Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - October 31, 2013
Rev. 4
Page 6.4.14
Weight and balance samples (in, lbs)
▲ CAUTION ▲
Lo
ading samples - see figure 6.4.5 or 6.4.6 - are only given as an
example ; for calculation concerning your airplane, refer to the diagram
corresponding to its validity.
▲
Fig. 6.4.6
1 - Airplane basic characteristics :
W = Empty weight
Moment
Balance arm
CG (MAC %)
4 638 lbs
864 173 in.lbs
186.3 in
22.6 %
2 - Foreseen loading :
FWD compartment
1 Pilot and 1 front passenger
1 Intermediate passenger
2 Rear seats removed
Rear cargo
AFT Cargo in baggage compartment
Fuel
0 lbs
400 lbs
220 lbs
- 105.8 lbs
176 lbs
220 lbs
1 850 lbs
3 - Foreseen fuel :
Taxi fuel
Trip fuel
- 36 lbs
- 1 400 lbs
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