Beechcraft 1977 C24R Sierra 200

Staff

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

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Key Takeaways:

The article provides detailed specifications for the 1977 Beechcraft C24R Sierra 200, highlighting its Lycoming IO-360-A1B6 200 hp engine.
Key performance figures include a 75% power cruise speed of 131 knots, a maximum range of 561 nautical miles (at 75% power), and a service ceiling of 14,342 feet.
The aircraft offers a 4-6 seating capacity, a useful load of 1054 lbs, and features a constant speed propeller and retractable tricycle landing gear.
It demonstrates efficient operation with a best rate of climb of 891 fpm, a takeoff ground roll of 1169 feet, and a landing ground roll of 803 feet.

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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.):

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.):

Cabin height (in.):

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):

Best rate of climb (fpm):

891

Service ceiling (ft.):

14,342

Takeoff ground roll (ft.):

1169

Landing ground roll (ft.):

803