Cirrus 1999 SR20

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

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Key Takeaways:

The Cirrus 1999 SR20 is a 4-seat aircraft powered by a 200 HP Lycoming IO-360-ES engine with a 2000-hour TBO and fixed tricycle landing gear.
It features a useful load of 1025 lbs, a gross weight of 2900 lbs, and a fuel capacity of 60 gallons.
Key performance indicators include a cruise speed of up to 160 knots, a maximum range of 801 nautical miles, and a service ceiling of 16,000 feet.
The aircraft has a best rate of climb of 961 fpm, a stall speed of 57 knots, and requires 1310 ft for takeoff ground roll.

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Cirrus 1999 SR20

Engine make/model:

Lyc. IO-360-ES

Horsepower:

200

TBO hrs.:

2000

Propeller:

Const. spd.

Landing gear type:

Tri/Fixed

Gross weight (lbs.):

2900

Empty weight, std. (lbs.):

1875

Useful load, std. (lbs.):

1025

Fuel (gals.):

60

Wingspan:

35 ft. 7 in.

Overall length:

28 ft. 3 in.

Height:

9 ft. 3 in.

Wing area (sq. ft.):

135

Seating capacity:

4

Cabin width (in.):

49

Cabin height (in.):

50

Baggage capacity (lbs.):

120

PERFORMANCE

Cruise speed (kts.):

75% power:

160

65% power:

155

Max range (w/ reserve) (nm):

75% power:

686

65% power:

801

Fuel consumption (gph):

75% power:

10.4

65% power:

9.4

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

5 hrs. 30 mins.

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

57

Best rate of climb (fpm):

961

Service ceiling (ft.):

16,000

Takeoff ground roll (ft.):

1310

Landing ground roll (ft.):

1000