The Ultravia Pelican is a versatile series of high-wing, single-engine, tractor-configuration ultralight aircraft originally designed in Canada by Jean Rene Lepage and produced in kit form for amateur construction by Ultravia Aero International. The Pelican family encompasses a range of aircraft from the earliest single-seat ultralights of the 1980s, through widely built two-seat touring models, to later derivatives developed under new manufacturers after Ultravia’s closure. Known for its classic high-wing design and adaptability, the Pelican has been offered with a variety of powerplants, airframe configurations and performance options that suit recreational flying, sport touring and light training roles.
Design Philosophy and Airframe Construction
The design of the Pelican reflects traditional aviation thinking blended with ultralight simplicity. Early models like the Le Pelican were constructed with aluminum tube fuselages, gusset joints and pop rivets, featuring wings built around a “D” cell spar with foam and aluminum ribs, all covered in doped aircraft fabric for lightweight strength and rigidity. Strut-braced high wings provide stable flight characteristics and excellent downward visibility, while the tractor-configuration engine installation ahead of the cabin enhances propeller efficiency and cooling. Landing gear configurations vary by version, from conventional taildragger arrangements on early ultralights to fixed tricycle gear on later two-seat variants. The Pelican’s adaptable structure allowed for optional floats, skis and amphibious gear on some models, demonstrating its utility across different environments and seasons.
Le Pelican and Single-Seat Variants
The original Le Pelican was conceived as a minimalist ultralight, typically powered by a small two-cylinder Briggs & Stratton engine of roughly 18 hp to keep weight low and simplicity high. This model exemplifies the core ultralight ethos with an empty weight often around 210 – 250 lb and a maximum gross weight under 525 lb, enabling compliance with early ultralight regulations and simplicity of operation. Wingspans for these single-seat designs could exceed 35 ft to generate ample lift at low speeds, while control surfaces like one-third span ailerons and conventional three-axis control offered predictable handling. Typical cruise speeds were modest, generally in the 50 – 70 mph range, with stall speeds low enough to satisfy regulatory requirements and promote safe short-field operations.
Two-Seat Pelican Club and Pelican PL
Responding to demand for greater capability, Ultravia introduced two-seat models beginning with the Pelican Club in the mid-1980s and later the improved Pelican PL. These side-by-side aircraft expanded payload and performance significantly. The Pelican PL retained the high-wing layout but transitioned to a composite fuselage with rigid PVC and all-metal wings for enhanced durability. Typical dimensions for this model include a wingspan around 29.5 ft, a length near 19.8 ft, and a cabin width over 40 in to accommodate pilot and passenger. Gross weights for the PL hovered around 1,400 lb, with baggage capacity around 75 lb and strong load factor limits (±4 G) for aerobatic safety margins in recreational flight. (ultraligero.net)
Powerplant Options and Performance
Pelican series aircraft were designed to accept a range of four-stroke engines, with later two-seat models commonly using Rotax powerplants. The Pelican PL could be equipped with engines like the Rotax 912ULS producing approximately 100 hp or the turbocharged Rotax 914 with about 115 hp, enabling cruise speeds over 115 mph and robust climb performance. Fuel capacity on such models could approach 24 US gallons in dual wing tanks, providing useful range for sport touring. Variants such as the Pelican Sport and Sport 600 – aimed at light sport aircraft (LSA) categories – further refined aerodynamics with higher-lift airfoils and even STOL (short takeoff and landing) enhancements like drooping ailerons. Typically, stall speeds on these larger variants remained low enough for safe operating margins, while cruise figures balanced speed and fuel efficiency to appeal to recreational cross-country pilots.
Flight Characteristics and Handling
The high-wing configuration, generous wing area, and strut bracing contribute to forgiving low-speed behavior and stable flight. Control systems include mechanically actuated flaps and conventional stick/rudder linkages, with optional trim systems to reduce pilot workload on longer flights. Landing gear choices impact ground handling: taildragger configurations yield classic, rugged performance for rough fields, while tricycle gear simplifies taxiing and landings for less experienced pilots. The underlying airframe design ensures that stalling characteristics remain benign, with well-behaved responses near minimum flying speeds and ample lift to support short takeoffs and landings.
Legacy and Continued Development
Despite Ultravia Aero International’s closure in 2006, the Pelican design lineage has continued through various companies. After bankruptcy, the design assets passed to Kolb Aircraft and later Ballard Sport Aircraft, which have offered modern kit and ready-to-fly versions, sometimes incorporating advanced materials such as carbon fiber in fuselage structures and updated avionics. Regional manufacturers in Brazil like Aerodesign and Flyer Indústria Aeronáutica have also developed Pelican-based derivatives tailored to local regulatory categories, such as LSA rules in Brazil. These ongoing evolutions reflect the enduring appeal of the Pelican concept: versatile, efficient, and accessible sport aircraft that remain relevant decades after their original conception.
Technical Summary
Across its various incarnations, the Ultravia Pelican family exhibits common technical threads: high-wing stability, modular airframe construction accommodating composite and metal elements, a broad range of compatible powerplants from small two-stroke lawnmower derivatives to robust Rotax four-strokes, and performance profiles tailored to both ultralight simplicity and light sport capability. Variants differ in weight, size and performance, but all adhere to an underlying design philosophy that prizes ease of construction, economical operation, and enjoyable piloting characteristics. Whether in its original single-seat form or as a later two-seat touring ultralight, the Pelican series occupies a distinctive place in amateur-built aviation history.
