Aircraft › Piper › Piper PA-34 Seneca › Piper PA-34 Seneca I to V

Piper PA-34 Seneca I to V

This page covers every mark of the PA-34: the Seneca (PA-34-200) with two fuel-injected 200 hp Lycoming IO-360 engines, the turbocharged Seneca II (PA-34-200T), and the Seneca III, IV and V, all PA-34-220T with Continental engines of 220 hp for takeoff. The figures are the Seneca V's: span 11.86 m, length 8.72 m and height 3.02 m from the EASA data sheet, a maximum weight of 4,750 pounds, 122 US gallons of fuel usable and a maximum operating altitude of 25,000 feet. The first three marks seat up to seven; the Seneca IV and V seat six. The ICAO code is PA34.

Seats
About 6
Engines
Two piston engines on the wings: Continental TSIO-360-RB and LTSIO-360-RB (Seneca V); TSIO-360-KB and LTSIO-360-KB (Seneca III and IV)
Max takeoff weight
4,800 lb (2,155 kg)
Piper PA-34 Seneca I to V seen from above: length 28 ft 7 in (8.72 m), wingspan 38 ft 11 in (11.86 m)
Drawing: cwsi.net, from published dimensions (a schematic, not to exact detail)

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Specifications

Length28 ft 7 in (8.72 m)
Wingspan38 ft 11 in (11.86 m)
Height9 ft 11 in (3.02 m)
Fuselage width3 ft 11 in (1.20 m)
Ceiling25,000 ft (7,600 m)
Fuel capacity120 US gal (462 L)
StatusIn service
Type codesICAO PA34

Private aircraft show specs only. No flight data is shown for them.

Sources

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