Sling 4 TSi - 6.5 Determination of CG

Sling 4 TSi Section 6
Pilot Operating Handbook
Weight and Balance
Document Number: DC-POH-001-X-F-3.0 Page | 6-4
Revision: 3.0 Date: 2021/07/14
6.5 Determination of CG
Sling Aircraft makes use of a numerical method in calculating the CG
of the aircraft. The following will be required to complete a CG check:
#
Item
1
Empty CG Value
2
Blank CG Form
3
Forward CG Check
4
Rear CG Check
The principal formula for CG calculation is:
 =
 
 
The %MAC formulas are:
% = (  1613) ×
100
1302
,
% = (  5.292. ) ×
100
4.272.
WARNING
For each flight, the most forward CG (full take-off fuel) and the most
rearward CG (landing fuel) must be calculated to be within aircraft CG
range limits.