PZL-106 Kruk Civil Aircraft Model Details

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General Information of PZL-106 Kruk

First Flight : April 17, 1973

Manufacturer : WSK PZL Warszawa-Okecie

National Origin : Poland

Number Built : 275+[1]

Primary Users : Polish civilian aviation; East Germany / Argentina

Produced : 1976-

Role : Agricultural aircraft

Status : in production

General characteristics of PZL-106 Kruk

Capacity : 1 seat for mechanic (optional), hopper for 1,400 L (370 US Gallons)

Crew : 1, pilot

Empty Weight : 1,790 kg (3,946 lb)

Height : 3.32 m (10 ft 10 3/4 in)

Length : 9.25 m (30 ft 4 1/2 in)

Max Takeoff Weight : 3,450 kg (7,606 lb) (restricted category)

Powerplant : 1 × PZL-3SR air-cooled radial engine, 448 kW (600 hp)

Wing Area : 31.69 m2 (341.1 m2)

Wingspan : 14.90 m (48 ft 10 1/2 in)

Performance of PZL-106 Kruk

Cruise Speed : 160km/h (86 knots, 99 mph) (operating speed)

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

Range : 900 km (485 nmi, 559 mi)

Rate Of Climb : 3.8 m/s (748 ft/min)

Stall Speed : 100 km/h (54 knots, 62 mph)

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