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  • SAE ARP 5935 : 2013

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    USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  25-10-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. RECOMMENDATIONS

    Abstract - (Show below) - (Hide below)

    Electrolytically deposited chrome plate is the current standard surface treatment for landing gear component interface surfaces that require good wear resistance and corrosion protection.

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

    Committee A-5
    Document Type Standard
    Publisher SAE International
    Status Current
    Supersedes

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

    SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
    SAE AIR 1594 : 2010 PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS
    SAE AS 4941 : 2015 AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
    SAE AS 4716C: 2017 GLAND DESIGN, O-RING AND OTHER SEALS

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

    SAE AMS 2447 : 2012 COATING, THERMAL SPRAY, HIGH VELOCITY OXYGEN/FUEL PROCESS
    SAE AMS QQ C 320 : 2000 CHROMIUM PLATING (ELECTRODEPOSITED)
    SAE AMS 7881 : 2013 TUNGSTEN CARBIDE-COBALT POWDER, AGGLOMERATED AND SINTERED
    SAE AMS 2449 : 2004 GRINDING OF HVOF SPRAYED TUNGSTEN CARBIDE COATINGS APPLIED TO HIGH STRENGTH STEELS
    SAE ARP 4462 : 1991 BARKHAUSEN NOISE INSPECTION FOR DETECTING GRINDING BURNS IN HIGH STRENGTH STEEL PARTS
    SAE AMS 7882 : 2013 TUNGSTEN CARBIDE-COBALT CHROME POWDER, AGGLOMERATED AND SINTERED
    SAE AMS 2649 : 2013 ETCH INSPECTION OF HIGH STRENGTH STEEL PARTS
    SAE AMS 2448 : 2016 APPLICATION OF TUNGSTEN CARBIDE COATINGS ON ULTRA HIGH STRENGTH STEELS HIGH VELOCITY OXYGEN/FUEL PROCESS
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