Aeroplast (Italy), BDC Aero Industrie (Canada) Puma

Fixed Wing Single Engine

Aircraft Information

ICAO Code
BPUM
Manufacturer
Aeroplast (Italy), BDC Aero Industrie (Canada)
Model
Puma
Aircraft Type
Fixed Wing Single Engine
Primary Role
General Aviation

Technical Data

Engine Type
Inline
Engine Model
912UL/912ULS/912iS/914
Production Years
2007, 2010-2016
Units Produced
7
First Flight
1985

The BDC Aero Puma is a Canadian-manufactured ultralight aircraft that bridges Italian design heritage with modern regulatory compliance. First flown in the mid-1980s as the Bortolanza design, it was restructurally redesigned by BDC Aero Industrie in 2006 to meet Canadian Advanced Ultralight and US light-sport aircraft requirements. This high-wing, side-by-side two-seat aircraft features mixed aluminum and composite construction with a 27.9-foot wingspan and tricycle landing gear. Only seven examples were ever built, with BDC Aero Industrie of Lachute, Quebec producing six aircraft between 2010 and 2016.

Design Evolution and International Heritage

The Puma's story begins with Italian designer Antonio Bortolanza, who conceived the aircraft in the mid-1980s under a series of evolving names. Initially called the Pluto, then renamed Drakken (Swedish for "dragon"), the design finally settled on the Puma designation. Bortolanza's original vision centered on creating a sophisticated ultralight that would combine modern materials with traditional high-wing configuration, featuring an enclosed cockpit and side-by-side seating arrangement.

The design underwent significant transformation when BDC Aero Industrie acquired the rights and completely restructured the aircraft in 2006. This Canadian redesign was specifically engineered to comply with Transport Canada's Advanced Ultralight regulations and anticipated US light-sport aircraft rules, representing a careful balance between performance and regulatory requirements.

Limited Production History

Production of the Puma tells a story of boutique manufacturing in the ultralight sector. Aeroplast of Sale, Piedmont, Italy produced one example of the original Bortolanza design in 2007, establishing the aircraft's Italian roots. However, the primary production run occurred at BDC Aero Industrie's facility in Lachute, Quebec, where exactly six aircraft rolled out between 2010 and 2016.

The Quebec production run was methodically distributed across two certification categories: three Advanced Ultralight variants manufactured between 2010 and 2011, and three LSA/Limited category variants completed in 2013 and 2016. This production strategy reflected BDC Aero's adaptation to evolving certification requirements and market demands. Initially offered as kits until around 2015, the company transitioned exclusively to factory-built aircraft, recognizing the complexity of the mixed-material construction.

Engineering and Powerplant Integration

The Puma's technical specifications reveal sophisticated engineering within ultralight constraints. The aircraft measures 20.8 feet in length with a 27.9-foot wingspan, generating 124 square feet of wing area. The mixed-material construction combines an aluminum wing structure with a composite fuselage, topped by composite doors that provide weather protection while maintaining weight efficiency.

Powerplant options centered exclusively on the Austrian Rotax engine family, manufactured by BRP-Rotax in Gunskirchen. Three variants were available: the 80-horsepower Rotax 912UL for basic operations, the 100-horsepower 912ULS or fuel-injected 912iS for enhanced performance, and the turbocharged 115-horsepower Rotax 914 for high-altitude operations. These four-cylinder, liquid-and-air-cooled engines drive a two-bladed propeller measuring 5 feet 5 inches in diameter.

Performance and Operating Characteristics

The Puma's performance envelope reflects its ultralight heritage while delivering respectable capability. With an empty weight of 683 pounds, the aircraft achieves a maximum gross weight of 1,232 pounds in Advanced Ultralight configuration or 1,323 pounds in LSA category. This weight distribution yields a wing loading of 9.9 pounds per square foot, contributing to gentle handling characteristics.

Cruise performance reaches 132 miles per hour, while stall speed drops to just 40 miles per hour with flaps extended. The aircraft climbs at 1,000 feet per minute and achieves an 11:1 glide ratio, respectable figures for the ultralight category. Fuel capacity of 23.8 US gallons provides adequate range for recreational flying, while g-limits of +4/-2 accommodate normal aerobatic maneuvers.

Operational Service and Current Status

The Puma's operational history reflects its boutique production numbers. By November 2017, Canadian registration records showed three Advanced Ultralight and two Limited category BDC Pumas actively registered, alongside one aircraft registered in the United States and one Italian-built example imported to Canada. This represents virtually the entire production run remaining in service, an unusually high survival rate.

The aircraft serves exclusively in private recreational roles, with no commercial or military applications. Its two-seat side-by-side configuration makes it suitable for flight training or recreational flying, though the limited production numbers prevent widespread adoption. Video documentation shows at least one example operating from St-Hyacinthe, Quebec, demonstrating the type's continued airworthiness.

Legacy and Manufacturing Reality

BDC Aero Industrie appears to maintain the capability to produce additional Pumas, with the most recent example delivered in 2016. However, the extremely limited production numbers reflect the challenges facing small-scale aircraft manufacturers in the ultralight and light-sport markets. The Puma's significance lies not in numerical success but in demonstrating the evolution from kit-built to factory-produced aircraft within regulatory frameworks.

The aircraft represents a bridge between European ultralight design philosophy and North American certification requirements, showcasing how international aviation designs adapt to different regulatory environments. While production remains minimal, the Puma's mixed-material construction and Rotax integration illustrate modern approaches to ultralight aircraft development.