Weight and Balance Information 4 - 3
Rev. 01 – 07-01-2008
4
Weight and Balance Information
4.3
Center of Grafity (CG) Range and Determination
To determine “CG”, put the aircraft on 3 weighing scales, positioned on a level surface. Before weighing,
a level wing main chord has to be established (use pads between main wheels and scale beneath). A
check-mark (R.P.) on the leading edge of the left wing, adjacent to the wing root is provided to ease
examination to level wing main chord - use a flexible clear hose, filled with water as a spirit level. The total
weight
G
=
G1
+
G2
, has to be used for calculating “CG”, located at the distance “X” behind R.P.
Summary of Contents for G 2008 Series
Page 1: ...i...
Page 7: ...vii Rev 01 07 01 2008 Views The REMOS GX is designed as full composite carbon fiber aircraft...
Page 15: ...Airplane and Systems Description 2 5 Rev 01 07 01 2008 2 Airplane and Systems Description...
Page 47: ...Performance 5 5 Rev 01 07 01 2008 5 Performance 5 5 Pressure Altitude Diagramm...
