-----v
MAX
MAST
ITYPJ
5
MARKING
LOCATION
OPTIONAL
SEE-
NOTE
4
W
DIA
MAX
AX
---~-.490
TO
REAR
OF
STATIC
SEAL
GROOVE
.380
MIN
KEYWAY
LENGTH
--
INCH-POUNDINCH-POUND
MIL-DTL-83723/73F
19 August 2009
SUPERSEDING
MIL-DTL-83723/73E
20 October 2000
DETAIL SPECIFIC ATION SHEET
CONNECTOR, ELECTRIC, (CIRCUL AR, ENVIRONMENT RESISTING),
RECEPTACLE, (SINGLE HOLE MOUNT, BAYONET COUPLING, CRIMP SOCKET CONTACT)
(SERIES III, CLASSES A, G, M, R, T, W AND Z)
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
The requirements for acquiring the product described herein
shall consist of this specification sheet and MIL-DTL-83723.
FIGURE 1. Dimensions and configurations.
AMSC N/A FSC 5935
.005MAX
,054
.048
TO
END
OF
FLAT--tr-~
DETAILP
DETAIL A
.Ol9 t
,008
EXTENSION
50
~
(TYP)
.098
.093
PANEL CUTOUT
.054
DIA
120
.076
DIA
tl6
DETAILS
MOUNTING
FLAT
.09
6
DIA
120
• 092 SEE
NOTE
6
.llB
DIA
120
.lllt
.150
DIA
116
,llt6
,210
DIA
112
.206
MS3186
NUT
MIL-DTL-83723/73F
FIGURE 1. Dimensions and configurations -Continued.
2
MIL-DTL-83723/73F
Shell
size
B C D
max
F
max
G N
thread
8 .428
(10.87)
.433
(11.00)
.312
(7.92) .561
(14.25) .536
(13.61)
.531
(13.49)
.625 20UN-2A
10 .530 .388 .696 .659 .750 20UNEF-2A
(13.46) (9.86) (17.68) (16.74)
.535 .654
(13.59)
(16.61)
12 .700 .558 .875 .829 .9375 20UNEF-2A
(17.78) (14.17) (22.23) (21.06)
.705 .824
(17.91)
(20.93)
14 .769 .627 .935 .898 1.000 20UNEF-2A
(19.53) (15.93) (23.75) (22.81)
.137 .774 .893
(3.48)
.097
(19.66)
(22.68)
16 .869 .772 1.062 1.025 1.125 20UNEF-2A
(2.46) (22.07) (19.61) (26.97) (26.04)
.901 1.020
(22.89)
(25.91)
18 1.002 .860 1.187 1.131 1.250 20UNEF-2A
(25.45) (21.84) (30.15) (28.73)
1.007 1.126
(25.58)
(28.60)
20 1.127 .985 1.312 1.256 1.375 20UNEF-2A
(28.63) (25.02) (33.32) (31.90)
1.132 1.251
(28.75)
(31.78)
22 .168
(4.27)
.128
(3.25)
1.252
(31.80)
1.257
(31.93)
1.110
(28.19) 1.437
(36.50) 1.381
(35.08)
1.376
(34.95)
1.500 20UNEF-2A
24 1.377 1.235 1.562 1.506 1.625 20UNEF-2A
(34.98) (31.37) (39.67) (38.25)
1.382 1.501
(35.10)
(38.13)
FIGURE 1. Dimensions and configurations - Continued.
3
MIL-DTL-83723/73F
Shell
size U V S
+.005
-.000
W
max EE FF JJ
8
.670
(17.02)
.979
(24.87)
.508
(12.90)
1.068
(27.13)
.605
(15.37)
.635
(16.13)
.596
(15.14)
.590
(14.99)
10
.796
(20.22)
1.104
(28.04)
.636
(16.15)
1.192
(30.28)
.730
(18.54)
.760
(19.30)
.721
(18.31)
.715
(18.16)
12
.984
(24.99)
1.291
(32.79)
.806
(20.47)
1.380
(35.05)
.917
(23.29)
.947
(24.05)
.908
(23.06)
.902
(22.91)
14
1.046
(26.57)
1.391
(35.33)
.875
(22.23)
1.505
(38.23)
.980
(24.89)
1.010
(25.65)
.971
(24.66)
.965
(24.51)
16 1.171
(29.74) 1.516
(38.51) 1.002
(25.45) 1.630
(41.40) 1.105
(28.07) 1.135
(28.83) 1.096
(27.84)
1.090
(27.69)
18
1.296
(32.92)
1.641
(41.68)
1.108
(28.14)
1.756
(44.60)
1.229
(31.22)
1.260
(32.00)
1.220
(30.99)
1.214
(30.84)
20
1.484
(37.69)
1.766
(44.86)
1.233
(31.32)
1.860
(47.24)
1.354
(34.39)
1.385
(35.18)
1.345
(34.16)
1.339
(34.01)
22 1.609
(40.87) 1.954
(49.63) 1.358
(34.49) 2.086
(52.98) 1.479
(37.57) 1.510
(38.35) 1.470
(37.34)
1.464
(37.19)
24
1.734
(44.04)
2.079
(52.81)
1.483
(37.67)
2.160
(54.86)
1.604
(40.74)
1.635
(41.53)
1.595
(40.51)
1.589
(40.36)
FIGURE 1. Dimensions and configurations -Continued.
4
MIL-DTL-83723/73F
mm
Inches
mm
Inches
mm
Inches
mm
Inches
0.06
.120
3.05
.536
13.61
.875
22.23
1.233
.005 0.13 .125 3.18 .540 13.72 .893 22.68 1.235 31.37
.008 0.20 .138 3.51 .558 14.17 .896 22.76 1.250 31.75
.015 0.38 .144 3.66 .560 14.22 .898 22.81 1.251 31.78
.018 0.46 .149 3.78 .561 14.25 .901 22.89 1.252 31.80
.020 0.51 .198 5.03 .594 15.09 .906 23.01 1.256 31.90
.022 0.56 .204 5.18 .627 15.93 .935 23.75 1.257 31.93
.032 0.81 .211 5.36 .636 16.15 .937 23.80 1.312 33.32
.042 1.07 .250 6.35 .654 16.61 .969 24.61 1.343 34.11
.046 1.17 .259 6.58 .659 16.74 .985 25.02 1.375 34.93
.052 1.32 .312 7.92 .696 17.68 1.002 25.45 1.376 34.95
.065 1.65 .366 9.30 .700 17.78 1.007 25.58 1.377 34.98
.069 1.75 .376 9.55 .705 17.91 1.020 25.91 1.381 35.08
.071 1.80 .378 9.60 .708 17.98 1.025 26.04 1.382 35.10
.072 1.83 .380 9.65 .719 18.26 1.062 26.97 1.385 35.18
.076 1.93 .388 9.86 .728 19.49 1.070 27.18 1.437 36.50
.084 2.13 .392 9.96 .769 19.53 1.108 28.14 1.483 37.66
.089 2.26 .428 10.87 .772 19.61 1.125 28.58 1.501 38.13
.090 2.29 .433 11.00 .774 19.66 1.126 28.60 1.506 38.25
.094 2.39 .490 12.45 .806 20.47 1.127 28.63 1.562 39.67
.097 2.46 .508 12.90 .812 20.62 1.131 28.73 1.703 43.26
.101 2.57 .530 13.46 .824 20.93 1.132 28.75
.106 2.69 .531 13.49 .829 21.06 1.156 29.36
2.84
.535
13.59
.860
21.84
1.187
30.15
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for information only.
3. Unless otherwise specified, tolerances are ± .005 (0.13 mm) for three place decimals,
± .01 (0.25 mm) for two place decimals and ± 1° for all angles.
4. Rear accessory interchangeability dimensions shall be accordance with SAE-AS85049.
5. The centerline of indicated projection must be located on vertical centerline ± 2°.
6. See table I for contact cavities requiring this dimension.
FIGURE 1. Dimensions and configurations -Continued.
5
_J
---
--
MIL-DTL-83723/73F
REQUIREMENTS:
Dimensions and configurations: See figure 1.
For insert arrangements, see MIL-STD-1554 and table I.
TABLE I. Inserts requiring reduced diameters for lead-in chamfers on contact cavities.
Shell
Insert
arrangements
Contact cavities
8 03 1, 2, 3
10 06 1, 2, 3, 4, 5, 6
For connector accessories: See SAE-AS85049.
This connector mates with MIL-DTL-83723/76 and /78.
Part or Identifying Number (PIN) example:
M83723/ 73 R 22 55 N
Military designation
Specification sheet number
Class
Shell size
Insert arrangement
Polarizing position
Changes from previous issue. Marginal notations are not used in this revision to identify changes with
respect to the previous issue due to the extent of the changes.
Referenced documents. In addition to MIL-DTL-83723, this document references the following:
MS3186
MIL-DTL-83723/76
MIL-DTL-83723/78
MIL-STD-1554
SAE-AS85049
6
MIL-DTL-83723/73F
CONCLUDING MATERIAL
Custodians: Preparing activity:
Army -CR DLA -CC
Navy -AS
Air Force -85 (Project 5935-2008-175)
DLA -CC
Review activities:
Army -AR, AV, MI
Navy - EC
Air Force – 19, 99
NOTE: The activities listed above were interested in this document as of the date of this document. Since
organizations and responsibilities can change, you should verify the currency of the information above
using the ASSIST Online database at http://assist.daps.dla.mil.
7