Comco Ikarus C42-E - Conditions of Weighing; Equipment List

C42E 540kg LSA POH Issue 3 China 15.03.2016
Page 23 of 36
Loading plan
Position weight x lever arm = moment
kg mm kg.mm
Empty weight
1. Seats 400
2. Under seat bags 400
3. Fuel 950
4. Samsonite case 950
Total W eight kg T otal Moment kg.mm
Total Moment kg.mm
centre of gravity CG =
------------------------------------------ = cm
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 540 kg, 1191lb is the pilot’s
responsibility.
6.1 Equipment list
When weighing the aircraft make a note of the aircraft configuration. Such an equipment list may include:
Spats
Seat cushions
Radio
Intercom
GPS
Baggage bag
Reserve parachute