Start | PZL | CSS-12

PZL CSS-12


General information


ManufacturerPZL
ModelCSS-12
ModificationCSS-12
CountryPoland
Years19
TypePassenger aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan18.50 m
Length12.75 m
Height5.00 m
Wing area40.10 m2
Zero fuel weight-
Empty weight3734 kg
Maximum takeoff weight5500 kg
Normal takeoff weight-
Flight duration-
Engine2 Argus As411 A1
Power2 x 580 HP
Thrust-
Maximum speed365 km/h
Cruising speed305 km/h
Rate of climb-
Practical range600 km
Service ceiling6440 m
Hovering ceiling-
Crew2