NSN: 5935-01-518-9396

Technical Characteristics

• Overall Width

  1.250 inches nominal

• Connector Locking Method

  bayonet pin

• Thread Direction

  right-hand and right-hand

• Nominal Thread Length

  0.306 inches and 0.281 inches

• Shell Material

  aluminum alloy

• Included Contact Quantity

  12 single mating end single contact grouping

• Body Style

  straight shape, external coupling

• Nominal Thread Size

  0.9375 inches and 1.0625 inches

• Unthreaded Mounting Hole Diameter

  0.116 inches minimum and 0.125 inches maximum

• Contact Removability

  removable single mating end single contact grouping

• Overall Length

  1.421 inches maximum

• Overall Height

  1.250 inches nominal

• Terminal Location

  back single mating end single contact grouping

• Distance From Mounting Shoulder To Front Face

  0.708 inches minimum and 0.728 inches maximum

• Thread Quantity Per Inch

  20 and 18

• Shell Type

  solid

• Contact Position Arrangement Style

  24 number 20 single mating end

• Shell Surface Treatment

  anodize

• Terminal Type

  crimp single mating end single contact grouping

• Threaded Device Type

  back shell and coupling facility

• Special Features

  environment resistant

• Included Contact Type

  round pin single mating end single contact grouping

• End Item Identification

  boeing b757 aircraft

• Mating End Quantity

  1

• Mounting Method (Non-Core)

  flange

• Center To Center Distance Between Mounting Facilities Parallel To Height

  0.969 inches nominal

• Thread Class

  2a and 2a

• Polarization Method

  keyway or multiple keyway

• Thread Series Designator

  unef and unef

• Shell Material Document And Classification

  sae-ams-qq-a-200 assn std single material response or sae-ams-qq-a-367 assn std single material response or astm-b211 assn std single material response

• Insert Position In Deg

  18.0 and 192.0 and 149.0 and 0.0 and 259.0

• Distance Between Centerlines Of Mounting Facilities Parallel To Body Width

  0.969 inches nominal

• Shell Surface Treatment Document And Classification

  mil-a-8625 mil spec single treatment response