标题 | 后燃油增压泵接头后壳处可能有线束摩擦 |
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编号 | 737-SL-28-098 |
章节 | 28 |
适用性 | 737NG |
日期 | 2021年3月 |
机队影响 | ALL |
概述 | 此服务信函通知,已经交付了受影响的飞机, 在与左右燃油增压泵配对的连接器D00070和D00074后壳 的线束W1134和W1136出现磨损。 上述情况可能会导致燃油增压泵连接器产生电弧和泵的中断运行。 |
背景 | 波音收到了营运人报告关于1号后燃油增压泵连接器D00070 后壳上的其中一条线束有磨损(与线束W1136线束配对), 会在打开燃油泵后使PRESSURE LOW灯亮。 排故发现连接器后壳的线束磨损和绝缘层损坏。 没有了绝缘层,裸露的线束连接器连接着线束后壳和短接接地。 同样的情况在与W1134后壳配对的2号后燃油泵连接器D00074上。 |
厂家措施 | 在对线束W1134和W1136进行了质量调查以确定摩擦原因后, 波音采取了纠正措施,通知线束制造商确保其符合工程和图纸的要求, 在线束和连接器后壳处有间隔。 要求堆积的电线与背面扣环之间有超过60度的 角度来保证线束和后壳之间的间隔。 |
厂家建议 | 为避免报告的情况可能导致燃油增压泵运行问题, 在方便维修的条件下, 建议按照相关步骤检查连接器 D00070和D00074上的线束W1134和W1136。 |
点评 | N/A |
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月度归档: 2021 年 3 月
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标题 | 可能前起落架锁传感器缺少密封胶 |
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编号 | 737-SL-32-219 |
章节 | 32 |
适用性 | 737MAX,737NG |
日期 | 2021年3月 |
机队影响 | ALL |
概述 | 此服务信函目的是通知营运人, 在前起落架锁定传感器安装在轮舱时, 可能没有使用封严。 |
背景 | 在生产安装期间,波音发现了图纸要求在 传感器件号PN 10-61226-45(供应商 P/N 80-207-01) 装到支架上时去需使用BMS 5-95封严, 这一要求无意中被忽略了。 |
厂家措施 | 波音生产线上采取了纠正措施以确保按照参考 a)图纸要求正确使用封严。 |
厂家建议 | 按程序核实封严的使用。 |
点评 | N/A |
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标题 | Honeywell rdr-400气象雷达(WXR) 系统雷达处理器服务信函可升级 |
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编号 | 737-SL-34-259 |
章节 | 34 |
适用性 | 737MAX,737NG |
日期 | 2021年3月 |
机队影响 | 装有Honeywell WXR雷达处理器 (RP)P/N 930-1000-002 / -003的飞机 |
概述 | 此服务信函通知营运人,Honeywell已经发布了 服务信息信函(SIL)和服务通告, 其中记录了RDR-4000气象雷达处理器(RP) 件号930-1000-002和930-1000-003(WXR)软件更新。 在正常运行时,通过限制系统传输, RP改装有望消除导致收发机P/N 930-2000-010内部故障的故障情况。 |
背景 | Honeywell发现了收发机TR P/N 930-2000-010的问题, 在发射机模块组件中的MOSFET晶体管可能过热, 导致TR失效。在正常运行期间, 过热是由于正常运行过程中的温度差导致晶体管下的 电路板接合物损坏和故障。 |
厂家措施 | 发布了服务信息信函(SIL)和服务通告(SB)。 |
厂家建议 | 参考服务信息信函(SIL)和服务通告(SB) |
点评 | N/A |
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标题 | 前门区域热空气软管凹陷情况 |
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编号 | 737-SL-21-134-A |
章节 | 21 |
适用性 | 737MAX |
日期 | 2021年3月 |
机队影响 | ALL |
概述 | 在前区域门加热系统和多个线束之间的软管接头 有潜在的凹陷情况。如果发现需进行纠正。 |
背景 | 在737MAX飞机上报告过前勤务舱门加热软管接头 和主电子舱的线束之间有几例凹陷的情况。 调查显示在这几个737MAX飞机上的STA295, WL185和RBL40的主电子舱中的线束和前勤务门 加热软管之间有凹陷。 这个凹陷是由于没有按照图纸要求去安装软管。 虽然不会立即造成线束损坏,但是从长远来看, 组件高温可能会造成绝缘层失效和系统故障(取决于线束)。 |
厂家措施 | 已经执行了生产线检查和发现一些飞机出现了不一致情况。 不正确安装的软管会重新安装以符合图纸要求。 |
厂家建议 | 为了确保没有凹陷情况, 波音建议在方便维修时机下时采取措施进行检查。 |
点评 | N/A |
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.