示器的设计
截至2020年4月,重新设计的襟翼位置指示器的可用日期尚未完全确定。
点评可参考监控效果分析和指示器导致旁通的说明。
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