Sample Airplane
|
! Your Airplane
SAMPLE LOADING PROBLEM
Weight
(lbs)
Mo ment
(lb-ins.
1
/1000)
Weight
Mo
me n
t
1. Licensed Empty Weight (Sample Airplane)
1045 34.6
2.
Oil - 6
Qts.*
11
-0.1
11
-0.1
3. Pilot
&
Passenger
340 13.3
4. Fuel
- Std.
Tanks
(22.5 Gal at
6#/Gal)
135
5.7
5. Baggage-Area
1 (or
children
on
child's seat)
....
69 4.4
6. Baggage-Area
2
0 0.0
7. Total Aircraft Weight (Loaded)
1600
"
' III
|
8. Locate this point
(1600 at 57.9 ) on the
center
of
gravity envelope
point falls within envelope
the
loading
is
acceptable.
•Note? Normally full
oil may be
assumed
for all
flights.
and since this
BAGGAGE LOADING
AND
TIE-DOWN
baggage area
maximum allowable loads
tie down
net
attach points
Hs
A
<argo tie-down net
is
provided
to
secure baggage
in
the baggage area.
The net attaches
to six
tie-down rings. Two rings
are
located on the floor
Just aft
of
the seat backs-and one ring
is
located two inches above the floor
on each cabin wall
at
the aft end
of
area
(?) .
Two additional rings
are
located
at
the top, aft end
of
area
(2) . At
least four rings should
be
used
to restrain the maximum baggage load
of
120
120 pounds
40 pounds
=
120
pounds
area
© =
area©
=
areas
© + ©
If the airplane
is
equipped with
an
optional utility shelf,
it
should
be re-
moved prior
to
loading and tying down large baggage items. (Slide the tab
of
the locking clips on each end
of
the shelf inboard
to
disengage
the
shelf from
the aircraft structure.) After baggage
is
loaded and secured, either stow
the shelf
or, if
space permits, install
it
for storing small articles.
3-4
UTILITY SHELF
1
2
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