ZLIN Z-50 Civil Aircraft Model Details

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General Information of ZLIN Z-50

First Flight : 27593

Introduction : 1975

Manufacturer : Zlin Aircraft

Role : aerobatic aircraft

General characteristics of ZLIN Z-50

Aspect Ratio : 5.89:1

Airfoil : NACA 0018 at root, NACA 0012 at tip

Crew : 1

Empty Weight : 570 kg (1,257 lb)

Height : 1.86 m (6 ft 1¼ in)

Length : 6.62 m (21 ft 8¾ in)

Max Takeoff Weight : 720 kg (1,587 lb)

Powerplant : 1 × Lycoming AEIO-540-D4B5 air-cooled flat-six engine, 194 kW (260 hp)

Wing Area : 12.5 m² (134.55 ft²)

Wingspan : 8.58 m (28 ft 1¾)

Performance of ZLIN Z-50

Cruise Speed : 240 km/h (129 kt, 149 mph) economy cruise at 500 m (1,640 ft)

Maximum Speed : 293 km/h (158 knots, 182 mph) at 500 m (1,640 ft)

Never Exceed Speed : 337 km/h (181.5 knots, 209 mph)

Power/Mass : 3.71 kg/kW (6.10 lb/hp)

Range : 640 km (345nmi, 397 mi) with max fuel, including tip tanks

Rate Of Climb : 12 m/s (2,360 ft/min)

Service Ceiling : 6,000 m (19,675 ft)

Stall Speed : 98 km/h (53 knots, 61 mph)

Wing Loading : 57.6 kg/m² (11.8 lb/ft²)

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