Tecnam P2008 JC - Center of Gravity Range

Section 2 – Limitations
CENTER OF GRAVITY RANGE
Ed.1, Rev. 0
Page 2 - 14
15. CENTER OF GRAVITY RANGE
Datum Vertical plane tangent to the propeller flange (the aircraft
must be levelled in the longitudinal plane)
Levelling Refer to the seat track supporting beams (see procedure in
Section 6)
Forward limit 1.841 m (20% MAC) aft of datum for all weights
Aft limit 1.978 m (30% MAC) aft of datum for all weights
WARNING
The pilot is responsible for ensuring that the airplane is
properly loaded. Refer to Section 6 for appropriate instruc-
tions.