Beechcraft 1961 V35 “N” Bonanza

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

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Key Takeaways:

The article presents detailed specifications for the 1961 Beechcraft V35 "N" Bonanza aircraft.
It is powered by a 260 hp Continental IO-470N engine, features a constant speed propeller, retractable landing gear, and a seating capacity for 4.
The aircraft has a gross weight of 3125 lbs (1270 lbs useful load) and a fuel capacity of 74 gallons.
Key performance includes a cruise speed of 170 knots (at 75% power), a max range of 880 nautical miles (at 65% power), a service ceiling of 19,200 feet, and a best rate of climb of 1150 fpm.

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Beechcraft 1961 V35 “N” Bonanza

Engine make/model:

Cont. IO-470N

Horsepower:

260

TBO:

1500

Propeller:

Const. spd.

Landing Gear type:

Tri./Retr.

Gross weight (lbs.):

3125

Empty weight (lbs.):

1855

Useful load (lbs.):

1270

Fuel (gals.):

74

Wingspan:

33 ft. 6 in.

Overall length:

25 ft. 2 in.

Height:

6 ft. 5 in.

Wing area (sq. ft.):

181

Seating capacity:

4

Cabin width (in.):

42

Cabin height (in.):

50

Baggage capacity (lbs.):

270

PERFORMANCE

Cruise speed (kts.):

75% power:

170

65% power:

162

Max range (w/ reserve) (nm):

75% power:

800

65% power:

880

Fuel consumption (gph):

75% power:

14.0

65% power:

12.1

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

5 hrs.

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

52

Best rate of climb (fpm):

1150

Service ceiling (ft.):

19,200

Takeoff ground roll (ft.):

1050

Landing ground roll (ft.):

650