Cub Crafters CC18-180 Maintenance Manual page 78

Position
-
Left Front Wheel
-
Right Front Wheel
Left Rear Wheel
Right Rear Wheel
Figure 08-00-6 - Calculation of Arm for Aircraft with Wipaire 2100A Floats
Record actual arm in Figure 08-00-7.
Line
Number Position
1 Left Front Wheel
2 Right Front Wheel
3 Left Rear Wheel
4 Right Rear Wheel
(weight in lines 1+2+3+4)
Figure 08-00-7 - Weighing Form for Aircraft with Wipaire 2100A Amphibious Floats
Compute the empty weight of the aircraft and position of center of gravity.
EMPTY WEIGHT OF AIRCRAFT = TOTAL WEIGHT (Lines 1+2+3+4)
= _____________________ LB.
POSITION OF CENTER OF GRAVITY = TOTAL MOMENT
= ______________
=_______________
Manual number TC10000AMM
Date: 6/30/14
CUB CRAFTERS, INC.
CC18-180 MAINTENANCE MANUAL
Column 1
Measurement (in)
Recorded
Weight
TOTAL WEIGHT

______________
Column 2
+/- Distance From
Datum (in)
+ 40.1
+ 40.1
+ 40.1
+ 40.1
Actual
Tare Weight Actual Arm
-
-

TOTAL WEIGHT
Column 3
Arm (in)
Column 1+2
-
-
Moment
TOTAL
MOMENT
(moment in
lines
1+2+3+4)
08-00
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