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- Agusta_GA.40 abstract "The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 60s.".
- Agusta_GA.40 wikiPageID "31732111".
- Agusta_GA.40 wikiPageLength "2456".
- Agusta_GA.40 wikiPageOutDegree "16".
- Agusta_GA.40 wikiPageRevisionID "668339240".
- Agusta_GA.40 wikiPageWikiLink Agusta.
- Agusta_GA.40 wikiPageWikiLink Aircraft_engine.
- Agusta_GA.40 wikiPageWikiLink Category:Agusta_aircraft_engines.
- Agusta_GA.40 wikiPageWikiLink Category:Aircraft_piston_engines_1950–1959.
- Agusta_GA.40 wikiPageWikiLink Category:Boxer_engines.
- Agusta_GA.40 wikiPageWikiLink Corby_Starlet.
- Agusta_GA.40 wikiPageWikiLink Flat_engine.
- Agusta_GA.40 wikiPageWikiLink Horizontally_opposed.
- Agusta_GA.40 wikiPageWikiLink Italy.
- Agusta_GA.40 wikiPageWikiLink Kokkola_Ko-04.
- Agusta_GA.40 wikiPageWikiLink M._Ginnini.
- Agusta_GA.40 wikiPageWikiLink Motor_glider.
- Agusta_GA.40 wikiPageWikiLink Motorglider.
- Agusta_GA.40 wikiPageWikiLink Octane.
- Agusta_GA.40 wikiPageWikiLink Stromberg_NAS_3A1_carburettor.
- Agusta_GA.40 wikiPageWikiLink Zenith_carburettor.
- Agusta_GA.40 wikiPageWikiLinkText "Agusta GA.40".
- Agusta_GA.40 coolingsystem "Air-cooled".
- Agusta_GA.40 designer M._Ginnini.
- Agusta_GA.40 designer "M. Ginnini".
- Agusta_GA.40 firstRun "1955".
- Agusta_GA.40 fuelsystem Stromberg_NAS_3A1_carburettor.
- Agusta_GA.40 fuelsystem Zenith_carburettor.
- Agusta_GA.40 fueltype "80".
- Agusta_GA.40 hasPhotoCollection Agusta_GA.40.
- Agusta_GA.40 manufacturer Agusta.
- Agusta_GA.40 nationalOrigin Italy.
- Agusta_GA.40 oilsystem "Pressure lubrication with a gear driven pump".
- Agusta_GA.40 power "at 2,700rpm".
- Agusta_GA.40 weight "0.559".
- Agusta_GA.40 ref "Jane's All the World's Aircraft 1962-63".
- Agusta_GA.40 specpower "20.99".
- Agusta_GA.40 type "2".
- Agusta_GA.40 type "4".
- Agusta_GA.40 unitCost "$685 in 1958".
- Agusta_GA.40 valvetrain "pushrod operated overhead valve, 1x inlet + 1x exhaust per cylinder".
- Agusta_GA.40 weight "dry".
- Agusta_GA.40 wikiPageUsesTemplate Template:AgustaWestland_aircraft.
- Agusta_GA.40 wikiPageUsesTemplate Template:Cite_book.
- Agusta_GA.40 wikiPageUsesTemplate Template:Commons_category.
- Agusta_GA.40 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Agusta_GA.40 wikiPageUsesTemplate Template:Pistonspecs.
- Agusta_GA.40 wikiPageUsesTemplate Template:Refbegin.
- Agusta_GA.40 wikiPageUsesTemplate Template:Refend.
- Agusta_GA.40 wikiPageUsesTemplate Template:Reflist.
- Agusta_GA.40 subject Category:Agusta_aircraft_engines.
- Agusta_GA.40 subject Category:Aircraft_piston_engines_1950–1959.
- Agusta_GA.40 subject Category:Boxer_engines.
- Agusta_GA.40 hypernym Cylinder.
- Agusta_GA.40 type MeanOfTransportation.
- Agusta_GA.40 comment "The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 60s.".
- Agusta_GA.40 label "Agusta GA.40".
- Agusta_GA.40 sameAs Agusta_GA.40.
- Agusta_GA.40 sameAs m.0gtt1nm.
- Agusta_GA.40 sameAs Agusta_GA.40.
- Agusta_GA.40 sameAs Q4694616.
- Agusta_GA.40 sameAs Q4694616.
- Agusta_GA.40 wasDerivedFrom Agusta_GA.40?oldid=668339240.
- Agusta_GA.40 isPrimaryTopicOf Agusta_GA.40.