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PZL Krosno KR-03A Puchatek

pzl-kr03


The tandem two place metal framed sailplane was designed by Jerzy Krawczyk and Eugeniusz Pelczar as a basic training glider and first flew in 1985. It has an oleo pneumatic sprung fixed main wheel, a tail wheel and a rubber sprung nose skid. Approach control is by top and bottom surface Schempp-Hirth type airbrakes.

KR-03A Puchatek
Wing span: 16.4 m / 53.8 ft
Wing area: 19.44 sq.m / 209.25 sq.ft
Aspect ratio: 13.9
Airfoil: Wortmann FX-S-01-158
Empty Weight: 350 kg / 771 lb
Payload: 190 kg / 419 lb
Gross Weight: 540 kg / 1190 lb
Wing Load: 27.78 kg/sq.m / 5.69 lb/sq.ft
L/DMax: 27 88 kph / 48 kt / 55 mph
MinSink: 0.78 m/s / 2.38 fps / 1.41 kt
Seats: 2

 

 


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