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SAMPLE
SAMPLE
AIRPLANE
YOUR
AIRPLANE
LOADING
PROBLEM
Moment Moment
Weight (lb. -ins.
Weight (lb. -
ins.
(lbs.)
/1000) (lbs.)
/1000)
1.
Basic
Empty Weight
(Use
the data pertaining
to
your
airplane
as
it
is
presently equipped. Includes unusable
fuel
and
full oil) . . . .
..
. .
.
.
.
.
. . . . .
.
. 1136 34.0
2.
Usable
Fuel
(At
6 Lbs./Gal.}
Standard Tanks (24.5
Gal.
Maximum)
...
. . .
.
147 6.2
Long
Range
Tanks (37.5
Gal.
Maximum) .
.
. .
. . .
Reduced
Fuel
(As
limited by maximum weight)
...
3.
Pilot
and
Passenger
(Station 33
to
41)
.....
. .
.
.
.
340 13.3
4.
*
Baggage
-
Area
1 (Or
passenger
on child's
seat)
(Station 50
to
76, 120
Lbs.
Max.) . . . . . . . .
•
■
••
52
3.3
5.
*
Baggage
-
Area
2 (Station 76
to
94, 40
Lbs.
Max.)
.....
6.
RAMP WEIGHT
AND
MOMENT
1675
56.8
7.
Fuel
allowance
for
engine start, taxi,
and
runup
I O
o
O 0
-5
- .2
8.
TAKEOFF WEIGHT
AND
MOMENT
(Subtract Step 7 from Step
6)
1670 56.6
9.
Locate this point (1670 at 56.6) on the Center
of
Gravity Moment Envelope,
and
since
this point falls within.the envelope, the loading
is
acceptable.
*
The
maximum allowable combined weight capacity
for
baggage
areas
1
and
2
is
120 pounds.
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