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Lycoming TIO-540-J2BD Turbocharged 350 HP

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The Textron Lycoming aircraft engine model TIO-540-J2BD is a direct drive, six cylinder, fuel injected, horizontally opposed, turbocharged, air cooled engine with up exhaust and cross-flow cylinder heads.

Detail Specifications

• 350 HP @ 2575 to 15,000 ft.

• 260 HP @ 2575 to 20,000 ft.

• 210 HP @ 2200 economy cruise

• AiResearch Turbocharger

• Automatic Servo Operated Wastegate Turbo Controller

• Bendix Fuel Injection & Magneto

• Dynamic Crankshaft Counterweights

Advantages Over The IO-520 Engine

• 65 More Horsepower (continuous)@ Sea Level 

• 40% More Horsepower @ 10,000 ft.

• 350 HP Continuous vs. 285 HP

• Reduced Vibration & Noise Due To Lower RPM Range

• 350 HP To 15,000 ft.

• Higher TBO Of Up To 2000 Hours*

• No VAR Crankshaft AD's

• Current Production Engine

• Best Support In The Industry

• Top End Typically Goes To TBO

*1800 hrs standard with 200 hr extension if operated continuously at 40 hrs per month.