INSPECTIONS / EMPTY WEIGHT AND CG MEASUREMENT 3-33
CHANGE C2 ICON A5 / MAINTENANCE MANUAL
4. Complete the following worksheet.
5. Perform the calculations to obtain the required weight and balance information.
VERIFICATION METHOD:
Fill out blank cells in table below.
Calculate the FS location of the CG by dividing the total moment by the total weight.
Total Wt (from above)= ______lbs
FS Position of CG (Total M/Total Wt)=______ in
Verify readings and calculations and compare them with the Pilot’s Operating Handbook records. Enter
the new weight and balance information as a new baseline in the POH.
RELATED INFORMATION:
"Weight and Balance Information" on page 2-23
"Weight and Balance—General" on page 3-27
"Interval Maintenance—Calendar Intervals" on page 3-5
"Main Landing Gear Inspection" on page 14-8
"Nose Gear Inspection" on page 14-56
"Check Landing Gear Extended Position" on page 14-5
"Check Landing Gear Retracted Position" on page 14-6
"Landing Gear Indicator Lights" on page 14-10
"Main Landing Gear (MLG) Wheel and Axle Removal" on page 14-45
"Main Landing Gear (MLG) Wheel and Axle Installation" on page 14-48
"Pump Usable Fuel From Fuel Tank" on page 10-8
"Cockpit Floor Board Removal" on page 3-46
"Landing Gear Excessive Friction Check" on page 14-16
Load Cell Position
Weight, Wt (lb
f
)
Arm, FS (in)
Moment, M=Wt x Arm
(in-lb)
Wing Left Jack Point 147.7
Wing Right Jack Point 147.7
Tail Jack Point 294.63
Tota l
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