Maximum Takeoff Thrust
30.71 kN
Overall Pressure Ratio
20.4
Fuel Flow Take Off
0.3604 kg/s
NOx Unitaryto CAEP8
74.9 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
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
Annular |
| 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
4.1 |
Overall Pressure Ratio
20.4 |
Afterburner
No |
Pictures
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All data (75 fields)
- Name
- PW308A
- EASA ID
- 01P07PW145
- Aircraft Engine Manufacturer
- Pratt & Whitney Canada
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A-1
- Geared Fan
- No
- Combustion Chamber
- Annular
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.1
- Overall Pressure Ratio
- 20.4
- Maximum Takeoff Thrust (kN)
- 30.71
- Hydrocarbon Take Off (g/kg fuel)
- 0
- Hydrocarbon Climb Out (g/kg fuel)
- 0
- Hydrocarbon Approach (g/kg fuel)
- 0.02
- Hydrocarbon Idle (g/kg fuel)
- 6.62
- Hydrocarbon Unitary Average (g/kN)
- 14.98
- Hydrocarbon Unitary Range (g/kN)
- 14.4-15.88
- Hydrocarbon Unitary Characteristic (g/kN)
- 17.5
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 89.3
- Hydrocarbon LTO (g)
- 460
- Carbon Monoxide Take Off (g/kg fuel)
- 0.83
- Carbon Monoxide Climb Out (g/kg fuel)
- 1.06
- Carbon Monoxide Approach (g/kg fuel)
- 4.08
- Carbon Monoxide Idle (g/kg fuel)
- 38.21
- Carbon Monoxide Unitary Average (g/kN)
- 92.08
- Carbon Monoxide Unitary Range (g/kN)
- 87.17-98.01
- Carbon Monoxide Unitary Characteristic (g/kN)
- 99.6
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 84.4
- NOx Take Off (g/kg fuel)
- 16.74
- NOx Climb Out (g/kg fuel)
- 14.06
- NOx Approach (g/kg fuel)
- 8.03
- NOx Idle (g/kg fuel)
- 3.65
- NOx Unitary Average (g/kN)
- 42.33
- NOx Unitary Range (g/kN)
- 41.21-42.94
- NOx Unitary Characteristic (g/kN)
- 44.8
- NOx Unitaryto Standard (% of limit)
- 55.4
- NOx Unitaryto CAEP2 (% of limit)
- 69.3
- NOx Unitaryto CAEP4 (% of limit)
- 70.2
- NOx Unitaryto CAEP6 (% of limit)
- 70.7
- NOx Unitaryto CAEP8 (% of limit)
- 74.9
- NOx LTO (g)
- 1300
- Smoke Take Off (SN)
- 15
- Smoke Climb Out (SN)
- 15
- Smoke Approach (SN)
- 2.5
- Smoke Idle (SN)
- 1.7
- Smoke Max (SN)
- 15.1
- Smoke Range (SN)
- 15-15.3
- Smoke Characteristic (SN)
- 17.1
- Smoke Characteristicto Regulatory (% of limit)
- 52.3
- Fuel Flow Take Off (kg/s)
- 0.3604
- Fuel Flow Climbout (kg/s)
- 0.2991
- Fuel Flow Approach (kg/s)
- 0.1235
- Fuel Flow Idle (kg/s)
- 0.0445
- Fuel LTO (kg)
- 154
- Carbon Monoxide LTO (g)
- 2828
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 d)
- nvPME Imass Approach (mg/kg)
- 48.4559
- nvPME Imass Climb Out (mg/kg)
- 154.8257
- nvPME Imass Idle (mg/kg)
- 66.5208
- nvPME Imass Max (mg/kg)
- 209.6305
- nvPME Imass Take Off (mg/kg)
- 209.6305
- nvPME Inum Approach (#/kg)
- 474283900000000
- nvPME Inum Climb Out (#/kg)
- 932817100000000
- nvPME Inum Idle (#/kg)
- 1030769000000000
- nvPME Inum Max (#/kg)
- 1030769000000000
- nvPME Inum Take Off (#/kg)
- 924354200000000
- nvPMLTO Mass (mg)
- 15340.3
- nvPMLTO Mass Per Thrust (mg/kN)
- 694.3569
- nvPMLTO Number (#)
- 136440900000000000
- nvPMLTO Number Per Thrust (#/kN)
- 6175801000000000
- nvPM Mass Concentration Characteristic (mg/m³)
- 1290.581
- nvPM Mass Concentration Max (mg/m³)
- 1002.652
- nvPM Mass Concentration To CAEP10 (% of limit)
- 9.4641