170941

Technical Characteristics

• End Item Identification

  aircraft, hercules c-130, aircraft, hercules c-130f, aircraft, hercules kc-130, aircraft, sof ( ac-130h, mc-130h, ec-130e, hc-130)

• Mounting Hole Diameter

  0.194 inches nominal single group

• Mounting Facility Quantity

  4 single group

• Center To Center Distance Between Mounting Facilities Parallel To Length

  2.000 inches nominal single mounting facility single center group

• Body Length

  2.250 inches nominal

• Inclosure Type

  open

• Criticality Code Justification

  feat

• Center To Center Distance Between Mounting Facilities Parallel To Width

  1.500 inches nominal single mounting facility single center group

• Special Features

  primary rated but not included. weapon system essential.

• Body Outside Diameter

  0.250 inches maximum

• Mounting Method

  flange single group and unthreaded hole single group

• Winding Function And Quantity

  1 secondary single component

• Winding Operating Current

  111.1 amperes nominal b and better drop siding single component single primary

• Reliability Indicator

  not established

• Frequency Rating

  350.0 hertz minimum single component and 450.0 hertz maximum single component

• Winding Operating Current

  50.0 milliamperes nominal b and better drop siding single component single secondary

• Input-Output Phase Relationship

  single phase to single phase single component

• Installation For Which Designed

  indoor nonportable

• Terminal Type And Quantity

  2 bus (bar) conductor