SAE ARP1786B-2005
Wheel Roll on Rim Criteria for Aircraft Application

Standard No.

SAE ARP1786B-2005

Release Date

2005

Published By

SAE - SAE International

Status

Be replaced

Replace By

SAE ARP1786B-2010

Latest

SAE ARP1786C-2019

Scope

Purpose: 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 split wheel hub and lock-ring wheel designs. Applicability: This document sets forth minimum roll performance capability for a main landing gear wheel to be rolled without tire installed. The recommended test requirements establish a laboratory dynamometer demonstration level to equate with satisfactory experience on aircraft.

SAE ARP1786B-2005 history

• 2019 SAE ARP1786C-2019 Wheel Roll on Rim Criteria for Aircraft Applications
• 2013 SAE ARP1786C-2013 Wheel Roll on Rim Criteria for Aircraft Application
• 2010 SAE ARP1786B-2010 Wheel Roll on Rim Criteria for Aircraft Application
• 2005 SAE ARP1786B-2005 Wheel Roll on Rim Criteria for Aircraft Application
• 2000 SAE ARP1786A-2000 Wheel Roll on Rim Criteria for Aircraft Application
• 2000 SAE ARP1786-2000 Wheel Roll on Rim Criteria for Aircraft Application
• 1994 SAE ARP1786-1994 WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION
• 1984 SAE ARP1786-1984 Wheel Roll on Rim Criteria for Aircraft Application