Two engines and an anti-icing system give users of the DA42-VI the ability to fly in all weather conditions, at any time of the day or night, over mountains, seas and cities - wherever your dreams or necessity will carry you.
The four-seat cabin, large fuel tanks, a range of more than 2,000 kilometers and low operating costs make it a model often chosen by our customers as a target aircraft. In addition, the DA42-VI is an easy and pleasant unit to fly.
The aircraft is offered in both a basic school version and an executive version with a luxurious interior. High-quality leather seats, LED lighting or air conditioning are just some of the premium equipment options.
Diamond DA42 - VI

maximum range: 2,038 km
cruising speed: max. 252 km/h
maximum flight ceiling: 5 486 m
payload: 579 kg
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DIamond DA42-VI
Versatile and useful

DIamond DA42 - VI
Economical operation

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Fly anywhere at any time
Fully integrated Garmin G1000 NXi avionics equipped with the latest features, including the state-of-the-art GFC700 digital autopilot system. The system can be enhanced with weather radar, Synthetic Vision, Stormcope and TAS for superior situational awareness, convenience and safety.

Quality for years to come
The DA42-VI airframe is made entirely of glass and carbon composite. Advanced aerodynamic solutions combined with the latest passive safety technology provide excellent passenger protection. The airframe is durable, easy to maintain and maintains a great appearance for many years.
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Anti-icing system
The anti-icing system prevents the accumulation of ice on the leading edges of the wings and on the propellers - thanks to this the aircraft is FIKI (Flight Into Known Icing Conditions) certified. The DA42-VI gives you the assurance of safety in all weather conditions and at any time of the day or night.
Expert section
Details
Dimensions
- length: 8.56 m (28 ft, 1 in)
- wingspan: 13.55 m (44 ft, 4 in)
- Height: 2.49 m (8 ft, 2 in)
Weights
- maximum takeoff weight: 4,407 lb (1999 kg)
- payload: 4407 lb (579 kg)
- empty aircraft weight (standard equipment): 3131 lb (1420 kg)
- fuel volume and weight: 289 l / 76.4 US Gal (231 kg / 512 lb)
Performance
- maximum cruising speed: 190 kts (252 km/h)
- maximum range: 1100 nm (2038 km)
- maximum flight ceiling: 18,000 ft (5486 m)
- run-up (MTOW, sea level, standard atmosphere): 1230 ft (375 m)
- 15m obstacle launch: 2129 ft (649 m)
- run: 1269 ft (387 m)
- landing from an obstacle 15 m: 2122 ft (647 m)
- fuel consumption: 39.4 kg/h
- cabin type: unpressurized
Drive unit
- engine: 2 x Austro Engine AE300
- engine power: 2 x 168 HP
- propeller: 2 x MT propeller MTV-6-R-C-F/CF 190-69
- number of blades: 3
- propeller diameter: 1900 mm
- fuel: JET-A1
Avionics
- avionics type: Glass Cockpit Garmin G1000NXi
- autopilot: Garmin GFC 700
- spare instruments: Mechanical optional MD-302 SAM
Operating parameters
- type of operations: VFR Day, VFR Night, IFR, FIKI
- crew: 1
- number of passenger seats: 3
Accessory equipment
- optional: Air conditioning, TKS anti-ice, GARMIN ESP, TAS, Stormscope, Weather Radar


The DA42-VI is a very successful pilot training aircraft that revolutionized the twin-engine piston aircraft market with its capabilities.