|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Curtiss's_aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Curtiss_C-55
gptkb:Curtiss_C-54
gptkb:Curtiss_C-58
gptkb:item
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:aircraft
Curtiss design team
Curtiss engineers
|
|
gptkbp:economic_impact
|
limited market impact
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:financial_performance
|
good stability characteristics
|
|
gptkbp:first_flight
|
1947
successful test flights
|
|
gptkbp:flaps
|
slotted flaps
|
|
gptkbp:fuel_capacity
|
1,200 L
|
|
gptkbp:handles
|
easy handling characteristics
|
|
gptkbp:historical_significance
|
early post-war transport aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-57
|
|
gptkbp:influenced
|
future transport aircraft designs
|
|
gptkbp:influenced_by
|
gptkb:Curtiss_C-46_Commando
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:legacy
|
influenced future aircraft designs.
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:notable_features
|
high wing configuration
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:produced_by
|
limited production
|
|
gptkbp:production_years
|
1947-1950
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1950s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
1948
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Curtiss_C-58
|
|
gptkbp:surface
|
elevator and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Curtiss_C-57_A
gptkb:Curtiss_C-57_B
|
|
gptkbp:weight
|
3,600 kg
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
15.2 m
|