PZL SW-4 Puszczyk
Summary
Category | Training aircraft |
Origin country | 🇵🇱 Poland |
First flight | 29 October 1996 |
Year of introduction | 2002 |
Number produced | 40 units |
Description
The PZL SW-4 Puszczyk is a military aircraft developed by the Polish manufacturer PZL-Świdnik in the late 1980s. Primarily designed for training purposes, it is a versatile single-engine helicopter that offers excellent maneuverability and reliability. The aircraft features a compact design and lightweight construction, making it suitable for various types of missions, including pilot training, reconnaissance, and transport. With its efficient engine and advanced avionics, the PZL SW-4 Puszczyk has been successfully deployed by several countries and is well-regarded for its capabilities in both civilian and military operations.
Technical specifications
Version: SW-4 | |
---|---|
Crew | 1 pilot |
Maximum speed | 260 km/h (162 mph) |
Height | 3.1 m (10.0 ft) |
Length | 10.6 m (34.7 ft) |
Service ceiling | 5200 m (17060 ft) |
Empty weight | 1050 kg (2315 lbs) |
Max. takeoff weight | 1800 kg (3968 lbs) |
Climb rate | 10.3 m/s (33.8 ft/s) |
Powerplant | 1 × turbine Rolls-Royce 250-C20R2 delivering 336 kW |
Current operating countries
Country | Units | ||
---|---|---|---|
Poland | 24 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.