9T58K0047

Technical Characteristics

• Reliability Indicator

  not established

• Center To Center Distance Between Mounting Facilities Parallel To Width

  3.125 inches nominal single mounting facility single center group

• Inclosure Type

  fully inclosed

• Winding Function And Quantity

  1 primary single component and 2 secondary single component

• Winding Operating Current

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

• Winding Operating Voltage

  120.00 ac pounds per hour with retaining chain single component all secondary

• Winding Operating Voltage

  480.00 ac pounds per hour with retaining chain single component single primary

• Mounting Method

  bracket single group and slot single group

• Special Features

  weapon system essential

• Center To Center Distance Between Mounting Facilities Parallel To Length

  3.375 inches nominal single mounting facility single center group

• Criticality Code Justification

  feat

• Terminal Type And Quantity

  6 tab, solder lug

• Mounting Facility Quantity

  4 single group

• Mounting Slot Width

  0.562 inches nominal single group

• End Item Identification

  helicopter, ch-53a/d/e; aircraft, viking s-3b; forrestal class cv; aircraft, hawkeye e-2c; usns stalwart class tagos; hayes class t-ag 195; sirius class t-afs 8; aircraft, hornet f/a-18; nimitz class cvn

• Maximum Transformer Power Rating

  0.25 kilovolt-ampere single component

• Body Width

  3.625 inches maximum

• Overall Length

  5.125 inches maximum

• Body Height

  3.937 inches maximum

• Frequency Rating

  60.0 hertz nominal single component

• Input-Output Phase Relationship

  single phase to single phase single component