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.

 

 

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