Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 188

SECTION 6
WEIGHT AND BALANCE/EQUIPMENT LIST
I
ESSNA
MODEL 172E NAV III
I
AIRPLANE WEIGHING FORM
Locating Percent MAC
BolO73
Locating CG with Airplane on Landing Gear
X (Inches Aft of Datum)
=
A {Nosewheel Weight
x
8 ]
Total Weight*
*(Nose
+
L
+
R Wheel Weights)
CG Percent MAC
=
(CG Arm of Airplane) -
25.90
0.5880
Measuring A and B
Levelin Provisions
Longitudinal - Left side of tailcon
at
FS 108.00
and
142.00
Measure A and B per pilot's
operating handbook
instructions to assist in locating
CG with airplane weighed on
landing gear.
Airplane as Weighed Table
Position Scale reading
Scale drift
Tare Net weight
Left Wheel
Right Wheel
Nose Wheel
Airplane total as weighed
Basic Empty Weight and Center-of-Gravity Table
-
Weight
CGArm
Moment
Item
(Inch-Pounds
Pounds (Inches)
11000)
Airplane (calculated or as
weighed) Oncludes all
undrainable fluids and
full oio
Drainable unusable
fuel at
6.0
pounds per
18.0
46.00 0.83
gallon -
(3
gallons)
Basic Empty Weight
I
16-6
u.s.
. . Figure 6-1 (Sheet 2)
172SPHAUS-01