Self-Locking or Non-Self-Locking
CONNECTOR DESIGNATOR:
Dash No.
Table I
Page 62-28
Finish
Table II
Page 62-28
F
MIL-DTL-38999 Series I and II,
MIL-DTL-27599
Product Series and
Basic Part Number
M85049/121
S
08
W
S
=
Detented Self-Locking
N
= Non-Detented Self-Locking
Use Dash (–) for Non-Self-Locking
(See Note 5)
E
Coupling Nut
A Thread
F
Captive
Self-locking Nut
-typ-
C
See Note 4
Screw
B
G
D
Knurl Style
Optional
.590
(14.99)
Max
.060/.250
(1.52/6.35)
Screw
Extension
APPLICATION NOTES
1.
2.
3.
4.
5.
6.
Captive
Assembly to be identified with manufacturer’s name and part number, space permitting.
C
-typ-
Glenair Series 600 Backshell Assembly Tools are recommended for assembly and
installation.
Self-locking Nut
See Note 4
Screw
62
Metric equivalents in parentheses (mm) are given for general information only and are
based on 1.000 inch = 25.4 mm.
Cable entry is measured with saddle bars closed and bottomed on clamp ears.
Detented self-locking has a positive audible detented coupling.
Material/Finish:
Clamp body, coupling nut, saddles - Al alloy or 300 Series SST/See Table II.
Clamp screws and lock nuts - CRES/Passivated, Silver plate optional.
Anti-rotation device - Corrosion resistant material
CAGE Codes 06324
Printed in U.S.A.
© 2012 Glenair, Inc.
GLENAIR, INC.
•
1211 AIR WAY
•
GLENDALE, CA 91201-2497
•
818-247-6000
•
FAX 818-500-9912
E-Mail: sales@glenair.com
www.glenair.com
62-27
Strain Reliefs
AS85049/121
Straight Strain Relief
Self-Locking or Non-Self-Locking
TABLE I: Dash Number, Shell Size, Thread and Dimensions (Continued Below)
Dash Screw
No.
Size
08
10
12
14
16
18
20
22
24
4-40
4-40
4-40
4-40
4-40
6-32
6-32
6-32
8-32
Connector Shell
Size
Series I Series II
9
11
13
15
17
19
21
23
25
8
10
12
14
16
18
20
22
24
A Thread
Class 2B
7/16-28 UNEF
9/16-24 UNEF
B Dia
Max
.858 (21.8)
.984 (25.0)
C Dim
± .031 (0.79)
See Note 4
.219 (5.6)
.264 (6.7)
.344 (8.7)
.460 (11.7)
.545 (13.8)
.615 (15.6)
.698 (17.7)
.780 (19.8)
.850 (21.6)
D
Min
E Max
Length
F
Dim
.77 (19.6)
.51 (13.0)
.89 (22.6)
.64 (16.3)
1.01 (25.7)
.76 (19.3)
1.01 (25.7)
.76 (19.3)
1.13 (28.7)
.88 (22.4)
1.38 (35.1)
1.13 (28.7)
1.51 (38.4)
1.26 (32.0)
1.63 (41.4)
1.38 (35.1)
1.76 (44.7)
1.51 (38.4)
AS85049/121
Straight Strain Relief
62
Strain Reliefs
Symbol
A
N
W
X
Y
Z
S
Material
© 2012 Glenair, Inc.
G
Max
.88 (22.4)
.94 (23.9)
1.12 (28.4)
1.19 (30.2)
1.44 (36.6)
1.56 (39.6)
1.69 (42.9)
1.75 (44.5)
1.88 (47.8)
.22 (5.6) 1.01 (25.7)
.27 (6.9) 1.13 (28.7)
.35 (8.9) 1.25 (31.8)
.47 (11.9) 1.25 (31.8)
.55 (14.0) 1.37 (34.8)
.62 (15.7) 1.62 (41.1)
.70 (17.8) 1.75 (44.5)
.78 (19.8) 1.87 (47.5)
.85 (21.6) 2.00 (50.8)
11/16-24 UNEF 1.157 (29.4)
13/16-20 UNEF 1.297 (32.5)
15/16-20 UNEF 1.406 (35.7)
1 1/16-18 UNEF 1.516 (38.5)
1 3/16-18 UNEF 1.642 (41.7)
1 5/16-18 UNEF 1.768 (44.9)
1 7/16-18 UNEF 1.869 (47.5)
TABLE II: Material and Finish
Finish
Black Anodize
Electroless Nickel
Cadmium, Olive Drab
Nickel Fluorocarbon Polymer
Pure Dense Electrodeposited
Aluminum
Zinc Nickel
Passivated
Aluminum Alloy
300 Series SST
CAGE Codes 06324
Printed in U.S.A.
GLENAIR, INC.
•
1211 AIR WAY
•
GLENDALE, CA 91201-2497
•
818-247-6000
•
FAX 818-500-9912
E-Mail: sales@glenair.com
www.glenair.com
62-28