Centennial 100
Development and First Flight
The Centennial 100 is a light, multi-purpose aircraft developed by the Canadian company Found Brothers Aviation. This aircraft was designed as an evolution of their existing Found FBA-2 model. Detailed design work for the Centennial 100 modification officially commenced in October 1966, leading to the prototype’s maiden flight on April 7, 1967.
Aircraft Specifications
This impressive six-seater was configured as a cantilever high-wing monoplane. Power was supplied by a robust six-cylinder Lycoming IO-540-G1D5 piston engine, capable of producing 290 hp (216 kW). The engine drove a two-bladed Hatzell metal propeller, ensuring reliable performance across various applications.
Flight Testing and Company Exit
The flight test program for the Centennial 100 was comprehensive, involving three prototypes alongside two production-ready Centennial aircraft. Despite successfully obtaining a type certificate for the aircraft in July 1968, Found Brothers Aviation soon made the strategic decision to exit the aircraft manufacturing business, bringing an end to the Centennial 100’s production.
Technical Specifications
| Modification | Centennial 100 |
| Wingspan, m | 11.89 |
| Length, m | 8.08 |
| Height, m | 2.54 |
| Wing area, m2 | 18.26 |
| Empty weight | 907 |
| Maximum takeoff weight | 1588 |
| Engine type | 1 Piston engine Lycoming IO-540-G1D5 |
| Power, hp | 1 x 290 |
| Maximum speed, km/h | 261 |
| Cruising speed, km/h | 230 |
| Practical range, km | 1100 |
| Rate of climb, m/min | 384 |
| Service ceiling, m | 5500 |
| Crew, crew members | 1 |
| Payload | 5 passengers |
Image gallery of the Centennial 100
