Weight and Balance Form and Diagram (m, kg)
Moment = Weight × Arm
CG (MAC %) =
Arm (m) − 4.392
1.51
× 100
Table 6.4.1 - Weight and Balance Form (m, kg)
Item
Weight
(kg)
Arm
(m)
Moment
(m.kg)
C.G.
(MAC %)
Empty weight
(kg)
Baggage FWD (< 50 kg)
3.250
Front seats
(kg)
4.534
Inter. seats
- 15.4 kg per
seat removed *
5.710
Pax
Rear
bench/net
- 21 kg per seat
removed *
6.785
Pax
Cargo (< 80 kg)
Baggage AFT
(< 100 kg)
7.695
Zero fuel
weight
(< 2,836 kg)
Fuel
(kg)
4.820
Ramp weight
(< 3,470 kg)
Taxi fuel
(kg)
4.820
Takeoff weight
(< 3,454 kg)
Trip fuel
(kg)
4.820
Landing weight (< 3,225 kg)
* Seat weights include the seat heating system
Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.7
PIM - DO NOT USE FOR FLIGHT OPERATIONS
