Tecnam P2006T - 15. Center of Gravity Range

Section 2 – Limitations
CENTER OF GRAVITY RANGE
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15. CENTER OF GRAVITY RANGE
Datum
Vertical plane tangent to the wing leading edge (the aircraft
must be levelled in the longitudinal plane)
Levelling
Refer to the seat track supporting beams (see procedure in
Section 6)
Forward limit
0.221 m (16.5% MAC) aft of datum for all weights
Aft limit
0.415 m (31% 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.