Nelson H-63
http://dbpedia.org/resource/Nelson_H-63 an entity of type: WikicatNelsonAircraftEngines
The Nelson H-63, known in the US military designation system as the YO-65, is an American dual ignition, four-cylinder, horizontally opposed, two-stroke aircraft engine that was developed by the Nelson Engine Company for use in helicopters and light aircraft. The engine designation means horizontally opposed 63 cubic inch displacement.
rdf:langString
rdf:langString
Nelson H-63
xsd:integer
31173759
xsd:integer
1111456712
xsd:integer
2
rdf:langString
at 4000 rpm
rdf:langString
FAA Type Certificate Data Sheet, Aircraft engines of the World 1957
rdf:langString
Two-stroke aircraft engine
rdf:langString
Four-cylinder, two-stroke, dual ignition, vertically mounted helicopter engine
rdf:langString
Bare engine: ; including the cooling fan, cooling shroud and clutch
rdf:langString
The Nelson H-63, known in the US military designation system as the YO-65, is an American dual ignition, four-cylinder, horizontally opposed, two-stroke aircraft engine that was developed by the Nelson Engine Company for use in helicopters and light aircraft. The engine designation means horizontally opposed 63 cubic inch displacement.
xsd:integer
8
rdf:langString
fan forced air
xsd:integer
63
rdf:langString
Nelson E-500 carburetor
xsd:integer
80
rdf:langString
premixed oil in fuel, SAE 30 outboard motor oil mixed at 16:1 fuel to oil
rdf:langString
none
rdf:langString
*List of aircraft engines
xsd:nonNegativeInteger
5283