737翼身过热探测灯在测试时不亮

自有案例,罕见故障

2023年5月,有飞机反应左翼身过热灯在测试时不亮,按压灯泡和灯光测试正常,自检有32 KEEL BEAM信息,重装计算机无效。测量D742PIN9-PIN29为1.3M欧(手册要求是小于15欧)。重装D742自检正常无32信息,初步判断D742后方的线束有问题。对于64信息(初步判断为之前做M项,出的警告信息)。

从线路看

经验小结:

1,该故障信息可以MEL放行,方式是使用加温强对探测线加温验证过热灯点亮。

2,机组操作手册中,仅要求对翼身过热灯亮做测试,因而该缺陷可能长时间不能得到识别。

737MAX的地扰控制故障

2023年5月,有MAX飞机反应MAINT灯亮。

状态信息1为SPOILER CONTROL CHANNEL ,相应维护信息为27-01330 GROUND SPOILER OUTPUT DRIVER SIGNAL IS OUT OF RANGE Detected by: SPOILER CONTROL ELECTRONICS (SCE);

状态信息2为GROUND SPOILER CONTROL,相应维护信息为27-01220 GROUND SPOILER CONTROL MODULE IS NOT IN COMMANDED POSITION Detected by: SPOILER CONTROL ELECTRONICS (SCE)。

复位P18-1 B4 和P6-1 A16跳开关故障依旧,整机断电后重新上电,故障依旧,27 – Spoiler Control, SYSTEM TEST, Ground Spoilers测试时发现地面扰流板升不起来,27 – Spoiler Control, OPERATIONAL TEST, SCE Test测试通过。

27-01330 GROUND SPOILER OUTPUT DRIVER SIGNAL IS OUT OF RANGEDetected by: SPOILER CONTROL ELECTRONICS (SCE)的可能性故障部件为:

(a)The ground spoiler control module, M2988.

(b)The ground spoiler control relay, R1169.

(c)The spoiler control electronics, M2940

(d)The problem with the wiring.

27-01220 GROUND SPOILER CONTROL MODULE IS NOT IN COMMANDED POSITION Detected by: SPOILER CONTROL ELECTRONICS (SCE)的可能性故障部件为:

(a)The ground spoiler control relay, R1169.

(b)The spoiler control electronics, M2940

(c)The ground spoiler control module, M2988.

(d)The problem with the wiring.

从故障信息看,SCE取的是GSCM的预位和控制电磁线圈的电流值,用于监控是否在可控范围。当不在范围时,就给出相关警告。从排故结果看,是R1169故障导致的。符合IFIM中关于27-01220的故障可能排序。SCE自检测试能通过,也表明SCE是没有问题的。关于GSCM内部液路作动原理课参看另外一篇关于扰流板无法收回的说明。

截止2023年6月,波音全球的统计数据如下

RECOMMENDATION:
27-02790 SPOILER FAULT OUTPUT DRIVER SIGNAL IS OUT OF RANGE:
Operators have reported SPOILER CONTROL CHANNEL status messages. Boeing finds these messages may occur during power up, often with maintenance message 27-02790.

To minimize the chance of dispatch delay, Boeing recommends to perform the following FIM based maintenance checks for occurrence of SPOILER CONTROL CHANNEL status message with MMsg 27-02790 (SPOILER FAULT OUTPUT DRIVER SIGNAL IS OUT OF RANGE):
– Use the OMF to perform the ground test 27 – Spoiler Control OPERATIONAL TEST, SCE Test.
-Refer to AMM Task 27-61-45-730-801 – Spoiler Control Electronics Self – Test.
-Note that the SCE ground test requires the Master Dim and Test (MD&T) be in the bright (BRT) position.
-Confirm the MMsg 27-02790 is cleared by the Ops Test.
-If cleared, the system is OK for dispatch.
-If the fault is still active, use FIM Task 27-61-00-810-922 to troubleshoot and diagnose the issue.

MEL dispatch relief is available for SPOILER CONTROL CHANNEL.
MEL 27-61-01-01 should be reviewed for applicability.

MITIGATION:
27-02790 SPOILER FAULT OUTPUT DRIVER SIGNAL IS OUT OF RANGE:
Boeing and the SCE supplier (BAE) are investigating the root cause of this message and assessing the appropriate Spoiler Control Electronics software change(s) to appropriately address these faults.
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