Daher TBM 940 - Page 469

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - March 05, 2019
Rev. 0
Page 6.4.14
Moment = Weight x Arm
CG (MAC %) =
(
Arm (m)
−
4.392
)
1.51
× 100
Item
Weight
(kg)
Arm
(m)
Moment
(m.kg)
CG
(MAC %)
Empty weight (kg) 2 126 4.738 10 073 22.9
Baggage
FWD
(< 50 kg) 0 3.250 0
Front seats (kg) 200 4.534 907
Inter. seats
- 15.4 kg per
seat
removed *
0
5.710
0
Pax 0 0
Rear
bench/net
- 21 kg per
seat
removed *
0
6.785
0
Pax 160 1 086
Cargo
(< 80 kg)
0 0
Baggage AFT (< 100 kg) 50 7.695 385
Zero fuel
weight
(< 2736 kg) 2 536 4.910 12 451 34.3
Fuel (kg) 820 4.820 3 952
Ramp weight (< 3370 kg) 3 356 4.888 16 403 32.8
Taxi fuel (kg) - 16 4.820 - 77
Takeoff
weight
(< 3354 kg) 3 340 4.888 16 326 32.8
Trip fuel (kg) - 600 4.820 - 2 892
Landing
weight
(< 3186 kg) 2 740 4.903 13 434 33.8
* Seats weights include seat heating system
PIM - DO NOT USE FOR FLIGHT OPERATIONS