| EASA ID |
|
05P25PW206 |
| Aircraft Engine Manufacturer |
Pratt & Whitney |
Pratt & Whitney Canada |
| Aircraft Engine Type |
Turbojet |
Turbofan |
| Dry Weight (kg) |
1291.831 |
|
| Diameter (mm) |
1021.08 |
|
| Length (mm) |
4109.72 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Pratt_%26_Whitney_PW1120 |
|
| Fuel |
|
Jet A-1 |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
TALON X |
| Afterburner |
Yes |
No |
| Streams |
1 |
2 |
| Bypass Ratio |
|
4.5309 |
| Overall Pressure Ratio |
|
34.7667 |
| Maximum Takeoff Thrust (kN) |
61.18 |
61.0115 |
| Thrust To Weight |
7.23 |
|
| Hydrocarbon Take Off (g/kg fuel) |
|
0.0219 |
| Hydrocarbon Climb Out (g/kg fuel) |
|
0.029 |
| Hydrocarbon Approach (g/kg fuel) |
|
0.0367 |
| Hydrocarbon Idle (g/kg fuel) |
|
0.1283 |
| Hydrocarbon Unitary Average (g/kN) |
|
0.3028 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
0.1268 |
| Hydrocarbon Unitary Range (g/kN) |
|
0.2-0.4 |
| Hydrocarbon Unitary Characteristic (g/kN) |
|
0.3533 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
|
1.8026 |
| Hydrocarbon LTO (g) |
|
18.4773 |
| Carbon Monoxide Take Off (g/kg fuel) |
|
0.0473 |
| Carbon Monoxide Climb Out (g/kg fuel) |
|
0.043 |
| Carbon Monoxide Approach (g/kg fuel) |
|
2.5083 |
| Carbon Monoxide Idle (g/kg fuel) |
|
14.4762 |
| Carbon Monoxide Unitary Average (g/kN) |
|
28.2187 |
| Carbon Monoxide Unitary SD (g/kN) |
|
1.2081 |
| Carbon Monoxide Unitary Range (g/kN) |
|
27.2-29.5 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
|
30.5201 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
|
25.8645 |
| NOx Take Off (g/kg fuel) |
|
21.4036 |
| NOx Climb Out (g/kg fuel) |
|
17.3108 |
| NOx Approach (g/kg fuel) |
|
12.681 |
| NOx Idle (g/kg fuel) |
|
5.4203 |
| NOx Unitary Average (g/kN) |
|
48.2932 |
| NOx Unitary SD (g/kN) |
|
1.2642 |
| NOx Unitary Range (g/kN) |
|
46.8-49.2 |
| NOx Unitary Characteristic (g/kN) |
|
51.1916 |
| NOx Unitaryto Standard (% of limit) |
|
46.7357 |
| NOx Unitaryto CAEP2 (% of limit) |
|
58.4196 |
| NOx Unitaryto CAEP4 (% of limit) |
|
62.8022 |
| NOx Unitaryto CAEP6 (% of limit) |
|
66.4033 |
| NOx Unitaryto CAEP8 (% of limit) |
|
72.572 |
| NOx LTO (g) |
|
2946.443 |
| Smoke Take Off (SN) |
|
0 |
| Smoke Climb Out (SN) |
|
0 |
| Smoke Approach (SN) |
|
0 |
| Smoke Idle (SN) |
|
0 |
| Smoke Max (SN) |
|
0 |
| Smoke Sigma (SN) |
|
0 |
| Smoke Range (SN) |
|
0-0 |
| Smoke Characteristic (SN) |
|
0 |
| Smoke Characteristicto Regulatory (% of limit) |
|
0 |
| Fuel Flow Take Off (kg/s) |
|
0.6454 |
| Fuel Flow Climbout (kg/s) |
|
0.5291 |
| Fuel Flow Approach (kg/s) |
|
0.1825 |
| Fuel Flow Idle (kg/s) |
|
0.0712 |
| Fuel LTO (kg) |
|
251.79 |
| Fuel Venting Compliant |
|
Yes |
| Carbon Monoxide LTO (g) |
|
1721.668 |
| Compressor Description |
axial compressor with 3 fan and 10 compressor stages; Bypass ratio: 0.36:1 |
|
| Emissions Data Status |
|
C |
| NOx Compliance Demonstration |
|
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
0.131 |
| nvPME Imass Climb Out (mg/kg) |
|
1.4833 |
| nvPME Imass Idle (mg/kg) |
|
0.1285 |
| nvPME Imass Max (mg/kg) |
|
3.6801 |
| nvPME Imass Take Off (mg/kg) |
|
3.6801 |
| nvPME Inum Approach (#/kg) |
|
947986200000 |
| nvPME Inum Climb Out (#/kg) |
|
59054460000000 |
| nvPME Inum Idle (#/kg) |
|
20778930000000 |
| nvPME Inum Max (#/kg) |
|
97669840000000 |
| nvPME Inum Take Off (#/kg) |
|
97669840000000 |
| nvPMLTO Mass (mg) |
|
223.3545 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
5.0888 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
0.6136 |
| nvPMLTO Number (#) |
|
9120941000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
207805700000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
2.0843 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
22.2989 |
| nvPM Mass Concentration Max (mg/m³) |
|
17.324 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
0.2559 |
| Turbine Description |
2 low-pressure and 2 high-pressure stages |
|