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Cessna 210B - Sample Loading Problem; Loading Graph; Center of Gravity Moment Envelope

Cessna 210B
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i
Operating
Limitations
.'
Your
A i
rplane
Sample
Airplane
Moment
We
i
ght
Moment
SAMPLE
LOADING
PROBLEM
Weight
(lb
· ins .
(Ibs)
2:
S
/
1000)
1810
.0
62
.6
1.
licensed
Empt
y
Weight
(Somple
Airplane)
•.•
·0
.4
22
.5
22
.5 ·0 .4
2.
Oil
.
12
QIs.·
••
•.
••••
.••.•.•
•
.••.
••. . ••
•••.•.•••.••••.•
12 . 2
340
.0
3 .
Pilot
&
Front
Po
s
senger
•••
••••••
•••••••••••••• ••••••
18.3
381.0
4.
Fuel
.
(63
.5
Gal
at
6 # /
Gal)
...........
...
..
......
.
23
.8
340.0
.5
.
Reor
Passengers
.......
.
....
..
...
.
......
...
.
..
...
.
....
.
I
11
.2
106
.5
6 .
8ag9age
.
...
....
.....
..
.
......
.........
...
........
..
..
..
.
127.7
3000
.0
7 .
Total
Aircraft
We
i
ght
(
loaded
)
•.•••.
.•.•
.•
••
.•
••
I
II
I~II
I
I ,
8 .
Locote
this
point
(
3000
at
127.71
on
the
center
of
grO
'l
it
y
en
v
elope
,
and
since
th is
point
falls
.....
ith
i n
the
en
v
elop
e
the
lood
i
ng
is
a c c e
ptable
.
-Note
:
Normally
full
o i l
ma
y b e
assumed
for
a l l
flights
.
Step
4.
Proceed
as
you did in
step
3,
except
use
the line identified
as
"FUEL"
and
6
lbs.
per
gallon
for
the
amount
of
gasoline
you
are
carrying,
and
read
the
moment
/
lOOO
from
the
Loading
Graph.
Write
the
weight
and
moment
/
lOOO
in
the
proper
columns~
Step
5.
Proceed
as
you did
in
step
3,
except
use
the
line
identified
as
"REAR
PASSENGERS,"
and
read
the
moment
/
lOOO
for
the
combined
weight
of
the
rear
passengers
being
carried.
Write
the
weight and
moment
/
1000 in
the
proper
columns
.
Step
6.
Proceed
as
you did
in
step
3,
except
use
the
line
identified
as
"BAG-
GAGE,"
and
read
the
moment
/
lOOO
for
the
number
of
pounds
of
baggage
being
carried.
Write
the
weight
and
moment
/
lOOO
in
the
proper
columns.
Step
7. Add
the
weight
column.
The
total
must
be
3000
lbs.
,
or
below,
or
you
must
lighten
your
aircraft
load.
Add
the
moment
column
(re-
member
to
subtract
rather
than
add
the
oil
moment
because
it
is
a
minus
quantity).
Step
8.
Refer
to
the
Center
of
Gravity
Moment
Envelope.
Locate
the
total
.\
~
Operating
Limitations
~
g
;
1-<
~
LOADED
AIRCRAFT
MOMENT/
IOOO
I
g
1-<
;
5
~
1-<
Q
~
5-4
5-5

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