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Converted with kit
NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10
DETERMING CENTER OF GRAVITY
Before each flight the pilot must ensure that the airplane is loaded correctly. The Fig. 7c - 3
provides an example how to accomplish this
To determine the CG, proceed as follows:
1)
Determine the sum of the individual weights. This gives you the takeoff weight..
2)
Determine the sum of the individual moments / 1000 of the weights. This gives you the
takeoff moment.
3)
Check from the table Fig. 7c - 5, to determine that the takeoff weight and moment lies in
permissible area
Note
Moments/1000 can be found from Fig. 7c - 4
Airplane Flight
Manual Cessna F150L
Nr. 160
7-2c
Page:
Revision 1
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