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DA42
Technical Specifications

Power Plant

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, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8

Performance

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

365 km/h TAS

197 kts TAS

Cruise speed at 75 % (16,000 ft)

326 km/h TAS

176 kts TAS

Stall speed, landing configuration

113 km/h CAS

61 kts CAS

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

7.9 m/s

1,550 ft/min

Single Engine Service Ceiling

5,486 m

18,000 ft

Range at 60 % (2,000 ft, incl. auxiliary tank)

2,250 km

1,215 nm

Consumption at 60 % in total

39.4 l/h

10.4 US gal/h

Take-off ground roll (ISA SL), 1,760 kg TOW

280 m

919 ft

Landing ground roll (ISA SL)

340 m

1,115 ft

Max. operating altitude

5,486 m

18,000 ft

Max. demonstrated crosswind

46 km/h

25 kts

Dimensions

Mass and Loading

Seats

44

Empty weight

1,410 kg

3,109 lbs

Useful load

589 kg

1,299 lbs

Max. take off mass

1,999 kg

4,407 lbs

Fuel capacity total
main tank
auxiliary tank

289 l / 231 kg
189 l / 151 kg
100 l / 80 kg

76.4 US gal / 512 lbs
50.0 US gal / 335 lbs
26.4 US gal / 177 lbs

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