Form default data is for.Use your own AC data !
Weight (lbs)
Arm (inches)
Moment (in-lb)
Empty Weight
Oil (qt max, 7 lb/gal)
qt :
Front Seat L & R
Fuel (gal useable)
gal:
Rear Seat L & R
Baggage 1 (lb max)
Baggage 2 (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 envelope limits per the Airplane Flight Manual...
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 purposes only. You, as pilot in command, are solely responsible for assuring correct data and proper loading of your aircraft prior to flight.
Empty weight and C.G. data comes from your AC current weight & balance records.
Station arms, load limits, and airspeed limits come from the Airplane Flight Manual (before 03-01-79) or Pilot's Operating Handbook [POH] (after 03-01-79) [pop-up more detail], or the FAAType Certificate Data Sheet (TCDS). Downloading the TCDS is recommended to learn more about your AC.
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 = 1862; df.ewarm.value = 37.2; ... etc.
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