Ran
s
Inc.
Section
3
Model S-7
L
S CO
URIER
Weig
ht and Balan
c
e Inform
ation
Origin
al Issue
March 3, 2005
3- 9
Sample Loa
ding Problem
Sample
Ai
rp
la
n
e
Your
Your
Your
Ai
rp
la
n
e
Ai
rp
la
n
e
Ai
rp
la
n
e
Item
We
ight
Ar
m
Moment
We
ight
A
rm
Moment
We
ight
A
rm
Moment
We
ight
A
rm
Moment
( lb.)
(in)
(lb.-
in)
( lb.)
(in)
(lb.-
in)
( lb.)
(in)
(lb.-
in)
( lb.)
(in)
(lb.-
in)
B
a
sic E
m
pt
y
Weig
ht
751
47.7
358
22
(use data of
you
r AC; includes
unusable fuel an
d oil)
Usable Fu
el (at 6 lb./ gall)
72
52.20
375
8
52.20
52.20
52.20
Front Seat O
c
cupa
nt (35.1
5
to 37.4)*
170
37.40
635
8
(use arm cor
resp
onding to
y
o
ur se
at pos.)
Rea
r Seat Occup
ant (63.1
5
to 65.4)*
170
65.4
111
18
(use arm cor
resp
onding to
y
o
ur se
at pos.)
Baggag
e in Bagga
ge Com
partme
n
t*
20
92.50
185
0
Tota
l
Tota
l
Tota
l
Tota
l
Tota
l
Tota
l
Tota
l
Tota
l
We
ight
Moment
We
ight
Moment
We
ight
Moment
We
ight
Moment
118
3
589
06
C
e
nt
e
r of
G
ra
v
it
y
CG
CG
CG
(to
tal Mom
e
nt/ tot
a
l
w
e
ig
ht)
49.79
* Reference Figure 3-3 L
oading Arrangements
Check that
obtained CG position f
a
lls within th
e Center of Gravit
y Envelope (Figur
e 3-5)
Figure 3-4.
Sample Loading Proble
m
(Sheet 2
of 2)
