007104

Coils and Transformers

REACTOR

007104

5950-01-257-1144

5950 - Coils and Transformers

Ge Aviation Systems Llc

REACTOR

ACT NOW! SUBMIT A QUICK QUOTE.

Technical Characteristics

  • Winding Operating Current

    4.5 amperes nominal b and better drop siding single component single winding

  • Body Width

    1.260 inches maximum

  • Inclosure Type

    fully inclosed

  • Mounting Method

    unthreaded hole single group

  • Body Length

    2.020 inches maximum

  • Winding Quantity

    1 single component

  • Reliability Indicator

    not established

  • Frequency Rating

    400.0 hertz nominal single component

  • Center To Center Distance Between Mounting Facilities Parallel To Width

    0.988 inches minimum single mounting facility single center group and 1.012 inches maximum single mounting facility single center group

  • Terminal Type And Quantity

    2 tab, solder lug

  • Rating Method

    electrical single component single winding

  • Mounting Hole Diameter

    0.140 inches nominal single group

  • Maximum Operating Temp

    130.0 deg celsius

  • Center To Center Distance Between Mounting Facilities Parallel To Length

    1.613 inches minimum single mounting facility single center group and 1.637 inches maximum single mounting facility single center group

  • Unpackaged Unit Weight (Non-Core)

    0.240 pounds

  • Inductance Type

    fixed

  • Mounting Facility Quantity

    4 single group

  • Dummy Terminal Quantity (Non-Core)

    3

  • Body Height

    1.940 inches maximum

Certified to
AS6081 Methods

Implementing Quality Procurement

A rigorous vendor selection process and vendor management system are essential to ensuring quality.
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Supplying Quality Products

We take every measure to ensure that we supply quality, authentic parts including a strict vendor selection process and rigorous product inspections..
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Providing Quality People

Our team of dedicated account managers, procurement professionals and specialized inspectors is the most valuable resource we have.
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