Weight and Balance Form

Aircraft Name    Youngster       Serial Number     075    Registration Number N661JH
Owner's Name    James E. Hardy
Datum    Front Prop Face at hub        Leveling    Top Longeron
C.G. Limits:  Forward  47.5"  inches _22% Rearward limit is 50.75 inches 30.0%

Empty Weight Calculations

Item
                    Weight      Arm(inches)       Moment(inch lbs)
Left Wheel        187              40.5                 7573.5
Right Wheel      192              40.5                  7776
Tail Wheel          12             171                    2052
Fuel                     0                32.                      75  0
Battery/took kit   10               75                    750
    Empty Weight  401lbs      Total Moment  18151.5

Empty Weight C.G. Location:   __45.27____  Inches.
Empty Weight with oil               401
 

Empty weight c.g. = Total Moment  = ____181515__ Inches = 45.27
                               Empty Weight                401

Forward and Rearward C.G. Extremes

Most forward C.G. Loading    Most rearward C.G. loading
Item                        Weight     arm           Moment   * Weight      arm        Moment
A/C Empty Weight   401         45.27       18151.5   * 401        45.27        18151.5
Pilot                         170          61           10370      * 185         61            11285
Fuel                           57           2.75         1867      * 12.0        32.75          393

Totals                      628                          30388.5  *  598                        29829.5

Forward C.G. _48.4__Inches                 Rearward C.G. _49.9__Inches

CGf=Ttl moments/Ttl weight = _48.4    CGr=Ttl Moments/Ttl weights=_49.9_In.
With no Cargo compartment, The Forward CG loading is also the Max loading
CG.

Maximum Allowable Weight is: 650 lbs

CG at max loading= 48.8 inches

Aircraft weighed by:___________________
    James E. Hardy

Date of weighing:  _____________________ 6/11/2001_
 
 


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