The Normand Dube Aerocruiser 450 Turbo is a six-seat Canadian amateur-built aircraft, designed by Normand Dube and produced by Aviation Normand Dube of Sainte-Anne-des-Plaines, Quebec. The aircraft is a development of the four-seat Norman Dube Aerocruiser Plus.[1][2]
| Aerocruiser 450 Turbo | |
|---|---|
| Role | Amateur-built aircraft |
| National origin | Canada |
| Manufacturer | Aviation Normand Dube |
| Designer | Normand Dube |
| Introduction | 1997 |
| Status | In production (2015) |
| Number built | one prototype |
| Developed from | Norman Dube Aerocruiser Plus |
Design and development
editThe Aerocruiser 450 Turbo features a strut-braced high-wing, a six-seat enclosed cabin accessed by doors, fixed conventional landing gear and a single engine in tractor configuration.[1][2]
The aircraft is made with a welded 4130 steel tubing fuselage and a riveted 2024 aluminum wing. Its 39.25 ft (12.0 m) span wing has an area of 207 sq ft (19.2 m2) and mounts flaps. The engine used on the prototype is a 450 hp (336 kW) turbocharged, geared and fuel-injected Lycoming TIGO-541 four-stroke powerplant.[1][2][3]
Operational history
editReviewers Roy Beisswenger and Marino Boric described the design in a 2015 review as "a two-ton giant".[1][2]
By December 2018, one example, the prototype, had been registered with Transport Canada.[4]
In December of 2014, the designer of the Aerocruiser 450 Turbo, Normand Dube, used his own aircraft to sabotage two of Hydro-Quebec's high-tension power lines, causing over 180,000 customers to lose electrical power. He was convicted for the attack in Quebec court in November 2018 and sentenced to seven years in prison for the attack. The aircraft used in the attack, the prototype Aerocruiser 450 Turbo, was seized as evidence.[5][6][7]
Specifications (Aerocruiser 450 Turbo)
editData from Bayerl, Tacke and the manufacturer[1][2][3]
General characteristics
- Crew: one
- Capacity: five passengers
- Length: 35 ft (11 m)
- Wingspan: 39 ft 3 in (11.96 m)
- Height: 14 ft 1 in (4.29 m) (tail level)
- Wing area: 207 sq ft (19.2 m2)
- Empty weight: 3,040 lb (1,379 kg)
- Gross weight: 4,650 lb (2,109 kg)
- Fuel capacity: 522 litres (115 imp gal; 138 US gal)
- Powerplant: 1 × Lycoming TIGO-541 six cylinder, air-cooled, turbocharged, geared and fuel-injected four stroke aircraft engine, 450 hp (340 kW)
- Propellers: 3-bladed Hartzell Propeller
Performance
- Cruise speed: 200 kn (230 mph, 370 km/h) at 75% power and 25,000 feet
- Stall speed: 54 kn (62 mph, 100 km/h)
- Range: 1,400 nmi (1,600 mi, 2,600 km)
- Service ceiling: 35,000 ft (11,000 m)
- Rate of climb: 1,800 ft/min (9.1 m/s)
- Wing loading: 13.6 lb/sq ft (66.4 kg/m2)
References
edit- ^ a b c d e Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 94. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 99. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ^ a b Saint-Georges, Richard. "L'Aerocruiser Turbo 450 Quelques chiffres" (PDF). aviationnormanddube.com. Retrieved 31 March 2017.
- ^ Transport Canada (14 December 2018). "Canadian Civil Aircraft Register". Retrieved 14 December 2018.
- ^ Niles, Russ. "Terrorism By Homebuilt?". AVweb. Retrieved 5 November 2018.
- ^ Cherry, Paul (4 November 2018). "Pilot's attack on 'spinal column' of Hydro-Québec is unprecedented: lawyer". Montreal Gazette. Retrieved 5 November 2018.
- ^ Drinkwater, Steve (13 November 2018). "Aircraft Designer Normand Dubé Imprisoned". Canadian Owners and Pilots Association. Retrieved 14 November 2018.