Piper PA-34 Seneca V Cockpit and Avionics The Piper PA-34 Seneca V cockpit is equipped with the Garmin G1000 avionics device which integrates a sophisticated communication and navigation system. The service ceiling of the aircraft is 7,620 m, while the climbing rate is 1,455 ft / min. The aircraft requires a take-off distance of 520 m and a landing distance of 664 m. This aircraft can fly with a maximum speed of 370 km / h and a maximum range of 1,534 km with a 45-minute reserve. Each engine produces a maximum power of 220 hp to drive the three-bladed McCauley Propeller propeller at constant speed. Piper PA-34 Seneca V Engine and Performance The Piper PA-34 Seneca V aircraft is powered by two Continental TSIO-360-RB engines equipped with an intercooler. The aircraft can carry a maximum of 604 kg of standard useful load, while the fuel tank is designed to carry 462 l of usable fuel. The maximum takeoff weight and weight that are equipped with aircraft standards are 2,155 kg and 1,561 kg, respectively.
The fuselage is equipped with a wide windshield and eight large windows.ĭimensions of the Piper PA-34 Seneca V include a length of 8.7 m, a height of 3 m, and a wing span of 11.9 m. Piper PA-34 Seneca V Specs The Piper PA-34 Seneca V airframe has a low wing configuration design, which allows for more lift and significant drag reduction.
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