C42 Owner’s Manual (Microlight) Page 18
Loading plan
Position weight x lever arm = moment
kg mm kg.mm
Empty weight
1. Seats 400
2. Under seat bags 400
3.
F
uel 950
4.
S
amsonite case 950
Total W eight kg Total Moment kg.mm
Total Moment kg.mm
centre of gravity CG = ------------------------------------------ = mm
Total W eight kg
6.2 Conditions of Weighing
The dry empty weight of the aircraft is defined under the following conditions:
All normal installed equipment fitted.
Oil and coolant levels normal.
No usable fuel.
Note: Remaining within the maximum Take-off Weight (MTOW) of 450 kg (or 472.5kg with
appropriate modifications fitted) is the pilot’s responsibility.
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