Vulcanair V1.0

Overview

The Vulcanair V1.0 is a single-engine, four-seat, high-wing certified piston airplane built by Vulcanair S.p.A. of Naples, Italy. Its strut-braced wing, fixed tricycle gear, and all-metal airframe place it squarely in the training-and-touring segment long defined by the Cessna 172. The design is not new so much as renewed: it descends from the 1968 Partenavia P.64B “Oscar,” grandfathered under CAR Part 3 and certificated in the Utility category, then updated with a fuel-injected Lycoming and a Garmin glass panel. It carries EASA type-certificate data sheet A.613, and the FAA type-certificated the V1.0 on 20 December 2017. Airframes are built in Casoria near Naples, with US assembly running from Elizabethtown, North Carolina since 2024.

Power comes from a 180-hp Lycoming IO-360-M1A, fuel-injected and normally aspirated, with a 2,000-hour TBO turning a two-blade Hartzell constant-speed propeller in the equipped US configuration. That yields a 130-KTAS cruise at 75% power, a service ceiling of 14,700 ft, and 591 nm of range on 50 usable gallons with reserve. Useful load is about 919 lb, and direct operating cost sits near $138 per hour, roughly Cessna-172 class. The V1.0 was pitched as an affordable factory-new certified four-seater whose 2017 launch price undercut a comparably-equipped new Cessna 172, and its buyer base reflects that: Part 141 flight schools, university programs such as Delaware State University, and owner-operators who want new-airplane systems without composite construction. It suits a flight department or private owner shopping for a current-production metal trainer with IFR glass standard, provided they can accept a thin US field fleet and support that still leans on a young North Carolina operation and the Naples factory.

Key Features for GA Buyers

• Factory-new certified four-seater with Garmin glass standard and IFR capability out of the box; the launch configuration paired a Garmin G500 suite with the all-metal airframe.
• 180-hp fuel-injected Lycoming IO-360-M1A with a 2,000-hour TBO – one of the most common Lycoming types, with wide shop and parts support.
• Cruise of 130 KTAS at 75% power against a direct operating cost near $138/hr and about 11 gph fuel burn, keeping trip economics in 172 territory.
• Utility-category certification and three cabin doors, with useful load around 919 lb and baggage up to 88 lb.
• Two propeller paths are certified: the equipped two-blade Hartzell metal constant-speed unit, and a basic-trainer configuration with a fixed-pitch wooden MT propeller.
• All-metal construction, marketed as a durability and repairability contrast to composite rivals in the same class.

Trade-offs

• The V1.0 is a new type in the US with a thin field fleet, so parts availability and technical support depend on the Elizabethtown, NC operation and the Naples factory rather than a deep independent service network.
• No authoritative total-built or fleet-size figure is published, which limits the resale and long-term-support data a buyer can lean on.
• Performance is adequate rather than commanding: sea-level climb is about 730 fpm and cruise around 130 KTAS, in line with the training class it targets rather than ahead of it.
• Introductory pricing near $259,000 at 2017 launch had risen to roughly $450,000 for equipped examples by 2024, eroding the low-price appeal it launched on.
• The airframe concept is decades old; buyers drawn to the latest aerodynamic or cabin design will find a modernized 1968 lineage rather than a clean-sheet airplane.

See Also

• Cessna 172 Skyhawk – the high-wing four-seat trainer benchmark the V1.0 is pitched against. Compare
• Tecnam P2010 – the other modern Italian high-wing four-seat certified single, the closest current peer. Compare
• Diamond DA40 Star – a modern low-wing composite trainer to cross-shop for glass and efficiency. Compare
• Vulcanair P.68 – Vulcanair’s own high-wing twin, the step up to multi-engine in the same family. Compare