|
|
 |
| The most successful six place light twin since its introduction, the Seneca is a twin engine development of the Cherokee Six fitted with two fuel injected 150kW (200hp) IO-360s. Production deliveries of the initial PA-34-200 Seneca began in late 1971. Handling and performance criticisms were addressed from the 1974 model year with the PA-34-200T Seneca II which introduced changes to the flight controls and, more importantly, two turbocharged Continental TSIO-360-Es. With the PA-34-220T Seneca III Piper introduced in 1981 the counter rotating 165kW (220hp) TSIO-360s and a revised interior and instrument panel. New Piper's improved PA-34-220T Seneca IV was introduced in 1994 with aerodynamic refinements, axisymetric engine inlets and a revised interior. The latest PA-34-220T Seneca V was introduced in January 1997. It features intercooled turbocharged L/TSIO-360-RB engines which maintain rated power to 19,500ft, and seating for five, with an optional entertainment/executive workstation with extendable worktable. |
 |
|
|
|
| Seating (normal) |
5 |
Max Takeoff (lbs) |
4,750 |
| Seating (maximum) |
6 |
Certified Ceiling (ft) |
25,000 |
|
| Engines |
2 Continental L/TSIO-360-RB |
To (Sealevel, ISA Temp) (ft) |
1,210 |
| Output lbs ea. Flat Rating |
220 shp |
Landing Distance (ft) |
1,978 |
| Maximum Mach No. |
- |
Max Range (fuel) (nm) |
700 |
| High Speed Cruise (Kts) |
205 |
Max Range (payload) (nm) |
- |
|
| Flight Time 300nm |
1 + 42 |
Flight Time 1000nm |
- |
| Flight Time 600nm |
3 + 16 |
|
|
|
| External |
|
Internal |
|
| Length (ft) |
28.50 |
Length (ft) |
10.30 |
| Height (ft) |
9.90 |
Height (ft) |
3.90 |
| Span (ft) |
38.90 |
Width: Max floor (ft) |
4.10 |
|
|
|
