Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the PZL SW-4 Light Utility Helicopter (LUH).
1 x Rolls-Royce 250-C20R/2 turboshaft engine developing 451 horsepower driving three-bladed main rotor and two-bladed tail rotor (facing port side).
Propulsion
162 mph
260 kph | 140 kts
Max Speed
17,060 ft
5,200 m | 3 miles
Service Ceiling
491 miles
790 km | 427 nm
Operational Range
2,030 ft/min
619 m/min
Rate-of-Climb