Lycoming IO-360

GPTKB entity

Statements (101)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:Piper_Seminole
gptkb:aircraft
gptkb:Cessna_177
gptkb:Cessna_152
gptkb:Piper_Navajo
gptkb:Piper_Cherokee
gptkb:Piper_Super_Cub
gptkb:Grumman_AA-5
gptkb:Piper_Cub
gptkb:Mooney_M20
gptkb:Cessna_185
gptkb:Cessna_210
gptkb:Cessna_150
gptkb:Beechcraft_Musketeer
gptkb:Piper_Comanche
gptkb:Piper_Aztec
gptkb:Piper_Arrow
gptkb:Cessna_172_SP
gptkb:Piper_Warrior
gptkb:Piper_Archer
gptkb:Cessna_182
gptkb:Cessna_172_M
gptkb:Cessna_172_RG
gptkb:Cessna_172_S
gptkb:Cessna_177_RG
Piper PA-28
general aviation aircraft
Piper Sport Cruiser
Diamond D A40
Cirrus S R20
Lancair 235
gptkbp:bore 5.125 inches
4.00 inches
gptkbp:ceo 1800 hours
1,800 hours
gptkbp:certification FAA certified
gptkbp:compression_ratio 8.5:1
8.5:1 to 10.5:1
gptkbp:cooling_system air-cooled
gptkbp:displacement 360 cubic inches
gptkbp:engine gptkb:4
gptkb:IO-360_family
gptkbp:first_introduced 1960s
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Lycoming IO-360
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:power_output 180 horsepower
180 to 200 horsepower
gptkbp:propulsion fixed-pitch or constant-speed
gptkbp:setting inline engine
horizontally opposed
gptkbp:stroke 4.00 inches
3.50 inches
gptkbp:type four-stroke engine
four-cylinder engine
gptkbp:used_in gptkb:Piper_PA-32
gptkb:aircraft
gptkb:Piper_Aerostar
gptkb:Cessna_177
gptkb:Beechcraft_Bonanza
gptkb:Grumman_AA-5
gptkb:Mooney_M20
gptkb:Cessna_185
gptkb:Cessna_150
gptkb:Cessna_182
gptkb:Piper_PA-24
gptkb:American_Champion_7_GCBC
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_N
gptkb:Cessna_172_P
gptkb:Cessna_172_Q
gptkb:Cessna_172_R
gptkb:Cessna_172_RG
gptkb:Cessna_172_S
gptkb:Cessna_177_RG
gptkb:Lancair_360
gptkb:Piper_PA-28-161
gptkb:Piper_PA-28_R
gptkb:Piper_PA-31
Piper PA-28
general aviation aircraft
Diamond D A40
Cirrus S R20
gptkbp:valve_configuration overhead valve
gptkbp:variant gptkb:IO-360-L2_A
gptkb:IO-360-M1_A
IO-360-B1 A
gptkbp:weight approximately 300 lbs
gptkbp:bfsParent gptkb:Cessna_172_RG_Cutlass
gptkbp:bfsLayer 4