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- Avia_Rk.17 abstract "One of Avia's own designs and built in Czechoslovakia, the 1930s Avia Rk.17 was a 9-cylinder radial engine, developed from the 7-cylinder Avia Rk.12, with a rated output of 270 kW (360 hp).".
- Avia_Rk.17 wikiPageID "30087889".
- Avia_Rk.17 wikiPageLength "4232".
- Avia_Rk.17 wikiPageOutDegree "23".
- Avia_Rk.17 wikiPageRevisionID "694513473".
- Avia_Rk.17 wikiPageWikiLink Avia.
- Avia_Rk.17 wikiPageWikiLink Avia_B.122.
- Avia_Rk.17 wikiPageWikiLink Avia_Rk.12.
- Avia_Rk.17 wikiPageWikiLink Category:Aircraft_piston_engines_1930–1939.
- Avia_Rk.17 wikiPageWikiLink Category:Radial_engines.
- Avia_Rk.17 wikiPageWikiLink Crankcase.
- Avia_Rk.17 wikiPageWikiLink Crankshaft.
- Avia_Rk.17 wikiPageWikiLink Czechoslovakia.
- Avia_Rk.17 wikiPageWikiLink Hispano-Suiza.
- Avia_Rk.17 wikiPageWikiLink Letov_Š-50.
- Avia_Rk.17 wikiPageWikiLink Lorraine-Dietrich.
- Avia_Rk.17 wikiPageWikiLink Master_rod.
- Avia_Rk.17 wikiPageWikiLink Piston.
- Avia_Rk.17 wikiPageWikiLink Piston_rod.
- Avia_Rk.17 wikiPageWikiLink Prague.
- Avia_Rk.17 wikiPageWikiLink Prague_Aviation_Museum,_Kbely.
- Avia_Rk.17 wikiPageWikiLink Radial_engine.
- Avia_Rk.17 wikiPageWikiLink Rated_output.
- Avia_Rk.17 wikiPageWikiLink Supercharger.
- Avia_Rk.17 wikiPageWikiLink Y_alloy.
- Avia_Rk.17 wikiPageWikiLinkText "Avia Rk.17".
- Avia_Rk.17 bore "130.0".
- Avia_Rk.17 compression "6.4".
- Avia_Rk.17 coolingsystem "air-cooled".
- Avia_Rk.17 diameter "1184.0".
- Avia_Rk.17 displacement "16.72".
- Avia_Rk.17 fuelsystem "single barrel Stromberg NAR80G carburettor * Ignition system: Scintilla magnetos, automatic advance".
- Avia_Rk.17 fueltype "petrol, 85 Octane".
- Avia_Rk.17 length "1065.0".
- Avia_Rk.17 manufacturer Avia.
- Avia_Rk.17 manufacturer Prague.
- Avia_Rk.17 nationalOrigin Czechoslovakia.
- Avia_Rk.17 oilcon "8.7".
- Avia_Rk.17 oilsystem "dry sump, with one pressure and one scavenging pump".
- Avia_Rk.17 power "165000.0".
- Avia_Rk.17 reductionGear "direct drive".
- Avia_Rk.17 ref "Jane's All the World's Aircraft 1938".
- Avia_Rk.17 specfuelcon "255".
- Avia_Rk.17 stroke "140.0".
- Avia_Rk.17 supercharger "impeller drive ratio 10.7:1".
- Avia_Rk.17 type "9".
- Avia_Rk.17 valvetrain "one inlet and one exhaust valve per cylinder, operated by push-rods via rocker gear. Eight cam push-rod disc drive.".
- Avia_Rk.17 weight "260".
- Avia_Rk.17 wikiPageUsesTemplate Template:Aircontent.
- Avia_Rk.17 wikiPageUsesTemplate Template:Avia_aeroengines.
- Avia_Rk.17 wikiPageUsesTemplate Template:Cite_book.
- Avia_Rk.17 wikiPageUsesTemplate Template:Commons_category.
- Avia_Rk.17 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Avia_Rk.17 wikiPageUsesTemplate Template:Pistonspecs.
- Avia_Rk.17 wikiPageUsesTemplate Template:Reflist.
- Avia_Rk.17 subject Category:Aircraft_piston_engines_1930–1939.
- Avia_Rk.17 subject Category:Radial_engines.
- Avia_Rk.17 hypernym Engine.
- Avia_Rk.17 type Software.
- Avia_Rk.17 comment "One of Avia's own designs and built in Czechoslovakia, the 1930s Avia Rk.17 was a 9-cylinder radial engine, developed from the 7-cylinder Avia Rk.12, with a rated output of 270 kW (360 hp).".
- Avia_Rk.17 label "Avia Rk.17".
- Avia_Rk.17 sameAs Q4828510.
- Avia_Rk.17 sameAs m.0g58t_w.
- Avia_Rk.17 sameAs Avia_Rk.17.
- Avia_Rk.17 sameAs Q4828510.
- Avia_Rk.17 wasDerivedFrom Avia_Rk.17?oldid=694513473.
- Avia_Rk.17 isPrimaryTopicOf Avia_Rk.17.