Daher TBM 960 - Airplane Loading Form (M, Kg)

Airplane Loading Form (m, kg)
Moment = Weight × Arm
CG (MAC %) =
Arm (m) − 4.392
1.51
× 100
Item
Weight
(kg)
Arm
(m)
Moment
(m.kg)
C.G.
(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
(< 2,836 kg) (3a) (5) (3b) (5c)
Fuel (kg) (6a) 4.820 (6b)
Ramp weight (< 3,470 kg) (7a) (9) (7b) (9c)
Taxi fuel (kg) (10a) 4.820 (10b)
Takeoff weight (< 3,454 kg) (11a) (13) (11b) (13c)
Trip fuel (kg) (14a) 4.820 (14b)
Landing weight (< 3,225 kg) (15a) (17) (15b) (17c)
* Seat weights include the seat heating system
Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS