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Piper PA34-200T Seneca II

1,203 bytes added, 12:57, 4 July 2006
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== General Introduction ==
[[Image:SenecaII_real.jpg|thumb|left|The real Seneca II]]
This is a model of a Piper PA34-200T Seneneca II. The Seneca is made by Piper since the early 1970's and some 4500 were made since then. It has six seats in a pretty large cabin, two turbocharged counterrotating engines producing 200hp up to 12,000 ft. It cruises at 170ktas in 12,000ft at 65% power. Certification for flights into known icing conditions and the nice single engine behaviour made the Seneca a popular multi engine trainer.
The model was built using the Pilots Operating Handbook, a real Seneca (D-GEJL) and some flight performance data derived in real flights.
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== General ==
=== Engines ===
{| width="100%"
|Number of Engines
|2
|-
|Engine Manufacturer
|Continental
|-
|Engine Model Number
|(L)TSIO-360EB
|-
|Rated Horsepower
|Sea Lever: 200, 12,000ft.: 215
|-
|Rated Speed (rpm)
|2575
|-
|Bore (inches)
|4.438
|-
|Stroke (inches)
|3.875
|-
|Displacement (cubic inches)
|360
|-
|Compression Ratio
|7.5:1
|-
|Engine Type
| Six Cylinder, Direct Drive, Horizontally Opposed, Air Cooled
|}
 
=== Propellers ===
{| width="100%"
|Number of Propellers
|2
|-
|Propeller Manufacturer
|Hartzell
|-
|Number of Blades
|2
|-
|Propeller Diameter
| Maximum: 76 inches, Minimum: 75 inches
|-
|Propeller Type
|Constant Speed, Hydraulically Actuated, Full Feathering
|}
 
=== Fuel ===
{| width="100%"
|Fuel Capacity (U.S.gal) (total)
|128
|-
|Usable Fuel (U.S.gal) (total)
|123
|-
|Minumum Grade
|100 Green or 100LL Blue Aviation Grade
|-
|}
 
=== Oil ===
{| width="100%"
|Oil Capacity (U.S.quarts) (per engine)
|8
|}
=== Maximum Weights ===
{| width="100%"
|Maximum Takeoff Weight (lbs)
|4570
|-
|Maximum Landing Weight (lbs)
|4362
|-
|Maximum Zero Fuel Weight (lbs) - Standard
|4000
|-
|Maximum Weight in Baggage Compartment (lbs)
|Forward: 100, Aft: 100
|}
== Development status/Issues/Todo ==

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