Limits; Edition 0 - Daher-Socata TBM 900 Pilot's Information Manual

SECTION 2
PILOT'S OPERATING HANDBOOK
LIMITATIONS
EASA Approved
C.G. LIMITS
-- see Figure 6.4.2
Center of gravity range with landing gear down and flaps up, attitude 0° :
Forward limits :
181.3 inches (4.604 m) aft of datum at 4409 lbs (2000 kg) or less (14 % of m.a.c)
183.6 inches (4.664 m) aft of datum at 6250 lbs (2835 kg) (18 % of m.a.c)
185.3 inches (4.707 m) aft of datum at 6579 lbs (2984 kg) (20.85 % of m.a.c)
187 inches (4.752 m) aft of datum at all weights above 7024 lbs (3186 kg) (23.8 % of m.a.c)
Aft limits :
193.65 inches (4.921 m) aft of datum at 7394 lbs (3354 kg) (35 % of m.a.c.)
194 inches (4.928 m) aft of datum at 6986 lbs (3169 kg) (35.5 % of m.a.c.)
Reference datum : 118.1 inches (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
Page 2.5.2 Edition 0 -- October 31, 2013
Rev. 1