Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

Page: 116 / 204

Page 6-6 EASA Approved Initial issue
Aircraft Weighing Form
Aircraft: Serial Number: Reg. Number: Date:
WT9 Dynamic LSA / Club
Measured:
X =………………… m (in)
Y =………………… m (in)
Calculated:
A = X + 1.975 m (77.76 in)
B = A
– Y
AIRCRAFT EMPTY WEIGHT / MOMENT AND CG AS WEIGHED
(Including operating fluids without unusable fuel)
Weighing
point Scale reading
(kg / lb)
- Tare
(kg / lb)
= Net weight
(kg / lb)
x Arm
(m / in)
= Moment
(kg.m / lb.in/100)
Main LH A =
Main RH A =
Nose B =
Empty Weight / Moment CG =
𝑪𝑮 =
𝑻𝒐𝒕𝒂𝒍 𝑴𝒐𝒎𝒆𝒏𝒕
𝑻𝒐𝒕𝒂𝒍 𝑾𝒆𝒊𝒈𝒉𝒕
BASIC EMPTY WEIGHT / MOMENT AND CG
(Including operating fluids with unusable fuel)
Unusable fuel
(Add to empty aircraft weight and moment)
5.0 kg /
11 lb
2.580 m /
101.57 in 12.90 kg.m /
11.17 lb.in/100
Basic Empty Weight / Moment CG =