• SAE AIR 1899 : 2001

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    AEROSPACE MILITARY AIRCRAFT HYDRAULIC SYSTEM CHARACTERISTICS

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    Published date:  03-01-2001

    Publisher:  SAE International

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

    1 SCOPE
    1.1 Purpose
    1.2 Field of Application
    2 APPLICABLE DOCUMENTS
    2.1 SAE Publications
    2.2 U.S. Government Publications
    3 ATTACK AIRPLANES
    3.1 Northrop Grumman A-6A
    3.2 Northrop Grumman A-7E
    3.3 Fairchild A-10A
    3.4 Lockheed F-117A
    4 FIGHTER AIRPLANES
    4.1 Northrop Grumman F-5E
    4.2 Northrop Grumman F-14A
    4.3 Boeing F-15A
    4.4 Lockheed Martin F-16A
    4.5 Boeing F/A-18A
    4.6 MRCA
    5 BOMBERS
    5.1 Boeing B-1B
    5.2 Northrop Grumman B-2A
    6 ANTI-SUB - FIXED WING AIRCRAFT
    6.1 Lockheed Martin P-3
    6.2 Lockheed Martin S-3A
    7 TRANSPORT AIRPLANES
    7.1 Lockheed Martin C-5A
    7.2 Boeing C-17A Globemaster III
    7.3 Lockheed Martin C-130
    7.4 Lockheed Martin C-141B
    8 HELICOPTERS
    8.1 Bell 214
    8.2 Sikorsky CH-53E
    8.3 Sikorsky S-76
    9 BOATS
    9.1 M-161 Boat

    Abstract - (Show below) - (Hide below)

    Provides hydraulic system information to military vehicle system and component designers in order to assist them in future aircraft fluid power system designs. Information may be used to find similar type systems, components and materials which will in turn help solve specific problems and lower costs.

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

    Committee A-6A2
    Document Type Revision
    Publisher SAE International
    Status Current

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

    SAE AS 5586 : 2005 GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS
    SAE ARP 1280 : 2014 AEROSPACE - APPLICATION GUIDE FOR HYDRAULIC POWER TRANSFER UNITS
    SAE AIR 5696 : 2013 AEROSPACE FLUID POWER - FAA REGULATORY HISTORY - TRANSPORT AIRPLANE HYDRAULIC SYSTEMS
    SAE ARP 4940 : 2014 APPLICATION GUIDE FOR AEROSPACE HYDRAULIC MOTORS
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