Lycoming T53-L-31

URI: https://gptkb.org/entity/Lycoming_T53-L-31
GPTKB entity
Statements (31)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:helicopter
gptkbp:average_temperature maximum 650 ° C
gptkbp:compression_ratio 8.5:1
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter approximately 14 in
gptkbp:engine Brayton cycle
single spool
single-stage centrifugal
gptkbp:engine_type turbo-shaft
gptkbp:first_flight gptkb:1960
gptkbp:fuel_capacity 0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
hydromechanical fuel control system
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53-L-31
gptkbp:ignition_system dual ignition system
gptkbp:length approximately 40 in
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:operational_range up to 30,000 ft
gptkbp:power_output 1,400 shp
gptkbp:propulsion 1,400 lbf
4.67 shp/lb
gptkbp:setting free turbine
gptkbp:status in production
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:weight approximately 300 lb
gptkbp:bfsParent gptkb:Lycoming_T53-L-13
gptkbp:bfsLayer 6