737-NG - ME口试考题

737NG

手册题14个

1． 请在AMM手册中找到IDG勤务的章节号，并根据内容说出IDG勤务包含哪几项工作？

TASK 12-13-21-200-801

A. This procedure has these tasks: (1) IDG Oil Level Check

(2) IDG Servicing (Oil Fill)

(3) IDG Differential Pressure Indicator (DPI) Check (4) IDG Oil Change

2．请根据AMM中的主电瓶拆装工卡，说出主电瓶的安装位置，拆装时所需的工装（件号）。

A. This procedure has these tasks: (1) A removal of the Battery.

(2) An installation of the Battery. TASK 24-31-11-000-801-001 (1) The M6 Battery is located below the E3 equipment rack in the main equipment area.

(2) The battery is removed and installed in the forward cargo area. The circuit breakers on the J9panel are installed in the main equipment center. B. Tools/Equipment

SPL-1633 Equipment - Battery Installation

(Part #: C24003-1, Supplier: 81205, A/P Effectivity: 737-600, -700, -700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)

3．请找出发动机燃油翼梁活门的工卡并回答拆装作动器是否需要油箱放油，完成作动器安装后所需要做的测试。

A. The spar valve contains three parts: the actuator, the valve adapter, and the valve body.

B. It is not necessary to defuel the fuel tank to remove the actuator. It is necessary to defuel the fuel tank to remove the valve adapter or valve body. C. This procedure contains these tasks: (1) Remove the Actuator of the Spar Valve (2) Install the Actuator of the Spar Valve (3) Remove the Valve Adapter of the Spar Valve (4) Install the Valve Adapter of the Spar Valve (5) Remove the Valve Body of the Spar Valve (6) Install the Valve Body of the Spar Valve

(7) Rework the Electrical Faying Surface Bonds for the Spar Valve TASK 28-22-11-000-801

For the actuator that you installed, do this task: Engine Fuel Spar Valve - Electrical Control and

Indication Test, TASK 28-22-00-710-801

4．某根导线的线号为W0342-0001-18,请根据手册查出该导线所连接的两个电插头的设备号，该导线所在导线束的件号。

W0342 286A0342 FORWARD RIGHT HAND DOORWAY LINING

0001 18 PA 1-10 35-21-31 D40042J 5 D12606

5．请根据手册回答更换发动机启动活门时，需更换的封圈有几个？完成安装后所需要的工作有哪些？

TASK 80-11-03-400-801-F00 2个

6．已知某部件件号RSE120028, 请查出该部件的波音规范号、可选件号，是否适用于

B-5118飞机？

27-31-11-02 001012 7．请查出适用于B-5118飞机的液压A系统交流电动马达泵壳体回油滤滤芯的件号和其油滤维护工作包的件号 29-11-41-01

FILTER MAINTENANCE KIT REF:65-90305-58

8．请查出适用于B-5111飞机右侧风挡雨刷马达的件号 30-42-21-01 2313M347-4

9．查找适用于B-5111飞机的PRSOV件号。 36-11-04-01A 3214552-5

10．B-5117飞机某跳开关的设备号为C00413,请根据手册查出它的件号，该跳开关供电的电源

C00413 BACC18AD3 S281A0601 33-29-11

CB-BRT ENTRY LT 07217 P091-00/ /E010

11．B-5117飞机上某插头的设备号为D00476,请根据手册查出它的件号，该电插头在系统图纸中哪两根销钉与地连接。

D00476 BACC63BP12C12SN 33-42-11

PLUG-RETRACTABLE LANDING LT,R 81205 533/154/R034

12．请查出适用于B-5119飞机的整体驱动发电机的件号和波音规范号。

24-11-11-50

13．查找件号为MS24523-21的部件名称和设备号，是否适用于B-5118飞机

33-14-00-07 001005

14．青岛过站B-5119飞机后货舱门中央表面蒙皮上有一凹坑，经测量其深度为0.8mm，

直径为2.6cm，请问损伤是否超过放行标准，修理方法的章节号？ 该损伤是否超标 52-30-01-1A 不超标 修理方法 52-30-01-2R

737NG故障题12个

1．B-5117飞机P5板的液压B系统ELEC1泵的 OVERHEAT灯亮，简述故障原因和排故方

法？

FAULT DESCRIPTION FAULT CODE GO TO FIM TASK

ELEC 1 OVERHEAT light

* light on . . . . . . . . . 293 030 29-30 TASK 805

2．B-5111飞机“防滞/自动刹车控制器”自检维护信息为 “ADIRU L”,请根据故障隔离手册指出与该故障有关的跳开关（要求说出设备号和位置），若检查线路正常，接下来的排故措施？

LRU/SYSTEM MAINTENANCE MESSAGE GO TO FIM TASK

ANTISKID ADIRU L 32-42 TASK 824

C. Circuit Breakers

(1) These are the primary circuit breakers related to the fault: F/O Electrical System Panel, P6-3 Row Col Number Name

E 16 C00196 LANDING GEAR ANTISKID INBD E 18 C00195 LANDING GEAR ANTISKID OUTBD

(e) If you do not find a problem with the wiring, then continue. （1) Re-install the AACU, M162.

(2) Install a new left ADIRU, M1749. (3) Replace the AACU, M162.

3．B-5118飞机左空调“组件/区域控制器”自检维护信息为 “THIS PACK —TCV” 请根据故障隔离手册指出该故障可能的原因有哪些？

21-62 TASKS 830. Left Temperature Control Valve - Fault Isolation

A. Description

(1) This task is for this maintenance message: (a) THIS PACK - TCV (2) The left pack/zone temperature controller has detected a fault from the left temperature control valve. B. Possible Causes

(1) Left temperature control valve, V139 (2) Air conditioning relays No. 1, M324 (3) Wiring

(4) Cabin temperature controller, M1442 (No. 1).

4．B-5117左发动机EEC自检有75-10571信息，请简述此故障代码的含义及可能的故障件？

ENGINE – 1

75-10571 THE HMU TBV CONTROL CURRENT IS OUT OF RANGE 75-23 TASK 804

5．B-5119飞机APU无法启动，自检维护信息为49-41010，请根据故障隔离手册指出该故障最有可能的原因？

LRU/SYSTEM MAINTENANCE MESSAGE GO TO FIM TASK APU 49-41010 NO ACCELERATION SHUTDOWN 49-40 TASK 801

6．青岛过站B-5118飞机右发动机的余油管漏煤油，经检查为70滴/分钟，请问需要采取的措施？

(4) These leakage limits are given in threshold limits and serviceable limits:

(a) For fuel leaks:

1) If the total leakage rate from the drains is less than the threshold limit, you can continueto operate the engine. Maintenance action is not necessary. 2) If the total leakage rate from the drains is more than the threshold limit, but less than the serviceable limit, corrective action must be done before 25 flight cycles. 3) If the total leakage rate from the drains is more than the serviceable limit, you must do the corrective action.

F. Engine Vents and Drains Leakage Limits and Corrective Action

SUBTASK 71-71-00-790-007-F00

(1) Fuel drain system (a) Fluid: Fuel

(b) Threshold limit: 180 cc/hr (60 drops per minute)

1) If the leakage is less than the threshold limit, no maintenance action is necessary.

2) If the leakage is more than the threshold limit and less than the serviceable limit, youcan continue the engine in service for not more than 25 flight cycles before you replacethe applicable component. (c) Serviceable limit: 270 cc/hr (90 drops per minute)

7．请简述ENGINE FUEL SPAR VALVE活门的作用，结合P5板的SPAR VALVE CLOSED灯说明活门的状态，过站关车后出现SPAR VALVE CLOSED灯明亮的情况如何处置？ （1）起动发动机时打开给发动机供油，火警时关断。

（2）打开熄灭，关断暗亮，活门位置与起动杆位置不一致明亮 （3）参考MEL处置，测试不通过参考FIM排故。

8．过站时机组反映：使用防冰时发动机防冰活门故障灯“COWL ANTI-ICE ”亮，主要故障原因，作为放行人员你将如何处理？

活门下游压力超标大于65psi

（1）可简单进行故障处理。参考FIM30-21。

（2）如时间不足，按照MEL30-3放行，填写飞行记录本；过站根据实际情况锁定活门在开位（有结冰天气时，同时还要锁定9TH HPV）或锁定在关位放行；执行M程序（提醒机组执行O程序）。

（3）通知生产（生产通知签派）。

9．请根据下图简述PRSOV的工作原理，引气脱开的原因是什么，450F传感器怎样控制，如果PRSOV和450F传感器之间的信号管漏气对引气压力有何影响?

10．青岛过站B-5119飞机的PSEU灯亮，请找出该灯亮的原因，怎样处理？ （1）参考MEL32-17决定能否放行 PSEU light

light on . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . .

320 050 00 32-09 TASK 801

11．请根据下图简述引气预冷系统的工作原理，预冷器控制活门在发动机关车后在什么

位置，如果预冷器控制活门和传感器之间的信号管堵塞，活门向何方向转动，对引气压力有何影响？

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