Pratt & Whitney R-1340 Wasp

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:piston_engine
gptkbp:bore	5.75 in
gptkbp:category	1920s aircraft piston engines air-cooled radial piston engines
gptkbp:coolingSystem	air-cooled
gptkbp:diameter	51.5 in
gptkbp:displacement	1,344 in³
gptkbp:engineType	gptkb:piston_engine
gptkbp:firstFlight	1925
gptkbp:fuelType	aviation gasoline
gptkbp:introduced	1925
gptkbp:manufacturer	gptkb:Pratt_&_Whitney
gptkbp:notableFor	first engine produced by Pratt & Whitney first engine to receive U.S. Department of Commerce Approved Type Certificate No. 1
gptkbp:numberOfEngines	9
gptkbp:powerOutput	up to 600 hp
gptkbp:status	historic
gptkbp:stroke	5.75 in
gptkbp:usedDuring	gptkb:World_War_II
gptkbp:usedIn	gptkb:North_American_T-6_Texan gptkb:Douglas_DC-2 gptkb:Consolidated_PBY_Catalina gptkb:Sikorsky_S-39 gptkb:Beechcraft_Model_18 gptkb:Lockheed_Vega gptkb:Grumman_Goose gptkb:Stearman_PT-17 gptkb:Fairchild_71 gptkb:Curtiss-Wright_AT-32_Condor
gptkbp:weight	650 lb (dry)
gptkbp:bfsParent	gptkb:Fairchild_71_aircraft gptkb:T-6_Texan gptkb:Lockheed_Electra_10E
gptkbp:bfsLayer	6
https://www.w3.org/2000/01/rdf-schema#label	Pratt & Whitney R-1340 Wasp