page_title: PZL SW-4
section_title: Specifications (SW-4)
hierarchical_section_title: PZL SW-4 / Specifications (SW-4)
caption_attribution_description: Deutsch: PZL SW-4 auf der ILA 2010. English: PZL SW-4 at ILA 2010.
context_page_description: The PZL SW-4 Puszczyk is a Polish light single-engine multipurpose helicopter manufactured by PZL-Świdnik. Following a protracted development, the SW-4 entered service in 2002, the primary operator of the type has been the Polish Armed Forces. The SW-4 was further developed by PZL-Świdnik and corporate parent AgustaWestland into an optionally piloted vehicle, the SW-4 Solo. From 2016 onwards, the type has been marketed to civil operators as the AW009, while the SW-4 designation shall be continue to be used for the military market.
context_section_description: Data from AgustaWestland
  General characteristics
  Crew: 1
  Capacity: 4 passengers
  Length: 10.57 m (34 ft 8 in)
  Height: 3.05 m (10 ft 0 in)
  Empty weight: 1,050 kg (2,315 lb)
  Gross weight: 1,600 kg (3,527 lb)
  Max takeoff weight: 1,800 kg (3,968 lb)
  Powerplant: 1 × Rolls-Royce 250-C20R/2 turboshaft engine, 336 kW (451 hp)
  Main rotor diameter:  9 m (29 ft 6 in)
  Main rotor area: 64 m² (690 sq ft)
  Performance
  Maximum speed: 260 km/h (160 mph, 140 kn)
  Range: 790 km (490 mi, 430 nmi)
  Service ceiling: 5,200 m (17,100 ft)
  Rate of climb: 10.3 m/s (2,030 ft/min)
  Disk loading: 25 kg/m² (5.1 lb/sq ft)
  Power/mass: 0.21 kW/kg (0.13 hp/lb)
caption: SW-4 on static display, 2010
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