Lycoming T53-L-723

GPTKB entity

Statements (58)
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:Bell_UH-1_Iroquois
gptkbp:average_temperature up to 1200 ° F
gptkbp:certification FAA certified
gptkbp:compression_ratio 12:1
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
forced air cooling
gptkbp:developer 1950s
gptkbp:diameter approximately 1.5 feet
gptkbp:drivetrain reduction gearbox
gptkbp:emissions_standard meets FAA regulations
gptkbp:engine gptkb:Lycoming_T53-L-703
high reliability
Brayton cycle
twin-spool
flexible mount
T53 family
gptkbp:engine_type 2 stages
nickel-based superalloy
14 stages
gptkbp:features modular design
gptkbp:first_flight gptkb:1960
gptkbp:fuel_capacity high efficiency
0.5 lb/hp/hr
dry sump
gptkbp:fuel_type gptkb:railway_station
kerosene
annular combustor
hydromechanical fuel control
gptkbp:has_documentation available from manufacturer
gptkbp:historical_significance widely used in Vietnam War
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53-L-723
gptkbp:ignition_system spark ignition
gptkbp:investment up to 30 psi
gptkbp:is_tested_for bench tested
gptkbp:launch_site electric starter
gptkbp:legacy influenced future turbine designs
gptkbp:length approximately 4.5 feet
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Lycoming_Engines
various suppliers
gptkbp:market_segment gptkb:aircraft
gptkbp:max_speed 15000 RPM
gptkbp:noise_level low noise output
gptkbp:operational_history used in various conflicts
gptkbp:operational_range up to 3000 hours
gptkbp:power_output 1500 horsepower
gptkbp:propulsion 7.5:1
3000 lbf
gptkbp:retirement_year still in use today
gptkbp:successor gptkb:Lycoming_T53-L-701
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:helicopter
gptkbp:weight approximately 400 pounds