(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the PZL SW-4 production variant)
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).
(260 kph | 140 kts)
(5,200 m | 3 mi)
(790 km | 1,463 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.