Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Aviat_Super_Decathlon
|
| gptkbp:application |
gptkb:Piper_PA-32
gptkb:Beechcraft_Bonanza gptkb:Cessna_182 |
| gptkbp:ceo |
1,500 hours
|
| gptkbp:compression_ratio |
8.5:1 to 10:1
|
| gptkbp:controls |
throttle and mixture control
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
540 cubic inches
|
| gptkbp:emissions_standard |
dual exhaust
|
| gptkbp:engine |
aluminum alloy
inline engine front-mounted major overhaul required every 1,500 hours Lycoming IO-540 family up to 2,000 hours with proper maintenance |
| gptkbp:engine_type |
reciprocating engine
gear-driven camshaft AEIO-540-K1 A5 AEIO-540-L1 A5 AEIO-540-L2 A AEIO-540-U AEIO-540-U1 A5 |
| gptkbp:fins |
integrated cooling fins
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:fuel_capacity |
12 quarts
|
| gptkbp:fuel_type |
aviation gasoline
carbureted or fuel injected aviation grade oil |
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming AEIO-540
|
| gptkbp:ignition_system |
dual ignition
Champion RE M40 E |
| gptkbp:is_tested_for |
bench testing required
|
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:modifications |
turbocharging
propeller upgrades fuel injection conversion |
| gptkbp:power_output |
250 to 300 horsepower
|
| gptkbp:propulsion |
constant speed propeller
0.83 hp/lb |
| gptkbp:regulatory_compliance |
FAA certified
|
| gptkbp:service_ceiling |
15,000 feet
|
| gptkbp:setting |
6-cylinder
|
| gptkbp:type |
horizontally opposed engine
|
| gptkbp:used_in |
general aviation aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:water_source |
up to 30 gallons per hour
|
| gptkbp:weight |
approximately 300 lbs
|