*****AIRCRAFT “Cessna - C206 Turbine”*****

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: 10.97 m

Length: 8.61 m

Height: 2.83 m

Power plant: 1 x 420 SHP Allison 250-C20S turboprop engine with

3 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 1972. Turboprop engine powered convertion of CESSNA 206 with much better performance based on CESSNA 206 Stationair 6 airframe.
Alternative names:
CESSNA 206 (turbine), SOLOY Turbine 206, Turbine 206

 

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

000,000 lbs - 1.632 kg

VMO - Maximum Operating Speed 150 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:         300 mt

V2 (IAS):         75 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 105 kt

ROC:               800 ft/min

-(to FL150)

IAS:                 110 kt

ROC:               700 ft/min

-(to FL240)

IAS:                 nd kt

ROC:               nd ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                150 kt

MACh:             nd data

Ceiling:            FL200

Range:             630 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 140 kt

ROD:               500 ft/min

 

*****Approach*****

IAS:                 110 kt

MCS:               75 kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        70 kt

APC:                A

Distance:         330 mt