MIL-DTL-83723/68B
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for information only.
3. Unless otherwise specified, tolerances shall be ± .005 (.13 mm) for three place decimals,
± .01 (0.25 mm) for two place decimals, and ± 1o and ± 30' for angular dimensions.
FIGURE 2. Plug and backshell assembly, dimensions and configurations Continued.
REQUIREMENTS:
Dimensions and configurations: See figures 1 and 2.
For insert arrangements, see MIL-STD-1554 and table I.
TABLE I. Inserts requiring reduced diameters for raised seal barriers on contact cavities.
Insert
Contact
Shell
size
arrangements
cavities
8
03
1, 2, 3
10
06
1, 2, 3, 4, 5, 6
For connector accessories: See SAE-AS85049 and MIL-C-83723/16.
Unless otherwise specified in the purchase order, the following components shall be furnished with the
connector:
a. Contacts in accordance with SAE-AS39029 shall be furnished with the connector. Spare
contacts are required for each size contact. The total quantity of spare contacts shall be
10 percent or 1, whichever is greater, of the total number of each size contact required.
b. Grommet seal plugs in accordance with MS27488 shall be furnished with the connector. Total
quantity shall be 15 percent of each contact size or 3, whichever is greater.
c. Contact extraction tools in accordance with MIL-I-81969 shall be included in the connector
package.
Connector assembly shall include a backshell to ensure compliance with moisture sealing requirements.
See SAE-AS85049 and MIL-C/83723/16.
The coupling mechanism of the connector plug shall withstand a minimum tensile load of 100 lb
(45.36 kg) minimum. Load shall be applied to the rear accessory hardware in a straight axial direction.
The quick-disconnect connector plug shall meet the vibration and shock requirements in accordance with
MIL-DTL-83723. The coupling mechanism shall maintain the plug and receptacle in the locked position
during testing.
The tensile force required to unlock the coupling mechanism shall be 5 lb minimum and 20 lb maximum.
The locking mechanism shall meet the performance requirements of MIL-DTL-83723.
6
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