BRAND and MODEL
CZL LD-40 META SOKOL
TYPE
Four-seat cabin monoplane
ORIGIN
Czechoslovakia
ENGINE
One 104 kw (140 hp) Walter M-332 four-cylinder in-line inverted air-cooled supercharged engine
SPECIFICATIONS
Wingspan: 10.32 m (33 ft 9½ in)
Length: 7.56 m (24 ft 9½ in)
Height: 2.52 m (8 ft 3 in)
Wing area: 14.5 m² (156 sq ft)
Max speed at sea level: 240 km/h (149 mph)
Cruising speed: 215 km/h (134 mph)
Landing speed: 95 km/h (59 mph)
Initial rate of climb: 270 m/min (885 ft/min)
Service ceiling: 4,999 m (16,400 ft)
Take-off run to 15 m (50 ft) on grass: 525 m (1,722 ft)
Range: 1,107 km (688 miles)
Endurance: 7 hrs 5 mins
Empty weight: 534 kg (1,177 lb)
Useful load: 400 kg (882 lb)
Loaded weight: 935 kg (2,062 lb)
PHOTO
alchetron.com:Source of phothograph
