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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 (MTOM, ISA)

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 TAS175 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 m16,000 ft
Single engine absolute ceiling (climb rate 0 ft/min)5,335 m17,500 ft
Range at 60% (12,000 ft, incl. auxiliary tank) incl. climb, no reserves2,038 km1,100 nm
Max. range (FL 180, 50% PWR) incl. climb, no reserves2,269 km1,225 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 m1,230 ft / 2,129 ft

Landing ground roll (ISA SL)

340 m

1,115 ft

Landing performance (MSL,
ground roll / landing distance)
387 m / 647 m1,269 ft / 2,122 ft
Max. operating altitude5,488 m18,000 ft

Max. demonstrated crosswind

46 km/h

25 kts

Dimensions

Mass and Loading

Seats

44
Empty weight without options1,420 kg

3,131 lbs

Max. useful load579 kg

1,276 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 / 333 lbs
26.4 US gal / 176 lbs

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