Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 192

SECTION 6
WEIGHT AND BALANCE/EQUIPMENT LIST
CESSNA
MODEL 172S NAV III
I
SAMPLE I n1LniNG PRORI
I=M
WEIGHT AND MOMENT
TABULATION
SAMPLE
YOUR
ITEM DESCRIPTION
AIRPLANE AIRPLANE
Weight
Moment
Weight
Moment
(Lb-ins.
(Lb-ins.
(Lbs.)
/1000)
(Lbs.)
/1000)
1. Basic Empty Weight
(Use the data pertaining to your
airplane as it is presently
equipped. Includes unusable
fuel and full oil)
1642 62.6
2. Usable Fuel (At 6 Lbs.lGal.)
I
Standard Fuel
53 Gallons Maximum
Reduced Fuel
(30 Gallons)
180 8.6
3. Pilot and Front Passenger
(FS 32 to 50) 340 12.6
4. Rear Passengers (FS 74) 340 24.8
5. * Baggage "A" (FS 82 to 108)
120 Pounds Maximum 56 4.6
6.* Baggage liB" (FS 108 to 142)
50 Pounds Maximum
7. RAMP WEIGHT AND MOMENT 2558 113.2
8. Fuel allowance for engine start,
taxi and runup -8.0 -0.4
9. TAKEOFF WEIGHT AND
MOMENT
(Subtract Step 8 from Step 7)
2550 112.8
I
I
10. Locate this point (2550 at 112.8) on the Center-of-Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
* The maximum allowable combined weight capacity for baggage in areas
A and B is 120 pounds.
Figure 6-3 (Sheet 1 of 2)
16-10
U.S.
172SPHAUS-01