Venturi VFE-25

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:avionics basic instrumentation
gptkbp:category Experimental aircraft
gptkbp:cockpit enclosed
gptkbp:control_surfaces gptkb:elevator
ailerons
rudder
gptkbp:country_of_origin gptkb:France
gptkbp:crew gptkb:1
gptkbp:cruise_speed 150 km/h
gptkbp:design Jean-Marie Gounon
gptkbp:design_purpose leisure flying
gptkbp:elevation 3000 meters
gptkbp:engine Rotax 912
gptkbp:first_flight gptkb:1995
gptkbp:flaps gptkb:manual
gptkbp:fuel_capacity 100 liters
gptkbp:fuselage_material composite
https://www.w3.org/2000/01/rdf-schema#label Venturi VFE-25
gptkbp:landing_gear tricycle gear
gptkbp:length 7.2 meters
gptkbp:manufacturer Venturi Aircraft
gptkbp:market_segment recreational flying
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 600 kg
gptkbp:notable_features community support
high performance
lightweight construction
comfortable seating
modern design
customizable options
easy handling
short takeoff and landing capabilities
easy maintenance
low operating costs
good visibility
good fuel efficiency
good resale value
stable flight characteristics
training friendly
gptkbp:passenger_capacity 2
gptkbp:production_status in production
gptkbp:propeller variable pitch
gptkbp:range 800 km
gptkbp:regulatory_compliance LSA regulations
gptkbp:stall_speed 60 km/h
gptkbp:tail_type T-tail
gptkbp:trim_levels gptkb:manual
gptkbp:type gptkb:light_aircraft
gptkbp:weight 300 kg
gptkbp:wing_area 15 m²
gptkbp:wing_configuration aluminum
gptkbp:wingspan 10.5 meters
gptkbp:year_established gptkb:1995
gptkbp:bfsParent gptkb:Venturi_Racing
gptkbp:bfsLayer 5