MIL-DTL-12883/11E
Electrical:
Insulation resistance: 1,000 megohms minimum. Test pin diameter: .040 + .001 inch
(1.02 + .03 mm).
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: 660 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 socket(s) under test, the
pins of the test-gage(s) and the contacts of the socket(s) under test, shall result in a series
circuit. The header shall be the one used for electron tube 12AT7WC.
Mechanical:
Insertion and withdrawal force:
Initial insertion force: 20 pounds (89 newton) maximum.
Average insertion force: 15 pounds (67 newton) maximum.
Initial withdrawal force: 4 pounds (18 newton) minimum, 15 pounds (67 newton) maximum.
Vibration: The test gage shall be an approved electron-tube type 12AT7WC, in accordance with
MIL-E-1/1097.
Durability: After the durability test, the withdrawal force shall be 2 pounds (8.90 newton) minimum.
Static load: 52 pounds (231 newton).
The part shall be designed to operate at the following conditions:
Environmental:
Operating temperature: See table I.
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