PZL-101 Gawron Civil Aircraft Model Details

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General Information of PZL-101 Gawron

Developed From : Yakovlev Yak-12

First Flight : 21289

Manufacturer : WSK-Okecie

Number Built : 325

Primary Users : Poland; Bulgaria; Hungary; Austria

Produced : 1960-1968

Role : Agricultural and utility aircraft

General characteristics of PZL-101 Gawron

Capacity : 3 passengers or 500 kg (1,100 lb) powdered chemicals or 605 L (133 Imp Gal) liquid chemicals

Crew : one

Empty Weight : 1,004 kg (2,313 lb)

Height : 3.12 m (10 ft 3 in)

Length : 9.00 m (29 ft 6½ in)

Max Takeoff Weight : 1,660 kg (3,660 lb)

Powerplant : 1 × Ivchenko AI-14R air-cooled 9-cylinder radial engine, 191 kW (260 PS)

Wing Area : 23.86 m² (256.8 sq ft)

Wingspan : 12.68 m (41 ft 7 in)

Performance of PZL-101 Gawron

Cruise Speed : 130 km/h (70 knots, 81 mph)

Maximum Speed : 170 km/h (86 knots, 99 mph)

Range : 525 km (284 nmi, 325 mi)

Rate Of Climb : 2.4 m/s (482 ft/min)

Service Ceiling : 3,600 m (11,800 ft)

Stall Speed : 50 km/h (27 knots, 31 mph)

Take Off Run : 102 m (335 ft)

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