Cessna 172SPHUSR05 Pilot Operating Handbook page 163

CESSNA
MOD EL 1 72S
LOCATING CG WITH AIRPLANE ON LANDING GEAR
FORMULA for Longitudinal CG:
(NOSE G EAR N ET WEIGHT) (
(X) (A)-
=
NOSE AND MAIN LAND I NG G EAR WEIGHT TOTALED (
LOCATING PERCENT MAC
FORMULA for Percent MAC:
CG Percent MAC
=
POSITION
LEFT SIDE
RIGHT SIDE
NOSE
AIRPLANE TOTAL AS WEIGHED
BASIC E M PTY WEIGHT AN D C ENTE R-O F-G RAVITY
ITEM
AIRPLANE (CALCULATED
OR AS WEIGHED)
(INCLUDES ALL
UNDRAINABLE FLUIDS
AND FULL OIL)
DRAINABLE UNUSABLE
FUEL AT POUNDS PER
6.0
GALLON -
(3 GALLONS)
BASIC EMPTY WEIGHT
Fig u re 6-1 . Airplane Weighing Form (Sh eet 2 of 2)
J u ly 8/98
WE IG HT
(CG Arm of Airplane) - 25.90
0.5880
A I RP LAN E AS WEIG H E D TAB L E
SCALE READING SCALE DRIFT
WEIGHT
POUNDS
18.0
&
BALANCE / EQU I P M E NT L IST
) X (B)
M EASU R I N G A AN D B
MEASURE A AND B PER PILOT'S
OPERATI NG HANDBOOK
I NSTRUCTIONS TO ASSIST IN
LOCATING CG WITH AIRPLANE
WEIGHED ON LANDING G EAR.
LEVELING P ROVISIONS
LONGITUDINAL - LEFT SIDE OF
TAILCONE AT FS 1 08.00
TARE
CG ARM
(INCHES)
46.0
SECTION 6
INCHES
( AFT OF
=
)
DATUM
&
1 42.00
NET WEIGHT
MOMENT
(INCH-POUNDS
11000)
0.83
6-5