Daher TBM 900 - Page 430

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - October 31, 2013
Rev. 4
Page 6.4.15
Moment = Weight x Arm
CG (MAC %) =
(
Arm (in) − 172.93
)
59.45
× 100
Item
Weight
(lbs)
Arm
(in)
Moment
(in.lbs)
CG
(MAC %)
Empty weight (lbs) 4 638 186.3 864 173 22.6
Baggage
FWD
(< 110 lbs) 0 128.0 0
Front seats (lbs) 400 178.5 71 400
Inter. seats
- 37.5 lbs
per seat
removed
0
224.8
0
Pax 220 49 456
Rear
bench/net
- 52.9 lbs
per seat
removed
- 105.8
267.1
- 28 259
Pax 0 0
Cargo
(< 176 lbs)
176 47 010
Baggage AFT (< 220 lbs) 220 303.0 66 660
Zero fuel
weight
(< 6032 lbs) 5 548 192.9 1 070 440 33.6
Fuel (lbs) 1 850 189.8 351 130
Ramp weight (< 7430 lbs) 7 398 192.2 1 421 570 32.4
Taxi fuel (lbs) - 36 189.8 - 6 833
Takeoff
weight
(< 7394 lbs) 7 362 192.2 1 414 737 32.4
Trip fuel (lbs) - 1 400 189.8 - 265 720
Landing
weight
(< 7024 lbs) 5 962 192.7 1 149 017 33.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS