Statements (87)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Liberty_XL-1
gptkb:Pipistrel_Sinus_912_ULS gptkb:Van's_Sidekick |
| gptkbp:aircraft_operated |
gptkb:Aero_AT-3
gptkb:Cessna_162_Skycatcher gptkb:Pipistrel_Alpha_Trainer gptkb:Aeroprakt_A22 gptkb:Rans_S-19_Venterra gptkb:Cessna_150 gptkb:Aero_Vodochody_L-39 gptkb:Evektor_Sport_Star gptkb:Flight_Design_CT gptkb:Pipistrel_Virus gptkb:Tecnam_P92 gptkb:Zenith_CH_701 gptkb:Jabiru_J160 gptkb:Rans_S-6_Coyote gptkb:Skycatcher_162 Avid Flyer |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
EASA certified
|
| gptkbp:compression_ratio |
10.5:1
|
| gptkbp:controls |
electronic control unit
mechanical or electronic |
| gptkbp:cooling_system |
liquid-cooled
ethylene glycol liquid and air cooled |
| gptkbp:displacement |
100 hp
|
| gptkbp:emissions_standard |
dual exhaust
|
| gptkbp:engine |
gptkb:4
four varied by model lightweight design high reliability 2000 hours global service network flat-four flat engine active user forums and support groups horizontally opposed rubber isolated available for performance enhancement alternator, starter motor flexible mounting options comprehensive manuals available widely used in ultralight aircraft |
| gptkbp:engine_type |
piston engine
912 ULS, 912 ULT, 912 ULM |
| gptkbp:first_introduced |
gptkb:1990
1990s |
| gptkbp:fuel_capacity |
3.5 L
approximately 10 L/h approximately 5.5-7.5 L/h |
| gptkbp:fuel_type |
aviation gasoline
carbureted or fuel injected MOGAS or AVGAS SAE 20 W-50 |
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 912 ULS
|
| gptkbp:ignition_system |
gptkb:NGK
dual ignition |
| gptkbp:is_often_used_in |
ultralight aircraft
|
| gptkbp:is_tested_for |
bench tested
|
| gptkbp:launch_site |
electric starter
electric start |
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:BRP-Rotax
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:noise_level |
low noise
low vibration |
| gptkbp:power_output |
100 hp at 5,500 rpm
100 hp at 5800 rpm |
| gptkbp:propulsion |
up to 1.8 m
variable-pitch propeller 1.2 kg/hp variable pitch or fixed pitch |
| gptkbp:regulatory_compliance |
FAR 33
|
| gptkbp:setting |
horizontally opposed
|
| gptkbp:torque |
105 Nm at 3,800 rpm
112 Nm at 5000 rpm |
| gptkbp:type |
four-stroke engine
|
| gptkbp:valve_configuration |
SOHC
2 valves per cylinder |
| gptkbp:warranty |
2 years or 1000 hours
|
| gptkbp:weight |
approximately 120 kg
approximately 60 kg |