| EASA ID |
3RR034 |
|
| Aircraft Engine Manufacturer |
Rolls-Royce |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Dry Weight (kg) |
|
3628.739 |
| Diameter (mm) |
|
2463.8 |
| Length (mm) |
|
7924.8 |
| Wikipedia Article (URL) |
|
en.wikipedia.org/wiki/General_Electric_TF39 |
| Fuel |
AVTUR |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
|
Annular |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
4.1 |
|
| Overall Pressure Ratio |
27.65 |
|
| Maximum Takeoff Thrust (kN) |
191.73 |
193 |
| Thrust To Weight |
|
5.4 |
| Hydrocarbon Take Off (g/kg fuel) |
0.01 |
|
| Hydrocarbon Climb Out (g/kg fuel) |
0 |
|
| Hydrocarbon Approach (g/kg fuel) |
0.03 |
|
| Hydrocarbon Idle (g/kg fuel) |
0.28 |
|
| Hydrocarbon Unitary Average (g/kN) |
0.45 |
|
| Hydrocarbon Unitary Range (g/kN) |
0.41-0.49 |
|
| Hydrocarbon Unitary Characteristic (g/kN) |
0.7 |
|
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
3.6 |
|
| Hydrocarbon LTO (g) |
88 |
|
| Carbon Monoxide Take Off (g/kg fuel) |
0.94 |
|
| Carbon Monoxide Climb Out (g/kg fuel) |
0.6 |
|
| Carbon Monoxide Approach (g/kg fuel) |
1.05 |
|
| Carbon Monoxide Idle (g/kg fuel) |
11.76 |
|
| Carbon Monoxide Unitary Average (g/kN) |
19.67 |
|
| Carbon Monoxide Unitary Range (g/kN) |
19.35-19.92 |
|
| Carbon Monoxide Unitary Characteristic (g/kN) |
24.1 |
|
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
20.5 |
|
| NOx Take Off (g/kg fuel) |
54.46 |
|
| NOx Climb Out (g/kg fuel) |
36.82 |
|
| NOx Approach (g/kg fuel) |
7.35 |
|
| NOx Idle (g/kg fuel) |
3.52 |
|
| NOx Unitary Average (g/kN) |
76.97 |
|
| NOx Unitary Range (g/kN) |
75.9-77.9 |
|
| NOx Unitary Characteristic (g/kN) |
89.2 |
|
| NOx Unitaryto Standard (% of limit) |
93.6 |
|
| NOx Unitaryto CAEP2 (% of limit) |
117 |
|
| NOx Unitaryto CAEP4 (% of limit) |
141 |
|
| NOx Unitaryto CAEP6 (% of limit) |
160.3 |
|
| NOx Unitaryto CAEP8 (% of limit) |
190.6 |
|
| NOx LTO (g) |
14791 |
|
| Smoke Take Off (SN) |
1.73 |
|
| Smoke Climb Out (SN) |
1.84 |
|
| Smoke Approach (SN) |
0.96 |
|
| Smoke Idle (SN) |
0.5 |
|
| Smoke Max (SN) |
1.84 |
|
| Smoke Range (SN) |
1.5-2.2 |
|
| Smoke Characteristic (SN) |
2.4 |
|
| Smoke Characteristicto Regulatory (% of limit) |
12.1 |
|
| Fuel Flow Take Off (kg/s) |
2.08 |
|
| Fuel Flow Climbout (kg/s) |
1.65 |
|
| Fuel Flow Approach (kg/s) |
0.55 |
|
| Fuel Flow Idle (kg/s) |
0.19 |
|
| Fuel LTO (kg) |
734 |
|
| Fuel Venting Compliant |
No |
|
| Carbon Monoxide LTO (g) |
3837 |
|
| Compressor Description |
|
Axial, low pressure compressor, comprising single stage booster and a single stage fan, 16-stage high-pressure compressor |
| Emissions Data Status |
R |
|
| Engine Status |
Out of production |
|
| Turbine Description |
|
Axial, 2-stage high-pressure turbine, 6-stage low-pressure turbine |