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Rolls-Royce RB.183 Tay ✕ TAY 650 ✕
EASA ID 3RR031
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 Pedhead
Afterburner No No
Streams 2 2
Bypass Ratio 3.04 3
Overall Pressure Ratio 15.9
Maximum Takeoff Thrust (kN) 63 67.2
Thrust To Weight 4.2
Hydrocarbon Take Off (g/kg fuel) 0.11
Hydrocarbon Climb Out (g/kg fuel) 0.22
Hydrocarbon Approach (g/kg fuel) 0.11
Hydrocarbon Idle (g/kg fuel) 1.23
Hydrocarbon Unitary Average (g/kN) 3.9
Hydrocarbon Unitary Range (g/kN) 3.9
Hydrocarbon Unitary Characteristic (g/kN) 6
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 30.6
Hydrocarbon LTO (g) 261
Carbon Monoxide Take Off (g/kg fuel) 0.69
Carbon Monoxide Climb Out (g/kg fuel) 0.48
Carbon Monoxide Approach (g/kg fuel) 1.76
Carbon Monoxide Idle (g/kg fuel) 22.36
Carbon Monoxide Unitary Average (g/kN) 65.16
Carbon Monoxide Unitary Range (g/kN) 62.4-67.9
Carbon Monoxide Unitary Characteristic (g/kN) 80
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 67.8
NOx Take Off (g/kg fuel) 16.45
NOx Climb Out (g/kg fuel) 12.94
NOx Approach (g/kg fuel) 5.26
NOx Idle (g/kg fuel) 2.5
NOx Unitary Average (g/kN) 38.75
NOx Unitary Range (g/kN) 38.1-39.5
NOx Unitary Characteristic (g/kN) 44.9
NOx Unitaryto Standard (% of limit) 62.6
NOx Unitaryto CAEP2 (% of limit) 78.2
NOx Unitaryto CAEP4 (% of limit) 91.6
NOx Unitaryto CAEP6 (% of limit) 98.7
NOx Unitaryto CAEP8 (% of limit) 115.8
NOx LTO (g) 2591
Smoke Take Off (SN) 5.6
Smoke Climb Out (SN) 7.9
Smoke Approach (SN) 4
Smoke Idle (SN) 0.56
Smoke Max (SN) 9.87
Smoke Range (SN) 9.3-10.4
Smoke Characteristic (SN) 12.7
Smoke Characteristicto Regulatory (% of limit) 48.1
Fuel Flow Take Off (kg/s) 0.86
Fuel Flow Climbout (kg/s) 0.71
Fuel Flow Approach (kg/s) 0.25
Fuel Flow Idle (kg/s) 0.12
Fuel LTO (kg) 377
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 4361
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