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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
Trent 970B-84 Rolls-Royce Turbofan No Phase5 Tiled No 2 8.38 352.90 39.35 0.00 0.09 0.07 0.04 0.16 0.05 0.13-0.21 0.18 0.90 56.00 0.33 0.31 1.05 15.50 1.63 14.13-17.3 16.77 14.20 41.34 31.30 12.37 5.57 52.68 1.94 50.92-54.77 55.80 47.00 58.80 65.10 71.90 81.10 18591.00 6.10 6.30 3.30 0.60 7.10 2.70 5.2-9 8.30 49.70 2.74 2.26 0.75 0.26 1001.00 Yes
Trent 972E-84 Rolls-Royce Turbofan No Phase5 Tiled No 2 8.41 345.90 38.68 0.01 0.11 0.07 0.04 0.17 0.05 0.13-0.24 0.20 1.00 60.00 0.32 0.31 1.10 16.06 1.69 14.64-17.93 17.37 14.70 39.78 30.36 12.23 5.51 51.16 1.92 49.39-53.2 54.19 46.20 57.70 64.20 71.00 80.30 17699.00 6.10 6.40 3.20 0.60 7.10 2.70 5.2-9 8.30 49.40 2.67 2.21 0.74 0.26 983.00 Yes
CF34-8C1 GE Aircraft Engines Turbofan No No 2 5.13 56.36 23.03 0.02 0.02 0.06 0.08 0.20 0.00 0.2-0.2 0.30 1.50 13.00 0.41 0.50 2.91 51.30 1.04 50.1-52.0 63.00 53.40 14.67 12.82 11.10 4.31 37.20 0.74 36.6-38.0 43.10 50.10 62.60 68.70 72.50 80.60 2120.00 5.33 1.48 0.00 0.00 5.33 1.00 4.6-6.5 6.90 24.90 0.60 0.49 0.17 0.07 239.00 No
Trent 553-61 Rolls-Royce Turbofan No Phase5 Tiled No 2 7.50 251.90 35.19 0.02 0.01 0.04 0.14 0.20 0.17 0.1-0.4 0.30 1.50 60.00 0.18 0.44 0.66 15.80 1.20 14.6-16.9 17.00 14.40 40.55 30.98 11.37 5.96 57.30 1.48 55.9-58.8 60.70 55.00 68.70 78.40 87.50 100.30 14444.00 4.29 4.15 1.95 0.91 4.90 2.97 2.8-8.4 5.40 29.30 2.11 1.73 0.60 0.23 820.00 Yes
Trent 970-84 Rolls-Royce Turbofan No Phase5 Tiled No 2 7.50 334.70 38.97 0.00 0.00 0.00 0.20 0.20 0.09 0.2-0.3 0.40 1.90 81.00 0.40 0.20 1.40 19.30 0.08 19-19.2 23.60 20.00 37.20 29.10 11.40 5.10 49.50 0.77 49-50.5 57.40 48.70 60.80 67.60 74.60 84.30 16555.00 4.10 4.70 2.60 0.70 5.23 1.20 4.1-6.5 6.80 39.60 2.60 2.20 0.70 0.30 980.00 No
V2531-E5 International Aero Engines Turbofan No Floatwall No 2 4.52 134.80 32.30 0.01 0.02 0.09 0.07 0.20 0.30 1.50 28.00 0.39 0.41 1.57 18.60 21.20 18.00 32.17 24.28 11.14 5.58 55.80 61.40 58.70 73.40 85.80 96.70 112.20 7521.00 2.30 6.00 6.30 1.30 9.40 11.10 50.90 1.33 1.08 0.39 0.14 517.00 Yes
PW1127G1-JM Pratt & Whitney Turbofan Yes TALON X No 2 12.20 120.44 32.11 0.03 0.03 0.04 0.11 0.20 0.30 1.53 21.00 0.22 0.32 5.49 27.80 34.10 28.90 17.76 14.18 8.85 6.55 26.90 31.20 29.94 37.42 43.81 49.38 57.42 3244.00 1.40 0.30 0.36 0.56 1.40 1.80 8.00 0.80 0.66 0.23 0.09 316.60 Yes
PW1127G-JM Pratt & Whitney Turbofan Yes TALON X No 2 12.20 120.44 32.11 0.03 0.03 0.04 0.11 0.20 0.30 1.53 21.00 0.22 0.32 5.49 27.80 34.10 28.90 17.76 14.18 8.85 6.55 26.90 31.20 29.94 37.42 43.81 49.38 57.42 3244.00 1.40 0.30 0.36 0.56 1.40 1.80 8.00 0.80 0.66 0.23 0.09 316.60 Yes
BR700-715C1-30 Rolls-Royce Deutschland Turbofan No No 2 4.55 95.33 32.01 0.00 0.00 0.00 0.14 0.23 0.17-0.29 0.40 1.80 22.00 0.75 0.78 3.06 27.77 27.22-28.85 34.10 28.90 31.39 22.41 11.55 5.72 55.71 55.26-56.04 64.60 62.10 77.60 90.90 102.50 119.30 5314.00 3.98 3.09 1.09 0.87 3.98 3.61-4.26 5.10 21.30 0.98 0.80 0.27 0.10 370.00 No
V2533-A5 International Aero Engines Turbofan No No 2 4.46 140.56 33.44 0.05 0.04 0.05 0.10 0.25 0.40 2.00 35.00 0.46 0.52 1.65 16.00 19.60 16.60 36.48 28.67 10.83 5.24 61.60 71.40 66.80 83.50 96.60 108.40 125.30 8646.00 4.70 6.20 4.80 2.40 9.00 11.60 53.80 1.43 1.14 0.39 0.14 517.00 No