• MIL T 81259 : B

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR

    Available format(s):  Hardcopy, PDF

    Superseded date:  09-22-2016

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Outlines the design and construction prerequisites for Naval Aircraft Tie Down Fittings, Attachment Points, and related aircraft carry through structures.

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

    Committee FSC 15GP
    Development Note B NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 81259. (09/2016)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

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

    SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
    JSSG 2001 : B AIR VEHICLE
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    JSSG 2009 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    MIL L 87139 : 0 LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503
    SAE AIR 1489 : 2012 AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY

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

    DOD STD 100 : C NOTICE 6 ENGINEERING DRAWING PRACTICES
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL STD 805 : B TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
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