Titan X-370 Experimental Engine

The Titan X-370 Experimental Engine is the ultimate choice for builders seeking maximum power and flexibility for their aircraft. Delivering between 195 to 205 horsepower, the X-370 is a stroked version of the proven 360 platform, designed to offer more power without significantly increasing weight or size.

The Titan 370 series offers a range of horsepower and incredible low-end torque. Built with the same OEM quality standards as Continental’s certified engines, the X-370 provides a perfect balance of performance, reliability, and customization. Whether you are aiming for enhanced speed, improved climb rates, or efficient fuel consumption, the Titan X-370 is engineered to elevate your flying experience to new heights.

Titan X-370 Experimental Engine

Airframe

Experimental

Performance

185 to 195 HP

Est Dry Weight

277 to 296 lbs

Fuel Delivery

Carb/Injection

FAA and PMA Approved Parts

The Titan X-370 engine is built predominantly with FAA and PMA-approved parts, ensuring that you receive a powerplant that meets stringent aviation standards. The X-370 incorporates many parts from the Prime line, which is known for its reliability and quality. These parts are often enhanced with modern improvements over the original designs, offering superior performance, durability, and safety. Backed by Continental’s legacy of over 120 years in general aviation manufacturing, the Titan X-370 combines the best of certified and experimental technologies to deliver a robust and dependable engine. weight-saving configuration, the X-340 provides the flexibility to match your vision.

Understanding the Difference: The X-370 vs Other titan™ engines

The Titan X-370 engine is essentially a stroked version of the popular 360 engine, much like how the X-340 relates to the 320. By lengthening the crankshaft stroke of the 360, the X-370 produces between 195 and 205 horsepower, offering more power while retaining the same core technology and design. The primary physical difference is that the X-370 has a slightly wider deck—about an inch and a half—to accommodate the longer stroke, but it remains nearly identical to the 360 in other respects. This design allows for easy integration into aircraft, particularly in the RV market, where the 360 engine is already prevalent. Builders and engineers can seamlessly replace a 360 with the X-370 without any significant modifications, making it a convenient and powerful upgrade option for experimental aircraft like the RV-8.

Weight Advantages

This engine offers significant weight advantages, thanks to innovative design and material choices. By tapering the barrel of the cylinder as it narrows towards the case, approximately a pound and a half is saved per cylinder, resulting in a total weight reduction of six pounds on a four-cylinder engine. Additionally, using magnesium for the sump instead of aluminum reduces weight by another three to three and a half pounds. For engines equipped with electronic ignition, further weight savings are achieved by using magnesium for the accessory case, eliminating the need for mag drive gears and vacuum pump drive gears. This meticulous attention to weight reduction can result in up to 13 pounds saved at the back end of the engine, enhancing overall performance and fuel efficiency.

TECHNICAL DATA

Certified fuels

100/100LL

BORE

length

Displacement

Power

Stroke

Comp. Ratio

CONFIGURATION type

recommended tbo

2000 hrs

Speed

Height

Width

Further technical information can be found in the engine data sheet.

Highlighted Applications

Rans S-21 (Titan X-370)

Zenith CH-750 (Titan X-370)

Vans Aircraft RV-8 (Titan X-370)

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