Weight and Balance Examples (m, kg)
CAUTION
These loading tables (
) are provided
only as examples. For calculations concerning your airplane, use the
appropriate diagram.
Table 6.4.3 - Loading Example (m, kg)
1 - Airplane basic characteristics:
W = Empty weight
2,170 kg
Moment
10,258 m.kg
Balance arm
4.727 m
C.G. (MAC %)
22.2%
2 - Anticipated loading:
1 Pilot
90 kg
1 passenger on intermediate seat
90 kg
2 Rear passengers
160 kg
AFT Cargo in baggage compartment
35 kg
Fuel
915 kg
3 - Anticipated fuel:
Taxi fuel
- 30 kg
Trip fuel
- 600 kg
Moment = Weight × Arm
CG (MAC %) =
Arm (m) − 4.392
1.51
× 100
Table 6.4.4 - Weight and Balance Form Example (m, kg)
Item
Weight
(kg)
Arm
(m)
Moment
(m.kg)
C.G.
(MAC %)
Empty weight
(kg)
2,170
4.727
10,258
22.2
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Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.11
PIM - DO NOT USE FOR FLIGHT OPERATIONS
