*****AIRCRAFT “Cessna - C206”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: High wing (wing struts)

Engine position: Nose mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle fixed

Wing Span: 10.9 m

Length: 8.6 m

Height: 3.0 m

Power plant: 206: 1 x 260 HP Continental IO-470-S piston engine

with 2 blade propeller.

T206: 1 x 285 HP Continental TSIO-520-C turbocharged piston engine

with 3 blade propeller.

Accommodation: One pilot and 5 passengers.

Notes: Utility light aircraft. In service since 1964 (Turbo 206 since 1998).

Replacement for the CESSNA 205 (ICAO Designator: C205). Primary model Super

Skywagon was replaced by more powerful turbocharged Skywagon in 1969 and by

T206 Stationair in 1971. Production ceased in 1984. CESSNA re-introduced the

Turbo 206 Stationair mid 1997. The SOLOY Turbine 206 uses an Allison 250-C20S

turboprop engine which gives a much better performance. Note: Has 3 side windows.

Alternative names:
AVIONES COLOMBIA 206, CESSNA (Turbo)Skywagon 206, CESSNA, (Turbo)Stationair, (Turbo)Stationair 6, CESSNA (Turbo)Super Skylane, CESSNA (Turbo)Super Skywagon, CESSNA 206,P206,T206,TP206,U206,TU206, P206, Skywagon 206,
Stationair, Stationair 6, Super Skylane, Super Skywagon, T206, TP206, TU206
Turbo Skywagon 206, Turbo Stationair, Turbo Stationair 6, Turbo Super Skylane
Turbo Super Skywagon, U206, CESSNA 206

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 1.650 kg

VMO - Maximum Operating Speed 140 KIAS

MMO - Maximum Operating Speed Mach  nd Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees KIAS

1                      000

2                      000

5                      000

10                    000

15                    000

25                    000

30                    000

40                    000

 

*****Take-off*****

WTC:               L

Distance:         250 mt

V2 (IAS):         75 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 105 kt

ROC:               800 ft/min

-(to FL150)

IAS:                 110 kt

ROC:               500 ft/min

-(to FL240)

IAS:                 130 kt

ROC:               500 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                140 kt

MACh:             nd data

Ceiling:            FL170

Range: 560 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 140 kt

ROD:               500 ft/min

 

*****Approach*****

IAS:                 120 kt

MCS:               nd kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        70 kt

APC:                A

Distance:         450 mt