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PW1130G-JM ✕ PW1133G1-JM ✕
EASA ID 01P18PW155 15PW107
Aircraft Engine Manufacturer Pratt & Whitney Pratt & Whitney
Aircraft Engine Type Turbofan Turbofan
Fuel Jet A Jet A
Geared Fan Yes Yes
Combustion Chamber TALON X, Block-C TALON X
Afterburner No No
Streams 2 2
Bypass Ratio 11.58 11.4
Overall Pressure Ratio 38.07 38.85
Maximum Takeoff Thrust (kN) 147.28 147.28
Hydrocarbon Take Off (g/kg fuel) 0.02 0.03
Hydrocarbon Climb Out (g/kg fuel) 0.05 0.03
Hydrocarbon Approach (g/kg fuel) 0.02 0.04
Hydrocarbon Idle (g/kg fuel) 0.26 0.05
Hydrocarbon Unitary Average (g/kN) 0.35 0.1
Hydrocarbon Unitary Characteristic (g/kN) 0.41 0.2
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 2.1 1.02
Hydrocarbon LTO (g) 48 16
Carbon Monoxide Take Off (g/kg fuel) 0.23 0.14
Carbon Monoxide Climb Out (g/kg fuel) 0.22 0.2
Carbon Monoxide Approach (g/kg fuel) 3.44 3.59
Carbon Monoxide Idle (g/kg fuel) 24.06 17.89
Carbon Monoxide Unitary Average (g/kN) 24.88 20.5
Carbon Monoxide Unitary Characteristic (g/kN) 26.91 25.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 22.8 21.36
NOx Take Off (g/kg fuel) 25.46 25.23
NOx Climb Out (g/kg fuel) 19.84 18.92
NOx Approach (g/kg fuel) 9.4 9.14
NOx Idle (g/kg fuel) 5.31 6.98
NOx Unitary Average (g/kN) 31.3 33
NOx Unitary Characteristic (g/kN) 33.62 38.3
NOx Unitaryto Standard (% of limit) 29 32.54
NOx Unitaryto CAEP2 (% of limit) 36.2 40.68
NOx Unitaryto CAEP4 (% of limit) 40.4 45.22
NOx Unitaryto CAEP6 (% of limit) 44.8 49.96
NOx Unitaryto CAEP8 (% of limit) 50.8 56.48
NOx LTO (g) 4736 4864
Smoke Take Off (SN) 15.2 4.4
Smoke Climb Out (SN) 13.9 2.01
Smoke Approach (SN) 0.5 0.34
Smoke Idle (SN) 1 0.54
Smoke Max (SN) 15.2 4.4
Smoke Characteristic (SN) 16.7 5.7
Smoke Characteristicto Regulatory (% of limit) 78.4 26.78
Fuel Flow Take Off (kg/s) 1.023 1.02297
Fuel Flow Climbout (kg/s) 0.8385 0.838543
Fuel Flow Approach (kg/s) 0.2783 0.278342
Fuel Flow Idle (kg/s) 0.0988 0.09878
Fuel LTO (kg) 375 374.6
Fuel Venting Compliant Yes Yes
Carbon Monoxide LTO (g) 3971 3025
Emissions Data Status C C
Engine Status Out of production Out of production
NOx Compliance Demonstration 2.3.2 e) 2.3.2 e)
nvPME Imass Approach (mg/kg) 6.9151
nvPME Imass Climb Out (mg/kg) 70.7868
nvPME Imass Idle (mg/kg) 7.0406
nvPME Imass Max (mg/kg) 93.3457
nvPME Imass Take Off (mg/kg) 93.3457
nvPME Inum Approach (#/kg) 425475400000000
nvPME Inum Climb Out (#/kg) 956537700000000
nvPME Inum Idle (#/kg) 665217800000000
nvPME Inum Max (#/kg) 963869000000000
nvPME Inum Take Off (#/kg) 708296400000000
nvPMLTO Mass (mg) 13398.92
nvPMLTO Mass Per Thrust (mg/kN) 126.4607
nvPMLTO Mass To CAEP11 (% of limit) 54.3202
nvPMLTO Number (#) 267491300000000000
nvPMLTO Number Per Thrust (#/kN) 2524616000000000
nvPMLTO Number To CAEP11 (% of limit) 84.1602
nvPM Mass Concentration Characteristic (mg/m³) 3051.25
nvPM Mass Concentration Max (mg/m³) 2370.516
nvPM Mass Concentration To CAEP10 (% of limit) 55.7209