Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:SNECMA
gptkb:IAE_V2500 |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:armament |
composite materials
|
| gptkbp:average_temperature |
high operating temperature
|
| gptkbp:bypass_ratio |
4.5:1
|
| gptkbp:certification |
certified by FAA and EASA
|
| gptkbp:competes_with |
CF M56
|
| gptkbp:compression_ratio |
high pressure ratio engine
|
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1.8 m
|
| gptkbp:emissions_standard |
low N Ox emissions
|
| gptkbp:engine |
high performance
high reliability global support network air start pylon-mounted advanced engine technology upgrade options available two engines per aircraft fuel-efficient commercial aviation engine legacy engine in service |
| gptkbp:engine_type |
gptkb:V2500-D5
gptkb:V2500-E5 turbofan axial high-pressure and low-pressure V2500-A5 Plus V2500-A5 Select compatible with A320neo |
| gptkbp:first_flight |
gptkb:1988
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
V2500-A5
|
| gptkbp:length |
2.8 m
|
| gptkbp:maintenance |
4,000 hours
scheduled maintenance required |
| gptkbp:manufacturer |
gptkb:International_Aero_Engines
|
| gptkbp:market |
significant in narrow-body aircraft
|
| gptkbp:noise_level |
noise reduction technologies
Stage 3 compliant |
| gptkbp:notable_users |
Airbus, Indian Airlines
|
| gptkbp:produced_by |
over 6,000 engines
|
| gptkbp:propulsion |
22,000 to 33,000 lbf
7.33:1 |
| gptkbp:services |
gptkb:1997
|
| gptkbp:setting |
dual-spool
|
| gptkbp:weight |
3,000 kg
|