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  • MIL-DTL-7034 Revision F:2005

    Current The latest, up-to-date edition.

    PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s):  PDF

    Language(s): 

    Published date:  01-04-2005

    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)

    Describes the requirements for single grove pulleys with antifriction bearings.

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

    Committee FSC 1640
    Development Note Supersedes MIL P 7034 (D) (01/2000) F NOTICE 1 - Notice of Validation. (02/2015) NEW CHILD NOT 2 IS NOW ADDED
    Document Type Standard
    Product Note NEW CHILD NOT 2 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-DTL-7034-3 Revision A:2005 PULLEY, GROOVE, HEAVY DUTY, CONTROL, AIRCRAFT
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    TT-P-1757 Revision B:1997 PRIMER COATING, ALKYD BASE, ONE COMPONENT
    SAE AS 7949 : 2004 BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD
    MIL-DTL-83420 Revision P:2017 WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE AMS 4037 : 2014 ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
    SAE AS 21443 : 2012 BEARING, BALL, AIRFRAME, ANTI-FRICTION, PULLEY
    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    SAE AS 27640 : 2012 BEARING, BALL, AIRFRAME, ANTI-FRICTION, HEAVY DUTY
    MIL-DTL-7034-4 Revision A:2005 PULLEY, CONTROL, ANTI-FRICTION BEARING, AIRCRAFT
    MIL-PRF-81322 Revision G:2005 GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395
    MIL-DTL-7034-1 Revision A:2005 PULLEY, GROOVE, SECONDARY CONTROL, AIRCRAFT
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL-DTL-7034-2 Revision A:2005 PULLEY, GROOVE, FLIGHT CONTROL, AIRCRAFT
    SAE AMS QQ A 225/6 : 1998 ALUMINUM ALLOY, 2024, BAR, ROD, AND WIRE; ROLLED, DRAWN, OR COLD FINISHED
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