V1.0
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vulcanair aircraft AIRCRAFT DIMENSIONS Overall Height 9 ft 1 in (2.77 m) Overall Length 23 ft 9 in (7.23 m) Wingspan 32 ft 10 in (10.00 m) Maximum Seating Capacity 4 Baggage Capacity 88 lb (40 kg) DESIGN WEIGHTS & CAPABILITIES Maximum Takeoff Weight 2546 lb (1155 kg) Typically Equipped Empty Weight 1664 lb (755 kg) Maximum Useful Load 882 lb (400kg) Usable Fuel Capacity 50 gal (190 I) PERFORMANCE Maximum Cruise Speed 135 ktas (250 km/hr) Range (3 persons of 77 kg., 45-min reserve, 45% power, 10000 ft) 550 nm (1019 km) Rate of Climb at Sea Level 730 ft/min (222 m/min) Service Ceiling 14700 ft (4500 m) Takeoff Distance to 50 ft 1440 ft (439 m) Landing Distance (over 50-ft obstacle) 1650 ft (480 m) “Short field” Landing Distance 1400ft (427 m) POWERPLANT Engine Lycoming IO-360-M1A Horsepower 180 hp Propeller Two-Bladed Costant Speed Propeller TBO 2,000 hours

Meet the VI .0! The new certified single-engine aircraft by Vulcanair. Built tough with quality materials; metal vs. plastic, durable versus expendable, in line with Vulcanair's design philosophy: durability safety and exceptional value. With the VI.0, Vulcanair leverages its long experience in designing and manufacturing more complex multi-engine aircraft and aims to the popular single-engine piston market. Excellent aircraft performance, state-of-the-art manufacturing techniques, with metal durable construction, modern avionics and exceptional value in terms of acquisition costs make the...