This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and lock-ring wheel designs for FAA Part 25 and military aircraft main wheels (not required for any nose wheels or main wheels on FAA Part 23, 27 or 29 applications).
SAE ARP1786C-2019 history
2019SAE ARP1786C-2019 Wheel Roll on Rim Criteria for Aircraft Applications
2013SAE ARP1786C-2013 Wheel Roll on Rim Criteria for Aircraft Application
2010SAE ARP1786B-2010 Wheel Roll on Rim Criteria for Aircraft Application
2005SAE ARP1786B-2005 Wheel Roll on Rim Criteria for Aircraft Application
2000SAE ARP1786A-2000 Wheel Roll on Rim Criteria for Aircraft Application
2000SAE ARP1786-2000 Wheel Roll on Rim Criteria for Aircraft Application
1994SAE ARP1786-1994 WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION
1984SAE ARP1786-1984 Wheel Roll on Rim Criteria for Aircraft Application