CESSNA SECTION 6
MODEL T182T NAV III WEIGHT AND BALANCE/
GFC 700 AFCS EQUIPMENT LIST
U.S.
SAMPLE LOADING PROBLEM
ITEM DESCRIPTION
WEIGHT AND MOMENT
TABULATION
SAMPLE
AIRPLANE
YOUR
AIRPLANE
Weight
(lbs)
Moment
(lb-ins/
1000)
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) 2029 73.0
2 - Usable Fuel (At 6 Lbs./Gal.)
- Standard Fuel - 87 Gallons Maximum 522 24.3
- Reduced Fuel - 64 Gallons
3 - Pilot and Front Passenger (FS 32 to 50) 340 12.6
4 - Rear Passengers (FS 74) 170 12.6
Cargo - Replacing Rear Passenger Seat
(FS 65 to 82)
5 - *Baggage “A” (FS 82 to 109)
120 Pounds Maximum
*Baggage “B” (FS 109 to 124)
80 Pounds Maximum 51 5.9
*Baggage “C” (FS 124 to 134)
80 Pounds Maximum
6 - RAMP WEIGHT AND MOMENT 3112 128.4
7 - Fuel allowance for engine start, taxi and
runup -12.0 -0.6
8 - TAKEOFF WEIGHT AND MOMENT
(Subtract Step 7 from Step 6)
3100 127.8
9 - Locate this point (3100 at 127.8) 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 6-3 (Sheet 1 of 2)
T182TPHBUS-00
6-11
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