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/ PWS-33 Wyżeł
PWS-33 Wyżeł
The PWS-33 Wyżeł was a Polish twin-engine military trainer aircraft.
Although destined for production it got no further than the two prototypes before Poland was invaded.
Specifications
Crew
2
Capacity
460 kg (1,010 lb) useful load
Length
6.94 m (22 ft 9 in)
Wingspan
9.26 m (30 ft 5 in)
Height
2.56 m (8 ft 5 in)
Wing area
12.7 m2 (137 sq ft)
Empty weight
950 kg (2,094 lb)
Gross weight
1,410 kg (3,109 lb)
Fuel capacity
250 l (54.99 imp gal; 66.04 US gal)
Powerplant
2 × PZI nż Major 4B 4-cyl. inverted air-cooled in-line piston engines, 97 kW (130 hp) each
Propellers
2-bladed Fixed pitch wooden propellers, 1.9 m (6 ft 3 in) diameter
Performance
Maximum speed
315 km/h (196 mph, 170 kn)
Cruise speed
260 km/h (160 mph, 140 kn)
Range
1,160 km (720 mi, 630 nmi)
Service ceiling
4,500 m (14,800 ft)
Rate of climb
4.5 m/s (890 ft/min)
Wing loading
111 kg/m2 (23 lb/sq ft)
Armament
Guns
1 x fixed 7.92 mm (0.312 in) PWU Wz.36 machine-gun in the fuselage
Bombs
2 x 12.5 kg (27.6 lb) practice bombs.
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