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- Avia_Rk.12 abstract "One of Avia's own designs, the 1930s Avia Rk.12 was a 7-cylinder radial engine with a rated output of 150 kW (200 hp), built in Czechoslovakia.".
- Avia_Rk.12 wikiPageID "30078459".
- Avia_Rk.12 wikiPageLength "3679".
- Avia_Rk.12 wikiPageOutDegree "16".
- Avia_Rk.12 wikiPageRevisionID "668349492".
- Avia_Rk.12 wikiPageWikiLink Avia_51.
- Avia_Rk.12 wikiPageWikiLink Category:Aircraft_piston_engines_1930–1939.
- Avia_Rk.12 wikiPageWikiLink Category:Radial_engines.
- Avia_Rk.12 wikiPageWikiLink Crankcase.
- Avia_Rk.12 wikiPageWikiLink Crankshaft.
- Avia_Rk.12 wikiPageWikiLink Czechoslovakia.
- Avia_Rk.12 wikiPageWikiLink Hispano-Suiza.
- Avia_Rk.12 wikiPageWikiLink Lorraine-Dietrich.
- Avia_Rk.12 wikiPageWikiLink Master_rod.
- Avia_Rk.12 wikiPageWikiLink Piston.
- Avia_Rk.12 wikiPageWikiLink Piston_rod.
- Avia_Rk.12 wikiPageWikiLink Prague.
- Avia_Rk.12 wikiPageWikiLink Radial_engine.
- Avia_Rk.12 wikiPageWikiLink Supercharger.
- Avia_Rk.12 wikiPageWikiLink Y_alloy.
- Avia_Rk.12 wikiPageWikiLink Zenith_Carburettor_Company_(British).
- Avia_Rk.12 wikiPageWikiLinkText "Avia Rk.12".
- Avia_Rk.12 wikiPageWikiLinkText "Rk.12".
- Avia_Rk.12 bore "130.0".
- Avia_Rk.12 compression "5.3".
- Avia_Rk.12 coolingsystem "air-cooled".
- Avia_Rk.12 diameter "1110.0".
- Avia_Rk.12 displacement "12.08".
- Avia_Rk.12 fuelcon "62".
- Avia_Rk.12 fuelsystem "single barrel Zenith 70P or Stromberg NAR68 carburettor * Ignition system: Scintilla magnetos, automatic advance".
- Avia_Rk.12 fueltype "petrol, 74 Octane".
- Avia_Rk.12 length "1047.5".
- Avia_Rk.12 manufacturer "Avia , Prague".
- Avia_Rk.12 nationalOrigin Czechoslovakia.
- Avia_Rk.12 oilcon "at cruising speed, 2 kg/h".
- Avia_Rk.12 oilsystem "dry sump, with one pressure and one scavenging pump".
- Avia_Rk.12 power "180000.0".
- Avia_Rk.12 reductionGear "direct drive".
- Avia_Rk.12 ref "Jane's All the World's Aircraft 1938".
- Avia_Rk.12 stroke "130.0".
- Avia_Rk.12 supercharger "impeller drive ratio 10.7:1".
- Avia_Rk.12 type "7".
- Avia_Rk.12 valvetrain "one inlet and one exhaust valve per cylinder, operated by push rods via rocker gear. Six cam push rod disc drive.".
- Avia_Rk.12 weight "dry, with ancillaries, without propeller hub 215.5 kg".
- Avia_Rk.12 wikiPageUsesTemplate Template:Aircontent.
- Avia_Rk.12 wikiPageUsesTemplate Template:Avia_aeroengines.
- Avia_Rk.12 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Avia_Rk.12 wikiPageUsesTemplate Template:Pistonspecs.
- Avia_Rk.12 wikiPageUsesTemplate Template:Reflist.
- Avia_Rk.12 subject Category:Aircraft_piston_engines_1930–1939.
- Avia_Rk.12 subject Category:Radial_engines.
- Avia_Rk.12 hypernym Engine.
- Avia_Rk.12 type Software.
- Avia_Rk.12 comment "One of Avia's own designs, the 1930s Avia Rk.12 was a 7-cylinder radial engine with a rated output of 150 kW (200 hp), built in Czechoslovakia.".
- Avia_Rk.12 label "Avia Rk.12".
- Avia_Rk.12 sameAs Q4828509.
- Avia_Rk.12 sameAs m.0g57q5c.
- Avia_Rk.12 sameAs Q4828509.
- Avia_Rk.12 wasDerivedFrom Avia_Rk.12?oldid=668349492.
- Avia_Rk.12 isPrimaryTopicOf Avia_Rk.12.