DA42-VI

Engine

2 × Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control system

Propeller

2 × MT propeller MTV-6-R-C-F/CF 190-69 3-blade constant speed propeller

Fuel grades

Jet A-1

Max. speed (16,000 ft, MCP) 1,760 kg TOW

365 km/h TAS

197 kts TAS

Max. cruising speed (16,000 ft, MCP)

352 km/h TAS

190 kts TAS

Cruise speed at 75% (16,000 ft)

324 km/h TAS

175 kts TAS

Stall speed, landing configuration

115 km/h CAS

62 kts CAS

Rate of climb (ISA SL) 1,760 kg TOW

5.7 m/s

1,114 ft/min

Single engine service ceiling (climb rate 50 ft/min)

4,878 m

16,000 ft

Single engine absolute ceiling (climb rate 0 ft/min)

5,335 m

17,500 ft

Range at 60% (12,000 ft, incl. auxiliary tank) incl. climb, no reserves

2,038 km

1,100 nm

Max. range (FL 180, 50% PWR) incl. climb, no reserves

2,269 km

1,225 nm

Consumption at 60 % in total

39.4 l/h

10.4 US gal/h

Take-off performance (MSL, ground roll / take-off obstacle) Short field t/o procedure

375 m / 649 m

1,230 ft / 2,129 ft

Landing ground roll (ISA SL)

340 m

1,115 ft

Landing performance (MSL, ground roll / landing distance)

387 m / 647 m

1,269 ft / 2,122 ft

Max. operating altitude

5,488 m

18,000 ft

Max. demonstrated crosswind

46 km/h

25 kts

Seats

4

Empty weight without options

1,420 kg

Max. useful load

579 kg

Max. take off mass

1,999 kg

Fuel capacity total

289 l / 231 kg

Main tank

189 l / 151 kg

Auxiliary tank

100 l / 80 kg