|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_C-57
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
aluminum
high-mounted wings
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:combat_role
|
transport and logistics
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1970
|
|
gptkbp:design
|
gptkb:public_transportation_system
Curtiss engineers
|
|
gptkbp:emergency_services
|
overwing exits
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
piston engine
Curtiss R-2800
|
|
gptkbp:features
|
high-wing monoplane
|
|
gptkbp:first_flight
|
gptkb:1956
pressurized cockpit
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historical_significance
|
used in military operations during the Cold War
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-57 B
|
|
gptkbp:influenced_by
|
gptkb:Curtiss_C-46_Commando
|
|
gptkbp:interior_features
|
modular seating
|
|
gptkbp:landing_gear
|
tricycle gear
retractable landing gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
6,350 kg
|
|
gptkbp:notable_users
|
gptkb:U._S._military
|
|
gptkbp:number_built
|
50
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:primary_user
|
gptkb:aircraft
|
|
gptkbp:production_location
|
gptkb:Buffalo,_New_York
|
|
gptkbp:production_years
|
1956-1960
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1965
|
|
gptkbp:retirement_year
|
replacement by newer models
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
up to 10
rear ramp door
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:successor
|
gptkb:Curtiss_C-58
|
|
gptkbp:surface
|
elevators and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Curtiss_C-57
|
|
gptkbp:wingspan
|
15.85 m
|