V2522-A5

Turbofan · International Aero Engines
Reaction Turbines
Maximum Takeoff Thrust
102.66 kN
Bypass Ratio
4.88
Overall Pressure Ratio
25.6
Fuel Flow Take Off
0.971 kg/s
NOx Unitaryto CAEP8
121.3 % 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 4.88 Overall Pressure Ratio 25.6 Afterburner No

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Airplanes

Name Model Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Two Class Typical Seating Max Seating
A319-131 A319 V2522-A5 2 33.84 35.8 124 160

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
V2522-A5 SelectOne™ Upgrade Package International Aero Engines 102.5 4.9 25.7 Compare
PW6124A Pratt & Whitney 105.87 4.8 28 Compare
CFM56-3C-1 CFM56-3 CFM International 104.6 5.1 25.5 Compare
PW6122A Pratt & Whitney 98.31 4.8 25.7 Compare
CFM56-7B22/3 CFM56-7B CFM International 101 5.3 24.2 Compare
V2524-A5 SelectOne™ Upgrade Package International Aero Engines 108.9 4.8 27 Compare
All data (54 fields)
Name
V2522-A5
EASA ID
3IA006
Aircraft Engine Manufacturer
International Aero Engines
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.88
Overall Pressure Ratio
25.6
Maximum Takeoff Thrust (kN)
102.66
Hydrocarbon Take Off (g/kg fuel)
0.041
Hydrocarbon Climb Out (g/kg fuel)
0.041
Hydrocarbon Approach (g/kg fuel)
0.062
Hydrocarbon Idle (g/kg fuel)
0.103
Hydrocarbon Unitary Average (g/kN)
0.29
Hydrocarbon Unitary Characteristic (g/kN)
0.5
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
2.3
Hydrocarbon LTO (g)
30
Carbon Monoxide Take Off (g/kg fuel)
0.57
Carbon Monoxide Climb Out (g/kg fuel)
0.67
Carbon Monoxide Approach (g/kg fuel)
2.6
Carbon Monoxide Idle (g/kg fuel)
13.42
Carbon Monoxide Unitary Average (g/kN)
26.9
Carbon Monoxide Unitary Characteristic (g/kN)
33
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
28
NOx Take Off (g/kg fuel)
24.5
NOx Climb Out (g/kg fuel)
20.8
NOx Approach (g/kg fuel)
8.7
NOx Idle (g/kg fuel)
4.5
NOx Unitary Average (g/kN)
46
NOx Unitary Characteristic (g/kN)
53.3
NOx Unitaryto Standard (% of limit)
58.5
NOx Unitaryto CAEP2 (% of limit)
73.1
NOx Unitaryto CAEP4 (% of limit)
88.9
NOx Unitaryto CAEP6 (% of limit)
101.1
NOx Unitaryto CAEP8 (% of limit)
121.3
NOx LTO (g)
4720
Smoke Take Off (SN)
5.4
Smoke Climb Out (SN)
7.5
Smoke Approach (SN)
4
Smoke Idle (SN)
2.6
Smoke Max (SN)
9
Smoke Characteristic (SN)
11.6
Smoke Characteristicto Regulatory (% of limit)
49.4
Fuel Flow Take Off (kg/s)
0.971
Fuel Flow Climbout (kg/s)
0.817
Fuel Flow Approach (kg/s)
0.311
Fuel Flow Idle (kg/s)
0.118
Fuel LTO (kg)
407
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
2760
Emissions Data Status
C
Engine Status
Out of production