Position Layout of Center of Gravity Measurement for CE-525 Aircraft
The center of gravity measurement layout of CE-525 aircraft is shown in the following figure, which can be measured by force measuring platform or top position. If the force measuring platform method is used, the attitude adjustment process of aircraft is more complicated. The best way is that the combination of attitude adjustment mechanism of force-measuring platform is more convenient.
1.Platform load:L'nd=87.250 in (2214.88);L'mn=175.11in(4447.79);L'md=262.31in(6662.67)
Relative to datum D, the longitudinal center of gravity CG=240.48in (6108.13mm).
2.Jack load:Lnd=93.70 in (2379.98);Lmn=181.61in(4612.00);Lmd=275.31in (6993.00)
Relative to datum D, the longitudinal center of gravity CG=252.67in (6417.82mm).
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