Skip to main content

Technical Specifications

Power Plant


2x Austro Engine AE330 turbocharged common-rail injected 2.0 liter jet fuel engine with 180 HP and EECU single lever control system


2x 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 85 % (12,000 ft)

333 km/h TAS

180 kts TAS

Stalling speed, landing configuration126 km/h68 kts CAS

Max. rate of climb (MSL)

5.2 m/s

1,028 ft/min

Max. range (incl. auxiliary tank) (FL160, 50% PWR)
incl. climb, no reserves
2,385 km1,288 nm
Fuel consumption at 60% (12,000 ft) in total44.7 l/h

11.8 US gal/h

Take-off performance (MSL, ground roll / take-off obstacle)480 m / 883 m1,574 ft / 2,730 ft
Landing performance (MSL, ground roll / landing distance)441 m / 779 m1,446 ft / 2,555 ft

Certified service ceiling

6,096 m

20,000 ft

Single engine service ceiling
(MTOM, ISA, rate of climb: 50 ft/min.)
3,354 m

11,000 ft

Single engine absolute ceiling
(MTOM, ISA, rate of climb: 0 ft/min.)
4,116 m13,500 ft

Max. demonstrated crosswind

46 km/h

25 kts


Mass and Loading


up to 7

up to 7

Empty weight without options1,598 kg3,523 lbs
Maximum useful load702 kg1,545 lbs
Max. take-off mass12,300 kg

5,071 lbs

Max. usable fuel capacity
main tank
auxiliary tank

327 l / 261 kg
189 l / 151 kg
138 l / 110 kg

86.4 US gal / 576 lbs
50 US gal / 333 lbs
36.4 US gal / 243lbs

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

1. The DA62 is also available with an MTOM of 1,999 kg (4,407 lbs). Our sales team will be happy to provide you with the necessary information: or +43 (2622) 26700-1317.