Figure 6.4.6 - Weight and Balance Diagram Example (in, lbs)
C
4
0
8
0
0
0
0
A
A
B
H
M
A
8
0
0
0
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
A
ir
p
la
n
e
w
e
ig
h
t
(l
b
s
x
1
0
0
)
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
