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DA40 NG

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DA40 New Generation

Light Craft Single Engine

All models of the DA40 are founded on a very successful development concept. Excellent security, best flight qualities, robustness, very high reliability and low operating costs. The highly modern avionics, perfect panorama view and the generous luggage compartment encourage vacation plans and excite pilots and flight schools all over the world.

Power Plant

Engine Austro Engine AE 300 Turbocharged Common-Rail Injected 2.0 Liter Diesel Engine with EECU Single Lever Control System
Propeller MT Propeller MTV-6-R-C/ 190 - 69 3-blade Constant Speed Propeller

 

Performance/Consumption

Take-off Distance (Ground Roll) MTOW 300 m
Take-off Distance (50 ft Obstacle) MTOW 600 m
Rate of Climb at Sea Level MTOW 4.1 m/s
Rate of Climb in 10.000 ft MTOW 3.6 m/s
Max. Cruise Speed in 6.000 ft 296 km/h TAS
Cruise Speed @ 70% in 10.000 ft 272 km/h TAS
Cruise Speed @ 60% in 10.000 ft 250 km/h TAS
Range @ 60% in 10.000 ft 1,372 km/2,006 km

 

Dimensions/Weights

Length 8.06 m
Height 1.97 m
Wing Span 11.50 m
Wing Area 13.54 m²
Seats 4
Empty Weight 860 kg
Useful Load 340 kg
Max. Take-off Weight (MTOW) 1,200 kg
Garmin G1000 364 kg / 344 kg
Fuel Capacity Standard/Long Range 114 lt/155 lt 1)
Fuel Grades Jet A1/Diesel 1)

Specifications apply to standard equipped aircraft, if not otherwise stated. The above quoted data are approximately specifications and may change without notice.

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