Sling 4 TSi Section 6
Pilot Operating Handbook
Weight and Balance
Document Number: DC-POH-001-X-F-3.0 Page | 6-2
Revision: 3.0 Date: 2021/07/14
6.3 Centre of Gravity Arms
Aircraft CG and MAUW limitations must be adhered to at all times.
• GC range is 1847mm (6.060 ft) to 2043 mm (6.703 ft) aft of the
reference datum (18 to 33% of MAC).
• The leading edge of the wing at MAC is 1613 mm (5.292 ft) aft of
the reference datum.
•
The MAC is 1302 mm (4.272 ft).
Datum: 52mm AFT OF FRONT FACE OF ENGINE PROPELLER FLANGE