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   
Rear Passenger #2        x   
Baggage Area #1 (max              lbs)        x   
Baggage Area #2 (max              lbs)        x   
Other:                   (max              lbs)        x   
       
            Max Gross Weight POH 3800    
            TOTAL Weight            /                 /          /                 /  
IS THIS WITHIN?  YES IS THIS WITHIN?   YES/YES/YES
Formulas
Weight x Arm = Moment
CG = Sum of Moments / Sum of Weights
Performance   Temperature   Altitude Basis:  
Time/Date:                       Altimeter      Fuel Burn Max/Min  
Field Elevation at (                )      Endurance @66  Max/Min  
Pressure Altitude      Range Max/Min  
Density Altitude  
Takeoff Ground Roll  
Takeoff Dist (over 50ft obs)  
Landing Dist (over 50ft obs)  
Landing Ground Roll   Rate of Climb (2 engines)  
Accelerate/stop distance   Rate of Climb (1 engine)  
         
Piper Seminole PA44-181 N2882C