DART Series
Preliminary Technical Specifications
- Brochure (6 MB)
| DART-450 | DART-550 | |
|---|---|---|
Engine | Motor Sich AI-450 SR turboprop engine | General 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-8 | Jet A, Jet A1, RT, TS1 and T1, No.3 Jet Fuel |
| DART-450 | DART-550 | |||
|---|---|---|---|---|
Max. take off power | 495 SHP | 369 kW | 550 SHP | 404 kW |
Max. continuous power (ISA, SL) | 400 SHP | 298 kW | 550 SHP | 404 kW |
| Max. operating speed (Vmo) | 490 km/h TAS | 265 KTAS | 490 km/h TAS | 265 KTAS |
| Max level cruise speed (VH) (10.000ft) | _ | _ | 404 km/h TAS | 218 KTAS |
| Typical cruise speed (10.000ft, 75%, 97 kg/h) | 352 km/h TAS | 190 KTAS | _ | _ |
Endurance | 5 hours + | 5 hours + | 5,5 hours + | 5,5 hours + |
Max. rate of climb | 8.9 m/s | 1,750 ft/min | 10.7 m/s | 2,100 ft/min |
Service ceilling | 7,000 m | 23,000 ft | 7,600 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 |
| 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 kg | 3,197 lbs | 1,450 kg | 3,197 lbs |
Basic empty mass (DART-550) | 1,550 kg | 3,417 lbs | 1,550 kg | 3,417 lbs |
Total fuel capacity (DART-450) | 240 kg or 300 ltr | 529 lbs or 79 US gal | 662 kg or 760 ltr | 1,459 lbs or 201 US gal |
Total fuel capacity (DART-550) | 240 kg or 300 ltr | 529 lbs or 79 US gal | 608 kg or 760 ltr | 1,340 lbs or 201 US gal |
Seats | 2 | 2 | ||
The above data are approximately specifications and may change without notice.