• MIL E 7016 : F

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    ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF

    Available format(s):  Hardcopy, PDF

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    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Prepares (ac) and (dc) electric load power source capacity analyses for aircraft.

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

    Committee FSC 1680
    Development Note F NOTICE 1 - Notice of Validation. (12/2009) F NOTICE 2 - Notice of Validation. (09/2014)
    Document Type Standard
    Product Note NEW CHILD NOT 3 2019 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    MIL D 8684 : B DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS
    PREN 3830 : 200P1 AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS
    SAE ARP 4404 : 2013 AIRCRAFT ELECTRICAL INSTALLATIONS
    AFGS 87219 : B ELECTRICAL POWER SYSTEMS, AIRCRAFT
    SAE ARP 4404 : 2013 : R2019 AIRCRAFT ELECTRICAL INSTALLATIONS
    MIL D 8685 : B DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    MIL STD 1822 : A NUCLEAR COMPATIBILITY CERTIFICATION OF NUCLEAR WEAPON SYSTEMS, SUBSYSTEMS AND SUPPORT EQUIPMENT
    MIL D 23222 : A DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    DIN EN 3830:1995-08 (Draft) AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS
    JSSG 2009 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    DIN 29571-3:1990-10 AEROSPACE - ELECTRICAL EQUIPMENT - ANALYSIS OF LOAD AND POWER SOURCE CAPACITY
    ADS-63-SP : 2001 AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS
    MIL E 25499 : C ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR
    MIL T 18232 : B TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR
    SAE ARP 4729 : 2017 DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM
    MIL D 8708 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL STD 1606 : A TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS
    ADS-65-HDBK : 2004 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS

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

    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
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