*****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