|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:Beechcraft_1900
gptkb:Air_Tractor_AT-802_U
gptkb:Dornier_228
gptkb:Beechcraft_1900_D
|
|
gptkbp:application
|
gptkb:aircraft
regional aircraft
|
|
gptkbp:armament
|
gptkb:6
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
free turbine
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
gptkb:Interpol
air-cooled
|
|
gptkbp:diameter
|
approximately 16 in
approximately 1.5 ft
|
|
gptkbp:engine
|
Brayton cycle
air start
air-start
|
|
gptkbp:engine_configuration
|
twin-engine
one
wing-mounted
pylon-mounted
twin-shaft
|
|
gptkbp:engine_type
|
turboprop
single-engine
PT6 A-67 A
PT6 A-67 B
PT6 A-67 C
PT6 A-67 D
PT6 A-67 P
PT6 A-67 R-1
PT6 A-67 E
PT6 A-67 F
PT6 A-67 G
PT6 A-67 H
PT6 A-67 J
PT6 A-67 K
PT6 A-67 L
PT6 A-67 M
PT6 A-67 N
PT6 A-67 O
PT6 A-67 Q
PT6 A-67 R
PT6 A-67 R-10
PT6 A-67 R-2
PT6 A-67 R-3
PT6 A-67 R-4
PT6 A-67 R-5
PT6 A-67 R-6
PT6 A-67 R-7
PT6 A-67 R-8
PT6 A-67 R-9
|
|
gptkbp:exhaust_system
|
rear exhaust
|
|
gptkbp:first_flight
|
gptkb:2004
|
|
gptkbp:fuel_capacity
|
136 kg
40.6 cm
137 cm
|
|
gptkbp:fuel_economy
|
approximately 600 lb/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney PT6 A-67 R
|
|
gptkbp:is_tested_for
|
bench testing
|
|
gptkbp:length
|
approximately 4.5 ft
approximately 54 in
|
|
gptkbp:maintenance
|
scheduled maintenance intervals
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_takeoff_weight
|
1,600 shp
|
|
gptkbp:operational_range
|
up to 1,000 nautical miles
|
|
gptkbp:power_output
|
1,600 shp
|
|
gptkbp:propeller
|
constant speed
approximately 5.0 ft
|
|
gptkbp:propulsion
|
0.53
4.0 shp/lb
5.33 shp/lb
|
|
gptkbp:reduction_gear
|
reduction gearbox
|
|
gptkbp:service_ceiling
|
30,000 ft
25,000 ft
|
|
gptkbp:torque
|
dry sump
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:water_requirement
|
approximately 50-60 lb/h
|
|
gptkbp:weight
|
approximately 400 lb
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Convair_CV-580_L
gptkb:Convair_CV-580_S
|
|
gptkbp:bfsLayer
|
8
|