BRAND and MODEL
VULCANAIR V1.O
TYPE
Four-seat, single-engine, cabin monoplane
ORIGIN
Italy
ENGINE
One 134 kw (180 hp) Lycoming IO-360-1A four-cylinder horizontally-opposed fuel-injected air-cooled engine
SPECIFICATIONS
Wingspan: 10.00 m (32 ft 10 in)
Length: 7.23 m (23 ft 9 in)
Height: 2.77 m (9 ft 1 in)
Cruising speed at 75% power at 1,829 m (6,000 ft): 241 km/h (150 mph)
Rate of climb at sea level: 270 m/min (900 ft/min)
Service ceiling: 4,500 m (14,700 ft)
Fuel capacity: 190 litres (42 Imp gals)
Take-off to 15 m (50 ft): 490 m (1608 ft)
Landing distance over 15 m (50 ft) obstacle: 503 m (1,650 ft)
Range with three persons of 77 kg (170 lb) with 45 mins reserve at 45% power at 3,048 m (10,000 ft): 1,094 km (680 miles)
Empty weight: 738 kg (1,627 lb)
Max useful load: 400 kg (882 lb)
Max luggage weight: 40 kg (88 lb)
Loaded weight: 1,155 kg (2,546 lb)
PHOTO
Airliners.net:Source of phothograph
