|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Tecnam_P2006_T
|
|
gptkbp:aircraft_operated
|
gptkb:Aero_AT-3
gptkb:aircraft
gptkb:Cessna_162_Skycatcher
gptkb:Pipistrel_Alpha_Trainer
gptkb:Beechcraft_Bonanza
gptkb:Grumman_AA-5
gptkb:Mooney_M20
gptkb:Cessna_150
gptkb:Aero_Vodochody_L-39_Albatros
gptkb:Evektor_Sport_Star
gptkb:Pipistrel_Virus
gptkb:Tecnam_P92
gptkb:Zenith_CH_701
gptkb:Aeroprakt_A-22
gptkb:Flight_Design_CT_series
gptkb:Jabiru_J160
gptkb:Quicksilver_MX_series
gptkb:Rans_S-6_Coyote
gptkb:Skycatcher_162
Piper PA-28
Diamond D A40
Diamond D A20
Cirrus S R20
Sierra 2000
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
EASA and FAA certified
|
|
gptkbp:compression_ratio
|
10.5:1
|
|
gptkbp:cooling_system
|
liquid-cooled
air-cooled and liquid-cooled options
|
|
gptkbp:displacement
|
100 hp
|
|
gptkbp:engine
|
gptkb:4
flat-four
flat engine
horizontally opposed
|
|
gptkbp:engine_type
|
reciprocating engine
|
|
gptkbp:first_introduced
|
gptkb:1989
|
|
gptkbp:fuel_capacity
|
3.5 liters
approximately 10 L/h
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted or fuel injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rotax 912 S
|
|
gptkbp:ignition_system
|
gptkb:NGK
dual ignition
|
|
gptkbp:is_often_used_in
|
ultralight and light sport aircraft
|
|
gptkbp:maintenance
|
100 hours or annually
|
|
gptkbp:manufacturer
|
gptkb:BRP-Rotax
|
|
gptkbp:marketed_as
|
912 S
|
|
gptkbp:max_speed
|
5500
|
|
gptkbp:power_output
|
73 k W
|
|
gptkbp:propulsion
|
constant speed or fixed pitch
|
|
gptkbp:successor
|
gptkb:Rotax_912i_S
|
|
gptkbp:torque
|
100 Nm at 4200 RPM
|
|
gptkbp:type
|
four-stroke engine
|
|
gptkbp:valve_configuration
|
SOHC
|
|
gptkbp:weight
|
approximately 60 kg
|