*****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