Tecnam P2010 - Center of Gravity Range; Flight Crew

Page 2 - 11
Section 2 – Limitations
WEIGHTS
2
nd
Edition, Rev.1
Approved
13. WEIGHTS
Refer to Section 6 for proper aircraft and baggage loading.
14. 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
0.262 m (10.3 in) (19% MAC) aft of datum for all weights
Aft limit
0.440 m (17.3 in) (32% 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.
15. FLIGHT CREW
Minimum crew: 1 pilot
Maximum seating configuration: 4 people (including the pilot)
Condition
Weight
Maximum takeoff weight
1160 kg
2557 lb
Maximum landing weight
1160 kg
2557 lb
Maximum baggage weight
40 kg
88 lb
Baggage Compartment
Weight
Maximum weight
40 kg
88 lb
Maximum specific pressure
0.72 kg/dm
2
14.9 lb/ft
2
NOTE