|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:climb_rate
|
2,500 ft/min
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
Curtis Pitts
|
|
gptkbp:engine
|
gptkb:Lycoming_AEIO-540
|
|
gptkbp:first_flight
|
gptkb:1966
|
|
gptkbp:fuel_capacity
|
20 US gal
|
|
gptkbp:fuselage_material
|
gptkb:NACA_4412
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pitts S-1
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
20 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Pitts_Special_Aircraft
|
|
gptkbp:max_speed
|
200 mph
|
|
gptkbp:max_takeoff_weight
|
1,800 lb
|
|
gptkbp:notable_features
|
high performance
lightweight design
high maneuverability
good visibility
simple maintenance
|
|
gptkbp:notable_pilots
|
gptkb:Patty_Wagstaff
|
|
gptkbp:produces
|
over 200 units
|
|
gptkbp:production_years
|
1966-1980
|
|
gptkbp:related_aircraft
|
gptkb:Pitts_S-2
Pitts S-4
Pitts S-6
Pitts S-5
Pitts S-3
Pitts S-7
|
|
gptkbp:role
|
aerobatic aircraft
|
|
gptkbp:roll_rate
|
360°/sec
|
|
gptkbp:seating_capacity
|
gptkb:1
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:stall_speed
|
60 mph
|
|
gptkbp:successor
|
gptkb:Pitts_S-2
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:type
|
gptkb:biplane
|
|
gptkbp:used_in
|
aerobatic competitions
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wing_configuration
|
gptkb:biplane
|
|
gptkbp:wingspan
|
24 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Pitts_S-2
|
|
gptkbp:bfsLayer
|
7
|