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AE3007C1 ✕ AE3007C1 ✕
EASA ID 6AL023 6AL024
Aircraft Engine Manufacturer Rolls-Royce Rolls-Royce
Aircraft Engine Type Turbofan Turbofan
Fuel Jet A Jet A
Geared Fan No No
Combustion Chamber Type 1 Type 2
Afterburner No No
Streams 2 2
Bypass Ratio 5.1 5.1
Overall Pressure Ratio 16.58 16.58
Maximum Takeoff Thrust (kN) 31.46 31.46
Hydrocarbon Take Off (g/kg fuel) 0.24 0
Hydrocarbon Climb Out (g/kg fuel) 0.277 0.01
Hydrocarbon Approach (g/kg fuel) 0.661 0.21
Hydrocarbon Idle (g/kg fuel) 4.837 5.88
Hydrocarbon Unitary Average (g/kN) 10.95 12.36
Hydrocarbon Unitary Characteristic (g/kN) 14.25 19.04
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 72.7 97.1
Hydrocarbon LTO (g) 344 389
Carbon Monoxide Take Off (g/kg fuel) 0.87 0
Carbon Monoxide Climb Out (g/kg fuel) 1.07 0
Carbon Monoxide Approach (g/kg fuel) 3.96 1.62
Carbon Monoxide Idle (g/kg fuel) 26.04 36.04
Carbon Monoxide Unitary Average (g/kN) 58.61 76
Carbon Monoxide Unitary Characteristic (g/kN) 66.78 93.29
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 56.6 79.1
NOx Take Off (g/kg fuel) 17.9 20.2
NOx Climb Out (g/kg fuel) 15.35 17.6
NOx Approach (g/kg fuel) 7.05 6.71
NOx Idle (g/kg fuel) 3.37 3.14
NOx Unitary Average (g/kN) 37.36 40.16
NOx Unitary Characteristic (g/kN) 41.08 46.55
NOx Unitaryto Standard (% of limit) 56.2 63.6
NOx Unitaryto CAEP2 (% of limit) 70.2 79.5
NOx Unitaryto CAEP4 (% of limit) 71.4 80.9
NOx Unitaryto CAEP6 (% of limit) 71.9 81.5
NOx Unitaryto CAEP8 (% of limit) 76.4 86.6
NOx LTO (g) 1175 1262
Smoke Take Off (SN) 1 0.01
Smoke Climb Out (SN) 0.01 0.01
Smoke Approach (SN) 0.01 0.01
Smoke Idle (SN) 0.01 0.01
Smoke Max (SN) 1 0.01
Smoke Characteristic (SN) 1.17 0.01
Smoke Characteristicto Regulatory (% of limit) 3.6 0
Fuel Flow Take Off (kg/s) 0.3222 0.3222
Fuel Flow Climbout (kg/s) 0.2689 0.2689
Fuel Flow Approach (kg/s) 0.0991 0.0991
Fuel Flow Idle (kg/s) 0.0418 0.0418
Fuel LTO (kg) 138 138
Carbon Monoxide LTO (g) 1842 2389
Emissions Data Status C C
Engine Status Out of production Out of production
NOx Compliance Demonstration 2.3.2 e)