Fleet 80 Canuck
The beginnings of the Fleet Model 80 Canuck go back to 1939, when J. Omer (Bob) Noury, an air engineer with the Ottawa Flying Club, decided to design and build a light aircraft for the Canadian market. The aircraft was a high-wing monoplane of conventional structure using a welded steel-tube fuselage and tail surfaces, and powered with a 65-horsepower Continental flat four-cylinder engine. The Noury T-65 Series 1 design was first flown on January 21, 1940. The aircraft was given a certificate of airworthiness and Noury sold it in 1941.
In 1942 he formed Noury Aircraft Ltd. at Stoney Creek, with himself as president and general manager. His intent was to design and build a light aircraft based on his own monoplane design. The Noury N-75 featured side-by-side seating and a 75-horsepower Continental engine. It was test flown from the Hamilton Airport at Mount Hope late in 1944.
Fleet Aircraft felt that the side-by-side design aircraft met most of their specifications, so in May 1945 they purchased the prototype and design rights for the plane from Noury Aircraft.
The Noury was shipped to Fleet's facilities at Fort Erie and test flown by Fleet's test pilot, Tommy Williams, on June 4, 1945. This resulted in modifications to the forward fuselage geometry, lowering the engine four inches to improve the forward visibility, and moving the engine forward four inches to allow the relocation of the fuel tank from the centre section of the wing to the forward fuselage. This made possible the installation of a clear skylight in the cabin roof. The original Continental C-75 engine was replaced by a more powerful Model C-85, and a new fin and rudder were installed. The Canuck was first flown in its modified form on September 26, 1945.
The side-by-side seating in the Fleet 80 Canuck was unusual for the period even though it was a far better arrangement for instruction than placing the instructor either in front of or behind the student.
Between 1945 and 1948, 198 Canuck aircraft were built by Fleet. The Canuck proved popular and initially sold well to flying clubs, charter companies, and private owners in Canada. In addition 24 were exported. By late 1947, plagued by postwar financial difficulties and the sales slowdown that affected all aircraft manufacturers, Fleet was forced to terminate production of the Canuck model.
The Museum's Canuck was flown in Alberta for about 20 years before joining the Musum in 2003.
Progress Report, May 2012
Progress Report, March 2012
Things are moving along a good pace over at Ray's place. More photos will be posted as they come.
Big thanks to Ray and his team for an awesome job
The Canuck fuselage is finally home in the CMF hangar!
April, 2012 - Masking removed, paint scheme takes shape!
April, 2012 - masking removed
April, 2012 - Blue coat goes on
April, 2012 - Front cowl and gear installed to setup the masking for the pattern
April, 2012 - White coat goes on
first coat complete ~ March 15, 2012
Ray starts the first coat of silver ~ March 15, 2012
tail all tied together nicely ~ March 15, 2012
Masking/taping just about done and ready for spray coats ~ March 13, 2012
Bill (rear) and Ray (front) turn the Canuck fuselage
Progress Report, Feb 2012
Ralph, Terry, Ray and Bill ~ Ray cutting the first length of fabric
A look inside at the Canuck's flight controls
Progress Report, July 2011
Progress Report, April 2011
The wings have been trial fitted to ensure the alignment of all components. If you are wondering why you can see through the Canuck's skeleton, it is because of the typical construction methods of the 1940s. The fuselage is steel tube with wooden battens used for shaping, the whole lot then being covered with cotton. These days we use a modern, long-lasting synthetic fabric covering. The wings are aluminum alloy structure also covered with fabric. Many coats of special finish are applied to make the covering aerodynamically smooth and long lasting.
Progress Report, March 2011
The final work on the wings is under way.
Progress Report, July 2010
Progress Report, May 2010
Progress Report, October 2009
Progress Report, November 2008