Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:C-85_A
|
| gptkbp:application |
gptkb:Taylorcraft_BC-12_D
gptkb:Cessna_140 gptkb:Piper_J-3_Cub gptkb:Aeronca_Champ |
| gptkbp:ceo |
1800 hours
|
| gptkbp:compression_ratio |
7.0:1
|
| gptkbp:cooling_system |
air-cooled
air-cooled engine |
| gptkbp:displacement |
85 cubic inches
1397 cc |
| gptkbp:engine |
gptkb:historical_event
gptkb:4 community support smooth operation lightweight design high reliability low maintenance easy installation inline engine versatile applications horizontally opposed proven track record retractable landing gear dual ignition good fuel efficiency good resale value widely used in homebuilt aircraft available parts support popular choice for trainers |
| gptkbp:engine_type |
four-stroke engine
|
| gptkbp:first_introduced |
1946
|
| gptkbp:fuel_capacity |
6 quarts
8-10 gallons per hour |
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental C85
|
| gptkbp:ignition_system |
magneto ignition
Champion RE M40 |
| gptkbp:maintenance |
50 hours
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:max_speed |
2700 RPM
|
| gptkbp:power_output |
85 horsepower
|
| gptkbp:propulsion |
fixed-pitch propeller
|
| gptkbp:setting |
inline-four
|
| gptkbp:successor |
gptkb:Continental_O-200
|
| gptkbp:type |
reciprocating engine
|
| gptkbp:used_in |
general aviation aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
approximately 150 pounds
|