
The Honda Worldwide Aircraft Engine Site: Technological details and products using Honda's aircraft engines
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| Takeoff thrust | 2,095 lbf |
| Bypass ratio | 2.9 |
| Engine pressure ratio | 24 |
| Thrust/weight ratio | Over 5 |
| Maximum diameter | 21.2 in. |
| Length** | 44 in. |
| Weight | Less than 400 lbs. |
| Noise | Achieves CFR36 Stage 4 requirements with substantial margin |
| Specific fuel consumption (cruise, lb. fuel/hr/lbf) |
Less than 0.7 |
| Time between overhaul | 5,000 hrs. |
| Control | Dual-channel FADEC |
| * | Specifications subject to change without notice |
| ** | Length does not include centerbody |