CAPRONI VIZZOLA
C 22 J
6-3
WEIGHT AND BALANCE LOADING FORM
WEIGHT
MOMENT (Kg * m)
Running empty Weight
738
1882
Pilot’s Seat
Copilot’s Seat
Baggage
(1)
Main Wings Tank Fuel
Tip Tanks Fuel
Other
Totals
C.G. Station (Moment/Weight)
Totals must be within approved weight and C.G. limits (Fig 6-3)
It is the responsibility of the pilot to ensure that the airplane is loaded properly
Note (1): The influence on C.G. is negligible.
Figure 6-2
Figure 6-3
Center of Gravity Envelope
NOTE:
This Flight Simulator Model provides an automated version of the Load Form in the
documents folder. Moments are automatically calculated, and the C.G. location is
automatically plotted on the Center of Gravity envelope.
832
1172
1255
832
1172
2464
2402
2361
92
93
94
95
96
97
1764
1964
2164
2364
2564
2764
800
850
900
950
1000
1050
1100
1150
1200
1250
1300
2340
2360
2380
2400
2420
2440
2460
2480
mm
Kg
Lb
In
Weight
MAXIMUM LANDING WEIGHT
