Beech K35 Bonanza
The Beech K35 Bonanza was manufactured in 1959, serial numbers D5726 through D6161. A total of 436 Model K35 were manufactured.
It is a single-engine, piston aircraft configured as a cantilever low-wing aircraft with a V-tail. Distinguishing features are: retractable landing gear, hydraulic (engine oil) adjusted propeller. Model K35 Bonanza seats up to 4 passengers and 1 pilot.
Specifications
Exterior Dimensions
Wing span: 32 ft 10 in
Length: 25 ft 2 in
Height: 7 ft 7 in
Interior Dimensions
Cabin width: 42 in
Cabin height: 50 in
Baggage capacity: 180 lbs
Weights
Max TO weight: 2,950 lb
Empty Weight: 1,832 lbs
Maximum Payload: 1,118
Fuel capacity: 50 U.S. gallons (44 usable)
Engine
Manufacturer: Continental Motors
Model: IO-470C
Horsepower: 250 hp
Overhaul (HT): 1500hr TBO or 12 years
Standard Avionics
Digital Nav/Coms
ADS-B In/Out
Performance
| Horsepower: 250.00 | Gross Weight: 2,950 |
| Top Speed: 183 | Empty Weight: 1,832 |
| Cruise Speed: 170 | Fuel Capacity: 49 |
| Stall Speed (dirty): 52 | Range: 495 |
| Rate of Climb: 1,170 | Rate of Climb (One Engine): |
| Service Ceiling: 20,000 | Ceiling (One Engine): |
| Takeoff | Landing |
| Ground Roll: 950 | Ground Roll 710 |
| Takeoff Roll Over 50 ft: 1,185 | Landing Roll Over 50 ft: 1,050 |
History
J35 with Continental IO-470C 250 hp, fuel load increase, optional fifth seat and increased takeoff weight. The Model K35 Bonanza was first to have fuel capacity and optional fifth seat in aft cabin. A total of 436 Model K35 were manufactured in the 1959 sales year. K35 cost $25,300.
Distinguishing Features and Equipment
The 1959 Beech K35 featured a V-tail design, giving the plane a distinctive appearance. The V-tail design reduced the number of flying surfaces from three to two, as compared to a standard, straight-tail plane. It was thought this design would also reduce drag, weight and production costs. The engine is fuel injected. The plane featured two small rear windows, long-chord stabilators and a single, throw-over yoke control. The plane sported optional in-wing auxiliary tanks (20 gal. total), an electric auxiliary fuel pump, and vernier engine controls. It featured a separate fuel gauge for auxiliary tanks. The gear handle was positioned on the right-side of the cockpit and the flap control was on the left. The K35 used “sight and touch” gear and flap control technology. It also sported stowable copilot rudder pedals when no copilot brakes are installed and individually adjustable rear seat backs.
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