239C0071-1

Technical Characteristics

• Mounting Method

  unthreaded hole single group

• Winding Operating Voltage

  0.00 ac pounds per hour dry single component single primary output and 140.00 ac pounds per hour with retaining chain single component single primary output

• Body Width

  3.500 inches nominal

• End Item Identification

  f/a-18 hornet, s-3b viking, e-2c hawkeye, f-14 tomcat aircraft. h-46 sea knight, h-3 sea king, h-2 seasprite, ch-53a/d/e, rh-53 helicopters.

• Reliability Indicator

  not established

• Input-Output Phase Relationship

  single phase to single phase single component

• Winding Operating Current

  2.4 amperes nominal b and better drop siding single component single primary input

• Dummy Terminal Quantity (Non-Core)

  2

• Terminal Type And Quantity

  3 screw

• Winding Operating Voltage

  120.00 ac pounds per hour wet single component single primary input

• Mounting Facility Quantity

  4 single group

• Center To Center Distance Between Mounting Facilities Parallel To Width

  2.750 inches nominal single mounting facility single center group

• Center To Center Distance Between Mounting Facilities Parallel To Length

  2.750 inches nominal single mounting facility single center group

• Winding Function And Quantity

  1 primary, fixed autotransformer type single component

• Inclosure Type

  open

• Criticality Code Justification

  feat

• Frequency Rating

  320.0 hertz minimum single component and 1.2 kilohertz maximum single component

• Special Features

  weapon system essential

• Mounting Hole Diameter

  0.281 inches nominal single group

• Body Height

  4.062 inches nominal

• Body Length

  3.687 inches nominal

• Winding Power Rating

  0.37 volts-amperes single component single primary input