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319HW136XW2519BRT14

Description
Connector Accessory
CategoryThe connector    Connector bracket   
File Size167KB,2 Pages
ManufacturerGlenair
Websitehttp://www.glenair.com/
Download Datasheet Parametric View All

319HW136XW2519BRT14 Overview

Connector Accessory

319HW136XW2519BRT14 Parametric

Parameter NameAttribute value
Objectid7007734274
Reach Compliance Codenot_compliant
Connector bracket typeCONNECTOR ACCESSORY
Composite
Backshells
CONNECTOR DESIGNATOR:
with Shrink Boot Porch and Self-Locking Rotatable Coupling
Product Series
319
- EMI/RFI Shield
Sock Assemblies
Angle and Profile
S
- Straight
T
- 45° Elbow
W
- 90° Elbow
Split Ring / Band Option
Split Ring (687-749) and Band
(600-052-1) supplied with
R
option
(Omit
for none)
Custom Braid Length
Specify In Inches
(Omit for Std. 12" Length)
319-136
Composite EMI/RFI Shield Sock
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
Finish Symbol
(See
Table III)
Entry Diameter
(See
Table IV)
SELF-LOCKING
ROTATABLE COUPLING
319
H
S
136
Basic Part
Number
XW
19
12
B
R
T - 14
Shrink Boot Option
Shrink boot and
o-ring supplied
with T option
(Omit
for none)
B
STANDARD PROFILE
Connector Designator
A, F, and H
Connector
Shell Size
(See
Table II)
Optional Braid
Material
Omit for Standard
(See
Table V)
Anti Decoupling
Device - TYP
1.25 (31.8) Max
12.00
Min. Standard
C
Supplied with Standard Nickel/
Copper Braid. See Table III for
Optional Material.
600-052-1 Band
Shrink Sleeve or
Boot Groove - TYP
F
E
H
NOTES
1.
770-001S**-0 shrink boot
supplied with T option. See
shrink boot product page for
more details.
Coupling nut supplied unpla-
ted.
See Table I in Intro for front-
end dimensional details.
O-Ring will not be supplied
with Designator A.
2.
3.
4.
D
E
Raised Configuration
(Mfr's Option) TYP
J
F
.44 (11.2)
TYP
Entry
Dia.
TYP
© 2009 Glenair, Inc.
G
G
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-18
Rev. 12 FEBRUARY 2013
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