Daher TBM 940 - Weight and Balance Form and Diagram (In, Lbs)

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - March 05, 2019
Rev. 0
Page 6.4.10
Weight and balance form and diagram (in, lbs)
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)
Baggage
FWD
(< 110 lbs) 128.0
Front seats (lbs) 178.5
Inter. seats
- 34 lbs per
seat
removed *
224.8
Pax
Rear
bench/net
- 46.2 lbs
per seat
removed *
267.1
Pax
Cargo
(< 176 lbs)
Baggage AFT (< 220 lbs) 303.0
Zero fuel
weight
(< 6032 lbs)
Fuel (lbs) 189.8
Ramp weight (< 7430 lbs)
Taxi fuel (lbs) 189.8
Takeoff
weight
(< 7394 lbs)
Trip fuel (lbs) 189.8
Landing
weight
(< 7024 lbs)
* Seats weights include seat heating system
PIM - DO NOT USE FOR FLIGHT OPERATIONS