Cessna 1999 206 Stationair

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

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Key Takeaways:

The article provides detailed specifications for the 1999 Cessna 206 Stationair, a 6-seater aircraft powered by a 300 HP Lycoming IO-540-AC1A engine.
It has a useful load of 1404 lbs and a fuel capacity of 88 gallons, supporting a maximum range of 600 nautical miles at 75% power.
Key performance figures include a 142-knot cruise speed (75% power), a 15,700 ft service ceiling, and impressive short-field capabilities with takeoff and landing ground rolls of 910 ft and 735 ft, respectively.

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stationair

Cessna 1999 206 Stationair

Engine make/model:

Lyc. IO-540-AC1A

Horsepower:

300

TBO hrs.:

2000

Propeller:

Const. spd.

Landing gear type:

Tri/Fixed

Gross weight (lbs.):

3600

Empty weight, std. (lbs.):

2146

Useful load, std. (lbs.):

1404

Fuel (gals.):

88

Wingspan:

35 ft.

Overall length:

28 ft. 3 in.

Height:

9 ft. 4 in.

Wing area (sq. ft.):

174

Seating capacity:

6

Cabin width (in.):

44

Cabin height (in.):

49

Baggage capacity (lbs.):

180

PERFORMANCE

Cruise speed (kts.):

75% power:

142

65% power:

134

Max range (w/ reserve) (nm):

75% power:

600

65% power:

660

Fuel consumption (gph):

75% power:

16.5

65% power:

14.3

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

5 hrs.

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

54

Best rate of climb (fpm):

988

Service ceiling (ft.):

15,700

Takeoff ground roll (ft.):

910

Landing ground roll (ft.):

735