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SAE ARP 5935 : 2013

Current

Current

The latest, up-to-date edition.

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

€79.68
Excluding VAT

1. SCOPE
2. REFERENCES
3. RECOMMENDATIONS

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

Committee
A-5
DocumentType
Standard
Pages
7
PublisherName
SAE International
Status
Current
Supersedes

SAE AS 4941 : 2015 AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
SAE AIR 1594 : 2010 PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS
SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
SAE AS 4716C: 2017 GLAND DESIGN, O-RING AND OTHER SEALS
SAE ARP1311D:2018(R2023) Landing Gear Structures and Mechanisms

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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