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时间:2011-04-04 10:05来源:蓝天飞行翻译 作者:航空
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 (c)  
Make sure that there is no unwanted force that is applied to the wire bundle.

 (d)  
Harnesses that touch a metal component are not permitted.

 (e)  
The routing of the different wire bundles can touch each other in some areas.


 NOTE: Wire bundles that go across and touch different wire
____ bundles are permitted if they are installed on the same bracket.
 (f)  It is permitted to let the wire bundles touch when they are parallel to each other. 1) This is permitted only if the wire bundles are of the same
 flexible conduit.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
E.  Visually Examine The Wiring Harnesses
 S 212-003-C00
 (1)  Visually examine the wiring harness for damage
 (a)  Cust, abrasions, chafing, rupture or damage to the outer cable sheet are acceptable if the first protective layer is not worn through. 1) Not serviceable if the first protective layer is worn
 through.
 S 212-004-C00
 (2)  Look for damage to the engine component receptacles and harness connectors.
 (a)  
Thread damage:

 1)  One lead-in thread of more than 30 percent damage, or two lead-in threads with 20 percent or more damage: a) Chase the threads if they meet the specified limits.

 (b)  
Connector and related receptacle pin damage:


 1)  Make sure the pin-to-socket connections are satisfactory, and the sockets are tightly attached in the connector or the receptacle. a) If the pin-to-socket connections are not tightly
 attached, do a retention test of the connection socket. 2) If the pins or sockets are broken, eroded, bent, or corroded, replace the engine component or connector.
 (c)  Contamination inside the connector and receptacle well. 1) None permitted.
 a)  Clean the area with a bristle brush and solvent, PD 680 Type I or II.
 F.  Retention Test Of The Connector Socket
 S 282-005-C00
 (1)  Do a check of the retention of the connector socket:
 (a)  Clean the checking pin tool with solvent, PD 680 Type I or II.
 NOTE: No trace of lubricant is permitted.
____
 CAUTION:_______BE CAREFUL WHEN YOU DO A CHECK OF THE CONTACTS. INCORRECT USE OF THE RETENTION TEST TOOL COULD CAUSE DAMAGE TO THE CONNECTORS, CONTACTS OR TEST TOOL.
 (b)  
Install the applicable pin of the tool in the connector socket.

 (c)  
Hold the connector vertically so the socket contacts point to the ground.

 (d)  
Put the tool in the socket.


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 ALL  ú ú C01 Page 202 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHECKING PIN NO. 20 0.0397-0.0399 INCH 0.41 INCH

CHECKING PIN NO. 20

Connector Socket Retention Checking Tool
Figure 201

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
L18554
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(e)  
With the connector and tool in this position, the connector socket must not let the tool drop out. 1) If the tool drops out, replace the harness.

 (f)  
Do the steps again for all other contacts in the connector.

 (g)  
When the connector test is complete, install the connector to the specified receptacle.
 
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