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Weight & Balance Calculator for C-170A N5528C


Weight (lbs)   x   Arm   =   Moment
Empty (lbs) x=
Front Seats x=
Rear Seats x=
Baggage x=
Fuel gal x=
Oil qts x=
Totals x=

 Maneuvering Speed   mph

 




It is important to keep the load carried by an airplane under the maximum allowable weight and in the proper position for the airplane. The C-170A has a maximum gross weight of 2,200 pounds. In addition to the maximum weight, the center of gravity must be within limits. The above calculator performs a W&B calculation for N5528C. This calculator will work for other C-170As however the weight and arm will need to be adjusted. Please don't use this calculator to calculate your weight and balance without rechecking all of the calculations.



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Modified 10/01/08