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Cessna 208B - Page 270

Cessna 208B
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CESSNA SECTION 6
MODEL 208B (675 SHP) WEIGHT
8
BALANCEIEQUIPMENT LIST
WEIGHT AND BALANCE
(Continued)
3. Assume the tanks are completely filled and the fuel temperature
is at
35'F (25°F below the 60°F noted on the chart).
A. calculate the revised fuel weight by multiplying
ihe total usable
fuel by the sum of the average density (stated on chart) plus
the increase in density estimated for the lower fuel
temperature. In this particular sample, as shown by the
calculation below, the resulting fuel weight increase due to
lower fuel temperature will be 33.6 lbs over the 2224
lbs (for
332 gallons) shown on the chart, which might be significant in
an actual loading situation:
(1)
332 gal
X
(6.7
+
0.1 lbslgal)
=
2257.6 lbs revised fuel
weight.
6.
Then calculate the revised fuel moment. the revised moment
is in direct proportion to the revised fuel weight:
(1)
X
(revised moment) 2257.6 (revised weight)
453.2 (average moment)
=
2224 (average weight)
X
=
(453.2
X
2257.6) 12224
(2) The revised moment of
X
=
460.0. This value would be
used on the Sample Loading Problem as the moment11000
in conditions represented
by
this sample.
=,
=,
:,
--
*,
-,
d
*
-,
e
-1
=,
*
9
I
Revision 23
-
~
-9
(Continued Next Page)
U.S. 6-9

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