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propelled by


Lycoming
TIO-540-J2BD

Turbocharged
350 HP

 


click on image to enlarge

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.


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