Rotax 914

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:MQ-1_Predator
gptkbp:aircraft_operated gptkb:Aero_AT-3
gptkb:aircraft
gptkb:Pipistrel_Alpha_Trainer
gptkb:Cessna_162
gptkb:Aero_AT-4
gptkb:Aero_Vodochody_L-159
gptkb:Aero_Vodochody_L-39
gptkb:Aero_Vodochody_L-39_Albatros
gptkb:Aero_Vodochody_L-39_C
gptkb:Aero_Vodochody_L-39_ZA
gptkb:Aero_Vodochody_L-59
gptkb:Evektor_Sport_Star
gptkb:Flight_Design_CT
gptkb:Pipistrel_Virus
gptkb:Rans_S-6
gptkb:Tecnam_P92
gptkb:Zenith_CH_701
Aerospool W T9
Diamond D A20
Skyboy
gptkbp:application gptkb:aircraft
gptkbp:certification EASA certified
gptkbp:compression_ratio 8.5:1
gptkbp:controls electronic fuel injection
gptkbp:cooling_system liquid-cooled
liquid and air cooled
gptkbp:displacement 1,200 cc
gptkbp:engine gptkb:4
gptkbp:engine_type turbocharged
gptkbp:first_introduced 1990s
gptkbp:fuel_capacity approximately 600 mm
4.5 L
approximately 500 mm
approximately 400 mm
approximately 30 L/h
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Rotax 914
gptkbp:ignition_system gptkb:4
dual ignition
gptkbp:is_often_used_in ultralight aircraft
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:BRP-Rotax
gptkbp:market_segment general aviation
gptkbp:max_speed 5,800 RPM
gptkbp:powers 100 hp
gptkbp:propulsion constant speed propeller
gptkbp:setting inline-four
gptkbp:torque 120 Nm
gptkbp:type four-stroke engine
gptkbp:valve_configuration DOHC
gptkbp:weight approximately 70 kg