Airplane Tundra

Excellent Tundra aircraft for sale

What could be more interesting than fishing and hunting in hard-to-reach, little-studied places? The only problem is how to get into such a wilderness. And this is not always possible even on a good SUV. But to solve such problems, Canadian aircraft designers have developed an amphibious aircraft with unique takeoff and landing characteristics - this is the high-wing "Tundra". Another example of this all-metal aircraft was built by experienced engineers from St. Petersburg in 2016. The aircraft has been adjusted, flown around and brought into full airworthiness, which is confirmed by the corresponding certificate. Airframe and engine operating time - less than 30 hours. Powerplant: injection Aerosport IO-375B1B (tuned Lycoming IO-540D4A5 engine), 260 hp, MOGAS (A-95 gasoline). Average consumption in horizontal flight on a wheeled chassis is about 36 l / h, on a float landing gear - 46 l / h. Tank capacity: 220 liters (110 liter tanks are located in the wings). Propeller: three-blade aluminum Hartzell HC-C3YR-IRF. The high-lying wing of the Tundra is equipped with powerful flaps with a pitch of 10 °, 20, and 40 °, and vortex generators (turbulators) are placed on the top of the leading edge, which reduce the stall speed. Similar generators are installed on the stabilizer for better controllability. Management is possible from both the left and right seats. The current lander configuration is amphibious floats (Montana Floats 2800) with retractable wheel struts. The kit also includes a conventional chassis with a tail wheel. It can also be equipped with a ski chassis. Instrumentation and electrical equipment: speed indicator, altimeter, variometer, gyrocompass, vacuum gauge, magnetic compass, Garmin 695 navigator, intercom, ICOM IC-A210 radio station, AWP, engine parameters monitoring devices, voltmeter, LCD BANO, landing / taxiing headlight. Aircraft empty weight: 760 kg. (wheeled chassis), 930 kg (amphibious floats) Maximum takeoff and landing weight: 1300 kg. Cruising speed: 200 km / h (wheeled chassis), 170 km / h (floats).

Speed ​​limits:

- 258 km / h - wheeled chassis; - 240 - ski chassis; - 220 - option with poplavkov chassis. Takeoff speed with maximum takeoff weight (wheels / skis / floats): - 90/100 / 100. Takeoff run: from the ground - 100, from the snow - 150, from the water - 300. Stall speed in the landing configuration (wheels / skis / floats ): - 50/55/60. Stall speed without wing mechanization (wheels / skis / floats): - 65/70/75. Maximum flight altitude - up to 4000 m. Maximum flight duration at an altitude of 500 m and a speed of V = 180 km / h: - wheeled and ski chassis - 5.5 hours; - float landing gear - 4 hours. Maximum wind speed during takeoff and landing, m / s: - oncoming component: 10; - lateral component: on the left - 5, on the right - 7. The aircraft is stored in hangar conditions at the airfield. All documentation is available. SLG is valid until August 26, 2019.

• State: Used

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