Cessna TP206 Turbo Super Skylane
The Cessna TP206A-E is a single-engine aircraft configured as a cantilever high-wing aircraft with a conventional tail. It features fixed gear, constant-speed propeller and has six seats.
The six-seat Model TP206 was built from 1966 through 1970, serial numbers 161 through 647, with a total production of 486.
Specifications
Exterior Dimensions
Wing span: 36 ft 7 in
Length: 28 ft 7 in
Height: 9 ft 7 in
Weights
Gross Weight: 3,600 lbs
Empty Weight: 1,915 lbs
Maximum Payload: 1,400 lbs
Fuel capacity: 65 gal (63 gallons useable) Long Range 84 gal (82 useable)
Engine
Manufacturer: Cont Motor
Model: TSIO-520-C
Horsepower: 285 HP
Overhaul (HT): 1400 hrs TBO
Years before overhaul: 12
Performance Specifications
| Horsepower: 285.00 | Gross Weight: 3,600 |
| Top Speed: 174 | Empty Weight: 1,915 |
| Cruise Speed: 160 | Fuel Capacity: 65 |
| Stall Speed (dirty): 53 | Range: 609 |
| Rate of Climb: 1,030 | Rate of Climb (One Engine): |
| Service Ceiling: 26,300 | Ceiling (One Engine): |
| Takeoff | Landing |
| Ground Roll: 910 | Ground Roll 735 |
| Takeoff Roll Over 50 ft: 1,810 | Landing Roll Over 50 ft: 1,395 |
History
The P206 was added to the line in 1965. In this case the “P” stood for “passenger”, as the P206 had passenger doors similar to the Cessna 210 from which it was derived, on both sides. The P206 had the same door arrangement as the 205, but with the bigger engine from the 206.
The P206 was produced from 1965 to 1970 and was powered by a Continental IO-520-A of 285 hp (213 kW). There was a turbocharged model designated TP206 which was powered by a Continental TSIO-520-A also of 285 hp.
Design and development
Turbocharging became available on both variants in 1966, with a 285-HP Continental TSIO- 520C.
Variants
Cessna TP206A
Six seats, powered by a turbocharged Continental TSIO-520-C of 285 hp (213 kW), with a gross weight of 3,600 lb (1,633 kg) landplane, 3,600 lb (1,633 kg) seaplane, 3,300 lb (1,497 kg) skiplane and certified on 20 December 1965.Cessna P206A
Cessna TP206B
Six seats, powered by a turbocharged Continental TSIO-520-C of 285 hp (213 kW), with a gross weight of 3,600 lb (1,633 kg) landplane, 3,300 lb (1,497 kg) skiplane and certified on 3 August 1966.
Cessna TP206C
Six seats, powered by a turbocharged Continental TSIO-520-C of 285 hp (213 kW), with a gross weight of 3,600 lb (1,633 kg) landplane, 3,300 lb (1,497 kg) skiplane and certified on 20 July 1967.
Cessna TP206D
Six seats, powered by a turbocharged Continental TSIO-520-C of 285 hp (213 kW), with a gross weight of 3,600 lb (1,633 kg) landplane, 3,300 lb (1,497 kg) skiplane and certified on 18 September 1968.
Cessna TP206E
Six seats, powered by a turbocharged Continental TSIO-520-C of 285 hp (213 kW), with a gross weight of 3,600 lb (1,633 kg) landplane, 3,300 lb (1,497 kg) skiplane and certified on 28 July 1969.
