|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:avionics
|
basic avionics
|
|
gptkbp:category
|
general aviation
|
|
gptkbp:climb_rate
|
700 ft/min
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:controls
|
yoke control
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
100 knots
|
|
gptkbp:design
|
gptkb:Cessna_Aircraft_Company
|
|
gptkbp:engine
|
gptkb:Continental_O-200
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1949
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
30 US gallons
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
gptkbp:fuselage_material
|
metal construction
|
|
gptkbp:height
|
7 ft 0 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 140 A
|
|
gptkbp:landing_distance
|
1,000 ft
60 knots
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Cessna_Aircraft_Company
|
|
gptkbp:market_segment
|
gptkb:trainer_aircraft
|
|
gptkbp:marketed_as
|
gptkb:Cessna_140_A
|
|
gptkbp:max_speed
|
120 knots
|
|
gptkbp:max_takeoff_weight
|
1,600 lb
|
|
gptkbp:model
|
gptkb:Cessna_140
|
|
gptkbp:nickname
|
gptkb:Cessna_140
|
|
gptkbp:number_built
|
1,500
|
|
gptkbp:offers_certificate
|
gptkb:TC_3_A2
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:power_consumption
|
12 lb/hp
|
|
gptkbp:predecessor
|
gptkb:Cessna_120
|
|
gptkbp:production_years
|
1949-1951
|
|
gptkbp:propeller
|
fixed-pitch propeller
two-blade
|
|
gptkbp:range
|
500 nautical miles
|
|
gptkbp:service_ceiling
|
12,000 ft
|
|
gptkbp:stall_speed
|
50 knots
|
|
gptkbp:successor
|
gptkb:Cessna_150
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
1,200 ft
|
|
gptkbp:transportation
|
20 knots
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:wing_area
|
175 sq ft
|
|
gptkbp:wing_configuration
|
high-wing
9.14 lb/sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Cessna_140
|
|
gptkbp:bfsLayer
|
7
|