PZL Kania Civil Aircraft Model Details

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General Information of PZL Kania

Developed From : Mil Mi-2

First Flight : 29009

Manufacturer : PZL-Swidnik

Number Built : 19

Primary Users : Poland

Produced : 1986-2006

Role : Helicopter

General characteristics of PZL Kania

Capacity : 9 passengers or 1,200 kg (2,645 lb) internal, 800 kg (1,763 lb) external cargo

Crew : One

Disc Area : 167 m² (1,792 ft²)

Empty Weight : 2,000 kg (4,409 lb)

Height : 3.75 m (12 ft 3½ in)

Length : 12.03 m (39 ft 5½ in)

Max Takeoff Weight : 3,550 kg (7,826 lb)

Powerplant : 2 × Allison 250-C20B turboshafts, 313 kW (420shp) each

Rotor Diameter : 14.56 m (47 ft 9¼ in)

Performance of PZL Kania

Cruise Speed : 190 km/h (102 knots, 118 mph) (econ cruise)

Ferry Range : 863 km (466 nmi, 536 mi) (max fuel, no reserves)

Maximum Speed : 215 km/h (116 knots, 134 mph)

Range : 493 km (266 nmi, 306 mi) (standard fuel, no reserves)

Rate Of Climb : 8.75 m/s (1,725 ft/min)

Service Ceiling : 4,000 m (13,120 ft)

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