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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:PT-26_A
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Piper_J-3_Cub
general aviation
1,200 kg
200 km/h
single-engine
cantilever wing
2.54 m
7.62 m
|
|
gptkbp:artistic_influence
|
gptkb:Piper_PA-32
|
|
gptkbp:certification
|
gptkb:Certification
|
|
gptkbp:climb_rate
|
3.5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
gptkb:Piper_Aircraft_Company
training pilots
|
|
gptkbp:engine
|
gptkb:musical
150 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1946
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
gptkbp:height
|
2.54 m
|
|
gptkbp:historical_significance
|
used in pilot training
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT-26
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
7.62 m
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:material
|
metal and fabric
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,600 kg
|
|
gptkbp:nickname
|
gptkb:Piper_Cub_Trainer
|
|
gptkbp:notable_features
|
low-wing design
|
|
gptkbp:operational_history
|
used by various flight schools
|
|
gptkbp:primary_user
|
gptkb:aircraft
|
|
gptkbp:produced_by
|
over 1,000 units
|
|
gptkbp:production_years
|
1946-1950
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
400 kg
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:successor
|
Piper PA-28
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:variant
|
gptkb:PT-26_A
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.67 m
|