• SAE AMS 5544 : 2014

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED

    Available format(s):  Hardcopy, PDF

    Superseded date:  17-07-2020

    Language(s):  English

    Published date:  01-01-2014

    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. ACKNOWLEDGMENT
    7. REJECTIONS
    8. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.

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

    Committee AMS-F
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE AMS 1551 : 2008 CLEANER, TURBINE ENGINE GAS PATH AQUEOUS TYPE
    MIL-PRF-8188 Revision D:1997 CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL L 87100 : 0 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE
    MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    SAE MA 1943 : 2012 NUTS, SELF-LOCKING, UNS N07001, 760 DEGREE C, 1100 MPA AND 1210 MPA, PROCUREMENT SPECIFICATION FOR, METRIC
    MIL-PRF-7808 Revision L:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL-PRF-87100 Revision A:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE
    SAE AMS 1548 : 2017 CLEANER, TURBINE ENGINE GAS PATH, SOLVENT EMULSION TYPE
    SAE AMS 2774 : 2016 HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS
    SAE ARP 1755 : 2000 EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD

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

    SAE AMS 2269 : 2006 CHEMICAL CHECK ANALYSIS LIMITS, NICKEL, NICKEL ALLOYS, AND COBALT ALLOYS
    ASTM E 384 : 2017 : REDLINE Standard Test Method for Microindentation Hardness of Materials
    SAE AMS 2371 : 2016 QUALITY ASSURANCE SAMPLING AND TESTING, CORROSION AND HEAT-RESISTANT STEELS AND ALLOYS, WROUGHT PRODUCTS AND FORGING STOCK
    SAE AS 4194 : 2012 SHEET AND STRIP, SURFACE FINISH NOMENCLATURE
    SAE AMS 2262 : 2013 TOLERANCES, NICKEL, NICKEL ALLOY, AND COBALT ALLOY SHEET, STRIP AND PLATE
    SAE AMS 2807B : 2012 IDENTIFICATION, CARBON AND LOW-ALLOY STEELS, CORROSION AND HEAT-RESISTANT STEELS AND ALLOYS, SHEET, STRIP, PLATE, AND AIRCRAFT TUBING
    ASTM E 290 : 2014 : REDLINE Standard Test Methods for Bend Testing of Material for Ductility
    ASTM E 354 : 2014 : REDLINE Standard Test Methods for Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys
    ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS
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