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PZL Swidnik SW-4

PZL Swidnik SW-4 © Karsten Palt
Photo ©: Karsten Palt

SW-4

Light Utility Helicopter

The PZL SW-4 is a single-engine five-seat light utility helicopter produced by the Polish manufacturer WSK PZL-Swidnik, today PZL-Swidnik S.A. (a subsidiary of AgustaWestland).

Crew1-2
Passengers3-4
 
Propulsion1 Turboshaft Engine
Engine ModelAllison / Rolls-Royce 250-C20 R/2SP
Engine Power336 kW451 shp
 
Speed232 km/h125 kts
  144 mph
Service Ceiling5.000 m16.404 ft
Range600 km324 NM
373 mi.
 
Empty Weight850 kg1.874 lbs
max. Takeoff Weight1.800 kg3.968 lbs
 
Rotor Blades (main/tail)3/23/2
Main Rotor Diameter9,00 m29,5 ft
Tail Rotor Diameter1,50 m4,9 ft
Rotor Disc Area63,6 m²685 ft²
Length (Fuselage)8,24 m27,0 ft
Length10,55 m34,6 ft
Height3,05 m10,0 ft
 
First Flight29.10.1996
Production Statusin production
 
EASA TCDSR.100
 
Data for (Version)PZL-Swidnik SW-4

WeblinksExtras
PZL-Swidnik S.A.

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