PZL-Swidnik SM-2, SP-SAP, c/n 202016  © Mick Bajcar
Photo ©: Mick Bajcar (photos at airliners.net)

SM-2

Light Utility Helicopter

The PZL Swidnik SM-2 is a light single-engine five-seat utility helicopter built by the Polish manufacturer WSK PZL Swidnik.

Crew1
Passengers4
 
Propulsion1 Radial Engine
Engine ModelPZL (Iwtschenko / Ivchenko) LiT-3 (AI-26W)
Engine Power423 kW567 hp
 
max. Cruise Speed130 km/h70 kts
  81 mph
max. Speed (vne)170 km/h92 kts
  106 mph
Service Ceiling3.500 m11.483 ft
Rate of climb144 m/min472 ft/min
Range309 km167 NM
192 mi.
 
Empty Weight1.930 kg4.256 lbs
max. Takeoff Weight2.570 kg5.666 lbs
 
Rotor Blades (main/tail)3 / 33 / 3
Main Rotor Diameter14,35 m47,1 ft
Tail Rotor Diameter2,50 m8,2 ft
Rotor Disc Area161,7 m²1741 ft²
Length (Fuselage)12,08 m39,6 ft
Length17,05 m55,9 ft
Height3,30 m10,8 ft
 
First Flight18.11.1959
Production Statusout of production
Total Production86
Developed fromPZL Swidnik SM-1 (Mil Mi-1)
 
Data for (Version)PZL Swidnik SM-2
VariantsSM-2D

Remarks
The SM-2 is a five-seat development of the PZL Swidnik SM-1, a license built Mil Mi-1, with enlarged cabin.


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