The Taylor C-2 was a light utility aircraft made by the Taylor Aircraft Company in the late 1920s.
| C-2 | |
|---|---|
| Role | light utility |
| Manufacturer | Taylor Aircraft Company |
| Designer | C. Gilbert Taylor |
| First flight | 1929 |
| Number built | 7 |
Design edit
The C-2 design featured a two-seat, parasol monoplane. The pilot and passenger sat in the cabin side by side. One of the seven C-2s built had a wing modified with a seven-degree, variable-incidence wing for entry into the Guggenheim Safe Airplane Competition.[1]
Specifications (C-2) edit
General characteristics
- Crew: 1
- Capacity: one passenger
- Length: 22 ft 6 in (6.86 m)
- Wingspan: 34 ft (10 m)
- Powerplant: 1 × Kinner K-5 5-cylinder air-cooled radial piston engine, 90 hp (67 kW)
- Propellers: 2-bladed fixed-pitch propeller
Performance
References edit
- ^ a b "Taylor, Taylorcraft".
- ^ Eckland, K.O. "Taylor, Taylorcraft". aerofiles.net. Retrieved 8 April 2020.