Cessna 1980 182Q Pilot's Operating Handbook And Flight Manual page 108

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SAMPLE
SAMPLE AIRPLANE
LOADING PROBLEM
Weight
Moment
(Ibs.)
(lb.-ins.
11000)
BaSIC Empty WI1I!lht (Use the data pertaining to your
"Irplane as it is prt!sently equipped. I neludes unusable
fuel and full oil) .
..
·
.
. . . .
.
.
. . .
1800 63.3
Usable Fuel (At 6 Lbs.lGal.)
Standard Tanks (88 Gal. Maximum) . . . .
.. · ..
Reduced Fuel (65 GaL) . .
·
...... . .
. . .
390
18.1
Pilot and Front Passenger (Station 32 to 50). . . . . ·
.
340 12.6
Second Row Passengers . . . .
·
.........
340 25.2
Cargo Replacing Second Row Seats (Sta. 65 to 82) . . .
Baggage (Area" A") or Passenger on Child's Seat
(Sta. 82 to 108) 120 Lbs. Maximum . . . . . . . .
· .
90 8.7
Baggage-Aft (Area "B") and Hatshelf
(Sta. 108 to 136) 80 Lbs. Maximum .
. .
. . . . .
RAMP WEIGHT AND MOMENT
2960 127.9
Fuel allowance for engine start, taxi and runup
... · .
-10
- .5
TAKEOFF WEIGHT AND MOMENT
(Subtract step 8 from step 7) 2950
127.4
,
Locate this point (2950 at 127.4) on the Center of Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
Figure 6-5. Sample Loading Problem
YOUR AIR PLAN E
Weight
Moment
(lbs.)
(lb.-ins.
11000)
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