Sample Loading Problem; Loading Graph; Center Of Gravity Moment Envelope - Cessna 210B Owner's Manual

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Operating Limitations
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Your A i rplane
Sample Airplane
Moment We ight
Moment
SAMPLE LOADING PROBLEM
Weight
(lb · in s . (Ibs)
2:
S
/ 1000)
1810.0 62 .6
1. licensed Empt y Weight (Somple Airplane) •.•
·0 . 4
22 .5 22 . 5 · 0 . 4
2. Oil . 12
QIs.· •• •. • ••• .••.•.• • .••. •• . . •• •••.•.•••.••••.•
12 . 2
340 .0
3 . Pilot & Front Po s senger ••• •••••• •••••• ••• ••••• ••••••
18 .3
381.0
4 . Fuel . (63 . 5 Gal at 6 # / Gal)
.......................
23 .8 340.0
.5 .
Reor Passengers ....... . .... .. ... . ...... ... . .. ... . .... .
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11 . 2 106 .5
6 . 8ag9age . ... .... ..... .. . ...... ......... ........... . . .. .. .
127.7
3000 .0
7 . Total Aircraft We i ght (loaded ) •.•••. .•. •.• •• .• ••
I I I I ~ I I I
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8 . Locote this point ( 3000 at 127.71 on the center of grO 'l it y en v elope , and since t h i s
point falls ..... ith i n the en v elop e the lood i ng is a c c e ptable .
-Note : Normally full o i l ma y b e assumed for a l l flights .
Step 4. Proceed as you did in step 3, except use the line identified as "FUEL"
and 6 lbs. per gallon for the amount of gasoline you are carrying,
and read the moment/ lOOO from the Loading Graph. Write the
weight and moment/ lOOO in the proper
columns~
Step 5. Proceed as you did in step 3, except use the line identified as "REAR
PASSENGERS," and read the moment/ lOOO for the combined weight
of the rear passengers being carried. Write the weight and moment/
1000 in the proper columns.
Step 6. P roceed as you did in step 3, except use the line identified as "BAG ­
GAGE," and read the moment/ lOOO for the number of pounds of
baggage being carried. Write the weight and moment/ lOOO in the
proper columns.
Step 7. Add the weight column. The total must be 3000 lbs. , or below, or
you must lighten your aircraft load. Add the moment column (re­
member to subtract rather than add the oil moment because it is a
minus quantity).
Step 8. Refer to the Center of Gravity Moment Envelope. Locate the total
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Operating Limitations
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g
;
1-<
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LOADED AIRCRAFT MOMENT/ IOOO
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g
1-<
;
5
~
1-<
Q
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5-4
5-5