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DA62
Technical Specifications

Power Plant

Engine

2 × Austro Engine AE 330 turbocharged common-rail injected 2.0 liter jet fuel engine with 180 HP and EECU single lever control system

Propeller

2 × MT propeller MTV-6-R-C-F/CF 194-80 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 (14,000 ft, MCP)

356 km/h TAS

192 kts TAS

Cruise speed at 75 % (12,000 ft)

317 km/h TAS

171 kts TAS

Cruise Speed at 85 % (12,000 ft)

342 km/h TAS

185 kts TAS

Max. rate of climb (MSL)

5.2 m/s

1,029 ft/min

Max. range (incl. auxiliary tank)

2,376 km

1,283 nm

Fuel consumption at 60 % (12,000 ft) in total

44.7 l/h

11.8 US gal/h

Takeoff performance
(MSL, ground roll / take-off distance)

480 m / 883 m

1,574 ft / 2,897 ft

Landing performance
(MSL, ground roll / landing distance)

441 m / 779 m

1,447 ft / 2,556 ft

Certified service ceiling

6,096 m

20,000 ft

Single engine service ceiling

3,962 m

13,000 ft

Max. demonstrated crosswind

46 km/h

25 kts

Max. operating altitude6,096 m20,000 ft

Dimensions

Mass and Loading (2,300 kg / 5,071 lbs MTOM2)

Seats

up to 7

up to 7

Empty weight

1,590 kg

3,505 lbs

Useful load1

710 kg

1,565 lbs

Max. take off mass

2,300 kg

5,071 lbs

Max. usable fuel capacity
main tank
auxiliary tank

326 l / 261 kg
189 l / 151 kg
137 l / 110 kg

86 US gal / 576 lbs
50 US gal / 335 lbs
36 US gal / 241 lbs

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

1. This value can deviate by 0.5 %
2. The DA62 is also available with an MTOM of 1,999 kg (4,407 lbs). Our sales force will be happy to provide you with the necessary information: sales@diamondaircraft.com or +43 (2622) 26700-1317.