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DART Series
Preliminary Technical Specifications

Power Plant

 DART-450

DART-550

Engine

Motor Sich AI-450 SR turboprop engine

General Electric GE H75-100 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-8

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

Calculated Performance

 DART-450

DART-550

Max. take off power

495 HP

369 kW

550 HP

404 kW

Max. continuous power (ISA, SL)

400 HP298 kW550 HP

404 kW

Expected top speed (12,000 ft, MCP, 114 kg/h)

370 km/h TAS200 KTAS

Expected top speed (20,000 ft, MCP, 159 kg/h)

491 km/h TAS

265 KTAS

Typical cruise speed (10,000 ft, 75 %, 97 kg/h)

352 km/h TAS190 KTAS

Typical cruise speed (10,000 ft, 60 %, 95 kg/h)

352 km/h TAS

190 KTAS

Endurance

8 hours +8 hours +8 hours +

8 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 Confguration

Utility (Multi Role) Configuration

Load factors

+7 / -4+5 / -2.4

Maneuvers

Aerobatic Cat.Utility Cat.

MTOM

2,080 kg

4,586 lbs

2,400 kg

5,291 lbs

Basic empty mass (DART-450)

1,450 kg3,196 lbs1,550 kg

3,417 lbs

Basic empty mass (DART-550)

1,500 kg3,307 lbs1,600 kg

3,527 lbs

Max. usable fuel

240 kg or 300 l529 lbs or 79 US gal662 kg or 826 l

1,459 lbs or 218 US gal

Seats

22

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