PW6000 engine

URI: https://gptkb.org/entity/PW6000_engine
GPTKB entity
Statements (45)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Airbus_A310-300
gptkbp:armament 24 fan blades
gptkbp:average_temperature up to 1,600 ° F
gptkbp:bypass_ratio 4.5:1
5.5:1
gptkbp:certification FAA certified
gptkbp:combustor_type annular combustor
gptkbp:compressor_type gptkb:6
axial compressor
gptkbp:configuration twin-spool
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter 68 inches
approximately 2.5 feet
gptkbp:emissions_standard ICAO Chapter 4
gptkbp:fan_art wide-chord fan blades
gptkbp:first_flight gptkb:1997
gptkbp:fuel_capacity 12 gallons
gptkbp:fuel_type gptkb:Jet_A
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label PW6000 engine
gptkbp:launched air starter
gptkbp:length 118 inches
approximately 11.5 feet
gptkbp:maintenance 6,000 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level Stage 3 compliant
gptkbp:original_run gptkb:1995
gptkbp:propulsion 15:1
24,000 lbf
18,500 to 24,000 lbf
60,000 to 70,000 lbf
gptkbp:service_ceiling 40,000 feet
gptkbp:service_entry gptkb:1998
gptkbp:total_engine_time over 1 million hours
gptkbp:turbine_type 2
two-stage high-pressure turbine
gptkbp:type high-bypass turbofan
gptkbp:used_in gptkb:Airbus
gptkbp:uses gptkb:Airbus
gptkbp:weight approximately 4,000 lbs
3,800 lb
gptkbp:bfsParent gptkb:Pratt_&_Whitney_Canada
gptkbp:bfsLayer 6