ZLIN TRENER Civil Aircraft Model Details

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General Information of ZLIN TRENER

First Flight : 1947

Introduction : 1948

Manufacturer : Moravan Otrokovice

Produced : 1948-1977

Role : Training aircraft

General characteristics of ZLIN TRENER

Airfoil : NACA 2418 / NACA 4412

Crew : 2 (pilot and passenger; could be flown from either seat)

Empty Weight : 700 kg (1,543 lb)

Height : 2.06 m (6 ft 9 in)

Length : 7.98 m (26 ft 2 in)

Max Takeoff Weight : 1,000 kg (2,205 lb) for standard flight (940 kg aerobatic)

Powerplant : 1 × Avia M137AZ 6-cyl. inverted air-cooled in-line piston engine, 134 kW (180 hp)

Propellers : 2-bladed

Wing Area : 14.89 m2 (160.3 sq ft)

Wingspan : 9.87 m (32 ft 5 in)

Performance of ZLIN TRENER

Cruise Speed : 216km/h (134mph; 117kn)

G Limits : 6/-3

Maximum Speed : 237km/h (147mph; 128kn) at sea level

Power/Mass : 7.46 kg/kW

Range : 440km (273mi; 238nmi) with std fuel

Rate Of Climb : 5m/s (980ft/min)

Service Ceiling : 4,500m (14,764ft)

Stall Speed : 98km/h (61mph; 53kn)

Wing Loading : 67.16kg/m2(13.76lb/sqft) std flight wt

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