|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
500 ft/min
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Don_Mc_Lean
|
|
gptkbp:design_purpose
|
general aviation
|
|
gptkbp:engine_power
|
300 hp
|
|
gptkbp:engine_type
|
gptkb:radial_engine
|
|
gptkbp:first_flight
|
gptkb:1930
1930-06-01
|
|
gptkbp:fuel_capacity
|
50 gallons
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
8 ft 0 in
|
|
gptkbp:historical_significance
|
early American aircraft design.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-90 B
|
|
gptkbp:landing_distance
|
60 mph
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
28 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:max_speed
|
150 mph
|
|
gptkbp:number_built
|
50
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:production_years
|
1930-1935
|
|
gptkbp:propeller
|
two-bladed propeller
|
|
gptkbp:range
|
600 miles
|
|
gptkbp:retired
|
1940s
|
|
gptkbp:role
|
gptkb:civil_aviation
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
12,000 ft
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
800 ft
|
|
gptkbp:type
|
gptkb:monoplane
|
|
gptkbp:used_by
|
gptkb:United_States_Army_Air_Corps
|
|
gptkbp:variant
|
gptkb:Curtiss_C-90_A
gptkb:Curtiss_C-90_C
|
|
gptkbp:wing_area
|
300 sq ft
|
|
gptkbp:wing_configuration
|
fabric-covered wood
|
|
gptkbp:wingspan
|
40 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_C-90
|
|
gptkbp:bfsLayer
|
6
|