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  • SAE AMS4897D : 2016

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI

    Available format(s):  Hardcopy, PDF

    Superseded date:  29-12-2020

    Language(s):  English

    Published date:  13-09-2016

    Publisher:  SAE International

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

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. TECHNICAL REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PREPARATION FOR DELIVERY
    6. ACKNOWLEDGEMENT
    7. REJECTIONS
    8. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness.

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

    Committee AMS G
    Document Type Revision
    Publisher SAE International
    Status Superseded
    Superseded By

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

    09/30199811 DC : 0 BS EN 4632-006 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 6: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    I.S. EN 4632-006:2013 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS
    BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
    NFL 06 380-24 : 2008 AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    EN 4632-006:2013 Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
    PREN 4632-006 : DRAFT 2008 WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    UNI EN 4632-006 : 2014 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS

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

    ASTM E 2371 : 2013 Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology)
    SAE AMS 2368 : 2017 SAMPLING AND TESTING OF WROUGHT TITANIUM RAW MATERIAL EXCEPT FORGINGS AND FORGING STOCK
    SAE AMS 2809 : 2007(R2011) IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS
    SAE AMS 2750 : 2012 PYROMETRY
    ASTM E 1409 : 2013 : REDLINE Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion
    SAE ARP 1917 : 2002 CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS
    SAE AMS 2642 : 2016 STRUCTURAL EXAMINATION OF TITANIUM ALLOYS ETCH-ANODIZE INSPECTION PROCEDURE
    SAE AS 6279 : 2016 STANDARD PRACTICE FOR PRODUCTION, DISTRIBUTION, AND PROCUREMENT OF METAL STOCK
    SAE AMS 2249 : 2013 CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS
    SAE AS 4194 : 2012 SHEET AND STRIP, SURFACE FINISH NOMENCLATURE
    SAE AMS 2242 : 2014 TOLERANCES, CORROSION AND HEAT RESISTANT STEEL, IRON ALLOY, TITANIUM, AND TITANIUM ALLOY SHEET, STRIP, AND PLATE
    ASTM E 290 : 2014 : REDLINE Standard Test Methods for Bend Testing of Material for Ductility
    ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS
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