CFM56-2B-1

Turbofan · Family: CFM56-2 · CFM International
Maximum Takeoff Thrust
97.86 kN
Bypass Ratio
6
Overall Pressure Ratio
23.5
Diameter
1735 mm
Dry Weight
2186 kg
Fuel Flow Take Off
0.985 kg/s
NOx Unitaryto CAEP8
113 % 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 6 Overall Pressure Ratio 23.5 Afterburner No

Pictures

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CFM56-2

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
CFM56-2-C5 97.86 6 23.5 0.985 3906 113 6 1CM003
CFM56-2B-1 97.86 6 23.5 0.985 3906 113 6 1CM002
CFM56-2A series 106.76 6 25.2 1.114 4571 114.4 7.9 1CM001

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CFM56-5A4 CFM56-5A CFM International 97.89 6 23.8 Compare
CFM56-5B5/3 CFM56-5B CFM International 97.9 6 23.1 Compare
CFM56-3B-2 CFM56-3 CFM International 98.3 5.1 24.1 Compare
CFM56-7B22 CFM56-7B CFM International 100.97 5.3 24.41 Compare
PW6122A Pratt & Whitney 98.31 4.8 25.7 Compare
Rolls-Royce RB.106 Rolls-Royce 96.7 Compare
All data (68 fields)
Name
CFM56-2B-1
Family
CFM56-2
EASA ID
1CM002
Aircraft Engine Manufacturer
CFM International
Aircraft Engine Type
Turbofan
Comment
DC-8-70, KC-135R, E-3, E-6
Dry Weight (kg)
2186
Diameter (mm)
1735
Max Rotating Diameter (mm)
1735
Wikipedia Article (URL)
en.wikipedia.org/wiki/CFM_International_CFM56
Fuel
Jet A
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
6
Overall Pressure Ratio
23.5
Maximum Takeoff Thrust (kN)
97.86
Hydrocarbon Take Off (g/kg fuel)
0.04
Hydrocarbon Climb Out (g/kg fuel)
0.05
Hydrocarbon Approach (g/kg fuel)
0.08
Hydrocarbon Idle (g/kg fuel)
1.83
Hydrocarbon Unitary Average (g/kN)
3.87
Hydrocarbon Unitary Sigma (g/kN)
0.41
Hydrocarbon Unitary Range (g/kN)
3.4-4.15
Hydrocarbon Unitary Characteristic (g/kN)
6
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
30.4
Hydrocarbon LTO (g)
378
Carbon Monoxide Take Off (g/kg fuel)
0.9
Carbon Monoxide Climb Out (g/kg fuel)
0.9
Carbon Monoxide Approach (g/kg fuel)
4.2
Carbon Monoxide Idle (g/kg fuel)
30.7
Carbon Monoxide Unitary Average (g/kN)
67.2
Carbon Monoxide Unitary SD (g/kN)
4.1
Carbon Monoxide Unitary Range (g/kN)
63.5-71.7
Carbon Monoxide Unitary Characteristic (g/kN)
82.5
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
69.9
NOx Take Off (g/kg fuel)
18.5
NOx Climb Out (g/kg fuel)
16
NOx Approach (g/kg fuel)
8.2
NOx Idle (g/kg fuel)
4
NOx Unitary Average (g/kN)
39.9
NOx Unitary SD (g/kN)
0.6
NOx Unitary Range (g/kN)
39.4-40.5
NOx Unitary Characteristic (g/kN)
46.3
NOx Unitaryto Standard (% of limit)
53.2
NOx Unitaryto CAEP2 (% of limit)
66.5
NOx Unitaryto CAEP4 (% of limit)
81.7
NOx Unitaryto CAEP6 (% of limit)
92.9
NOx Unitaryto CAEP8 (% of limit)
113
NOx LTO (g)
3906
Smoke Take Off (SN)
6
Smoke Climb Out (SN)
3
Smoke Approach (SN)
2.6
Smoke Idle (SN)
2.2
Smoke Max (SN)
6
Smoke Sigma (SN)
0.8
Smoke Range (SN)
5.4-6.9
Smoke Characteristic (SN)
7.7
Smoke Characteristicto Regulatory (% of limit)
32.4
Fuel Flow Take Off (kg/s)
0.985
Fuel Flow Climbout (kg/s)
0.819
Fuel Flow Approach (kg/s)
0.311
Fuel Flow Idle (kg/s)
0.128
Fuel LTO (kg)
424
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
6578
Emissions Data Status
C
Engine Status
Out of production