sonaca aircraft S201 - Datum & Center of Gravity Range

S201 AFM
2 - LIMITATIONS
2.7 - DATUM & CENTER OF
GRAVITY RANGE
27/06/2019
SONAIR-S2-D-MAN-006
Page : 2-12
Rev. : A
2.7 DATUM & CENTER OF GRAVITY RANGE
Metric
Imperial
% of MAC
Datum
Centreline of firewall front face bottom edge
Longitudinal horizontal
reference
Upper surface of canopy slides
Forward limit at 650 kg
and below
0.876 m*
2.873 ft*
20%
Forward limit at 750 kg
0.915 m*
3 ft*
23%
Rear limit at 650 kg and
below
1.021m*
3.349ft*
31%
Rear limit at 750 kg
1.034 m*
3.392 ft*
32%
*aft of datum.
There is a linear variation between all points of the centrogram (see section
6.4).
WARNING
It is the pilot’s responsibility to ensure that the airplane is properly
loaded. Refer to section 6 for information on weight and balance.