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Learjet 35 - Page 203

Learjet 35
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Leerjet 35/36 Developed for Training Purposes 3-19
February 1998
Limitations
Center-of-Gravity Envelope
18,300 lb takeoff weight
Forward CG limit is F.S. 366.31 (5% MAC) for all weights up to
and including 10,000 lbs; tapers through F.S. 377.75 (18.83%
MAC) at 18,300 lbs to F.S. 378.03 (19.17% MAC) at 18,500 lbs.
The aft CG limit is F.S. 387.00 (30% MAC) at all weights.
Figure 35-3.18,300Lbs Center-of-Gravity Envelope Chart

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