PA-34-200 Seneca - Two 150kW (200hp) Lycoming IO-360-A1A fuel injected flat fours driving two blade c/s props. PA-34-220T Seneca V - Two 165kW (220hp) Teledyne Continental L/TSIO-360-RB turbocharged, intercooled fuel injected counter rotating flat sixes driving two blade Hartzell or optional three blade McCauley c/s prop.
PA-34-200 Seneca - Max speed 314km/h (170kt), max cruising speed 300km/h (160kt), long range cruising speed 267km/h (144kt). Initial rate of climb 1360ft/min. Service ceiling 19,400ft. Max range with no reserves 1818km (982nm). PA-34-220T Seneca V - Max speed 379km/h (205kt), max cruising speed at 10,000ft 341km/h (184kt), at 18,500ft 367km/h (198kt), normal cruising speed at 10,000ft 322km/h (174kt), at 16,500ft 352km/h (190kt). Initial rate of climb 1550ft/min. Max certificated altitude 25,000ft. Range at max range power with reserves at 10,000ft 1295km (700nm), at 18,500ft 1222km (660nm).
PA-34-200 Seneca - Empty 1190kg (2623lb), max takeoff 1905kg (4200lb). PA-34-220T Seneca V - Empty equipped 1532kg (3377lb), max takeoff 2155kg (4750lb).
PA-34-200 Seneca - Wing span 11.85m (38ft 11in), length 8.69m (28ft 6in), height 3.02m (9ft 11in). Wing area 19.2m2 (206.5sq ft). PA-34-220T Seneca V - Same except length 8.72m (28ft 8in). Wing area 19.4m2 (208.7sq ft).
Seating for six in all but Seneca V which seats five or optionally six.
Approximately 4750 Senecas built by Piper (incl approx 200 Vs), plus approx 20 Seneca IIs licence built in Poland by PZL-Mielec as the M-20 Mewa, and over 870 in Brazil by Embraer as the EMB-810. |
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