Lycoming T53-L-711

URI: https://gptkb.org/entity/Lycoming_T53-L-711
GPTKB entity
Statements (31)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 7
gptkbp:bfsParent gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-91
gptkbp:application gptkb:helicopter
gptkbp:compression_ratio 8:1
gptkbp:controls hydromechanical
gptkbp:cooling_system air-cooled
gptkbp:designated_as military use
gptkbp:diameter approximately 16 in
gptkbp:emissions_standard axial
gptkbp:engine gptkb:Lycoming_T53-L-703
T53 family
gptkbp:first_introduced 1960s
gptkbp:fuel_capacity 0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53-L-711
gptkbp:legal_issue gptkb:engine
gptkbp:length approximately 40 in
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:notable_users gptkb:military_unit
gptkbp:number_of_stages 2
gptkbp:operational_range up to 30,000 ft
gptkbp:power_output 1,400 shp
gptkbp:propulsion 3.5:1
gptkbp:setting free turbine
gptkbp:successor gptkb:Lycoming_T53-L-703
gptkbp:type turbo shaft engine
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:weight approximately 400 lb