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DA62 MPP
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. cruise speed (14,000 ft, MCP)

352 km/h TAS

190 kts TAS

Min. operation speed

140 km/h TAS

76 kts TAS

Consumption at 35% power (loiter speed) in total

28 lt/hr

7.4 USGal/hr

Max. airborne operations time

11.7 hours

11.7 hours

Typical airborne operations time1)

6 - 8 hours

6 - 8 hours

Max. range at 50% power in
14,000 ft (standard tank / incl.
auxiliary tank)

1,356 km / 2,341 km

732 nm / 1,264 nm

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

480 m / 883 m

1,574 ft / 2,897 ft

Landing performance
(ISA, MSL, ground roll / landing distance)

441 m / 779 m

1,447 ft / 2,556 ft

Max. service ceiling

6,096 m

20,000 ft

Dimensions

Mass and Loading

Crew

1 or 2 pilots

1 or 2 operators

Typical mission crew

1 pilot

1 operator

Empty weight

1,590 kg

3,505 lbs

Useful load

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 are based on clean aircraft without sensor or mission equipment. Specifications can differ depending on the specific sensor equipment. The above quoted data are approximately specifications and may change without notice.
1. With standard mission equippment and 2-man crew.