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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
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|
gptkbp:aircraft_operated
|
1,800 lb
civil aircraft
good performance in short fields
influenced later designs.
|
|
gptkbp:aircraft_role
|
utility aircraft
|
|
gptkbp:ceiling
|
15,000 ft
|
|
gptkbp:climb_rate
|
600 ft/min
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
120 mph
|
|
gptkbp:design
|
Clarence A. Stinson
|
|
gptkbp:design_purpose
|
recreational flying
|
|
gptkbp:engine
|
gptkb:Lycoming_O-435
|
|
gptkbp:engine_type
|
horizontally opposed
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
40 US gallons
|
|
gptkbp:fuel_type
|
aviation gasoline
|
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gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
7 ft 6 in
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|
gptkbp:historical_significance
|
used in World War II
|
|
gptkbp:historical_use
|
civilian aviation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Stinson 165
|
|
gptkbp:landing_distance
|
1,000 ft
|
|
gptkbp:landing_gear
|
tailwheel
taildragger
|
|
gptkbp:length
|
25 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Stinson_Aircraft_Company
|
|
gptkbp:max_speed
|
140 mph
|
|
gptkbp:max_takeoff_weight
|
2,800 lb
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:production_location
|
gptkb:United_States
|
|
gptkbp:production_years
|
2 years
1939-1941
|
|
gptkbp:propeller
|
two-bladed
|
|
gptkbp:range
|
500 miles
|
|
gptkbp:registration
|
N-number
|
|
gptkbp:role
|
general aviation
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:stall_speed
|
55 mph
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
1,200 ft
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:variant
|
gptkb:Stinson_108
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wing_configuration
|
fabric-covered wood
high wing
|
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gptkbp:wingspan
|
36 ft 0 in
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gptkbp:bfsParent
|
gptkb:Stinson_Detroiter
|
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gptkbp:bfsLayer
|
6
|