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Piper PA34-200T Seneca II

2,610 bytes added, 13:43, 4 July 2006
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=== Propellers ===
{| width="100%"
| width="50%" |Number of Propellers| width="50%" |2
|-
|Propeller Manufacturer
=== Fuel ===
{| width="100%"
| width="50%" |Fuel Capacity (U.S.gal) (total)| width="50%" |128
|-
|Usable Fuel (U.S.gal) (total)
=== Oil ===
{| width="100%"
| width="50%" |Oil Capacity (U.S.quarts) (per engine)| width="50%" |8
|}
=== Maximum Weights ===
{| width="100%"
| width="50%" |Maximum Takeoff Weight (lbs)| width="50%" |4570
|-
|Maximum Landing Weight (lbs)
|Forward: 100, Aft: 100
|}
 
=== Standard Airplane Weights ===
{| width="100%"
| width="50%" | Standard Empty Weight (lbs): Weight of a standard airplane including unusable fuel, full operating fluids and full oil.
| width="50%" | 2823
|-
| Maximum Useful Load (lbs): The difference between the Maximum Takeoff Weight and the Standard Empty Weight. (All weight in excess off 4000lbs must consist of fuel)
|1747
|}
 
=== Specific Loadings ===
{| width="100%"
| width="50%" | Wing Loading (lbs per sq ft)
| width="50%" | 22
|-
| Power Loading (lbs per hp)
| Sea Level: 11.4 - 12,000ft: 10.6
|}
 
== Limitations ==
=== Airspeed Limitations ===
{| width="100%"
| width="50%" | Speed
| width="25%" | KIAS
| width="25%" | KCAS
|-
| Never Exceed Speed (V<sub>NE</sub>) - Do not exceed this speed in any operation
| 195
| 195
|-
| Maximum Structural Cruising Speed (V<sub>NO</sub>) - Do not exceed this speed except in smooth air and then only with caution.
| 163
| 165
|-
| Design Maneuvering Speed (V<sub>A</sub>) - Do not make full or abrupt control movements above this speed.
| &nbsp;
| &nbsp;
|-
| align="center"| At 4570 LBS G.W.
| 136
| 138
|-
| align="center"|At 3068 LBS G.W.
| 121
| 122
|-
| colspan="3" align="center" |
<b>CAUTION</b>
 
Maneuvering speed decreases at lighter weight as the effects of aerodynamic forces become more pronounced. Linear interpolation may be used for imtermediate gross weights. maneuvering speed should not be exceeded while operating in rough air.
|-
| Maximum Flaps Extended Speed (V<sub>FE</sub>) - Do not exceed this speed with flaps extended.
| 107
| 109
|-
| Maximum Gear Extended Speed (V<sub>LE</sub>) - Do not exceed this speed with landing gear extended
| 129
| 130
|-
| Maximum Landing Gear Extending Speed (V<sub>LO</sub>) - Do not extend landing gear above this speed
| 129
| 130
|-
| Maximum Landing Gear Retracting Speed (V<sub>LO</sub>) - Do not retract landing gear above this speed
| 107
| 109
|-
| Air Minimum Control Speed (V<sub>MC</sub>) - Lowes airspeed at which airplane is controllable with one engine operating and no flaps
| 66
| 69
|-
| Best Single Engine Rate of Climb Speed
| 89
| 90
|}
 
=== Airspeed Indicator Markings ===
 
=== Power Plang Limitations ===
 
=== Power Plant Instrument Markings ===
 
=== Center of Gravity Limits ===
 
=== Maneuver Limits ===
 
=== Flight Load Factor Limits ===
 
=== Types of Operations ===
 
=== Fuel Limitations ===
 
=== Gyro Pressuer Limits ===
 
=== Flight Into Known Icing Conditions ===
 
=== Operating Altitude Limitations ===
 
 
== Development status/Issues/Todo ==

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