Sling 4 TSi - 2.9 Centre of Gravity Range

Sling 4 TSi Section 2
Pilot Operating Handbook
Limitations
Document Number: DC-POH-001-X-F-3.0 Page | 2-5
Revision: 3.0 Date: 2021/07/14
2.9 Centre of Gravity Range
Item
Value
Datum
52mm aft of the centre of the front face of
the engine propeller flange
Reference
(Longitudinal Levelling)
Second row of rivets below the canopy frame
edge, on the outside of the fuselage, above
the wing.
Reference
(Transverse Levelling)
Upper surface of centre spar cap under pilot
and passenger seats.
Forward CG Limit
1,847 mm / 6.060 ft. (18% MAC) aft of datum
Rear CG Limit
2,043 mm / 6.703 ft. (33% MAC) aft of datum
WARNING
It is the pilot’s responsibility to ensure that the airplane is properly
loaded. Refer to Section 6 Weight and Balance for more information.