Statements (48)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:application |
aircraft
|
| gptkbp:bore |
5.125 inches
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:controls |
mechanical throttle
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:cylinderCount |
horizontally opposed
|
| gptkbp:displacement |
550 cubic inches
|
| gptkbp:drivetrain |
overhead valve
|
| gptkbp:engine |
300 lb-ft
high reliability air-cooled electric starter light aircraft dual ignition system front-mounted |
| gptkbp:engineConfiguration |
V-type
wet sump |
| gptkbp:engineDisplacement |
modular design
|
| gptkbp:engineType |
requires regular inspections
reciprocating engine excellent climb rate moderate fuel efficiency widely used in general aviation FAA_certified GTSIO-550-U |
| gptkbp:firstIntroduced |
1960s
|
| gptkbp:fuelCapacity |
12 quarts
15-20 gallons per hour |
| gptkbp:fuelType |
aviation gasoline
carbureted dual magneto Champion_REM40E |
| gptkbp:hasArea |
bench tested
|
| https://www.w3.org/2000/01/rdf-schema#label |
GTSIO-550 engine
|
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
Teledyne_Continental_Motors
|
| gptkbp:mayHave |
1800 hours
|
| gptkbp:operationalHistory |
developed for general aviation
|
| gptkbp:performance |
high power-to-weight ratio
|
| gptkbp:powers |
300 horsepower
|
| gptkbp:propulsion |
constant speed
|
| gptkbp:related_engine |
GTSIO series
|
| gptkbp:relatedApplication |
Cessna_206,_Piper_Aerostar
|
| gptkbp:setting |
6-cylinder
|
| gptkbp:stroke |
4.0 inches
|
| gptkbp:type |
horizontally opposed engine
|
| gptkbp:weight |
approximately 360 lbs
|