Tecnam P2010 2015 - Specific Loadings

7. FLIGHT CONTROL SURFACES TRAVEL
Ailerons
Up 19°; Down 14 ° (± 2°)
Stabilator•
Up 6°; Down 17° (± 2°)
Stabilator trim tab
Up 3°; Down 15° (± 1°)
Rudder
RH 25°; LH 25° (± 2°)
Rudder trim tab
RH 20°; LH 20° (± 2°)
Flaps
0°; 20°; 40° {± I
0
)
*degrees are measured from the Stabilator Leading Edge.
8. SPECIFIC LOADINGS
MTOW 1160 kg (2557 lb)
Wing Loading
83.45 kg/m
2
(17.09 Jb/ft2)
Power Loading 6.44 kg/hp (14.21 lb/hp)
Section 1 - General
2' "
1
Edition, Rev .a
GENERAL FEATURES