| EASA ID |
|
11RR048 |
| 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 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
10 can-annular combustion chambers |
Tubular |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
3.04 |
3.26 |
| Overall Pressure Ratio |
|
15.88 |
| Maximum Takeoff Thrust (kN) |
63 |
61.6 |
| Thrust To Weight |
4.2 |
|
| Hydrocarbon Take Off (g/kg fuel) |
|
0.03 |
| Hydrocarbon Climb Out (g/kg fuel) |
|
0.05 |
| Hydrocarbon Approach (g/kg fuel) |
|
0.65 |
| Hydrocarbon Idle (g/kg fuel) |
|
1.49 |
| Hydrocarbon Unitary Average (g/kN) |
|
4.465 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
1.308 |
| Hydrocarbon Unitary Range (g/kN) |
|
2.57-5.62 |
| Hydrocarbon Unitary Characteristic (g/kN) |
|
5.2 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
|
26.6 |
| Hydrocarbon LTO (g) |
|
275 |
| Carbon Monoxide Take Off (g/kg fuel) |
|
0.5 |
| Carbon Monoxide Climb Out (g/kg fuel) |
|
0.95 |
| Carbon Monoxide Approach (g/kg fuel) |
|
2.89 |
| Carbon Monoxide Idle (g/kg fuel) |
|
24.4 |
| Carbon Monoxide Unitary Average (g/kN) |
|
66.9 |
| Carbon Monoxide Unitary SD (g/kN) |
|
11.5 |
| Carbon Monoxide Unitary Range (g/kN) |
|
59.55-82.67 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
|
72.4 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
|
61.3 |
| NOx Take Off (g/kg fuel) |
|
19.3 |
| NOx Climb Out (g/kg fuel) |
|
15.4 |
| NOx Approach (g/kg fuel) |
|
5.31 |
| NOx Idle (g/kg fuel) |
|
2.53 |
| NOx Unitary Average (g/kN) |
|
40.58 |
| NOx Unitary SD (g/kN) |
|
0.9 |
| NOx Unitary Range (g/kN) |
|
39.5-41.7 |
| NOx Unitary Characteristic (g/kN) |
|
43 |
| NOx Unitaryto Standard (% of limit) |
|
59.9 |
| NOx Unitaryto CAEP2 (% of limit) |
|
74.9 |
| NOx Unitaryto CAEP4 (% of limit) |
|
85.7 |
| NOx Unitaryto CAEP6 (% of limit) |
|
91.2 |
| NOx Unitaryto CAEP8 (% of limit) |
|
105.1 |
| NOx LTO (g) |
|
2500 |
| Smoke Take Off (SN) |
|
4.39 |
| Smoke Climb Out (SN) |
|
3.46 |
| Smoke Approach (SN) |
|
0.46 |
| Smoke Idle (SN) |
|
0.21 |
| Smoke Max (SN) |
|
4.7 |
| Smoke Sigma (SN) |
|
0.59 |
| Smoke Range (SN) |
|
3.67-5.2 |
| Smoke Characteristic (SN) |
|
5.2 |
| Smoke Characteristicto Regulatory (% of limit) |
|
19.1 |
| Fuel Flow Take Off (kg/s) |
|
0.731 |
| Fuel Flow Climbout (kg/s) |
|
0.604 |
| Fuel Flow Approach (kg/s) |
|
0.215 |
| Fuel Flow Idle (kg/s) |
|
0.102 |
| Fuel LTO (kg) |
|
321 |
| Fuel Venting Compliant |
|
No |
| Carbon Monoxide LTO (g) |
|
4123 |
| Compressor Description |
Single-stage fan plus a 3-stage IP compressor (Same shaft.) and a 12-stage HP compressor |
|
| Emissions Data Status |
|
C/R |
| Engine Status |
|
Out of production |
| NOx Compliance Demonstration |
|
2.3.2 d) |
| Turbine Description |
2 stage HP turbine, 3 stage LP turbine |
|