C210M Weight and Balance Calculator

Form default data is for .
Update weights for this flight!
 Weight 
(lbs)
Arm
(inches)
Moment
(in-lb)
 Empty Weight
 Front Seat 1 & 2  
 Fuel ( gal useable) gal:
 Middle Seat 1 & 2  
 Rear Seat 1 & 2  
 Wheel Well ( lbs. max)  
 Aux Fuel ( gal max) gal:
 Baggage ( lb max)
     
 Gross Weight ( lb max):  
 Loaded Center of Gravity:  
 Maneuvering speed, Va (kts):  <=(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...


This active chart requires a CSS compliant browser like NS 7, Mozilla, IE 5, IE 6, Opera 7. CSS scheme for active graph is from C 172 G-BSEP W & B Calculator.

! This calculator is presented for educational or amusement purposes only. You, as pilot in command, are solely responsible for assuring correct data and proper loading of your aircraft prior to flight. Note that it's a fairly trivial exercise to copy the source of this page and edit the default data values to reflect your own situation and aircraft data for use on your local computer. Eg:

df.ew.value = 2322;
df.ewarm.value = 42.7;
  ... etc.

Mac made   Last tinkered with March 25, 2006 - A.J.G.   Valid 
  
  HTML 4.01!
Many Thanks to Bob Booty of the Oshkosh Brass Quintet who wrote the original version of this page!
See this link for the source and the weight and balance calculator for other airplanes!

Return to Balance Calculator Home.
  [top of page ]