Daher TBM 940 - Weight and Balance Form and Diagram (M, Kg)

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - March 05, 2019
Rev. 0
Page 6.4.8
Weight and balance form and diagram (m, kg)
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)
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
(< 2736 kg)
Fuel (kg) 4.820
Ramp weight (< 3370 kg)
Taxi fuel (kg) 4.820
Takeoff
weight
(< 3354 kg)
Trip fuel (kg) 4.820
Landing
weight
(< 3186 kg)
* Seats weights include seat heating system
PIM - DO NOT USE FOR FLIGHT OPERATIONS