Airplane Factory SLING 4
Pilot Operating Handbook
Page | 6-6
DC-POH-001-X-C-3
Revision : 1.3
6.4
Determining aircraft CG
Weight and balance report lists:
Empty CG check.
Forward CG check (example).
Rear CG check (example).
Blank CG form.
CG formulae:
( )
( )
The aircraft empty CG is determined in a conventional manner by weighing
the aircraft whilst it is standing level. (Refer to the aircraft maintenance
manual for instructions on aircraft leveling and weighing).
WARNING
For each flight the most forward CG (i.e. with take-off fuel) and the
most rearward CG (i.e. with landing fuel) must be calculated (to be
within aircraft CG range / limits).
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