Section 2 - Limitations 15

Question 1

Datum

Answer 1

Vertical plane tangent to the wing leading edge (the aircraft
must be levelled in the longitudinal plane)

Question 2

Levelling

Answer 2

Refer to the seat track supporting beams (see procedure in Section 6)

Question 3

Forward limit

Answer 3

0.221 m (16.5% MAC) aft of datum for all weights

Question 4

Aft limit

Answer 4

0.415 m (31% MAC) aft of datum for all weights