Daher TBM 960 - Weight and Balance Examples (M, Kg)

Weight and Balance Examples (m, kg)
CAUTION
These loading tables (Table 6.4.3, Table 6.4.4 and Figure 6.4.5) 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