32-0026-01

Technical Characteristics

• ~1

  sof (ac-130h, mc-130h, ec-130e, hc-130); rad

• ~1

  data on certain environmental and performanc

• Inductance Rating

  0.47 microhenries nominal single component single winding

• Body Outside Diameter

  0.085 inches minimum and 0.105 inches maximum

• Specification/Standard Data

  96906-ms75083 government standard

• Dc Resistance Rating In Ohms

  0.350 single component single winding

• End Item Identification

  missile, air-to-air phoenix (aim-54); an/sqq-34 carrier based asw module; communications, lha; support equipment, b-52 aircraft; radar set, an/pps-5b; communications terminal, satellite an/gsc-39(v)1; fire pumps; support equipment, b-1 aircraft; aircraft,

• Test Data Document

  81349-mil-c-15305 specification (includes engineering type bulletins, brochures,etc., that reflect specification type data in specification format; excludes commercial catalogs, industry directories, and similar trade publications, reflecting general type

• Criticality Code Justification

  feat

• Core Construction

  s0lid single component

• Special Features

  weapon system essential

• Quality Factor

  30 minimum single component single winding

• Winding Operating Current

  650.0 milliamperes maximum of standard range b and better drop siding single component single winding

• Inclosure Type

  fully inclosed

• Body Length

  0.240 inches minimum and 0.260 inches maximum

• Maximum Operating Temp

  125.0 deg celsius

• Terminal Type And Quantity

  2 wire lead

• Reliability Indicator

  not established

• Coil Form Type

  solid single component

• Rating Method

  electrical single component single winding

• Mounting Method

  terminal single group