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Name Family Aircraft Engine Manufacturer Aircraft Engine Type Comment Dry Weight Full Weight Diameter Length Height Width Control System List Price Program launch FETT First Flight Certification Production Start Production End Service End Number Built Fan Stages Fan Blades Fan Technology Geared Fan Gear Reduction Ratio Low-Pressure Compressor Stages Low-Pressure Compressor Technology Intermediary-Pressure Compressor Stages Intermediary-Pressure Compressor Technology High-Pressure Compressor Stages High-Pressure Compressor Technology Combustion Chamber High Pressure Compressor Stages High-Pressure Turbine Technology Intermediary-Pressure Turbine Stages Intermediary-Pressure Turbine Technology Low-Pressure Turbine Stages Low-Pressure Turbine Technology Afterburner Streams Bypass Ratio MaximumTakeoffThrust MaximumContinuousThrust MaximumClimbThrust MaximumCruiseThrust FlightIdleThrust ApproachIdleThrust GroundIdleThrust OEU30sec OEI2min OEI2min5 OEIContinuous OverallPressureRatio FanPressureRatio CompressorPressureRatio T3 T4 T9 BPMaxRotationSpeed IPMaxRotationSpeed HPMaxRotationSpeed MaxRotatingDiameter ThrustToWeight SpecificFuelConsumption Fuel TBO Modules HydrocarbonTakeOff HydrocarbonClimbOut HydrocarbotApproach HydrocarbonIdle HydrocarbonUnitaryAverage HydrocarbonUnitarySigma HydrocarbonUnitaryRange HydrocarbonUnitaryCharacteristic HydrocarbonUnitaryCharacteristictoRegulatory HydrocarbonLTO CarbonMonoxideTakeOff CarbonMonoxideClimbOut CarbonMonoxideApproach CarbonMonoxideIdle CarbonMonoxideUnitaryAverage CarbonMonoxideUnitarySD CarbonMonoxideUnitaryRange CarbonMonoxideUnitaryCharacteristic CarbonMonoxideUnitaryCharacteristictoRegulatory NOxTakeOff NOxClimbOut NOxApproach NOxIdle NOxUnitaryAverage NOxUnitarySD NOxUnitaryRange NOxUnitaryCharacteristic NOxUnitarytoStandard NOxUnitarytoCAEP2 NOxUnitarytoCAEP4 NOxUnitarytoCAEP6 NOxUnitarytoCAEP8 NOxLTO SmokeTakeOff SmokeClimbOut SmokeApproach SmokeIdle SmokeMax SmokeSigma SmokeRange SmokeCharacteristic SmokeCharacteristictoRegulatory FuelFlowTakeOff FuelFlowClimbout FuelFlowApproach FuelFlowIdle FuelLTO FuelVentingCompliant
TFE731-1100 Honeywell Turbofan Yes No 2 NA
D-30KU-154 Aviadvigatel Turbofan No No 2 2.30 107.50 17.00 0.40 0.50 1.90 12.70 40.80 5.00 53.10 270.90 4389.00 3.00 3.60 18.20 257.00 21.80 292.80 248.10 14.50 11.60 5.10 2.90 36.70 2.50 40.40 54.50 68.20 87.40 99.30 127.00 4000.00 1.42 1.10 0.42 0.21 629.00 No
NK-86A Kuznetsov Design Bureau Turbofan No No 2 1.13 130.47 13.20 0.20 0.20 2.20 15.30 45.20 69.60 355.20 5988.00 1.80 2.20 7.80 120.70 148.20 125.60 15.70 12.40 5.80 3.10 46.10 53.40 80.50 100.60 133.20 151.40 201.80 6106.00 2.05 1.70 0.60 0.24 821.00 No
TFE731-2-2B Allied Signal Turbofan Yes Planetary gear, 5 planet gears, roller bearings 1.80 No 2 2.64 15.60 13.90 0.11 0.13 4.26 20.04 53.40 50-58 62.30 317.60 823.00 1.39 2.03 22.38 169.40 161-177 183.20 155.30 15.25 13.08 5.90 2.82 40.50 39-43 42.90 63.30 79.10 75.90 76.20 78.20 630.00 0.21 0.17 0.07 0.02 85.00 No
AE3007A1E Rolls-Royce Turbofan No Type 3 No 2 4.72 37.16 19.06 0.03 0.03 0.03 3.52 7.10 10.93 55.80 264.00 0.77 0.64 5.63 81.18 99.64 84.40 17.17 14.91 7.42 4.26 40.38 46.81 59.90 74.90 77.60 78.90 84.80 1501.00 0.01 0.01 0.01 0.01 0.01 0.01 0.00 0.41 0.34 0.12 0.05 165.00 No
AE3007A2 Rolls-Royce Turbofan No Type 3 (reduced emissions) No 2 4.79 42.23 20.20 0.00 0.00 0.00 1.71 3.45 5.32 27.12 146.00 0.71 0.74 4.08 73.29 89.96 76.24 18.61 15.99 7.90 4.39 43.03 49.88 62.04 77.55 81.66 83.78 90.80 1817.00 0.01 0.01 0.01 0.01 0.01 0.01 0.04 0.47 0.39 0.14 0.06 189.00 No
AE3007C2 Rolls-Royce Turbofan No Type 2 No 2 4.99 32.73 17.44 0.00 0.01 0.22 2.57 5.94 9.15 46.68 194.80 0.00 0.00 1.97 53.40 65.55 55.55 21.25 18.11 6.56 3.14 40.54 46.99 70.25 78.44 80.12 80.88 86.15 1326.30 0.01 0.01 0.01 0.01 0.01 0.01 0.04 0.33 0.27 0.10 0.05 147.00 Yes
PW814GA Pratt & Whitney Canada Turbofan No TALON X No 2 5.66 68.63 33.87 0.00 0.00 0.02 0.05 0.10 0.07 0.0-0.2 0.10 0.50 6.00 0.00 0.00 1.76 23.10 1.53 20.8-24.7 24.70 20.90 23.26 17.94 11.46 6.25 46.10 1.19 45.0-49.5 48.40 44.90 56.20 61.70 66.20 73.50 3168.00 0.30 0.20 0.20 0.20 0.30 0.11 0.0-0.5 0.30 1.10 0.67 0.55 0.19 0.07 256.20 Yes
PW815GA Pratt & Whitney Canada Turbofan No TALON X No 2 5.60 71.22 35.00 0.00 0.00 0.02 0.05 0.10 0.07 0.0-0.2 0.10 0.51 7.00 0.00 0.00 1.50 21.90 1.38 19.9-23.3 23.40 19.80 24.88 18.89 11.47 6.41 48.10 1.11 47.0-51.7 50.50 45.91 57.39 63.05 67.88 75.37 3422.00 0.30 0.20 0.20 0.20 0.30 0.11 0.0-0.5 0.30 1.15 0.70 0.57 0.20 0.07 264.00 Yes
GEnx-1B54/P2 GE Aircraft Engines Turbofan No TAPS No 2 9.39 255.30 35.50 0.02 0.02 0.06 0.58 0.77 0.07 0.70-0.83 1.19 6.07 197.00 0.32 1.73 2.81 23.20 0.09 23.11-23.29 28.48 24.14 17.22 11.54 9.27 4.66 24.97 0.09 24.88-25.06 28.94 26.07 32.59 37.10 41.37 47.35 6374.00 0.00 0.00 0.07 0.10 0.58 0.34 0.35-0.97 0.75 4.10 1.88 1.55 0.53 0.20 727.00 Yes