Diamond DA40

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_configuration single-engine, low-wing
gptkbp:aircraft_operated gptkb:EASA_CS-23
varies by country
light sport aircraft market
high performance for training
popular among flight schools.
gptkbp:aircraft_type civil aircraft
gptkbp:aspect_ratio 7.5
gptkbp:avionics gptkb:Garmin_G1000
gptkbp:category gptkb:light_aircraft
gptkbp:climb_rate 1,000 ft/min
gptkbp:cockpit glass cockpit
gptkbp:country_of_origin gptkb:Austria
gptkbp:crew gptkb:1
gptkbp:cruise_speed 126 knots
gptkbp:design gptkb:Christian_Dries
gptkbp:design_purpose training and touring
gptkbp:engine gptkb:Lycoming_IO-360
gptkbp:engine_type four-stroke engine
gptkbp:first_flight gptkb:2002
gptkbp:fuel_capacity 50 liters
gptkbp:fuel_type aviation gasoline
gptkbp:height 2.3 m
https://www.w3.org/2000/01/rdf-schema#label Diamond DA40
gptkbp:landing_distance 500 m
gptkbp:landing_gear tricycle gear
gptkbp:length 8.1 m
gptkbp:manufacturer gptkb:Diamond_Aircraft_Industries
gptkbp:market_segment general aviation
gptkbp:max_speed 168 knots
gptkbp:max_takeoff_weight 1,150 kg
gptkbp:notable_users flying schools
gptkbp:passenger_capacity gptkb:3
gptkbp:production_status in production
gptkbp:production_years 2002-present
gptkbp:propeller variable-pitch propeller
gptkbp:range 1,000 km
gptkbp:safety_features crash-resistant fuel system
gptkbp:service_ceiling 5,000 m
gptkbp:stall_speed 54 knots
gptkbp:tail_type T-tail
gptkbp:takeoff_distance 600 m
gptkbp:type single-engine aircraft
gptkbp:variant DA40 F, DA40 NG
gptkbp:weight 750 kg
gptkbp:wing_area 15.9 m²
gptkbp:wing_configuration high-wing
gptkbp:wingspan 11.9 m
gptkbp:bfsParent gptkb:No._47_Squadron_RFC
gptkbp:bfsLayer 4