Daher TBM 960 - Weight and Balance Form and Diagram (In, Lbs)

Weight and Balance Form and Diagram (in, lbs)
Moment = Weight × Arm
CG (MAC %) =
Arm (in) − 172.93
59.45
× 100
Table 6.4.2 - Weight and Balance Form (in, lbs)
Item
Weight
(lbs)
Arm
(in)
Moment
(in.lbs)
C.G.
(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 *
267.1Pax
Cargo (< 176
lbs)
Baggage AFT (< 220 lbs) 303.0
Zero fuel
weight
(< 6,252 lbs)
Fuel (lbs) 189.8
Ramp weight (< 7,650 lbs)
Taxi fuel (lbs) 189.8
Takeoff weight (< 7,615 lbs)
Trip fuel (lbs) 189.8
Landing weight (< 7,110 lbs)
* Seat weights include the seat heating system
Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.9
PIM - DO NOT USE FOR FLIGHT OPERATIONS