Beechcraft 1977 C24R Sierra 200

Thursday, November 01, 2007 at 12:00 AM ET

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Key Takeaways:

The article details the specifications for the 1977 Beechcraft C24R Sierra 200, equipped with a 200-horsepower Lycoming IO-360-A1B6 engine.
This aircraft offers a seating capacity for 4-6 individuals, with a gross weight of 2750 lbs and a useful load of 1054 lbs.
Key performance figures include a cruise speed of 131 knots at 75% power, a maximum range of 561 nautical miles, and fuel consumption of 10.5 gallons per hour.
Operational capabilities include a best rate of climb of 891 feet per minute, a service ceiling of 14,342 feet, and short takeoff and landing ground rolls of 1169 ft and 803 ft respectively.

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Beechcraft 1977 C24R Sierra 200

Engine make/model:

Lyc. IO-360-A1B6

Horsepower:

200

TBO:

2000

Propeller:

Const. spd.

Landing Gear type:

Tri./Retr.

Gross weight (lbs.):

2750

Empty weight (lbs.):

1696

Useful load (lbs.):

1054

Fuel (gals.):

52

Wingspan:

32 ft. 9 in.

Overall length:

25 ft. 9 in.

Height:

8 ft. 5 in.

Wing area (sq. ft.):

146

Seating capacity:

4-6

Cabin width (in.):

44

Cabin height (in.):

49

Baggage capacity (lbs.):

270

PERFORMANCE

Cruise speed (kts.):

75% power:

131

65% power:

125

Max range (w/ reserve) (nm):

75% power:

561

65% power:

125

Fuel consumption (gph):

75% power:

10.5

65% power:

9.1

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

5 hrs. 18 mins.

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

60

Best rate of climb (fpm):

891

Service ceiling (ft.):

14,342

Takeoff ground roll (ft.):

1169

Landing ground roll (ft.):

803