FAA-H-8083-25C · Source PDF page 252
Weight and Balance
Determining Loaded Weight and CG · PHAK page 10-8

Searchable transcription
Load Moment/1,000 (kilogram-millimeters)
0 50 100 150 200 250 300 350 400
200
400
175
350 340 150
300 125
250
100
200
75
150
50
100
50 25
0 0
5 10 12.7 15 20 25 30
10-8
)smargolik(
thgieW
daoL
Load Moment/1,000 (inch-pounds)
)sdnuop(
thgieW
daoL
g/lit er) 60 g
6
a
2
l (
g
2
a
2
l
7
**
.1
*( 2
lit
3
e
4
r
.
s
7
)
lit
R
e
e
rs
a
)
r
passengers
2
k
n g er al; 0. 7 50 gal**(189.3 liters) e g
&
fr o
nt p a s
s
F u
el ( 6 l
b/
40
4
g
2
a
g
l*
a
(1
l
8
re
9
d
.3
u c
li
e
te
d
r
*
s
*
)
*(159 liters)
ot
Pil
30 gal (113.6 liters)
20 gal (75.7 liters)
Baggage area 1 or Maximum Usable Fuel
passenger on child’s seat * Standard tanks
10 gal (37.9 liters) ** Long range tanks
*** Internal tanks
Baggage area 2
Loaded Aircraft Moment/1,000 (kilogram-millimeters)
1,100
2,400
2,367
1,050
2,300
2,200 1,000
2,100 950
2,000
900
1,900
850
1,800
800
1,700
750
1,600
700
1,500
45 50 55 60 65 70 75 80 85 90 95 100 105 110
105.2
)smargolik(
thgieW
enalpriA
dedaoL
Loaded Aircraft Moment/1,000 (inch-pounds)
)sdnuop(
thgieW
tfarcriA
dedaoL
Figure 10-7. Loading graph.
600 700 800 900 1,000 1,100 1,200 1,300
Normal
category
y
or
g
e at
c
y Utilit
Figure 10-8. CG moment envelope.