C207
CESSNA 207 Stationair 7
CESSNA 207 Stationair 7
Aircraft
Name
207 Stationair 7
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufactured as
REIMS F207
CESSNA 207 Stationair 8
CESSNA Turbo Stationair 8
CESSNA Turbo Stationair 7
CESSNA Turbo Skywagon 207
CESSNA T207 Turbo Skywagon 207
CESSNA T207 Turbo Stationair 7
CESSNA Stationair 8
CESSNA Stationair 7
CESSNA T207 Turbo Stationair 8
CESSNA 207 Skywagon 207
CESSNA 207 Stationair 7
CESSNA Skywagon 207
C207
Utility light aircraft. In service since 1969. Stretched fuselage version of C206. Known as Stationair 7 from 1978, was replaced by 207A Stationair 8 from 1979. The Turbine 207 uses an Allison 250-C20S turboprop engine which has improved the performance significantly. Note: Has 4 side windows.
Technical Data
Wing span (metric)
10.92 m
Length (metric)
8.62 m
Height (metric)
2.92 m
Powerplant
1 x 300 HP Continental IO-520-F or
Engine Model(s)
Continental O-520
Indicative Performance Data
Take-Off
V2
n/a
Distance
460 m
MTOW
1600 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
161 kts
MACH
n/a
Ceiling
260
Range
690 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
570 m
