Centre of gravity
Table 2.6-1 displays the allowable Centre of Gravity (CG) range for the
JS-3 in the 15 m and 18 m configurations:
Table 2.6-1 Allowable CG range
The datum is defined as the wing leading edge at the wing root rib, i.e.
on the wing immediately outboard of the wing-fuselage fairing. The
correct aircraft attitude for weighing is defined as with the aft fuselage
boom forward of the fin positioned at gradient of 1000:18, as illustrated
in Figure 2.6-1.
Figure 2.6-1 CG Datum