TYPE: Light utility twin-prop transport.
PROGRAMME: First details announced in mid-2003. Due to enter production at Lukhovitsy plant in 2005-06.
CURRENT VERSIONS: MiG-201: As described.
MiG-201M: Alternative power plant of two 324 kW (435 hp) Teledyne Continental GTSIO-520F flat-six piston engines.
MiG-201MT1: Turboprop version with two 560 kW (751 shp) Walter M 601Es.
MiG-201MT2: Alternative turboprop version with two Pratt & Whitney PT6A-42s, each rated at up to 634 kW (850 shp). Range 755 n miles (1,400 km; 869 miles) with max payload.
COSTS: US$650,000 with M-9 engines; US$1,400,000 with PT6A-42 engines.
DESIGN FEATURES: Replacement for Antonov An-2 utility biplane, but with twin engines. Rugged construction and short-field performance with maximum of 10 occupants or equivalent freight.
High, constant-chord wing; moderately sweptback fin with ventral fillet; low-mounted, constant-chord tailplane. Service life 40,000 hours.
STRUCTURE: Generally of metal.
LANDING GEAR: Tricycle type; retractable.
POWER PLANT: Two 327 kW (434 hp) VOKBM M-9FS nine-cylinder radial engines, each driving an MT-Propeller MTV-9 three-blade, variable-pitch propeller.
|Freight door (port): Height||1.22 m (3 ft 11¼ in)|
|Width||1.30 m (4 ft 3¼ in)|
|Cabin: Length||4.50 (14 ft 9 in)|
|Max width||1.52 m (4 ft 11¾ in)|
|Max height||1.35 m (4 ft 5¼ in)|
|WEIGHTS AND LOADINGS:|
|Weight empty, equipped||2,850 kg (6,283 lb)|
|Max payload||1,000 kg (2,205 lb)|
|Max fuel weight||650 kg (1,433 lb)|
|Max T-O weight||3,900 kg (8,598 lb)|
|Max level speed||205 kt (380 km/h; 236 mph)|
|Econ cruising speed||162 kt (300 km/h; 186 mph)|
|Service ceiling||6.000 m (19,680 ft)|
|T-O run||390 m (1,280 ft)|
|Range: with 850 kg (1,874 lb) payload||297 n miles (550 km; 341 miles)|
|with 550 kg (1,213 lb) payload||1,025 n miles (1,900 km; 1,180 miles)|