Hall-Scott A-7

http://dbpedia.org/resource/Hall-Scott_A-7 an entity of type: Software

The Hall-Scott A-7 was an early liquid-cooled aircraft engine manufactured by the Hall-Scott company of Berkeley, California. Using a straight-4 configuration, the engine developed 90 horsepower (67 kW) as the A-7 and 100 horsepower (75 kW) as the A-7a. In service these engines suffered from reliability problems and were prone to catch fire while in operation. rdf:langString
rdf:langString Hall-Scott A-7
xsd:integer 10144259
xsd:integer 1094375982
xsd:integer 1
rdf:langString at 1,400 rpm
rdf:langString Airplane Engine Encyclopedia
rdf:langString Four-cylinder inline piston engine
rdf:langString The Hall-Scott A-7 was an early liquid-cooled aircraft engine manufactured by the Hall-Scott company of Berkeley, California. Using a straight-4 configuration, the engine developed 90 horsepower (67 kW) as the A-7 and 100 horsepower (75 kW) as the A-7a. In service these engines suffered from reliability problems and were prone to catch fire while in operation.
rdf:langString Water
<second> 1910.0
rdf:langString Miller or Zenith carburetors
rdf:langString *List of aircraft engines
xsd:nonNegativeInteger 5091

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