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Trent 1000-J2 ✕
EASA ID 12RR067
Aircraft Engine Manufacturer Rolls-Royce
Aircraft Engine Type Turbofan
Geared Fan No
Combustion Chamber Phase5 Tiled
Afterburner No
Streams 2
Bypass Ratio 9.04
Overall Pressure Ratio 46.08
Maximum Takeoff Thrust (kN) 350.9
Hydrocarbon Take Off (g/kg fuel) 0
Hydrocarbon Climb Out (g/kg fuel) 0
Hydrocarbon Approach (g/kg fuel) 0
Hydrocarbon Idle (g/kg fuel) 0.02
Hydrocarbon Unitary Average (g/kN) 0.03
Hydrocarbon Unitary Sigma (g/kN) 0.03
Hydrocarbon Unitary Range (g/kN) 0-0.07
Hydrocarbon Unitary Characteristic (g/kN) 0.03
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 0.15
Hydrocarbon LTO (g) 9.01
Carbon Monoxide Take Off (g/kg fuel) 0.43
Carbon Monoxide Climb Out (g/kg fuel) 0.49
Carbon Monoxide Approach (g/kg fuel) 0.62
Carbon Monoxide Idle (g/kg fuel) 6.8
Carbon Monoxide Unitary Average (g/kN) 8.5
Carbon Monoxide Unitary SD (g/kN) 2.32
Carbon Monoxide Unitary Range (g/kN) 5.71-11.08
Carbon Monoxide Unitary Characteristic (g/kN) 9.1
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 7.71
NOx Take Off (g/kg fuel) 58.04
NOx Climb Out (g/kg fuel) 43.07
NOx Approach (g/kg fuel) 14.06
NOx Idle (g/kg fuel) 5.91
NOx Unitary Average (g/kN) 67.06
NOx Unitary SD (g/kN) 1.04
NOx Unitary Range (g/kN) 66.09-68.25
NOx Unitary Characteristic (g/kN) 70.47
NOx Unitaryto Standard (% of limit) 53.32
NOx Unitaryto CAEP2 (% of limit) 66.65
NOx Unitaryto CAEP4 (% of limit) 71.07
NOx Unitaryto CAEP6 (% of limit) 77.34
NOx Unitaryto CAEP8 (% of limit) 85.65
NOx LTO (g) 23531
Smoke Take Off (SN) 3.9
Smoke Climb Out (SN) 3.6
Smoke Approach (SN) 4.1
Smoke Idle (SN) 0.5
Smoke Max (SN) 5.98
Smoke Sigma (SN) 2.26
Smoke Range (SN) 3-8.3
Smoke Characteristic (SN) 6.5
Smoke Characteristicto Regulatory (% of limit) 38.71
Fuel Flow Take Off (kg/s) 2.663
Fuel Flow Climbout (kg/s) 2.173
Fuel Flow Approach (kg/s) 0.696
Fuel Flow Idle (kg/s) 0.254
Fuel LTO (kg) 962
Fuel Venting Compliant Yes
Carbon Monoxide LTO (g) 2984
Emissions Data Status C
Engine Status Out of production
NOx Compliance Demonstration 2.3.2 e)