PW1200 G-9

URI: https://gptkb.org/entity/PW1200_G-9
GPTKB entity
Statements (31)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application regional jets
gptkbp:average_temperature high
gptkbp:bypass_ratio 9:1
gptkbp:cancellation_reason yes
gptkbp:certification gptkb:FAA
CAEP/6
gptkbp:competitors gptkb:CF34
gptkbp:compressor_type gptkb:3
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:design_purpose fuel efficiency
gptkbp:development gptkb:GTF_engine_family
gptkbp:diameter 81 in
gptkbp:fuel_type gptkb:Jet_A
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label PW1200 G-9
gptkbp:involved_technology geared fan technology
gptkbp:length 90 in
gptkbp:maintenance 5,000 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:market_segment commercial aviation
gptkbp:maximum_diameter 28 in
gptkbp:original_run gptkb:2013
gptkbp:propulsion 18,000 lbf
gptkbp:service_entry gptkb:2016
gptkbp:turbine_type 2
gptkbp:type geared turbofan
gptkbp:used_in gptkb:Bombardier_CSeries
gptkbp:weight 1,500 lb
gptkbp:bfsParent gptkb:Pratt_&_Whitney_PW1200_G
gptkbp:bfsLayer 6