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| The Piper Seneca evolved out an attempt to build a 3 engined Cherokee Six. It first flew as a two engine development in 1966 with 180 hp, but later on had 2' added to the wings, a large tail and more powerful engines. First sold in 1971, the Piper Seneca Max Takeoff Weight was increased by 200lbs in 1973. |
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|
| Seating (normal) |
6 |
Max Takeoff (lbs) |
4,200 |
| Seating (maximum) |
7 |
Certified Ceiling (ft) |
20,000 |
|
| Engines |
Lycoming L/IO 360A1A |
To (Sealevel, ISA Temp) (ft) |
1,420 |
| Output lbs ea. Flat Rating |
200 hp |
Landing Distance (ft) |
1,335 |
| Maximum Mach No. |
- |
Max Range (fuel) (nm) |
939 |
| High Speed Cruise (Kts) |
163 |
Max Range (payload) (nm) |
754 |
|
| Flight Time 300nm |
- |
Flight Time 1000nm |
- |
| Flight Time 600nm |
- |
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| External |
|
Internal |
|
| Length (ft) |
28.50 |
Length (ft) |
- |
| Height (ft) |
9.90 |
Height (ft) |
- |
| Span (ft) |
38.90 |
Width: Max floor (ft) |
- |
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