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AIPC
Aircraft Illustrated Parts Catalog
GL3 · Rev 17 · 15 Feb 2024 · D638A001-GL3-0256
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AMM
Aircraft Maintenance Manual, Part II
GL3 · Rev 83 · 15 Feb 2024 · D633A101-GL3
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CHAPTER 05
TIME LIMITS/MAINTENANCE CHECKS
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CHAPTER 06
DIMENSIONS AND AREAS
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CHAPTER 07
LIFTING AND SHORING
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CHAPTER 08
LEVELING AND WEIGHING
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CHAPTER 09
TOWING AND TAXIING
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CHAPTER 10
PARKING AND MOORING
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CHAPTER 11
PLACARDS AND MARKINGS
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CHAPTER 12
SERVICING
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CHAPTER 20
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CHAPTER 21
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AUTOFLIGHT
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CHAPTER 26
FIRE PROTECTION
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CHAPTER 27
FLIGHT CONTROLS
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CHAPTER 28
FUEL
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CHAPTER 29
HYDRAULIC POWER
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CHAPTER 30
ICE AND RAIN PROTECTION
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CHAPTER 31
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CHAPTER 32
LANDING GEAR
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CHAPTER 33
LIGHTS
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SECTION 33-17
FLIGHT CREW LIGHTS
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PASSENGER COMPARTMENT LIGHTS
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SECTION 33-26
WORK LIGHTS
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SECTION 33-27
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SECTION 33-29
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SECTION 33-32
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CHAPTER 34
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WINGS
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CHAPTER 70
STANDARD PRACTICES
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POWER PLANT
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CHAPTER 72
ENGINE
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ENGINE FUEL AND CONTROL
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CHAPTER 74
IGNITION
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AIR
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ENGINE INDICATION
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OIL
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CHAPTER 80
STARTING
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      EXPORT CONTROLLED
Issue Date: 15 Apr 2021
发行日期:2021 年 4 月 15 日
  the boeing company
 
 

TASK 33-18-00-710-802 任务 33-18-00-710-802

 
 

10.  Master Dim and Test - Operational Test (Figure 207)
10. 主调光和测试 - 操作测试(图 207)

 
 

A.   General 一个。  常规

 
 

(1)  This test makes sure the master dim and test system operates.
(1) 该测试确保主调光和测试系统正常运行。

 
 

B.   References B.  引用

 
 

Reference 参考

Title 标题

 

24-22-00-860-811

Supply Electrical Power (P/B 201)
电源 (P/B 201)

 

24-22-00-860-812

Remove Electrical Power (P/B 201)
移除电源 (P/B 201)

 
 
 

C.   Tools/Equipment C. 工具/设备

 
 

Reference 参考

Description 描述

 

STD-1176 性病-1176

Cover - Windshield Blackout Screen
盖 - 挡风玻璃遮光屏

 
 
 

D.   Location Zones
D. 位置区域

 
 

Zone 

Area 面积

 

211

Flight Compartment - Left
驾驶舱 - 左侧

 

212

Flight Compartment - Right
驾驶室 - 右

 
 
 

E.   Procedure E.  程序

 
 

SUBTASK 33-18-00-860-011 
子任务 33-18-00-860-011

 
 

(1)  Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
(1) 执行此任务:供电,任务 24-22-00-860-811。

 
 

SUBTASK 33-18-00-940-008 
子任务 33-18-00-940-008

 
 

(2)  On a bright day, put a windshield cover, STD-1176 on the windshield to make it easier to do this test.
(2)在阳光明媚的日子里,在挡风玻璃上放一个挡风玻璃罩STD-1176,以便更容易进行此测试。

 
 

SUBTASK 33-18-00-860-012 
子任务 33-18-00-860-012

 
 

(3)  Prepare to do the test:
(3)准备做测试:

 
 

(a)  At the overhead panel, P5, do these steps:
(a) 在头顶面板 P5 上,执行以下步骤:

 
 

1)  Set the emergency light switch to ARMED.
1) 将应急灯开关设置为 ARMED。

 
 

2)  Set the air conditioning switches to AUTO.
2) 将空调开关设置为 AUTO。

 
 

3)  Set the left and right mode select switches to ALIGN.
3) 将左右模式选择开关设置为 ALIGN。

 
 

4)  Set the yaw damper switch to ON.
4) 设置偏航 damp开关为 ON。

 
 

GL3 200

 
 

(b)  At the glareshield panel, P7, set the A/T switch to ON.

 
 

GL3 ALL GL3 全部

 
 

(c)  At the control stand, P10, release the parking brake.
(c) 在控制架 P10 处松开驻车制动器。

 
 

SUBTASK 33-18-00-710-006 
子任务 33-18-00-710-006

 
 

(4)  Do a test of the annunciators, pushbutton switches, and Liquid Crystal Display (LCD) segments connected to the master dim and test system (WDM 33-18-11 thru 33-18-99):
(4) 对连接到主调光和测试系统(WDM 33-18-11 至 33-18-99)的信号器、按钮开关和液晶显示器 (LCD) 段进行测试:

 
 

(a)  At the captain's main instrument panel, P1, set the switch for the master dim and test lights to TEST.
(a) 在船长的主仪表板 P1 上,将主调光和测试灯的开关设置为 TEST。

 
 

NOTE:  The CMD and CWS pushbuttons on Honeywell MCP (part number 4082260-937/-939) will not illuminate.
注意: 霍尼韦尔 MCP(部件号 4082260-937/-939)上的 CMD 和 CWS 按钮不会亮起。

 
 

NOTE:  The CMD and CWS pushbuttons on Collins MCP (part number 822-1567-101/-102) will illuminate.
注意:Collins MCP(部件号 822-1567-101/-102)上的 CMD 和 CWS 按钮将亮起。

 
 

(b)  On these panels, make sure the lamps in the annunciators come on brightly:
(b) 在这些面板上,确保信号器中的灯亮起:

 
 

1)  Captain's main instrument panel, P1
1) 船长主仪表板,P1

 
 

2)  Center main instrument panel, P2
2) 中央主仪表板,P2

 
 

3)  F/O's main instrument panel, P3
3) F/O的主仪表板,P3

 
 

4)  Overhead panel, P5
4) 顶置面板,P5

 
 

5)  Glareshield panel, P7
5) 防眩光板,P7

 
 

GL3 200, 203

 
 

NOTE:  The A/T light will be very dim.

 
 

GL3 ALL GL3 全部

 
 

6)  Aft electronics panel, P8
6) 船尾电子面板,P8

 
 

NOTE:  The fire warning lights are not checked during this test.
注意: 在此测试期间不检查火灾警告灯。

 
 

a)  To complete the test of the wheel well warning light and engine start lever lamp warning light, set the test switch to the OVHT/FIRE position, then back to its usual position.
a) 要完成轮井警告灯和发动机启动杆指示灯的测试,请将测试开关设置到 OVHT/FIRE 位置,然后返回其通常位置。

 
 

7)  Forward electronics panel, P9
7) 前向电子面板,P9

 
 

NOTE:  You will find five annunciators on each CDU; DSPY (or CALL), FAIL, MSG, OFST, and EXEC.
注意:您会在每个 CDU 上找到五个报警器;DSPY(或 CALL)、FAIL、MSG、OFST 和 EXEC。

 
 

8)  Control stand, P10
8) 控制支架,P10

 
 

a)  Make sure that the parking brake light is on.
a) 确保驻车制动灯亮起。

 
 

(c)  On the P5 panel, make sure the lamps in the pushbutton switches (engine module, P5-68) come on brightly.
(c) 在 P5 面板上,确保按钮开关(发动机模块,P5-68)中的灯亮起。

 
 

(d)  Make sure the LCD segments on these panels come on for 2 seconds then go off for 1 second:
(d) 确保这些面板上的 LCD 段亮起 2 秒钟,然后熄灭 1 秒钟:

 
 

1)  Captain's main instrument panel, P1
1) 船长主仪表板,P1

 
 

2)  F/O's main instrument panel, P3
2) F/O的主仪表板,P3

 
 

3)  Overhead panel, P5
3) 高架面板,P5

 
 

4)  Glareshield panel, P7
4) 防眩光板,P7

 
 

5)  Aft electronics panel, P8
5) 船尾电子面板,P8

 
 

(e)  At the P1 panel, set the switch for the master dim and test lights to the usual mode.
(e) 在 P1 面板上,将主调光和测试灯的开关设置为通常模式。

 
 

SUBTASK 33-18-00-860-013 
子任务 33-18-00-860-013

 
 

(5)  Put the airplane back to its usual condition:
(5)将飞机恢复到正常状态:

 
 

(a)  If necessary, at the P10 panel, set the parking brake.
(a) 如有必要,在 P10 面板上设置驻车制动器。

 
 

(b)  At the P5 panel, do these steps:
(b) 在 P5 面板上,执行以下步骤:

 
 

1)  Set the emergency light switch to the usual mode.
1) 将应急灯开关设置为常用模式。

 
 

2)  Set the air conditioning switches to the usual mode.
2)将空调开关设置为常用模式。

 
 

3)  Set the yaw damper switch to usual mode.
3) 将偏航 damp开关设置为常规模式。

 
 

4)  Set the left and right mode select switches to the usual mode.
4)将左右模式选择开关设置为常用模式。

 
 

SUBTASK 33-18-00-940-009 
子任务 33-18-00-940-009

 
 

(6)  If a windshield cover, STD-1176 was used on the windshield, remove it.
(6) 如果挡风玻璃上使用了STD-1176的挡风玻璃罩,请将其取下。

 
 

SUBTASK 33-18-00-860-014 
子任务 33-18-00-860-014

 
 

(7)  Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
(7) 执行此任务:断开电源,任务 24-22-00-860-812。

 
 

Figure 207. Master Dim and Test System Test
图 207.主调光和测试系统测试

 
 

Queue GraphicSheet 1  - Effectivity: GL3 ALL
Queue Graphic 表 1 - 有效性:GL3 ALL

 
Figure 207. Master Dim and Test System Test
图 207.主调光和测试系统测试




M23240 S0006575989_V2 FLIGHT COMPARTMENT MASTER DIM AND TEST SWITCH ANNUNCIATORS, PUSHBUTTON SWITCHES, AND LCD SEGMENTS
This section is not applicable for the selected airplane.
Corrective Actions
737-800TASK 33-18-00-710-802Rev Date : 01 Jan 1970Copyright © 2007, 2014 BoeingBoeing ProprietaryECCN 9E991