WARNING
For airplane with C.G. between 28% and 34.7% at takeoff, fuel
consumption during flight will move the C.G. rearwards. This is to be
taken into account to remain inside the C.G. limits.
See an example of C.G. moving outside the limits in
(red
dashed line).
Figure 2.5.3 - Example of C.G. Outside the Limits when Fuel on Board Decreases
C
4
0
8
0
0
0
0
A
A
B
IM
A
8
0
0
0
Max Ramp Weight (MRW)
Max Takeoff Weight (MTOW)
Max Landing Weight (MLW)
Max Zero Fuel
Weight (MZFW)
Ramp Weight
Takeoff 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 %)
17
20
25
30
35
A
ir
p
la
n
e
w
e
ig
h
t
(k
g
x
1
0
0
)
Pilot's Information Manual
Section 2
Limitations
PIM TBM 960 - Edition 0
Rev. 00
Page 2.5.4
PIM - DO NOT USE FOR FLIGHT OPERATIONS