Cessna 1981 207 Stationair

Saturday, December 01, 2007 at 12:00 AM ET

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Key Takeaways:

The article describes the specifications for a 1981 Cessna 207 Stationair, an 8-seat aircraft.
It is powered by a 300 horsepower Continental TSIO-520H engine with a TBO of 1700 hours.
The aircraft has a useful load of 1628 lbs and can carry 73 gallons of fuel.
Performance highlights include a cruise speed of up to 143 knots (75% power), a maximum range of 560 nautical miles (65% power), and a service ceiling of 13,300 feet.

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Cessna 1981 207 Stationair

Engine make/model:

Cont. TSIO-520H

Horsepower:

300

TBO hrs.:

1700

Propeller type:

Const. spd.

Landing gear type:

Tri/Fixed

Gross weight (lbs.):

3800

Empty weight, std. (lbs.):

2172

Useful load, std. (lbs.):

1628

Fuel (gals.):

73

Wingspan:

35 ft. 10 in.

Overall length:

32 ft. 2 in.

Height:

9 ft. 7 in.

Wing area (sq. ft.):

174

Seating capacity:

8

Cabin width (in.):

44.5

Cabin height (in.):

49

Baggage capacity (lbs.):

300

PERFORMANCE

Cruise speed (kts.):

75% power:

143

65% power:

138

Max range (w/ reserve) (nm):

75% power:

525

65% power:

560

Fuel consumption (gph):

75% power:

15.8

65% power:

13.7

Estimated endurance (65% power with 1-hr. reserve) (hrs):

4.5

Stall speed (gear, flaps down) (knots):

58

Best rate of climb (fpm):

810

Service ceiling (ft.):

13,300

Takeoff ground roll (ft.):

1100

Landing ground roll (ft.):

765