(m)
Install the heat-shrinkable sleeve (1) on the assembly against the contact body (8).
(n)
Heat-shrink the sleeve (1).
20-48-31 Page 22
20-48-31 Page 23
Oct 01/04
R
R
R
R
R
_______________________________________________5. Connection Procedure for Coaxial Contacts E0201
A. Contact P/N and Characteristics
(Ref. Fig. 015) --------------------------------------------------------------------| | USE WITH | | CONTACTS |------------------------------------------------| | PLUG | RECEPTACLE | --------------------------------------------------------------------| E0201 | E0165 | --| --------------------------------------------------------------------|
B. Wire Stripping
(Ref. Fig. 016)
C. Crimping Procedure and Tools
(1) RADIALL contacts (code 01)
(Ref. Fig. 017)
(a)
Strip the cable to dimensions A,B,C and D.
____
NOTE : Do not comb out the braid.
(b)
Slide the nut (1) and the ferrule (2) onto the cable.
(c)
Slide the crimping barrel (3) under the braid until it bears on the dielectric.
(d)
Place the ferrule (2) against the crimping barrel (3).
(e)
Crimp the ferrule (2) with the applicable crimping tool (Ref .Table).
(f)
Strip the corre of the cable flush with the collar of the crimping barrel.
(g)
Slide the washer (4) to against the crimping barrel.
(h)
Insert the core of the conductor into the contact core (5).
(i)
Crimp the contact.
(j)
Place the assembly thus formed in the outer body.
(k)
TORQUE the nut to between 0.11 m.daN (9.7345 lbf.in) and 0.17 m.daN (15.0442 lbf.in)
20-48-31 Page 24
Coaxial Contacts - P/N Characteristics SOURIAU and RADIALL E0201 R Figure 015
20-48-31 Page 25
Coaxial Contacts - Wire Stripping and Crimping Tools E0201 - 02 R Figure 016
20-48-31 Page 26
Coaxial Contacts - Wire Stripping and Crimping Tools E0201 - 01 R Figure 017
20-48-31 Page 27
(l) After torque application, make a longitudinal red line on the connector over the threaded cap and the body of the connector.
(2) SOURIAU and RADIALL (code 02) R (Ref. Fig. 016)
(a)
Strip the cable at the size A and B.
(b)
Install the ferrule (1) on the wire.
(c)
Install the threaded cap (2) on the braid support (3).
(d)
Put the braid support (3) in position with the braided shield (4) over the braid support (3).
(e)
Put the ferrule (1) on the braided shield (4) in position C.
(f)
Crimp the ferrule (1) with appropriate tool.
(g)
Strip the wire at level of the braid support (3).
(h)
Install the washer (5) in the stripped wire.
(i)
Engage the stripped wire in the core contact (6).
(j)
Crimp the contact core (6) on the stripped wire with tool.
(k)
Install the body contact (7) on the contact core (6).
(l)
Screw the threaded cap (2) on the body contact (7).
(m)
TORQUE the threaded cap (2) to 0.37 m.daN (3.73 lbf.in.).
(n)
After torque, mark a pencil red line on the threaded cap (2) and the body contact (7).
20-48-31 Page 28
_______________________________________________________________
COAXIAL CONTACTS FOR MIL CONNECTORS - DESCRIPTION AND OPERATION
_______
1. General The coaxial contacts for MIL connectors installed on aircraft have the codes that follow:
-ABS0714
-ABS0715
-E0305
-E0375 type and AMP22936-2
-CANNON 249-1741-000 and CANNON 249-9008-000
-NSA938400 type
-MIL-C-39029/55-344
_________________________________________________2. Connection Procedure for Coaxial Contacts ABS0714
A. Contact P/N and Characteristics
(Ref. Fig. 001) ---------------------------------------------------------------------| | USE WITH | | CONTACTS |------------------------------------------------| | | PLUG | RECEPTACLE | |------------------|-------------------------|----------------------| | ABS0714 | ABS0713 | ABS0713 | ---------------------------------------------------------------------
B. Contact Insertion / Extraction Tools
(Ref. Fig. 002)
(1)
Insertion of the contact from the rear.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 ESPM Electrical Standard Practices Manual 4(45)
