Aircraft with engine assembly mounted to wheel well

An assembly for an aircraft having a propeller, the assembly comprising:

• a wheel well configured for receiving a retracted landing gear, the wheel well including walls and a closable bottom opening for deploying the landing gear therethrough;
• an engine assembly including:
• a rotary internal combustion engine in driving engagement with an engine shaft, the engine shaft configured for driving engagement with the propeller, and
• a gearbox drivingly engaged to the engine shaft;
• and
• a mount assembly for supporting the engine assembly, the mount assembly interconnecting a casing of the gearbox to at least one of the walls of the wheel well, the mount assembly having upper and lower yokes connected to the casing of the gearbox, the lower yoke connected to the at least one of the walls of the wheel well, the upper yoke configured to be connected to a structure of the aircraft, wherein the walls of the wheel well include a top wall and side walls extending upwardly beyond the top wall, the upper yoke connected to a support upwardly spaced apart from the top wall and resting on top edges of the side walls, the support configured to be connected to a structure of the aircraft.