Maximum Takeoff Thrust
249.1 kN
Bypass Ratio
4.8
Overall Pressure Ratio
28.37
Fuel Flow Take Off
2.351 kg/s
NOx Unitaryto CAEP8
119.2 % 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 Phase 3
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 28.37 Afterburner No

Pictures

No pictures yet for this family.

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
JT9D-7R4H1 Pratt & Whitney 249.1 4.8 26.7 Compare
PW4056 Pratt & Whitney 249.1 4.7 29.3 Compare
PW4156 Pratt & Whitney 249.1 4.7 29.3 Compare
JT9D-7R4G2 Pratt & Whitney 243.5 4.8 26.3 Compare
PW4256 Pratt & Whitney 252.4 4.7 29.3 Compare
CF6-80C2B1 General Electric Company 249.01 5.1 29.53 Compare
All data (56 fields)
Name
PW4x56
EASA ID
1PW055
Aircraft Engine Manufacturer
Pratt & Whitney
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
Phase 3
Afterburner
No
Streams
2
Bypass Ratio
4.8
Overall Pressure Ratio
28.37
Maximum Takeoff Thrust (kN)
249.1
Hydrocarbon Take Off (g/kg fuel)
0.08
Hydrocarbon Climb Out (g/kg fuel)
0.09
Hydrocarbon Approach (g/kg fuel)
0.16
Hydrocarbon Idle (g/kg fuel)
4.75
Hydrocarbon Unitary Average (g/kN)
6.4
Hydrocarbon Unitary Characteristic (g/kN)
9.9
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
50.3
Hydrocarbon LTO (g)
1597
Carbon Monoxide Take Off (g/kg fuel)
0.48
Carbon Monoxide Climb Out (g/kg fuel)
0.56
Carbon Monoxide Approach (g/kg fuel)
1.89
Carbon Monoxide Idle (g/kg fuel)
29.96
Carbon Monoxide Unitary Average (g/kN)
41
Carbon Monoxide Unitary Characteristic (g/kN)
50.3
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
42.6
NOx Take Off (g/kg fuel)
30.44
NOx Climb Out (g/kg fuel)
24.24
NOx Approach (g/kg fuel)
11.97
NOx Idle (g/kg fuel)
3.93
NOx Unitary Average (g/kN)
49.2
NOx Unitary Characteristic (g/kN)
57
NOx Unitaryto Standard (% of limit)
59
NOx Unitaryto CAEP2 (% of limit)
73.7
NOx Unitaryto CAEP4 (% of limit)
88.6
NOx Unitaryto CAEP6 (% of limit)
100.6
NOx Unitaryto CAEP8 (% of limit)
119.2
NOx LTO (g)
12246
Smoke Take Off (SN)
8.5
Smoke Climb Out (SN)
5.8
Smoke Approach (SN)
0.6
Smoke Idle (SN)
0
Smoke Max (SN)
8.5
Smoke Characteristic (SN)
10.9
Smoke Characteristicto Regulatory (% of limit)
59.4
Fuel Flow Take Off (kg/s)
2.351
Fuel Flow Climbout (kg/s)
1.912
Fuel Flow Approach (kg/s)
0.643
Fuel Flow Idle (kg/s)
0.208
Fuel LTO (kg)
830
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
10202
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 c)