Continental IO-360

URI: https://gptkb.org/entity/Continental_IO-360

GPTKB entity

Statements (75)

Predicate	Object
gptkbp:instance_of	gptkb:jet_engine
gptkbp:application	General aviation aircraft
gptkbp:bore	5.125 inches
gptkbp:ceo	1800 hours
gptkbp:compression_ratio	8.5:1 to 9.0:1
gptkbp:configuration	Horizontally opposed
gptkbp:cooling_system	Air-cooled
gptkbp:displacement	360 cubic inches
gptkbp:first_introduced	1960s
gptkbp:fuel_type	Avgas or Mogas
https://www.w3.org/2000/01/rdf-schema#label	Continental IO-360
gptkbp:manufacturer	gptkb:Continental_Motors
gptkbp:power_output	180 to 200 horsepower
gptkbp:stroke	4.0 inches
gptkbp:type	Four-cylinder engine
gptkbp:used_in	gptkb:Piper_PA-32 gptkb:Boeing_707 gptkb:Piper_Aerostar gptkb:Cessna_177 gptkb:Cessna_152 gptkb:Beechcraft_Bonanza gptkb:Cessna_210_N gptkb:Piper_PA-30 gptkb:Cessna_172_I gptkb:Cessna_210_D gptkb:Cessna_210_E gptkb:Cessna_210_F gptkb:Cessna_210_H gptkb:Cessna_210_J gptkb:Cessna_210_K gptkb:Cessna_210_L gptkb:Cessna_210_M gptkb:Mooney_M20 gptkb:Cessna_207 gptkb:Cessna_185 gptkb:Cessna_210 gptkb:Cessna_208 gptkb:Cessna_150 gptkb:Grumman_American_AA-5 gptkb:Cirrus_SR20 gptkb:Cessna_172_SP gptkb:Cessna_182 gptkb:Cessna_210_A gptkb:Cessna_210_B gptkb:Cessna_210_C gptkb:Cessna_210_G gptkb:Piper_PA-24 gptkb:Diamond_DA40 gptkb:Cessna_210_R gptkb:Cessna_172_A gptkb:Cessna_172_B gptkb:Cessna_172_C gptkb:Cessna_172_D gptkb:Cessna_172_E gptkb:Cessna_172_F gptkb:Cessna_172_G gptkb:Cessna_172_H gptkb:Cessna_172_J gptkb:Cessna_172_K gptkb:Cessna_172_L gptkb:Cessna_172_M gptkb:Cessna_172_N gptkb:Cessna_172_P gptkb:Cessna_172_R gptkb:Cessna_172_RG gptkb:Cessna_172_S gptkb:Cessna_177_RG gptkb:Lancair_360 gptkb:Piper_PA-31 Piper PA-28
gptkbp:valve_configuration	Overhead valve
gptkbp:variant	IO-360-A, IO-360-B, IO-360-C
gptkbp:weight	Approx. 300 lbs
gptkbp:bfsParent	gptkb:Continental_IO-520
gptkbp:bfsLayer	7