Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

Page: 121 / 204

Initial issue EASA Approved Page 6-11
Weight and Balance Loading Form
It is the responsibility of the pilot in command to ensure that the aircraft will be properly loaded within
the weight and moment limits during takeoff, flight and landing. The weight and balance loading form
enables the pilot to determine the aircraft loading using Loading Data (6.5) and to compare with the limits
given in Weight and Moment Limits Chart (6.6).
The example is shown in the table below and on Fig. 6-4. For blank Weight and Moment Limits Chart refer
to Chapter 6.6.
Weight and Balance Loading Form
Aircraft: Serial Number: Reg. Number: Date:
WT9 Dynamic LSA / Club
No. Item
Example aircraft Your aircraft
Weight Moment Weight Moment
kg /
lb
kg.m /
lb.in/100
kg /
lb
kg.m /
lb.in/100
1.
Basic Empty Weight / Moment
(See Chapter 6.3)
(Including unusable fuel)
350.0 922.90
2.
Pilot
(Min. 55 kg / 121 lb, Max. 120 kg / 265 lb)
90.0 281.70
3.
Co-pilot (passenger)
(Max. 120 kg / 265 lb)
81.0 253.53
4.
Baggage compartment
(Max. 2 x 20 kg / 2 x 44 lb)
10.0 37.95
5.
Usable fuel
(max. 85.7 kg / 189 lb)
57.6 148.61
6.
Takeoff Weight / Moment
(Sum of lines No. 1 through 5)
588.6 1644.69
7.
Zero Fuel Weight / Moment
(Sum of lines No. 1 through 4)
531.0 1496.08