Aircraft > Single-Engine Piston > Vulcanair > N120VA: Vulcanair V1.0
The V1.0 is powered by the 180 hp Lycoming IO-360-M1A that is capable of using AvGas or alternative fuels. The aircraft is equipped standard with a constant speed propeller. The aircraft cabin is extremely functional with four seats and three doors, and a luggage capacity of 88 lbs. in a separate compartment. The aircraft cockpit has been designed to keep all avionics, displays, switches and circuit breakers in an ergonomic position for the pilot, and its shape has been designed to minimize parallax errors. The standard full IFR avionics package features a Garmin G500 TXi coupled with a GTN650, second Nav/Com, and ADS-B In and Out. An AoA (angle of attack) indicator is offered standard in the aircraft package. Finally, the V1.0 is a utility category aircraft that further expands the V1.0’s ambitions. https://ameraviainc.com/home/v1-0-single-engine/
Airframe: 135 Hours Total Time
Engine: 180 hp Lycoming IO-360-M1A
Performance: Engine: 180 hp Lycoming IO-360-M1A Max Take-Off Weight 2546 lb Typically Equipped Empty Weight 1627 lb Maximum Useful Load 919 lb Usable Fuel Capacity 50 gal Maximum Seating Capacity 4 Max Luggage Weight 88 lb Cruise Speed @ 75%, ISA, 6000ft 130 ktas Range (3 persons of 77 kg., 45-min reserve, 45% power, 10,000 ft) 591 nm Rate of Climb at Sea Level 900 ft/min Service Ceiling 14700 ft Takeoff Distance to 50 ft 1608 ft Landing Distance (over 50-ft obstacle) 1650 ft