Lycoming T53-L-47

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:helicopter
gptkbp:availability widely supported
gptkbp:average_temperature up to 1,000 ° F
gptkbp:certification FAA certified
gptkbp:compression_ratio 8:1
gptkbp:controls hydromechanical fuel control
gptkbp:cooling_system air-cooled
gptkbp:diameter approximately 14 in
gptkbp:drivetrain reduction gearbox
gptkbp:emissions_standard meets military standards
axial exhaust
gptkbp:engine gptkb:engine
Brayton cycle
electric starter
up to 5,000 hours
T53-L-703
gptkbp:engine_type free turbine
centrifugal compressor
gptkbp:features modular design
gptkbp:first_flight gptkb:1960
gptkbp:fuel_capacity varies by application
high fuel efficiency
0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
annular combustor
dual fuel system
gptkbp:historical_event developed in the late 1950s
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53-L-47
gptkbp:ignition_system spark ignition
gptkbp:is_tested_for digital engine monitoring system
gptkbp:legacy used in many military helicopters
gptkbp:length approximately 40 in
gptkbp:maintenance 500 hours
low maintenance requirements
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:market_segment gptkb:aircraft
gptkbp:max_speed 2,000 rpm
gptkbp:noise_level low noise level
low vibration level
gptkbp:number_of_stages 2
gptkbp:operational_area moderate operational cost
helicopter propulsion
gptkbp:operational_history used in various military applications
gptkbp:operational_range long operational range
gptkbp:power_output 1,400 shp
gptkbp:propulsion 4.67
0.71 lb/shp
4.67 hp/lb
gptkbp:reliability high reliability
gptkbp:safety_features multiple safety features
gptkbp:service_ceiling 20,000 ft
gptkbp:sport high endurance
gptkbp:type turbo shaft engine
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:variant T53-L-13
gptkbp:weight approximately 300 lb
gptkbp:bfsParent gptkb:Lycoming_T53-L-13
gptkbp:bfsLayer 6