SECTION 6 CESSNA
WEIGHT & BALANCE / EQUIPMENT LIST MODEL 182T
ITEM DESCRIPTION
WEIGHT AND MOMENT
TABULATION
SAMPLE
AIRPLANE
Weight
(lbs.)
Moment
(Lb>ins.
/1000)
YOUR
AIRPLANE
Weight
(lbs.)
Moment
(Lb>ins.
/1000)
1. Basic Empty Weight (Use the
data pertaining to your
airplane as it is presently
equipped. Includes unusable
fuel and full oil) 1919 70.9
2. Usable Fuel (At 6 Lbs./Gal.)
87 Gallons Maximum
528 24.6
Reduced Fuel
(64 Gallons)
3. Pilot and Front Passenger
(Station 32 to 50) 340 12.6
4. Second Row Passengers 200 14.8
Cargo Replacing Second
Row Seats (Sta. 65 to 82)
5. *Baggage Area A (Station 82
to 109; 120 Lbs. Max.) 100 9.7
6. *Baggage Area B (Station 109
to 124; 80 Lbs. Max.) 23 2.7
7. *Baggage Area C (Station 124
to 134; 80 Lbs. Max.)
8. RAMP WEIGHT AND MOMENT 3110 135.3
9. Fuel allowance for engine
start, taxi and runup >10 >0.5
10.TAKEOFF WEIGHT AND
MOMENT (Subtract Step 9
from Step 8) 3100 134.8
11.Locate this point (3100 at 134.8) on the Center of Gravity Moment
Envelope, and since this point falls within the envelope, the loading is
acceptable, providing that flight time is allowed for fuel burn>off to a
maximum of 2950 pounds before landing.
* The maximum allowable combined weight capacity for baggage in
areas A, B and C is 200 pounds. The maximum allowable combined
weight capacity in areas B and C is 80 pounds.
Figure 6-5. Sample Loading Problem (Sheet 1 of 2)
6-12 Feb 23/01
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