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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

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)

352 km/h TAS

190 kts TAS

Max. speed at typical configuration1

372 km/h TAS

201 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

Dimensions

Mass and Loading (2,300 kg / 5,071 lbs MTOM3)

Seats

up to 7

up to 7

Empty weight

1,590 kg

3,505 lbs

Useful load2

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. Typical configuration, average occupation, short trip loading, well serviced aircraft condition
2. This value can deviate by 0.5 %
3. 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@diamond-air.at or +43 (2622) 26700-1317.