*****AIRCRAFT
“Cessna - C207 Skywagon”*****
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: 9.8 m
Height: 2.9 m
Power plant: 1 x 300 HP
Continental IO-520-F or 1 x 310 HP Continental TSIO-520-M turbocharged piston
engine with 3 blade propeller.
Accommodation: One pilot and 6 to 7 passengers.
Notes: Utility light aircraft.
In service since 1969. Stretched fuselage version of C206
(ICAO
designator: C206). Known as Stationair 7 from 1978,
was replaced by 207A
Stationair 8 from 1979. The SOLOY Turbine 207 uses an Allison
250-C20S turboprop
engine which has improved the performance
significantly.
Note: Has 4
side windows.
Alternative names:
207 (Turbo)Stationair 7/8, CESSNA 207
(Turbo)Skywagon 207, CESSNA 207 (Turbo)Stationair 7/8,
Skywagon 207, Stationair 7/8, Turbo Skywagon 207, Turbo Stationair 7/8, CESSNA 207
Skywagon
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 1.720 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: 350
mt
V2 (IAS): 75
kts
*****Climbing*****
-(to 5000 ft)
IAS: 105
kt
ROC: 500
ft/min
-(to FL150)
IAS: 120
kt
ROC: 500
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: 500 NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 150
kt
ROD: 500
ft/min
*****Approach*****
IAS: 150
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 75 kt
APC: A
Distance: 250
mt