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, powered by a 300-horsepower Lycoming IO-540-AC1A engine.
This 6-seat aircraft has a useful load of 1404 lbs, making it capable of carrying significant passengers or cargo, further enhanced by its relatively short takeoff (910 ft) and landing (735 ft) capabilities.
Performance highlights include cruise speeds of 134-142 knots, a maximum range of 660 nautical miles, and a service ceiling of 15,700 feet.

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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