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SAMPLE
SAMPLE
AIRPLANE
1.
2.
LOADING
PROBLEM
Basic
Empty
Weight
(Use
the
data
pertaining
to
your
airplane
as
it
is
presently
equipped.
Includes
unusable
fuel
and
full
oil)
.
Usable
Fuel
(At
6
Lbs./Gal.)
..
.
.
.
.
Standard
Tanks
(40
Gal.
Maximum)
...
.
.
3.
4.
Long
Range
Tanks
(50
Gal.
Maximum)
Pilot
and
Front
Passenger
(Station
34
to
46)
Rear
Passengers
..
.
.
5.
*
Baggage
Area
1
or
Passenger
on
Child's
Seat
(Station
82
to
108,
120
Lbs.
Max.)
.
..
..
.
.
6.
*
Baggage
Area
2
(Station
108
to
142,
50
Lbs.
Max.)
.
.
7.
RAMP
WEIGHT
AND
MOMENT
8.
Fuel
allowance
for
engine
start,
taxi,
and
runup
9.
TAKEOFF
WEIGHT
AND
MOMENT
(Subtract
Step
8
from
Step
7)
.
.
..
Weight
(lbs.)
1454
240
340
170
103
2307
-7
2300
10.
Locate
this
point
(2300
at
103.6)
on
the
Center
of
Gravity
Moment
Envelope,
and
since
this
point
falls
within
the
envelope,
the
loading
is
acceptable.
Moment
(lb.
-ins.
/1000)
57.6
11.5
12.6
12.4
9.8
103.9
-
.3
103.6
YOUR
AIRPLANE
Moment
Weig
ht
(lb.
-
ins.
(lbs.)
/1000)
*
The
maximum
allowable
combined
weight
capacity
for
baggage
areas
1
and
2
is
120
lbs.
Figure
6-5.
Sample
Loading
Problem
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