*****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