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时间:2011-04-02 23:22来源:蓝天飞行翻译 作者:航空
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 INDICATOR LIGHTS - MAINTENANCE PRACTICES
________________________________________
 1. General
_______
 A. This procedure contains two tasks:
 (1)  
The removal of the indicator light.

 (2)  
The installation of the indicator light.


 TASK 33-11-81-002-001
 2. Indicator Light Removal (Fig. 201)
_______________________
 A. References
 (1)  WDM 33-18-02, 33-18-03, 33-18-04, 33-18-05
 B. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

 C. Procedure
 S 862-035
 (1)  Prepare for the Removal:
 (a)  Open the circuit breakers that supply the indicator light with power and attach DO-NOT-CLOSE tags.
 NOTE: Many systems in the airplane have indicator lights
____ installed in the flight compartment. Use the Wiring Diagram Manual to find the correct system circuit breakers for each light indicator (Ref WDM 33-18-02 thru 33-18-05).
 (b)  Get access to the rear of the indicator light.
 S 002-029
 (2)  Remove the Indicator Light:
 (a)  
Disconnect and tag the electrical wires attached to the indicator light terminals.

 (b)  
Pull the cap assembly away from the panel.


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CAPTIVE NUT 
(2 LOCATIONS) 
PRESS-TO-TEST 
CONTACT 
BODY AND  PHLLIPS 
CONTACT  MOUNTING SCREW 
ASSEMBLY  (2 LOCATIONS) 

TERMINAL PRESS-TO-TESTASSEMBLY ACTUATOR
FRONT EDGE FOR AN 1/16-INCH PANEL
SLEEVE CAP ASSEMBLY
FRONT EDGE FOR LAMP SPACERAN 1/8-INCH PANEL
(INSTALLED) LAMP (2 LOCATIONS)
PANEL
INDICATOR LIGHT WITH PHILLIPS MOUNTING SCREWS (EXAMPLE)
CAPTIVE NUT
PROTRUSION TO ALIGN THE TERMINAL ASSEMBLY
BODY AND CONTACT SLOT TO ALIGN THE
ASSEMBLY TERMINAL ASSEMBLY
TERMINAL ASSEMBLY
FRONT EDGE FOR AN 1/16-INCH PANEL
SLEEVE CAP ASSEMBLYFRONT EDGE FOR AN 1/8-INCH PANEL LAMP SPACER
(2 LOCATIONS) HEX MOUNTING LAMP SCREW (2 LOCATIONS)
PANEL
INDICATOR LIGHT WITH A HEX MOUNTING SCREW (EXAMPLE)
Indicator Light Lamp Replacement Figure 201
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 ALL  ú ú 01 Page 202 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (c)  
Loosen the screws that hold the indicator light to the panel.

 (d)  
Examine the sleeve to find the end which is adjacent to the panel.


 NOTE: The sleeve can be installed in one of two directions to
____ adjust for the thickness of different panels.
 (e)  
From behind the panel, remove the terminal assembly and the sleeve parts of the indicator light.

 (f)  
Pull the body and contact assembly from the front of the panel.


 TASK 33-11-81-402-009
 3. Indicator Light Installation (Fig. 201)
____________________________
 A. References
 (1)  AMM 24-22-00/201, Manual Control
 B. Access
 (1)  Location Zone
 101 Control Cabin - Left
 201 Control Cabin - Right

 C. Procedure
 S 422-030
 (1)  Install the Indicator Light:
 (a)  
Put the body and contact assembly through the front of the panel.

 (b)  
Put the sleeve on the contact assembly from the rear of the panel.

 (c)  
Make sure that you install the sleeve correctly.


 NOTE: The sleeve can be installed in one of two directions to
____ adjust for the thickness of different panels.
 (d)  
Hold the terminal assembly in the correct position.

 (e)  
Tighten the screws to attach the indicator light to the panel.
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 灯 LIGHTS(12)