I
I
I
\
Sample
Airplane
Your
Airplane
SAMPLE
LOADING
PROBLEM
Weight
(lbs)
Moment
(lb-ins.
/10001
Weight
Moment
b&
1.
licensed
Empty
Weight
(Sample
Airplane!
.........
1045
34.6
2. Oil · 6
Ots.'
.......................................................
.
11
-
0.1
11
3. Pilot &
Passenger
................................................. 3
40
13.3
4.
Fuel • Std.
Tanks
(22
.5
Gal
at
6#/Gal)............
135
5.7
5.
Baggage-Area
1
(or
children
on
child's
soot)....
69
4.4
6.
Baggage-Area
2
...................................................
0
0.0
7.
Total Aircralt
Weight
(Loaded!
............................. ·
1600
57.9
I
1!.
Locale
this
point
(
1600
at
57.9)
an
the
center
of
gravity
envelope
and
since
this
point
falls
within
envelope
the
loading
is
a'
cceptable.
•Note;
Normally
full
oil
may
be
assumed
lor
all
flights.
-0.1
BAGGAGE
LOADING
AND
TIE-DOWN
BAGGAGE
AREA
MAXIMUM ALLOWABlE
LOADS
=
40
POUNDS
=
120
POU~DS
NET
ATTACH
POINTS
* A r.argo lie-down net
is
provided to
secw·c
baggage
i~
the baggage
area.
The net attaches
to
si.x
tie-doW11
rings. Two rings
arc
located
on
the floor
just
aft
of
the
seat
backs
and one
ring
Is
located two
inches
above the floor
on
each cabin wall
ut
the aft
end
ol
area (D . Two addiUonal rings
are
located at
the
top, aft end of
area®.
At
least
four
ring
s should
be
used
to
re
strain the maximum baggage load of
120
H.
·
II
the airplane
is
equipped with
an
optional utility
shelf,
it
should be r
e-
moved p
rior
to loading and tying
down
large
baggage
items
. (Slide the
tab
of
the
locltio.g
clips on each end
of
the shelf Inboard
to
disengage the
shelf
from
the
alrcraft
st
ructure
.) Aller baggage
is
loaded
and
sec:urcd,
eit
her
slow
the shelf or,
if
space permits,
ln
stall
it
for sturi
nJ{
smal1
articles.
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