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For 1972 Piper introduced the six/seven-seat Piper PA-34 Seneca which, basically, was a twin-engine version of the Cherokee SIX with retractable tricycle landing gear, a new fuselage structure and power provided by two 149kW Avco Lycoming IO-360 flat-four engines. For 1975 149kW Continental TSIO-360-E turbocharged and counter-rotating engines were introduced and the landing gear was streng-, thened for operation at higher gross weight, the designation then changing to PA-34-200T Seneca II. In 1982 the Seneca II was superseded by an improved PA-34-220T Seneca III, and this remains the current production version in 1984. It differs from its immediate predecessor by having more powerful Continental TSIO-360-KB turbocharged and counter-rotating flat-six piston engines. During 1976-77 Piper signed an agreement with the Polish foreign trade association Pezetel under which P.Z.L. Mielec will assemble/manufacture the Seneca for sale in eastern Europe. Designated in Poland as the P.Z.L. Mielec M-20 Mewa (gull), the first Polish-built prototype was flown on 25 July 1979. Current production version is the M-20 03 one of the very few light-twins on the market. A total of 4,464 Seneca were delivered by 1 January 1991.
| MODEL | Piper PA-34-220T Seneca III |
| ENGINE | 2 x Continental TSIO-360-KB, 164kW |
| WEIGHTS |
| Take-off weight | 2155 kg | 4751 lb |
| Empty weight | 1294 kg | 2853 lb |
| DIMENSIONS |
| Wingspan | 11.86 m | 38 ft 11 in |
| Length | 8.72 m | 28 ft 7 in |
| Height | 3.02 m | 9 ft 11 in |
| PERFORMANCE |
| Max. speed | 364 km/h | 226 mph |
| Ceiling | 7620 m | 25000 ft |
| Range | 1667 km | 1036 miles |
John Ellul, jdellul2(@)bigpond.com, 02.01.2007 The Seneca 1 was certfied with the aileron and rudder controls interconected for stability requirements. I fly an old Seneca 1 and wish to know how I can tell if the system is working. When I taxi the aircraft the control wheel does not move when I push the rudder pedal. Any help would be appreciated
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Do you have any comments concerning this aircraft ?
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