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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:category
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Experimental aircraft
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gptkbp:climb_rate
|
1,000 ft/min
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gptkbp:cockpit
|
side-by-side seating
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gptkbp:construction_material
|
aluminum
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gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
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|
gptkbp:cruise_speed
|
120 mph
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gptkbp:design
|
Randall J. D. Rans
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gptkbp:engine_type
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Rotax 912
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gptkbp:first_flight
|
gptkb:1994
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gptkbp:flaps
|
slotted flaps
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gptkbp:fuel_capacity
|
20 US gallons
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gptkbp:fuselage_material
|
gptkb:NACA_4412
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rans S-6 Coyote
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gptkbp:landing_distance
|
1,000 ft
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
22 ft 0 in
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gptkbp:manufacturer
|
Rans Designs
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gptkbp:market_segment
|
light sport aviation
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gptkbp:marketed_as
|
gptkb:Rans_S-6_Coyote
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gptkbp:max_speed
|
140 mph
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|
gptkbp:max_takeoff_weight
|
1,320 lb
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gptkbp:notable_features
|
lightweight design
easy assembly
versatile use
good short field performance
high visibility cockpit
good fuel efficiency
low stall speed
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gptkbp:number_built
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over 1,000
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gptkbp:power_consumption
|
13.2 lb/hp
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gptkbp:production_status
|
in production
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gptkbp:propeller
|
fixed-pitch
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|
gptkbp:range
|
500 miles
|
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gptkbp:regulatory_compliance
|
LSA regulations
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gptkbp:seating_capacity
|
2
|
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gptkbp:service_ceiling
|
12,000 ft
|
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gptkbp:stall_speed
|
40 mph
|
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gptkbp:tail_type
|
conventional tail
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gptkbp:takeoff_distance
|
1,200 ft
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gptkbp:type
|
gptkb:light_aircraft
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gptkbp:variant
|
gptkb:Rans_S-6_Coyote_II
gptkb:Rans_S-6_Coyote_Super
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|
gptkbp:wing_area
|
200 sq ft
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gptkbp:wing_configuration
|
6.6 lb/sq ft
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gptkbp:wingspan
|
30 ft 0 in
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gptkbp:bfsParent
|
gptkb:Rans_S-6
gptkb:Rotax_912_S
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gptkbp:bfsLayer
|
6
|