Wheel Roll on Rim Criteria for Aircraft Applications
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).
Rationale: This document is intended to provide recommended practice for aircraft wheel roll on rim design criteria and validation test. This revision C is an update to revision B and incorporates an updated reference section.
Landing gearWheel wellsBraking systemsAir brakesBrake componentsElectronic braking systemsTires and tractionWheelsTire pressure monitoring systemsOn-board diagnostics (OBD)Maintainability and supportabilityBearingsSafetyTests and TestingMilitary aircraft
Also known as: SAE ARP 1786
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