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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
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gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:compression_ratio
|
8:1
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|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:emissions_standard
|
straight exhaust
|
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gptkbp:engine
|
gptkb:helicopter
Brayton cycle
electric starter
twin-spool
flexible mount
turbo-shaft
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gptkbp:engine_type
|
gptkb:engine
three stages
two stages
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
dry sump
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
gptkb:railway_station
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-39
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:investment
|
up to 30 psi
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
30,000 rpm
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:powers
|
4.67 hp/lb
|
|
gptkbp:propulsion
|
1,400 lbf
4.67 hp/lb
|
|
gptkbp:status
|
in production
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:variant
|
T53-L-13
T53-L-701
T53-L-703
T53-L-703 A
|
|
gptkbp:weight
|
approximately 300 lb
|