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C207

From SKYbrary Wiki
Aircraft
Name 207 Stationair 7
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
APC A
Type code L1P
Engine Piston
Engine count Single
Mass group 1


Manufacturered as:

CESSNA Skywagon 207
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 207 Stationair 8
REIMS F207


CESSNA 207 Stationair 7

CESSNA 207 Stationair 7

Description

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 10.92 m35.827 ft
Length 8.62 m28.281 ft
Height 2.92 m9.58 ft
Powerplant 1 x 300 HP Continental IO-520-F or

1 x 310 HP Continental TSIO-520-M turbocharged piston engine with 3 blade propeller.

Engine model Continental O-520

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 161 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 460 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 570 m
MTOW 16001,600 kg
1.6 tonnes
kg
Ceiling FL260 ROD ft/min APC A
WTC L Range 690690 nm
1,277,880 m
1,277.88 km
4,192,519.688 ft
NM

Accidents & Serious Incidents involving C207

None on SKYbrary