Cleveland Wheel Assembly 40-412

The Cleveland Wheel & Brake Systems 40-412 is a main wheel assembly for aircraft landing-gear installations. Cleveland describes its main wheel assemblies as supporting the tyre and aircraft load during landing and ground manoeuvring, while transmitting braking forces to the ground.

This 40-412 assembly has an internal, flange-driven wheel interface and a tubeless configuration. Cleveland’s split-rim wheel design uses inner and outer wheel halves secured with through-bolts, supporting tyre installation and wheel maintenance.

• Manufacturer: Cleveland Wheel & Brake Systems
• Manufacturer part number: 40-412
• Wheel interface: Internal – flange driven
• Tyre configuration: Tubeless
• Rim designation: 14.5 × 5.5-6 (approximately 368 × 140-152 mm)
• Matched brake reference: 030-23800
• Finish: Untinted white
• Manufacturer-listed certification: FAA TSO-C26c
• Recorded item weight: 4.536 kg

For correct installation and continued airworthiness, verify the part number, wheel/brake configuration and approved applicability against the aircraft maintenance documentation and current Cleveland technical publications before installation.

Product documentation and technical resources are available from Cleveland Wheel & Brake Systems.