Cessna SKYCATCHER 162 - Page 90

SECTION 4 CESSNA
WEIGHT AND BALANCE/ MODEL 162
EQUIPMENT LIST GARMIN G300
U.S.
SAMPLE LOADING PROBLEM - METRIC UNITS
Figure 4-4 (Sheet 2)
ITEM DESCRIPTION
WEIGHT AND MOMENT
TABULATION
SAMPLE
AIRPLANE
YOUR
AIRPLANE
Weight
(kgs)
Moment
(kg-mm/
1000)
Weight
(kgs)
Moment
(kg-mm/
1000)
1 - Basic Empty Weight
(Use the data pertaining to your airplane
as it is presently equipped. Includes
unusable fuel and full oil) 378.3 1268.4
2 - Usable Fuel (At 0.72 Kg./Liter)
- Standard Fuel - 90.82 Liters Maximum 65.4 244.5
- Reduced Fuel - 45.41 Liters
3 - Pilot and Front Passenger (FS 3607) 136.1 490.9
4 - Baggage (FS 3937 to 4826)
22.6 Kilograms Maximum 19.9 86.9
5 - RAMP WEIGHT AND MOMENT 599.7 2090.7
6 - Fuel allowance for engine start, taxi and
runup -1.8 -6.6
7 - TAKEOFF WEIGHT AND MOMENT
(Subtract Step 8 from Step 7) 597.9 2084.1
8 - Locate this point (597.9 at 2084.1) on the Center of Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
162PHUS-00
4-18