• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 22:14来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 -
Remove the front insulators (11), (7) and the retention plate (6).


 -On CANNON connector , remove the circlip (9).
 -Remove the central insulator (5).
 -Slide back the grommet (3)then the separator (2) with the seal
 (4) into the backshell (1).
 -Check the wires in the crimped contacts (10).


20-48-23 Page 32

 Normal Contacts - P/N Characteristics
 NSA938182 and NSA938183,CANNON and SOURIAU Contacts
 Figure 023

 

20-48-23 Page 33

 Normal Contacts - Stripping and Crimping Tools
 NSA938182, NSA938183, CANNON and SOURIAU Contacts
 Figure 024

 

20-48-23 Page 34

 -If a wire is damaged:
 -Cut the wires completely to remove the crimped contacts (10).
 -Strip the wires (12) at the size "A".
 -Insert the wires into the contacts.
 -Crimp the contacts (10) with the PICO 500 crimping tool.
 -Slide on the central insulator (5).
 -Install the retention plate (6).
 -Pass the contacts (10) through the front insulator (7).
 -Install the assembly in the housing (8). Make sure that the indexing keyway in insulator (7) is correctly positioned.
 -Slide insulator (7) over insulator (5).
 -On CANNON connector, install the circlip (9).
 -Push the assembly into the housing (8).
 -Tighten the backshell (1) by hand until the orange color appears in the window of the coupling nut. TORQUE 0.8 m.daN (70.7964 lbf.in)
 ____
NOTE : When you tighten the rear connector the torque value increases. This will cause the connector to click until fully engaged.
 -Make sure that the plug is tightened and torqued.
 -Check the pin retention with a dynamometer. The CANNON value is 1.2 daN (2.6977 lbf) minimum, the SOURIAU value is 2.8 daN (6.2946 lbf) minimum, in accordance with pin/socket type used.
 (d)
 For E0378, safety the connector with lockwire (Material N..V02147).

 (e)
 For E0098, install the four screws in the square flange of the receptacle.

 


20-48-23 Page 35

 _________________________________________________________9. Connection Procedure for Contacts NSA938184 and NSA938185
 A. Contacts P/N and Characteristics
 (Ref. Fig. 025, 026, 027, 028) ---------------------------------------------------------------------| | USE WITH | | CONTACTS |------------------------------------------------| | | PLUG | RECEPTACLE | |------------------|-------------------------|----------------------| | NSA938184 | E0094 | E0093 | | NSA938185 | NSA938932 | NSA938931 | ---------------------------------------------------------------------
B. Contacts Insertion / Extraction Tools
 (Ref. Fig. 029)

 C. Sealing (Ref. Fig. 030, 031, 032, 033, 034) If sealing is necessary, refer to the sealing sleeve allocation table. It gives you the quantity and Part Number of the shrinkable sleeve used for sealing. If it is necessary to use several sleeves. The first shrinkable sleeve has a length of 40 mm (1.5748 in.) The second shrinkable sleeve has a length of 30 mm (1.1811 in.) (Shrinking of the sleeve(s) is made after crimping).
 D. Wire Stripping
 (Ref. Fig. 029)

 (1) Normal wire
 -If sealing is necessary, install the heat-shrinkable sleeve on the wire before stripping.
 -Select the applicable tool.
 -Strip the wire at the length "A".
 E. Crimping Procedure and Tools
 (Ref. Fig. 035)

 (1)
 If necessary, install the reducer on the conductor.

 (2)
 Engage the stripped wire in the pin/socket.

 (3)
 Make sure that you can see the wire conductor through the pin/socket hole.

 (4)
 Install the pin/socket contact in the positioner.

 


20-48-23 Page 36

 Normal Contacts - P/N Characteristics
 NSA938184
 Figure 025

 

20-48-23 Page 37

 Normal Contacts - P/N Characteristics
 NSA938185
 Figure 026

 

20-48-23 Page 38

 Normal Contacts - P/N Characteristics
 NSA938185
 Figure 027

 

20-48-23 Page 39

 Normal Contacts - P/N Characteristics
 NSA938184 and NSA938185
 Figure 028

 

20-48-23 Page 40

 Normal Contacts - Stripping Tools and Ins/Ext Tools.
 NSA938184 and NSA938185
 Figure 029

 

20-48-23 Page 41

 Normal Contacts - Sleeve Allocation
 NSA938184 and NSA938185
 Figure 030

 


 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 ESPM Electrical Standard Practices Manual 4(33)