gptkbp:instanceOf
|
turboprop engine
|
gptkbp:application
|
military transport aircraft
maritime patrol aircraft
passenger aircraft
cargo_aircraft
|
gptkbp:climate
|
up to 1,500 °F
|
gptkbp:competitors
|
gptkb:Rolls-Royce_AE_2100
gptkb:Pratt_&_Whitney_Canada_PT6
gptkb:General_Electric_CT7
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
gptkbp:coolingSystem
|
air-cooled
|
gptkbp:design
|
designed for reliability and efficiency
|
gptkbp:developer
|
developed in the 1950s
|
gptkbp:diameter
|
1,200 mm
|
gptkbp:drivetrain
|
reduction gearbox
|
gptkbp:emissionsStandard
|
low emissions
|
gptkbp:engineType
|
free turbine
axial compressor
|
gptkbp:firstFlight
|
1954
|
gptkbp:fuel_capacity
|
good fuel efficiency
|
gptkbp:fuelType
|
Jet A
|
https://www.w3.org/2000/01/rdf-schema#label
|
Allison T56
|
gptkbp:is_used_in
|
gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion
gptkb:Boeing_707
|
gptkbp:length
|
1,800 mm
|
gptkbp:maintenance
|
3,600 hours
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
gptkbp:market
|
widely used in military and civilian aviation
|
gptkbp:noise_level
|
low noise level
|
gptkbp:notable_feature
|
T56-A-1
T56-A-3
T56-A-15
T56-A-427
T56-A-7
|
gptkbp:powerOutput
|
3,000 to 4,600 shp
|
gptkbp:produces
|
over 20,000 units produced
|
gptkbp:propulsion
|
up to 4,600 lbf
|
gptkbp:reach
|
used worldwide
|
gptkbp:reliability
|
high reliability
|
gptkbp:serviceHistory
|
in service since 1954
|
gptkbp:setting
|
twin-shaft
|
gptkbp:status
|
in production for military applications
|
gptkbp:successor
|
PW150
|
gptkbp:weight
|
1,200 kg
|