P70820-191345

CFM56-3C-1 (Rerated)

Turbofan · Family: CFM56-3 · CFM International
Maximum Takeoff Thrust
82.29 kN
Bypass Ratio
5.1
Overall Pressure Ratio
21.3
Diameter
1524 mm
Dry Weight
1951 kg
Fuel Flow Take Off
0.872 kg/s
NOx Unitaryto CAEP8
111.5 % of limit

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber —
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 5.1 Overall Pressure Ratio 21.3 Afterburner No

Pictures

CFM56-3

Name Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio Fuel Flow Take Off (kg/s) NOx LTO (g) NOx Unitaryto CAEP8 (% of limit) Smoke Max (SN) EASA ID
CFM56-3C-1 (Rerated) 82.29 5.1 21.3 0.872 3210 111.5 3 1CM006
CFM56-3-B1 89.41 5.1 22.44 0.946 3595 118.3 4 1CM004
CFM56-3B-2 98.3 5.1 24.1 1.056 4213 118.9 6 1CM005
CFM56-3C-1 104.6 5.1 25.5 1.154 4810 121.3 7.7 1CM007

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CF34-10E5A1 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E6A1 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E7 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E7-B GE Aircraft Engines 83.7 5.09 27.2 Compare
CF34-10A18 GE Aircraft Engines 82.1 5.4 26.5 Compare
BR700-730B2-14 Rolls-Royce Deutschland 81.65 5.377 35.533 Compare
All data (68 fields)
Name
CFM56-3C-1 (Rerated)
Family
CFM56-3
EASA ID
1CM006
Aircraft Engine Manufacturer
CFM International
Aircraft Engine Type
Turbofan
Comment
Boeing 737 Classic
Dry Weight (kg)
1951
Diameter (mm)
1524
Max Rotating Diameter (mm)
1524
Wikipedia Article (URL)
en.wikipedia.org/wiki/CFM_International_CFM56
Fuel
Jet A
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
5.1
Overall Pressure Ratio
21.3
Maximum Takeoff Thrust (kN)
82.29
Hydrocarbon Take Off (g/kg fuel)
0.05
Hydrocarbon Climb Out (g/kg fuel)
0.05
Hydrocarbon Approach (g/kg fuel)
0.08
Hydrocarbon Idle (g/kg fuel)
2.86
Hydrocarbon Unitary Average (g/kN)
6.18
Hydrocarbon Unitary Sigma (g/kN)
1.05
Hydrocarbon Unitary Range (g/kN)
5.47-7.38
Hydrocarbon Unitary Characteristic (g/kN)
9.5
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
48.6
Hydrocarbon LTO (g)
507
Carbon Monoxide Take Off (g/kg fuel)
0.9
Carbon Monoxide Climb Out (g/kg fuel)
1
Carbon Monoxide Approach (g/kg fuel)
4.2
Carbon Monoxide Idle (g/kg fuel)
38.1
Carbon Monoxide Unitary Average (g/kN)
85.2
Carbon Monoxide Unitary SD (g/kN)
6.4
Carbon Monoxide Unitary Range (g/kN)
79.7-92.2
Carbon Monoxide Unitary Characteristic (g/kN)
104.6
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
88.6
NOx Take Off (g/kg fuel)
16.6
NOx Climb Out (g/kg fuel)
14.7
NOx Approach (g/kg fuel)
8
NOx Idle (g/kg fuel)
3.8
NOx Unitary Average (g/kN)
39
NOx Unitary SD (g/kN)
0.78
NOx Unitary Range (g/kN)
38.2-40
NOx Unitary Characteristic (g/kN)
45.2
NOx Unitaryto Standard (% of limit)
54.7
NOx Unitaryto CAEP2 (% of limit)
68.4
NOx Unitaryto CAEP4 (% of limit)
82.9
NOx Unitaryto CAEP6 (% of limit)
92.6
NOx Unitaryto CAEP8 (% of limit)
111.5
NOx LTO (g)
3210
Smoke Take Off (SN)
3
Smoke Climb Out (SN)
2.4
Smoke Approach (SN)
2.5
Smoke Idle (SN)
2.1
Smoke Max (SN)
3
Smoke Sigma (SN)
0.4
Smoke Range (SN)
2.5-3.2
Smoke Characteristic (SN)
3.9
Smoke Characteristicto Regulatory (% of limit)
15.5
Fuel Flow Take Off (kg/s)
0.872
Fuel Flow Climbout (kg/s)
0.732
Fuel Flow Approach (kg/s)
0.273
Fuel Flow Idle (kg/s)
0.111
Fuel LTO (kg)
372
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
7002
Emissions Data Status
R
Engine Status
Out of production