SAE ARP 5935 : 2013
Current
The latest, up-to-date edition.
USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS
Hardcopy , PDF
English
25-10-2013
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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