ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (5): 326598-326598.doi: 10.7527/S1000-6893.2022.26598
• Electronics and Electrical Engineering and Control • Previous Articles Next Articles
Baohui JIA1, Fan JIANG2, Yuxin WANG1(), Du WANG2
Received:
2021-11-02
Revised:
2021-12-19
Accepted:
2022-02-22
Online:
2022-03-08
Published:
2022-03-04
Contact:
Yuxin WANG
E-mail:yuxinwang2009@126.com
Supported by:
CLC Number:
Baohui JIA, Fan JIANG, Yuxin WANG, Du WANG. Fault diagnosis method based on civil aircraft maintenance text data[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 326598-326598.
Table 2
Aircraft maintenance records of an airline after marking (part)
序号 | 故障描述 | 故障处理 | 故障原因 |
---|---|---|---|
1 | 3#主轮见线 | 根据AMM32-41-11PB401更换主轮后测试正常 | 机轮磨损、见线 |
2 | 济南关车后,ENG2 EGT指示不正确;长春关车后ENG2 EGT指示迅速下降。 | 机组在地面进行CFDS相关测试,发动机参数指示正常;航后FADEC 2A测试有故障信息:EGT SENS/HC/EEC2,按TSM77-20-00-810-808测量EGT热电偶、导线正常,清洁EEC插头,地面FADEC测试正常,试车双发温度一致。 | EGT指示 |
3 | 左边刹车踏板软易造成刹车向左跑偏 | 过站检查PFR无相关刹车系统故障信息,BSCU测试工作正常,操作人工刹车、左侧刹车压力在绿区以上,右侧刹车压力正常 | 轮偏 |
4 | 航后检查发现2#前轮外物割伤超标 | 根据AMM32-41-12PB401更换2#前轮 | 机轮扎伤 |
5 | 短停检查发现有BSCU1#,BRK PEDAL XMTR(9GG)信息 | 重置BSCU1#跳开关,测试系统工作正常 | BSCU |
… | … | … | … |
Table 3
Partial results of aircraft maintenance text preprocessing results
序号 | 未处理民机维修文本 | 预处理后民机维修文本 |
---|---|---|
1 | 空中出现"NAV TCAS FAULT"信息.1.参考MEL34-43-01飞机放行. (厦门) 2.串用351的TCAS计算机,通电测试TCAS系统工作正常,并关闭MEL保留. ()34. | 空中出现NAV TCAS FAULT信息.参考MEL34-43-01飞机放行厦门串用351的TCAS计算机,通电测试TCAS系统工作正常,关闭MEL保留 |
2 | 机组口头反映空中偏航阻尼开关断开一次,后接通正常。 On air,YD switch off.为判明故障与B2163机对调SYMD计算机第一部,地面测试正常。 P/N:285A1010-6 S/N ON:D02004 S/N OFF:D03809 | 空中偏航阻尼开关断开一次,后接通正常.ON AIR YD SWITCH OFF判明故障与B2163机对调SYMD计算机第一部,地测试正常.P/N:285A1010-6 S/N ON:D02004 S/N OFF:D03809 |
Table 4
Fault diagnosis results
序号 | 故障描述 | 故障原因 |
---|---|---|
1 | 空中出现"NAV TCAS FAULT"信息.1.参考MEL34-43-01飞机放行; 2.串用351的TCAS计算机,通电测试TCAS系统工作正常,关闭MEL保留 | TCAS |
2 | 航后非例行工卡DL08-2287-26A-01目视检查五号轴承滑油管及更换右发回油滤,检查正常. P/N QA05954 | 油路破损漏油 |
3 | 工卡A20J361143-01-1-1更换左发风扇活门温度控制恒温器气滤,检查正常(C2539) | 引气预冷 |
4 | 工卡5050010734NR/17测量EEC到电池阀之间线路,检查EGT导线与接线合异孔探检查左发点火嘴及燃油点火嘴正常,试车故障一样 | EGT指示 |
5 | 航后检查发现左前轮扎伤见线,更换充气至180PSI,检测无渗漏,力矩160/80lb.ft,设备号MFL00147 | 机轮扎伤 |
6 | 1号刹车磨平.航后更换1号刹车,测试正常 | 刹车磨损 |
7 | 升级EGPWS地形数据到437版本,包络调制数据库升级到B06版本,通电测试正常 | EGPWS |
8 | 备用罗盘灯光不亮.更换灯泡,通电测试正常 | 指示组件 |
9 | 排除前页故障,因航材无件,将 282飞机左发EEC装到本机左发,地面试车正常,检查FADEC自测试正常 | EEC故障 |
10 | 航后左发所有磁堵的检查(A8680) | 磁堵 |
… | … | … |
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