V2500-A1

Turbofan · International Aero Engines

Reaction Turbines

Maximum Takeoff Thrust

111.2 kN

Bypass Ratio

5.3

Overall Pressure Ratio

29.8

Fuel Flow Take Off

1.113 kg/s

NOx Unitaryto CAEP8

161.1 % of limit

First Flight

1988-05-07

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 5.3	Overall Pressure Ratio 29.8	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
A320-231	A320	V2500-A1	2	37.57	35.8	150	180

Similar reaction turbines

Name	Family	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
CFM56-7B24/3	CFM56-7B	CFM International	107.6	5.3	25.6	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
V2527E-A5		International Aero Engines	111.2	4.82	27.2	Compare
V2527M-A5		International Aero Engines	111.2	4.82	27.2	Compare
V2527-A5 SelectOne™ Upgrade Package		International Aero Engines	110.3	4.8	27.1	Compare

All data (52 fields)

Name: V2500-A1
EASA ID: 1IA001
Aircraft Engine Manufacturer: International Aero Engines
Aircraft Engine Type: Turbofan
FETT: 1985-12-12
First Flight: 1988-05-07
Fuel: Jet A
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 5.3
Overall Pressure Ratio: 29.8
Maximum Takeoff Thrust (kN): 111.2
Hydrocarbon Take Off (g/kg fuel): 0.1
Hydrocarbon Climb Out (g/kg fuel): 0.11
Hydrocarbon Approach (g/kg fuel): 0.15
Hydrocarbon Idle (g/kg fuel): 0.22
Hydrocarbon Unitary Average (g/kN): 0.65
Hydrocarbon Unitary Characteristic (g/kN): 1
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 5.1
Hydrocarbon LTO (g): 73
Carbon Monoxide Take Off (g/kg fuel): 0.55
Carbon Monoxide Climb Out (g/kg fuel): 0.55
Carbon Monoxide Approach (g/kg fuel): 0.77
Carbon Monoxide Idle (g/kg fuel): 7.76
Carbon Monoxide Unitary Average (g/kN): 14.8
Carbon Monoxide Unitary Characteristic (g/kN): 18.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 15.4
NOx Take Off (g/kg fuel): 37.13
NOx Climb Out (g/kg fuel): 30.82
NOx Approach (g/kg fuel): 13.45
NOx Idle (g/kg fuel): 5.91
NOx Unitary Average (g/kN): 69.3
NOx Unitary Characteristic (g/kN): 80.3
NOx Unitaryto Standard (% of limit): 80.7
NOx Unitaryto CAEP2 (% of limit): 100.8
NOx Unitaryto CAEP4 (% of limit): 120.5
NOx Unitaryto CAEP6 (% of limit): 136.9
NOx Unitaryto CAEP8 (% of limit): 161.1
NOx LTO (g): 7716
Smoke Max (SN): 3.5
Smoke Characteristic (SN): 4.5
Smoke Characteristicto Regulatory (% of limit): 19.6
Fuel Flow Take Off (kg/s): 1.113
Fuel Flow Climbout (kg/s): 0.924
Fuel Flow Approach (kg/s): 0.334
Fuel Flow Idle (kg/s): 0.124
Fuel LTO (kg): 442
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 1656
Emissions Data Status: C
Engine Status: Out of production

Airplanes 1