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 Figure 2.5.3 (red
dashed line).
Figure 2.5.3 - Example of C.G. Outside the Limits when Fuel on Board Decreases
C4080000AABIMA8000
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
Airplane weight (kg x 100)
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
To Next Page
Loading...