97A2446PCALL

Coils and Transformers

REACTOR

97A2446PCALL

5950-00-811-8645

5950 - Coils and Transformers

Eaton Aerospace Llc

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ACT NOW! SUBMIT A QUICK QUOTE.

Technical Characteristics

  • Inductance Type

    fixed

  • Inductance Rating

    17.40 henry nominal single component single winding

  • Body Length

    2.312 inches nominal

  • Body Width

    2.062 inches nominal

  • Body Height

    2.500 inches nominal

  • Winding Quantity

    1 single component

  • Inclosure Type

    hermetically sealed

  • Mounting Facility Quantity

    4 single group

  • Mounting Method

    threaded stud single group

  • Thread Quantity Per Inch

    32 single group

  • Nominal Thread Size

    0.138 inches single group

  • Dc Resistance Rating In Ohms

    480.000 single component single winding

  • Thread Series Designator

    unc single group

  • Reference Number Differentiating Characteristics

    material will be in accordance with ships parts control center activity hx quality control,manufacturing and testing specifications

  • Center To Center Distance Between Mounting Facilities Parallel To Length

    1.687 inches nominal single mounting facility single center group

  • Center To Center Distance Between Mounting Facilities Parallel To Width

    1.437 inches nominal single mounting facility single center group

  • Winding Operating Current

    10.0 milliamperes dc maximum single component single winding

  • Criticality Code Justification

    zzzy

  • Terminal Type And Quantity

    2 tab, solder lug

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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