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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
experimental
cantilever wing
18 lb/sq ft
|
|
gptkbp:avionics
|
varies by owner
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
gptkb:Larry_Lancair
personal and business travel
|
|
gptkbp:elevation
|
10,000 ft
|
|
gptkbp:engine
|
350 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_capacity
|
60 US gallons
|
|
gptkbp:fuel_type
|
100 LL avgas
|
|
gptkbp:height
|
7 ft 4 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lancair IV
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
26 ft 10 in
|
|
gptkbp:manufacturer
|
gptkb:Lancair_International
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:material
|
fiberglass and carbon fiber
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 ft
1,000 ft
3,600 lb
|
|
gptkbp:notable_features
|
low-wing design
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:power_consumption
|
10.3 lb/hp
|
|
gptkbp:produced_by
|
1986 to present
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:seating_capacity
|
gptkb:3
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:speed
|
180 knots
60 knots
Vne 200 knots
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
kit aircraft
|
|
gptkbp:weight
|
1,400 lb
2,200 lb
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wingspan
|
36 ft 10 in
|
|
gptkbp:bfsParent
|
gptkb:RNAS_Pembrey
gptkb:RAF_North_Weald
|
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gptkbp:bfsLayer
|
5
|