Poland
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
29.5 ft
(9.00 m)
Empty Wgt
2,315 lb
(1,050 kg)
Wgt Diff
+1,653 lb
(+750 kg)
(Showcased structural values pertain to the PZL SW-4 production variant)
Installed:
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).
Max Speed
162 mph
(260 kph | 140 kts)
Ceiling
17,060 ft
(5,200 m | 3 mi)
Range
491 mi
(790 km | 1,463 nm)
Rate-of-Climb
2,030 ft/min
(619 m/min)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
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.