Tecnam P-Mentor - 9. Weights and Center of Gravity Limits

1
st
Edition - Rev. 0
Section 2 – LIMITATIONS
WEIGHTS AND CENTER OF GRAVITY LIMITS
P-Mentor – Aircraft Flight Manual Page 2 - 11
EASA Approved
9. Weights and center of gravity limits
Table 2-4 – Weight Limits
Condition
Weight
Maximum Take-off Weight
720 kg
1587 lb
Maximum Landing Weight
720 kg
1587 lb
Datum
Propeller support flange without spacer (the aircraft
must be levelled in the longitudinal plane)
Levelling
Refer to the seat track supporting beams (see
procedure in Section 6)
Forward limit
0.312 m (1.024 ft) (23% MAC) aft of datum for all
weights up to 550 kg / 1213 lb
0.339 m (1.112 ft) (25% MAC) aft of datum for MTOW
Aft limit
0.448 m (1.47 ft) (33% MAC) aft of datum for all
weights
The pilot is responsible for ensuring that the airplane
is properly loaded. Refer to Section 6 for appropriate
instructions.