Weight and Balance Calculations for: |
Piper Seminole N2882C
(1/5/2016) |
|
Item |
Weight (lbs) |
Arm (in) |
Moment (x1000) |
|
Empty Weight |
2603 |
x |
223.7 |
|
Fuel (Gal full-108/60/empty_x 6lbs) |
648 / 360
/ 0 |
x |
/ / 0 |
|
Pilot |
|
x |
|
|
Co-Pilot |
|
x |
|
|
Rear Passenger #1 |
|
x |
|
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Rear Passenger #2 |
|
x |
|
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Baggage Area #1 (max lbs) |
|
x |
|
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Baggage Area #2 (max lbs) |
|
x |
|
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Other: (max lbs) |
|
x |
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Max Gross
Weight POH |
3800 |
|
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TOTAL Weight |
/ / |
|
/ / |
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IS THIS WITHIN? YES |
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IS THIS WITHIN?
YES/YES/YES |
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Weight x Arm = Moment |
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CG = Sum of Moments / Sum of
Weights |
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Performance |
Temperature |
|
Altitude Basis: |
|
Time/Date: |
Altimeter |
|
Fuel Burn Max/Min |
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Field Elevation at ( ) |
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Endurance @66 Max/Min |
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Pressure Altitude |
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Range Max/Min |
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Density Altitude |
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Takeoff Ground Roll |
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Takeoff Dist (over 50ft obs) |
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Landing Dist (over 50ft obs) |
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Landing Ground Roll |
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Rate of Climb (2 engines) |
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Accelerate/stop distance |
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Rate of Climb (1 engine) |
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Piper Seminole PA44-181 |
N2882C |
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