N6356J Weight and Balance

This calculator is presented for educational purposes only. You, as pilot in command, are solely responsible for assuring correct data and proper loading of your aircraft prior to flight.

The weight and balance numbers below are unofficial, and meant for advisory purposes only. The weight and balance values are subject to change at any time (upgrades), and thus the ONLY official source of the weight and balance data is the aircraft logbook, and it remains solely the responsibility of each pilot to obtain/verify/calculate the current weight and balance for each flight.

To Figure your weight and balance edit the values in the yellow boxes.

Form default data is for . Use your own aircraft data !  Weight  (lbs) Arm (inches) Moment (in-lb)  Empty Weight  Oil ( qt max, 7 lb/gal) qt :  Front Seat 1 & 2  Fuel ( gal useable) (36 Gal to the tabs) gal:  Rear Seat 1 & 2  Baggage ( lb max)        Gross Weight ( lb max):    Loaded Center of Gravity:    Maneuvering speed, Va (mph):  <=(decr. with decr. wt.)

Calculated Gross Weight and C.G. point must lie within the utility or normal category envelope limits per the Airplane Flight Manual, landplane example below...

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