Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

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Initial issue EASA Approved Page 2-7
2.4 Weight Limits
Maximum takeoff weight 600.0 kg 1323 lb
Maximum landing weight 600.0 kg 1323 lb
Minimum flying weight 405.0 kg 893 lb
Maximum load per seat 120.0 kg 265 lb
Maximum total baggage weight 2x 20.0 kg 2x 44 lb
WARNING
Do not exceed maximum takeoff weight 600.0 kg!
WARNING
Do not place any baggage or objects to the compartment below
your legs! It is not a baggage compartment!
NOTE
Actual aircraft empty weight is mentioned in Chapter 6.
2.5 Center of Gravity Limits
Metric Units
U. S. Standard Units
Reference Datum
1.975 m forward from inner surface
of the firewall
77.76 in forward from inner surface
of the firewall
Forward CG
2.704 m (18.3 %MAC) at 542.5 kg
with straight line taper to
2.748 m (22.0 %MAC) at 600.0 kg
106.48 in (18.3 %MAC) at 1196 lb
with straight line taper to
108.18 in (22.0 %MAC) at 1323 lb
Rearward CG 2.824 m (28.5 %MAC)
111.18 in (28.5 %MAC)
Center of gravity limits charts are shown at Fig. 6-2 (Metric Units) and Fig. 6-3 (U. S. Standard Units).
Rearward center of gravity limit is obtained at maximum crew weight and minimum fuel amount. Forward center
of gravity limit is obtained at minimum pilot weight and maximum fuel amount. For more details see the Chapter 6.
WARNING
A flight shall not be commenced until the pilot-in-command is
satisfied that the mass of the aircraft and CG location are within
the allowed limits for takeoff and landing!
Fuel consumption moves the CG rearwards, therefore the CG
location must be calculated for empty tanks as well!
The mass of the baggage must be taken into account for every CG
calculation!