• A high thrust-to-weight ratio allows for uncommonly long range and large payload.
• Specialized fluid dynamics software optimizes airflow within the compact engine, maximizing performance.
• The engine's simple, high-performance combustion chamber keeps emission levels well within requirements for compact jets.
• Honda created the first ultra-compact Full Authority Digital Electronic Control (FADEC) system for this class of engine. FADEC provides superior operation and reliability without variable mechanisms.

• Engine type: 2-spool turbofan, 1-stage fan, 2-stage compressor, 2-stage turbine
• Take-off thrust: 1,880 lbf
• Bypass ratio: 2.9
• Engine pressure ratio: 24
• Thrust/weight ratio: More than 5
• Maximum diameter: 21.2 inches
• Length**: 44 inches
• Weight: Less than 400 lb
• Noise: Achieves CFR36 stage 4 requirements with substantial margin
• Specific fuel consumption: Less than 0.70 lb/hr/lbf
• Control: Dual-channel FADEC

* Specifications provided by GE-Honda Aero Engines, LLC.
** Length does not include center body.