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- Agusta_GA.70 abstract "The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally opposed engine developed in Italy for light aircraft and helicopter use. The GA.70/V featured a bottom sump for vertical applications and was rated at 158 hp. It was produced in the 1950s and 60s.".
- Agusta_GA.70 wikiPageExternalLink Agusta.html.
- Agusta_GA.70 wikiPageID "10362183".
- Agusta_GA.70 wikiPageLength "3146".
- Agusta_GA.70 wikiPageOutDegree "14".
- Agusta_GA.70 wikiPageRevisionID "668339249".
- Agusta_GA.70 wikiPageWikiLink Agusta.
- Agusta_GA.70 wikiPageWikiLink Agusta_A.103.
- Agusta_GA.70 wikiPageWikiLink Bölkow_Bo_103.
- Agusta_GA.70 wikiPageWikiLink Category:Agusta_aircraft_engines.
- Agusta_GA.70 wikiPageWikiLink Category:Aircraft_piston_engines_1950–1959.
- Agusta_GA.70 wikiPageWikiLink Category:Boxer_engines.
- Agusta_GA.70 wikiPageWikiLink De_Bernardi_Aeroscooter.
- Agusta_GA.70 wikiPageWikiLink Flat_engine.
- Agusta_GA.70 wikiPageWikiLink Horizontally_opposed.
- Agusta_GA.70 wikiPageWikiLink Italy.
- Agusta_GA.70 wikiPageWikiLink M._Ginnini.
- Agusta_GA.70 wikiPageWikiLink Octane.
- Agusta_GA.70 wikiPageWikiLink Phoenix_Major.
- Agusta_GA.70 wikiPageWikiLink Phoenix_Minor.
- Agusta_GA.70 wikiPageWikiLink Stromberg_NAS_3_carburettor.
- Agusta_GA.70 wikiPageWikiLink Zenith_carburettor.
- Agusta_GA.70 wikiPageWikiLinkText "Agusta GA.70".
- Agusta_GA.70 wikiPageWikiLinkText "GA.70".
- Agusta_GA.70 coolingsystem "Air-cooled".
- Agusta_GA.70 designer M._Ginnini.
- Agusta_GA.70 firstRun "1955".
- Agusta_GA.70 fuelsystem Stromberg_NAS_3_carburettor.
- Agusta_GA.70 fuelsystem Zenith_carburettor.
- Agusta_GA.70 fueltype "80".
- Agusta_GA.70 hasPhotoCollection Agusta_GA.70.
- Agusta_GA.70 height ",".
- Agusta_GA.70 length ",".
- Agusta_GA.70 manufacturer Agusta.
- Agusta_GA.70 nationalOrigin Italy.
- Agusta_GA.70 oilsystem "Pressure lubrication with a gear driven pump".
- Agusta_GA.70 power "at 3,100rpm,".
- Agusta_GA.70 weight "0.671".
- Agusta_GA.70 ref "Jane's All the World's Aircraft 1962-63".
- Agusta_GA.70 specpower "23.352".
- Agusta_GA.70 type "4".
- Agusta_GA.70 unitCost "$1010 for the GA.70/O, $1340 for the GA.70/V in 1958".
- Agusta_GA.70 valvetrain "pushrod operated overhead valve, 2x inlet + 2x exhaust per cylinder".
- Agusta_GA.70 weight "dry".
- Agusta_GA.70 width ",".
- Agusta_GA.70 wikiPageUsesTemplate Template:AgustaWestland_aircraft.
- Agusta_GA.70 wikiPageUsesTemplate Template:Cite_book.
- Agusta_GA.70 wikiPageUsesTemplate Template:Commons_category.
- Agusta_GA.70 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Agusta_GA.70 wikiPageUsesTemplate Template:Pistonspecs.
- Agusta_GA.70 wikiPageUsesTemplate Template:Refbegin.
- Agusta_GA.70 wikiPageUsesTemplate Template:Refend.
- Agusta_GA.70 wikiPageUsesTemplate Template:Reflist.
- Agusta_GA.70 subject Category:Agusta_aircraft_engines.
- Agusta_GA.70 subject Category:Aircraft_piston_engines_1950–1959.
- Agusta_GA.70 subject Category:Boxer_engines.
- Agusta_GA.70 hypernym Cylinder.
- Agusta_GA.70 type MeanOfTransportation.
- Agusta_GA.70 comment "The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally opposed engine developed in Italy for light aircraft and helicopter use. The GA.70/V featured a bottom sump for vertical applications and was rated at 158 hp. It was produced in the 1950s and 60s.".
- Agusta_GA.70 label "Agusta GA.70".
- Agusta_GA.70 sameAs Agusta_GA.70.
- Agusta_GA.70 sameAs m.02q9gbh.
- Agusta_GA.70 sameAs Agusta_GA.70.
- Agusta_GA.70 sameAs Q4694617.
- Agusta_GA.70 sameAs Q4694617.
- Agusta_GA.70 wasDerivedFrom Agusta_GA.70?oldid=668339249.
- Agusta_GA.70 isPrimaryTopicOf Agusta_GA.70.