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PW1133G1-JM ✕ PW1130G-JM ✕
EASA ID 15PW107 01P18PW155
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 TALON X, Block-C
Afterburner No No
Streams 2 2
Bypass Ratio 11.4 11.58
Overall Pressure Ratio 38.85 38.07
Maximum Takeoff Thrust (kN) 147.28 147.28
Hydrocarbon Take Off (g/kg fuel) 0.03 0.02
Hydrocarbon Climb Out (g/kg fuel) 0.03 0.05
Hydrocarbon Approach (g/kg fuel) 0.04 0.02
Hydrocarbon Idle (g/kg fuel) 0.05 0.26
Hydrocarbon Unitary Average (g/kN) 0.1 0.35
Hydrocarbon Unitary Characteristic (g/kN) 0.2 0.41
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 1.02 2.1
Hydrocarbon LTO (g) 16 48
Carbon Monoxide Take Off (g/kg fuel) 0.14 0.23
Carbon Monoxide Climb Out (g/kg fuel) 0.2 0.22
Carbon Monoxide Approach (g/kg fuel) 3.59 3.44
Carbon Monoxide Idle (g/kg fuel) 17.89 24.06
Carbon Monoxide Unitary Average (g/kN) 20.5 24.88
Carbon Monoxide Unitary Characteristic (g/kN) 25.2 26.91
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 21.36 22.8
NOx Take Off (g/kg fuel) 25.23 25.46
NOx Climb Out (g/kg fuel) 18.92 19.84
NOx Approach (g/kg fuel) 9.14 9.4
NOx Idle (g/kg fuel) 6.98 5.31
NOx Unitary Average (g/kN) 33 31.3
NOx Unitary Characteristic (g/kN) 38.3 33.62
NOx Unitaryto Standard (% of limit) 32.54 29
NOx Unitaryto CAEP2 (% of limit) 40.68 36.2
NOx Unitaryto CAEP4 (% of limit) 45.22 40.4
NOx Unitaryto CAEP6 (% of limit) 49.96 44.8
NOx Unitaryto CAEP8 (% of limit) 56.48 50.8
NOx LTO (g) 4864 4736
Smoke Take Off (SN) 4.4 15.2
Smoke Climb Out (SN) 2.01 13.9
Smoke Approach (SN) 0.34 0.5
Smoke Idle (SN) 0.54 1
Smoke Max (SN) 4.4 15.2
Smoke Characteristic (SN) 5.7 16.7
Smoke Characteristicto Regulatory (% of limit) 26.78 78.4
Fuel Flow Take Off (kg/s) 1.02297 1.023
Fuel Flow Climbout (kg/s) 0.838543 0.8385
Fuel Flow Approach (kg/s) 0.278342 0.2783
Fuel Flow Idle (kg/s) 0.09878 0.0988
Fuel LTO (kg) 374.6 375
Fuel Venting Compliant Yes Yes
Carbon Monoxide LTO (g) 3025 3971
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