PW6124A

Turbofan · Pratt & Whitney
Reaction Turbines
Maximum Takeoff Thrust
105.87 kN
Bypass Ratio
4.8
Overall Pressure Ratio
28
Fuel Flow Take Off
1.169 kg/s
NOx Unitaryto CAEP8
96.6 % 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 Talon II
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 4.8 Overall Pressure Ratio 28 Afterburner No

Pictures

No pictures yet for this family.

Airplanes

Name Model Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Two Class Typical Seating Max Seating
A318-122 A318 PW6124A 2 31.44 34.1 107 136

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
V2524-A5 SelectOne™ Upgrade Package International Aero Engines 108.9 4.8 27 Compare
V2524-A5 International Aero Engines 109.06 4.81 26.9 Compare
V2522-A5 International Aero Engines 102.66 4.88 25.6 Compare
V2527-A5 SelectOne™ Upgrade Package International Aero Engines 110.3 4.8 27.1 Compare
V2527-A5E SelectOne™ Upgrade Package International Aero Engines 110.3 4.8 27.1 Compare
V2527-A5M SelectOne™ Upgrade Package International Aero Engines 110.3 4.8 27.1 Compare
All data (56 fields)
Name
PW6124A
EASA ID
7PW084
Aircraft Engine Manufacturer
Pratt & Whitney
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
Talon II
Afterburner
No
Streams
2
Bypass Ratio
4.8
Overall Pressure Ratio
28
Maximum Takeoff Thrust (kN)
105.87
Hydrocarbon Take Off (g/kg fuel)
0
Hydrocarbon Climb Out (g/kg fuel)
0.002
Hydrocarbon Approach (g/kg fuel)
0.001
Hydrocarbon Idle (g/kg fuel)
0.002
Hydrocarbon Unitary Average (g/kN)
0
Hydrocarbon Unitary Characteristic (g/kN)
0
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
0.1
Hydrocarbon LTO (g)
1
Carbon Monoxide Take Off (g/kg fuel)
0.68
Carbon Monoxide Climb Out (g/kg fuel)
0.81
Carbon Monoxide Approach (g/kg fuel)
3.69
Carbon Monoxide Idle (g/kg fuel)
25.19
Carbon Monoxide Unitary Average (g/kN)
46.2
Carbon Monoxide Unitary Characteristic (g/kN)
56.7
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
48.2
NOx Take Off (g/kg fuel)
21.03
NOx Climb Out (g/kg fuel)
15.85
NOx Approach (g/kg fuel)
6.88
NOx Idle (g/kg fuel)
3.58
NOx Unitary Average (g/kN)
39.4
NOx Unitary Characteristic (g/kN)
45.7
NOx Unitaryto Standard (% of limit)
47.6
NOx Unitaryto CAEP2 (% of limit)
59.5
NOx Unitaryto CAEP4 (% of limit)
71.6
NOx Unitaryto CAEP6 (% of limit)
81.4
NOx Unitaryto CAEP8 (% of limit)
96.6
NOx LTO (g)
4170
Smoke Take Off (SN)
5.16
Smoke Climb Out (SN)
4.71
Smoke Approach (SN)
1.32
Smoke Idle (SN)
1.51
Smoke Max (SN)
5.16
Smoke Characteristic (SN)
6.7
Smoke Characteristicto Regulatory (% of limit)
28.5
Fuel Flow Take Off (kg/s)
1.169
Fuel Flow Climbout (kg/s)
0.939
Fuel Flow Approach (kg/s)
0.325
Fuel Flow Idle (kg/s)
0.114
Fuel LTO (kg)
429
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
4901
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)