Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 37 of 73
8. Weight and Balance
Place the aircraft in a level position on three scales with the stabilizer and
elevator leveled.
The center of gravity is measured in mm behind the reference datum and
then calculated as a percentage of the wing chord.
Reference datum (leading edge)
Wing chord l = 1360 mm.
X1 = 230 mmm
X2 = 1770 mm ou 1775 mm (C42CS)
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