The automatic flight control system (AFCS) in the aircraft ensures the safety of personnel on board by improving handling quality. Further avionics suites include the GFC 700 autopilot system, digital audio panels, Garmin FliteCharts, transponders, electronic flight displays (EFD), air data computers and yaw dampening systems. High resolution screens provide environmental data, engine data, traffic, maps and graphics to increase the situational awareness of the crew. 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.

Piper seneca crossfeed drains