Daher TBM 960 - Determining Empty Airplane Characteristics

Figure 6.4.6 - Weight and Balance Diagram Example (in, lbs)
C4080000AABHMA8000
0 100 200 300 400 500 600 700 800 900
0
200
400 600 800
1,000 1,200
(kg)
(liters)
0 200 400 600 800 1,000 1,200 1,400 1,600 1,800 2,000
0
30 60 90 120 150 180 210 240 270 300
(lbs)
(USG)
Max Ramp Weight (MRW)
Max Takeoff Weight (MTOW)
Max Landing Weight (MLW)
Max Zero Fuel
Weight (MZFW)
Ramp Weight
Takeoff Weight
Landing Weight
Zero Fuel Weight
Empty Weight
14
16 18
20 22 24 26 28 30 32 34 36
(MAC %)
16
18
20
22 24
26
28
30
32
34
(MAC %)
40
44
48
52
56
60
64
68
72
76
Airplane weight (lbs x 100)
Determining Empty Airplane Characteristics
Empty airplane characteristics (weight
and balance) may vary in relation to those
indicated on the weighing form based on the installed optional equipment and
installed seats.
Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.16
PIM - DO NOT USE FOR FLIGHT OPERATIONS