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Composite Backshells
CONNECTOR DESIGNATOR:
319-137 Composite Shield Sock Strain Relief
with Self-Locking Rotatable Coupling
Optional Braid Material B - See Table IV for Options (Omit for Std. Nickel/Copper)
A
A F H
MIL-DTL-5015, -26482 Series II, and -83723 Series I and III MIL-DTL-38999 Series I, II MIL-DTL-38999 Series III and IV
Product Series 319 - EMI/RFI Shield Sock Assemblies Angle and Profile S - Straight A - 90 B - 45
Finish Symbol (See Table III)
Custom Braid Length Specify In Inches (Omit for Std. 12" Length)
SELF-LOCKING
B
ROTATABLE COUPLING LOW PROFILE
319
H
S
137
Basic Part Number
XO
15
B
R - 14
Connector Designator A, F, and H
Connector Shell Size (See Table II)
Split Ring / Band Option Split Ring (687-749) and Band (600-052-1) supplied with R option (Omit for none)
C
Anti-Rotation Device EMI Shroud
L
Std. Shield IAW 107-030 Nickel/Copper See Table III for Optional Material
E Closed
M
F
D
K
12.00 Min Standard Length
.25 Max Screw Extension
Crimp Ring
H Termination Area Free of Cadmium
E
J G .125 Dia. Drain Hole 3 Min. Equally Spaced Typ Sym "A" and "B" Band (600-052-1) Screw Head Same Side Typ Sym "A" and "B"
Detail "B" Finish XN
F
Split ring (687-749)
G
(c) 2009 Glenair, Inc.
CAGE Code 06324
Printed in U.S.A.
GLENAIR, INC. * 1211 AIR WAY * GLENDALE, CA 91201-2497 * 818-247-6000 * FAX 818-500-9912 www.glenair.com E-Mail: sales@glenair.com A-22
319-137 Composite Shield Sock Strain Relief
with Self-Locking Rotatable Coupling
TABLE II: SHELL SIZE
Shell Size A, F 08 10 12 14 16 18 20 22 24 H 09 11 13 15 17 19 21 23 25 E .031 .265 (6.7) .310 (7.9) .390 (9.9) .506 (12.9) .591 (15.0) .661 (16.8) .744 (18.9) .826 (21.0) .896 (22.8) F Min .22 (5.6) .27 (6.9) .35 (8.9) .47 (11.9) .55 (14.0) .62 (15.7) .70 (17.8) .78 (19.8) .85 (21.6) G Max .901 (22.9) .964 (24.5) 1.050 (26.7) 1.112 (28.2) 1.175 (29.8) 1.230 (31.2) 1.293 (32.8) 1.365 (34.7) 1.417 (36.0) H Max 1.388 (35.3) 1.428 (36.3) 1.498 (38.0) 1.548 (39.3) 1.648 (41.9) 1.768 (44.9) 1.808 (45.9) 1.858 (47.2) 1.898 (48.2)
TABLE II: SHELL SIZE (CONTINUED)
Shell Size A, F 08 10 12 14 16 18 20 22 24 H 09 11 13 15 17 19 21 23 25 J Max .91 (23.1) .97 (24.6) 1.06 (26.9) 1.16 (29.5) 1.34 (34.0) 1.41 (35.8) 1.53 (38.9) 1.66 (42.2) 1.78 (45.2) K Max 1.128 (28.7) 1.168 (29.7) 1.248 (31.7) 1.368 (34.7) 1.448 (36.8) 1.528 (38.8) 1.648 (41.9) 1.688 (42.9) 1.758 (44.7) L Max .939 (23.9) 1.059 (26.9) 1.199 (30.5) 1.199 (30.5) 1.329 (33.8) 1.509 (38.3) 1.609 (40.9) 1.759 (44.7) 1.859 (47.2) K Diameter A Code .265 (6.7) .370 (9.4) .506 (12.9) .580 (14.7) .705 (17.9) .784 (19.9) .909 (23.1) 1.034 (1.034) 1.149 (29.2) F Code .275 (7.0) .412 (10.5) .526 (13.4) .651 (16.5) .776 (19.7) .872 (22.1) 1.007 (25.6) 1.132 (28.8) 1.257 (31.9) H Code .264 (6.7) .390 (9.9) .504 (12.8) .630 (16.0) .756 (19.2) .843 (21.4) .969 (24.6) 1.091 (27.7) 1.217 (30.9)
TABLE III: FINISH
Symbol XB Finish Composite Material-No Plating, Color Black, Brass Interface Shroud and Adapter-Nickel Plated 2000 Hour Corrosion Resistant Ni-PTFE, Nickel-Fluorocarbon Polymer. 1000 Hour GreyTM Composite Material-No Plating, Color Black and Brown, Brass Interface Shroud and Adapter- Selectively Cadmium Plated (See Detail B)
TABLE IV: BRAID TYPE
Symbol A B Standard T Braid Type 100% AmberStrand(R) 75%/25% AmberStrand(R) Blend Nickel/Copper 34awg Tin/Copper 34awg
XMT
XN
NOTES
1. 2. 3. (c) 2009 Glenair, Inc. See composite thermoplastic shield sock assembly procedure for detailed installation instructions. See Table I in Intro for front-end dimensional details. Coupling nut supplied unplated. CAGE Code 06324 Printed in U.S.A.
GLENAIR, INC. * 1211 AIR WAY * GLENDALE, CA 91201-2497 * 818-247-6000 * FAX 818-500-9912 www.glenair.com E-Mail: sales@glenair.com A-23
Composite Backshells
A
B
C
D
E
F
G

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