Mi-2 (PZL W-3A Sokol) Multipurpose helicopter

Mi-2 (PZL W-3A Sokol) Multipurpose helicopter. First flight: 1979
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Technical specifications

DESIGNER PZ (OKB Mil)
COUNTRY Poland (Russia)
TYPE
Multipurpose helicopter
CREW 1 - 2
POWER-PLANT Two turboshaft engines PZL-10V (OMKB Mars TVD-10)
Power, h.p. 2x900
PERFORMANCE  
Length (with main and tail rotor), m 18,79
Length (with tail rotor), m 15,296
Main rotor diameter, m 25,70
Tail rotor diameter, m 3,03
Height, m 4,20
WEIGHT  
Maximum take-off, kg 6.400
Normal take-off, kg 6.100
Empty, kg 3.650 (3.299)
Internal fuel, kg 1.700 + available fuel 1.100
Weight of transported fuel with external tanks, kg -
Warload, kg -
Payload, kg 2.912
- passengers up to 12
- stretcher 4
- freight in cabin 2.000
- with on hook 2.086 (2.100)
PERFORMANCE  
Maximum speed, km/h 260 (270)
Cruising speed, km/h 243 (235)
Range, km 715 (798)
Ferry range, km 1.100
Combat range, km -
Service ceiling, m 5.430 (2.529)
Static ceiling, m 3.500 (2.011)
Rate of climb, m/min 612
Maximum overload, g -
ARMAMENT Doesn't have (defensive).