MIL-DTL-12883/2E
Dielectric withstanding voltage:
Sea level: Test voltage: 2,000 volts root mean square (ms). Test pin diameter .040 + .001
inch (1.02 + .03 mm).
High altitude: Test voltage: 600 volts ms. Test pin diameter: .040 + .001 inch
(1.02 + .03 mm).
Contact resistance:
Average for all contacts: 0.015 ohm maximum.
Individual contacts: 0.03 ohm maximum.
Continuity test circuit: With the header test-gage(s) inserted into the sockets(s) under test, the pins
of the test-gage(s) and the contacts of the sockets(s) under test shall result in a series circuit. The
header shall be the one used for electron tube 6AU6WB.
Mechanical:
Insertion and withdrawal force:
Initial insertion force: 15 pounds (67 newton) maximum.
Average withdrawal force: 12 pounds (53 newton).
Initial withdrawal force: 4 pounds (18 newton) minimum, 12 pounds (53 newton) maximum.
Vibration: The test gage shall be in approved electron-tube type 6AU6WC in accordance with
MIL-E-1/952.
Durability: After the durability test, the withdrawal force shall be 2 pounds (9 newton) minimum.
Static load: 40 pounds (178 newton).
Float: With a pin of .041 inch (1.04 mm) diameter and .271 inch (6.88 mm) minimum length fully
inserted in a socket contact, the contact shall be capable of free movement (float) within the contact
cavity.
Saddle (with shield base): The saddle shall be integral with the shield base. The method of
attaching the saddle (with shield base) to the insulator body, and the shape of the saddle (with
shield base) where attachment is effected, are optional.
The part shall be designed to operate at the following conditions:
Environmental:
Operating temperature: See table I.
3
For Parts Inquires submit RFQ to Parts Hangar, Inc.
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business