Daher TBM 940 - Airplane Loading Form (M, Kg)

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - March 05, 2019
Rev. 0
Page 6.4.4
Airplane loading form (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)
(1a) (1b) (1c)
Baggage
FWD
(< 50 kg)
(2a)
3.250
(2b)
Front seats (kg)
(2a)
4.534
(2b)
Inter. seats
-15.4 kg per
seat
removed *
(2a)
5.710
(2b)
Pax
(2a) (2b)
Rear
bench/net
-21 kg per
seat
removed *
(2a)
6.785
(2b)
Pax
(2a) (2b)
Cargo
(< 80 kg)
(2a) (2b)
Baggage AFT (< 100 kg)
(2a)
7.695
(2b)
Zero fuel
weight
(< 2736 kg)
(3a) (5) (3b) (5c)
Fuel (kg)
(6a)
4.820
(6b)
Ramp weight (< 3370 kg)
(7a) (9) (7b) (9c)
Taxi fuel (kg)
(10a)
4.820
(10b)
Takeoff
weight
(< 3354 kg)
(11a) (13) (11b) (13c)
Trip fuel (kg)
(14a)
4.820
(14b)
Landing
weight
(< 3186 kg)
(15a) (17) (17) (17c)
* Seats weights include seat heating system
PIM - DO NOT USE FOR FLIGHT OPERATIONS