Overview
The PZL Kania is a light utility helicopter developed in Poland as an improved derivative of the Mil Mi-2. Designed for civil and government roles, it incorporated Western avionics and engine upgrades. The aircraft aimed to modernize a proven platform for export markets.
Specifications
Units
- Engine
- 2 × Rolls Royce Allison 250C20B
- Engine type
- Turboshaft
- Power
- 2 × 420 shp · 313 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 9
- Crew
- —
- Cabin width
- 3 ft 7 in · 1.10 m
- Cabin height
- 5 ft 4 in · 1.62 m
- Cabin length
- 8 ft 6 in · 2.60 m
- Exterior length
- 57 ft 4 in · 17.47 m
- Tail height
- —
- Fuselage diameter
- 4 ft 3 in · 1.30 m
- Wing span
- 47 ft 7 in · 14.50 m
- Baggage volume
- 14 ft³ · 0.4 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 7,850 lb · 3,550 kg
- Max landing weight
- —
- Max payload
- 3,400 lb · 1,550 kg
- Fuel capacity
- 270 gal · 1,000 L · 800 kg (Jet A)
- Max cruise speed
- 116 kt · 133 mph · 215 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 266 nm · 310 mi · 490 km
- Fuel burn
- 1.72 nm/gal · 0.84 km/L
- Ceiling
- 13,120 ft · 4,000 m
- Rate of climb
- 1,722 ft/min · 9 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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