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DART Series
Preliminary Technical Specifications

Power Plant

 DART-450

DART-550

Engine

Motor Sich AI-450 SR turboprop engineGeneral Electric GE H75-A turboprop engine

Propeller

MT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering and reverse functionality

MT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering and reverse functionality

Fuel grades

Jet A-1, Jet A,TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8Jet A, Jet A1, RT, TS1 and T1, No.3 Jet Fuel

Calculated Performance

 DART-450

DART-550

Max. take off power

495 SHP

369 kW

550 SHP

404 kW

Max. continuous power (ISA, SL)

400 SHP298 kW550 SHP

404 kW

Max. operating speed (Vmo)490 km/h TAS265 KTAS490 km/h TAS

265 KTAS

Max level cruise speed (VH) (10.000ft) __404 km/h TAS218 KTAS
Typical cruise speed
(10.000ft, 75%, 97 kg/h)
352 km/h TAS190 km/h TAS_

_

Endurance

5 hours +5 hours +5,5 hours +

5,5 hours +

Max. rate of climb

8.9 m/s1,750 ft/min10.7 m/s

2,100 ft/min

Service ceilling

7,000 m23,000 ft7,600 m

25,000 ft

Take-off distance (ISA, SL)

≤ 600 m≤ 1,970 ft≤ 600 m

≤ 1,970 ft

Landing distance (ISA, SL)

≤ 400 m≤ 1,300 ft≤ 400 m

≤ 1,300 ft

Dimensions

Mass and Loading

 Aerobatic Configuration

Utility (Multi Role) Configuration

Load factors

+7 / -4+5 / -2.4

Maneuvers

Aerobatic Cat.Utility Cat.

MTOM

2,080 kg

4,586 lbs

2,300 kg

5,071 lbs

Basic empty mass (DART-450)

1,450 kg3,197 lbs1,450 kg

3,197 lbs

Basic empty mass (DART-550)

1,550 kg3,417 lbs1,550 kg

3,417 lbs

Total fuel capacity (DART-450)

240 kg or 300 ltr529 lbs or 79 US gal662 kg or 760 ltr

1,459 lbs or 201 US gal

Total fuel capacity (DART-550)

240 kg or 300 ltr529 lbs or 79 US gal608 kg or 760 ltr

1,340 lbs or 201 US gal

Seats

22

The above data are approximately specifications and may change without notice.