|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:cancellation_reason
|
acoustic lining
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:developer
|
Lycoming T53 series
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
axial
low emissions technology
|
|
gptkbp:engine
|
gptkb:Lycoming_T53-L-703
Brayton cycle
starter motor
1,400 shp
flexible mount system
approximately 5.5 ft³
|
|
gptkbp:engine_type
|
gptkb:3
2
centrifugal compressor
single spool
nickel-based superalloy
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
20 in
400 lb
0.5 lb/hp/hr
40 in
dry sump
14 in
|
|
gptkbp:fuel_type
|
gptkb:Company
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-97
|
|
gptkbp:ignition_system
|
spark ignition
|
|
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
|
gptkb:battle
3.5:1
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:suspension
|
active damping system
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:water_source
|
high-efficiency filter
|
|
gptkbp:weight
|
approximately 400 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
|
gptkbp:bfsLayer
|
6
|