BRAND and MODEL
BELLANCA DECATHLON
TYPE
Two-seat fully-aerobatic cabin monoplane
ORIGIN
United States of America
ENGINE
One 134 kw (180 hp) Lycoming AEIO-360-H1B fuel-injected inverted systems four-cylinder
horizontally-opposed air-cooled engine
SPECIFICATIONS
[8KCAB]
Wingspan:9.75 m (32 ft)
Length:6.98 m (22 ft 10¾ in)
Height:2.36 m (7 ft 9 in)
Wing area:15.71 m²(169.1 sq ft)
Max speed at 2,135 m (7,000 ft):254 km/h (158 mph)
Cruising speed at 75% power:241 km/h (150 mph)
Stalling speed:84 km/h (52 mph)
Initial rate of climb:375 m/min (1,230 ft/min)
Service ceiling:5,245 m (17,200 ft)
Take-off run:151 m (495 ft)
Landing run:130 m (425 ft)
Range no reserve at 75% power:944 km (587 miles)
Range at 55% power:1,006 km (625 miles)
Fuel capacity:151 litres (33 Imp gals)
Empty weight:596 kg (1,315 lb)
Loaded weight:816 kg (1,800 lb)
PHOTO
shop.pichler.de:Source of phothograph
