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  • MIL-PRF-7032 Revision H:2010

    Current The latest, up-to-date edition.

    INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s):  PDF

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    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. REQUIREMENTS
    4. VERIFICATION
    5. PACKAGING
    6. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies the general requirements for inverters that convert electrical power in aircraft from nominal 28 volts direct current (VDC) power to three-phase or single-phase alternating current (AC) power at 400 hertz.

    General Product Information - (Show below) - (Hide below)

    Committee FSC 6125
    Development Note Supersedes MIL I 7032 (G). (09/2010) Supersedes MIL I 85071. (10/2010) H NOTICE 1 - Notice of Validation. (09/2016) NEW CHILD NOT 2 2021 IS NOW ADDED
    Document Type Standard
    Product Note NEW CHILD NOT 2 2021 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current
    Supersedes

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    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    SAE AMS STD 2175 : 1998 CASTINGS, CLASSIFICATION AND INSPECTION OF
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    SAE AS 7928 : 2011 TERMINALS, LUG: SPLICES, CONDUCTOR: CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR
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    MIL-STD-202 Revision H:2015 ELECTRONIC AND ELECTRICAL COMPONENT PARTS
    MIL-DTL-15024 Revision F:1997 Plates and Tags for Identification of Equipment, General Specification for
    SAE AMS M 3171 : 1998 MAGNESIUM ALLOY, PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION ON
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