V2524-A5

Turbofan · International Aero Engines
Reaction Turbines
Maximum Takeoff Thrust
109.06 kN
Bypass Ratio
4.81
Overall Pressure Ratio
26.9
Fuel Flow Take Off
1.042 kg/s
NOx Unitaryto CAEP8
122.6 % 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 —
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 4.81 Overall Pressure Ratio 26.9 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
A319-132 A319 V2524-A5 2 33.84 35.8 124 160

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
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
V2525-D5 International Aero Engines 111.2 4.82 27.2 Compare
V2527-A5 International Aero Engines 111.2 4.82 27.2 Compare
All data (54 fields)
Name
V2524-A5
EASA ID
3IA007
Aircraft Engine Manufacturer
International Aero Engines
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.81
Overall Pressure Ratio
26.9
Maximum Takeoff Thrust (kN)
109.06
Hydrocarbon Take Off (g/kg fuel)
0.042
Hydrocarbon Climb Out (g/kg fuel)
0.042
Hydrocarbon Approach (g/kg fuel)
0.061
Hydrocarbon Idle (g/kg fuel)
0.1
Hydrocarbon Unitary Average (g/kN)
0.28
Hydrocarbon Unitary Characteristic (g/kN)
0.4
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
2.2
Hydrocarbon LTO (g)
31
Carbon Monoxide Take Off (g/kg fuel)
0.54
Carbon Monoxide Climb Out (g/kg fuel)
0.63
Carbon Monoxide Approach (g/kg fuel)
2.37
Carbon Monoxide Idle (g/kg fuel)
12.64
Carbon Monoxide Unitary Average (g/kN)
24.8
Carbon Monoxide Unitary Characteristic (g/kN)
30.4
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
25.8
NOx Take Off (g/kg fuel)
26.2
NOx Climb Out (g/kg fuel)
22
NOx Approach (g/kg fuel)
9
NOx Idle (g/kg fuel)
4.7
NOx Unitary Average (g/kN)
48.4
NOx Unitary Characteristic (g/kN)
56.1
NOx Unitaryto Standard (% of limit)
59.8
NOx Unitaryto CAEP2 (% of limit)
74.8
NOx Unitaryto CAEP4 (% of limit)
90.4
NOx Unitaryto CAEP6 (% of limit)
102.8
NOx Unitaryto CAEP8 (% of limit)
122.6
NOx LTO (g)
5278
Smoke Take Off (SN)
5.2
Smoke Climb Out (SN)
7.2
Smoke Approach (SN)
4.2
Smoke Idle (SN)
2.6
Smoke Max (SN)
9
Smoke Characteristic (SN)
11.6
Smoke Characteristicto Regulatory (% of limit)
50.2
Fuel Flow Take Off (kg/s)
1.042
Fuel Flow Climbout (kg/s)
0.868
Fuel Flow Approach (kg/s)
0.328
Fuel Flow Idle (kg/s)
0.123
Fuel LTO (kg)
429
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
2708
Emissions Data Status
C
Engine Status
Out of production