Maximum Takeoff Thrust
107.82 kN
Overall Pressure Ratio
28.78
Fuel Flow Take Off
0.71 kg/s
NOx Unitaryto CAEP8
53 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
Yes |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
TALON X, Block-C |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
12.72 |
Overall Pressure Ratio
28.78 |
Afterburner
No |
Pictures
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All data (75 fields)
- Name
- PW1124G1-JM
- EASA ID
- 01P18PW149
- Aircraft Engine Manufacturer
- Pratt & Whitney
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- Yes
- Combustion Chamber
- TALON X, Block-C
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 12.72
- Overall Pressure Ratio
- 28.78
- Maximum Takeoff Thrust (kN)
- 107.82
- Hydrocarbon Take Off (g/kg fuel)
- 0.1
- Hydrocarbon Climb Out (g/kg fuel)
- 0.1
- Hydrocarbon Approach (g/kg fuel)
- 0.02
- Hydrocarbon Idle (g/kg fuel)
- 0.55
- Hydrocarbon Unitary Average (g/kN)
- 0.77
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.9
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 5
- Hydrocarbon LTO (g)
- 80
- Carbon Monoxide Take Off (g/kg fuel)
- 0.26
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.38
- Carbon Monoxide Approach (g/kg fuel)
- 6.39
- Carbon Monoxide Idle (g/kg fuel)
- 29.78
- Carbon Monoxide Unitary Average (g/kN)
- 37.22
- Carbon Monoxide Unitary Characteristic (g/kN)
- 40.25
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 34
- NOx Take Off (g/kg fuel)
- 16.47
- NOx Climb Out (g/kg fuel)
- 13.85
- NOx Approach (g/kg fuel)
- 8.92
- NOx Idle (g/kg fuel)
- 4.72
- NOx Unitary Average (g/kN)
- 23.8
- NOx Unitary Characteristic (g/kN)
- 25.72
- NOx Unitaryto Standard (% of limit)
- 26
- NOx Unitaryto CAEP2 (% of limit)
- 33
- NOx Unitaryto CAEP4 (% of limit)
- 40
- NOx Unitaryto CAEP6 (% of limit)
- 45
- NOx Unitaryto CAEP8 (% of limit)
- 53
- NOx LTO (g)
- 2626
- Smoke Take Off (SN)
- 11.6
- Smoke Climb Out (SN)
- 7.9
- Smoke Approach (SN)
- 0.4
- Smoke Idle (SN)
- 1.2
- Smoke Max (SN)
- 11.6
- Smoke Characteristic (SN)
- 12.7
- Smoke Characteristicto Regulatory (% of limit)
- 55
- Fuel Flow Take Off (kg/s)
- 0.71
- Fuel Flow Climbout (kg/s)
- 0.6
- Fuel Flow Approach (kg/s)
- 0.21
- Fuel Flow Idle (kg/s)
- 0.08
- Fuel LTO (kg)
- 284
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 4076
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 5.7605
- nvPME Imass Climb Out (mg/kg)
- 17.512
- nvPME Imass Idle (mg/kg)
- 10.612
- nvPME Imass Max (mg/kg)
- 40.9689
- nvPME Imass Take Off (mg/kg)
- 40.9689
- nvPME Inum Approach (#/kg)
- 331366700000000
- nvPME Inum Climb Out (#/kg)
- 473541400000000
- nvPME Inum Idle (#/kg)
- 932418900000000
- nvPME Inum Max (#/kg)
- 944023300000000
- nvPME Inum Take Off (#/kg)
- 779832300000000
- nvPMLTO Mass (mg)
- 4223.353
- nvPMLTO Mass Per Thrust (mg/kN)
- 54.4487
- nvPMLTO Mass To CAEP11 (% of limit)
- 10.7684
- nvPMLTO Number (#)
- 193825800000000000
- nvPMLTO Number Per Thrust (#/kN)
- 2498860000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 40.3814
- nvPM Mass Concentration Characteristic (mg/m³)
- 1167.785
- nvPM Mass Concentration Max (mg/m³)
- 907.2523
- nvPM Mass Concentration To CAEP10 (% of limit)
- 18.3242