| EASA ID |
|
1RR019 |
| Aircraft Engine Manufacturer |
Rolls-Royce |
Rolls-Royce |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Dry Weight (kg) |
1501.391 |
|
| Diameter (mm) |
1117.6 |
|
| Length (mm) |
2405.38 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Rolls-Royce_RB.183_Tay |
|
| Fuel |
|
AVTUR |
| Geared Fan |
No |
No |
| Combustion Chamber |
10 can-annular combustion chambers |
|
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
3.04 |
3 |
| Overall Pressure Ratio |
|
16.1 |
| Maximum Takeoff Thrust (kN) |
63 |
61.6 |
| Thrust To Weight |
4.2 |
|
| Hydrocarbon Take Off (g/kg fuel) |
|
0.8 |
| Hydrocarbon Climb Out (g/kg fuel) |
|
0.3 |
| Hydrocarbon Approach (g/kg fuel) |
|
0.9 |
| Hydrocarbon Idle (g/kg fuel) |
|
3.4 |
| Hydrocarbon Unitary Average (g/kN) |
|
10.7 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
1.4 |
| Hydrocarbon Unitary Range (g/kN) |
|
9.11-12.97 |
| Hydrocarbon Unitary Characteristic (g/kN) |
|
13.9 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
|
71 |
| Hydrocarbon LTO (g) |
|
684 |
| Carbon Monoxide Take Off (g/kg fuel) |
|
0.7 |
| Carbon Monoxide Climb Out (g/kg fuel) |
|
0.8 |
| Carbon Monoxide Approach (g/kg fuel) |
|
3.9 |
| Carbon Monoxide Idle (g/kg fuel) |
|
24.1 |
| Carbon Monoxide Unitary Average (g/kN) |
|
69.3 |
| Carbon Monoxide Unitary SD (g/kN) |
|
4.1 |
| Carbon Monoxide Unitary Range (g/kN) |
|
65.5-74.8 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
|
79 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
|
66.9 |
| NOx Take Off (g/kg fuel) |
|
21.1 |
| NOx Climb Out (g/kg fuel) |
|
16.8 |
| NOx Approach (g/kg fuel) |
|
5.7 |
| NOx Idle (g/kg fuel) |
|
2.5 |
| NOx Unitary Average (g/kN) |
|
45.6 |
| NOx Unitary SD (g/kN) |
|
0.7 |
| NOx Unitary Range (g/kN) |
|
44.9-46.7 |
| NOx Unitary Characteristic (g/kN) |
|
50.1 |
| NOx Unitaryto Standard (% of limit) |
|
69.5 |
| NOx Unitaryto CAEP2 (% of limit) |
|
86.8 |
| NOx Unitaryto CAEP4 (% of limit) |
|
99.2 |
| NOx Unitaryto CAEP6 (% of limit) |
|
105.6 |
| NOx Unitaryto CAEP8 (% of limit) |
|
121.5 |
| NOx LTO (g) |
|
2814 |
| Smoke Take Off (SN) |
|
21.3 |
| Smoke Climb Out (SN) |
|
18.86 |
| Smoke Approach (SN) |
|
13.1 |
| Smoke Idle (SN) |
|
3.36 |
| Smoke Max (SN) |
|
21.3 |
| Smoke Sigma (SN) |
|
1.6 |
| Smoke Range (SN) |
|
18.9-22.8 |
| Smoke Characteristic (SN) |
|
25 |
| Smoke Characteristicto Regulatory (% of limit) |
|
92.4 |
| Fuel Flow Take Off (kg/s) |
|
0.76 |
| Fuel Flow Climbout (kg/s) |
|
0.63 |
| Fuel Flow Approach (kg/s) |
|
0.23 |
| Fuel Flow Idle (kg/s) |
|
0.11 |
| Fuel LTO (kg) |
|
342 |
| Fuel Venting Compliant |
|
No |
| Carbon Monoxide LTO (g) |
|
4440 |
| Compressor Description |
Single-stage fan plus a 3-stage IP compressor (Same shaft.) and a 12-stage HP compressor |
|
| Emissions Data Status |
|
C |
| Engine Status |
|
Out of production |
| Turbine Description |
2 stage HP turbine, 3 stage LP turbine |
|