Pilot's Operating Handbook
Section 2
Limitations
EASA Approved
Edition 1 - January 15, 2018
Rev. 0
Page 2.5.2
C.G. limits
Center of gravity range with landing gear down and flaps up, attitude 0° :
Forward limits :
181.3 in (4.604 m) aft of datum at 4409 lbs (2000 kg) or less (14 % of m.a.c)
183.6 in (4.664 m) aft of datum at 6250 lbs (2835 kg) (18 % of m.a.c)
185.3 in (4.707 m) aft of datum at 6579 lbs (2984 kg) (20.85 % of m.a.c)
187in (4.752 m)aft of datumat all weights above7024lbs (3186 kg)(23.8%of m.a.c)
Aft limits :
193.65 in (4.921 m) aft of datum at 7394 lbs (3354 kg) (35 % of m.a.c.)
194 in (4.928 m) aft of datum at 6986 lbs (3169 kg) (35.5 % of m.a.c.)
Reference datum : 118.1 in (3 m) in front of the firewall front face.
Straight line variation between points.
Leveling point : Cabin floor rails.
● NOTE ●
It is the responsibility of the pilot to insure that the airplane is properly loaded.
See section 6 Weight and balance for proper loading instructions.
●
Figure 2.5.2 - C.G. limits
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